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* EMERGENCY CORE COOLING SYS'1EMS HEA i TAAC ING LIMITING CONDITION FOR OPERATION 3.5.4.2 At least two independent channels of heat acing shall be OPERJl.BLE for the boron injection tank and for the eat traced portions of the associated flow paths. APPLICABILITY:
* EMERGENCY CORE COOLING SYS'1EMS HEA i TAAC ING LIMITING CONDITION FOR OPERATION 3.5.4.2 At least two independent channels of heat acing shall be OPERJl.BLE for the boron injection tank and for the eat traced portions of the associated flow paths. APPLICABILITY:
MODES l, 2 and 3. ACTION: With only one channel of heat tra ing on ither the boron injection tank or on the heat traced portion f an as o iated flow path OPERABLE, operation may continue for up 3 d y provided the tank and flow path temperatures are verified to b at least once per 8 hours; otherwise, be in HOT SHUT OWN wi 2 hours. 4.5.4.2 Each heat tracing hannel for the boron injection tank and associated flow path shall e demonstrated OPERABLE:  
MODES l, 2 and 3. ACTION: With only one channel of heat tra ing on ither the boron injection tank or on the heat traced portion f an as o iated flow path OPERABLE, operation may continue for up 3 d y provided the tank and flow path temperatures are verified to b at least once per 8 hours; otherwise, be in HOT SHUT OWN wi 2 hours. 4.5.4.2 Each heat tracing hannel for the boron injection tank and associated flow path shall e demonstrated OPERABLE:
: a. At least once p r 31 days by energizing each heat tracing channel, and b. At least once per 24 hours by verifying the tank and flow path tempera ures to be .!. 14S*F. The tank temperature shall be de nriined by measurement.
: a. At least once p r 31 days by energizing each heat tracing channel, and b. At least once per 24 hours by verifying the tank and flow path tempera ures to be .!. 14S*F. The tank temperature shall be de nriined by measurement.
The flow path temperature shall be de enriined by either measurement or recirculation flow until esta ishment of equilibrium temperatures within the tank.
The flow path temperature shall be de enriined by either measurement or recirculation flow until esta ishment of equilibrium temperatures within the tank.
* SALEM -UNIT l 3/4 5  
* SALEM -UNIT l 3/4 5  
* . EMERGENCY CORE COOLING SYSTEMS REFUELING wATER STORAGE TANK LIMITING CONDITION FOR OPERATION 3.5.4 The refueling water storage tank (RWST) shall be OPERABLE with: a. A contained volume of between 364 1 500 and 400,000 gallons of borated water, b. A boron concentration of between-2000 and 2200 ppm, and c. A minimum water temperature of 35°F. APPLICABILITY:
* . EMERGENCY CORE COOLING SYSTEMS REFUELING wATER STORAGE TANK LIMITING CONDITION FOR OPERATION 3.5.4 The refueling water storage tank (RWST) shall be OPERABLE with: a. A contained volume of between 364 1 500 and 400,000 gallons of borated water, b. A boron concentration of between-2000 and 2200 ppm, and c. A minimum water temperature of 35°F. APPLICABILITY:
MODES 1, 2, 3 and 4. ACTION: With the refueling water storage tank inoperable, restore the tank to OPERABLE status within 1 hour or be in at least HOT STANDBY within 6 hours and in COLO SHUTDOWN within the following 30 hours. SURVEILLANCE REQUIREMENTS 4.5.4 The RWST shall be demonstrated OPERABLE:  
MODES 1, 2, 3 and 4. ACTION: With the refueling water storage tank inoperable, restore the tank to OPERABLE status within 1 hour or be in at least HOT STANDBY within 6 hours and in COLO SHUTDOWN within the following 30 hours. SURVEILLANCE REQUIREMENTS 4.5.4 The RWST shall be demonstrated OPERABLE:
: a. At least once per 7 days by: 1. Verifying the water level in the tank, and 2. Verifying the boron concentration of the water.* b. At least once per 24 hours by verifying the RWST temperature when the outside air temperature is less than 35°F . 3/4 5-7 I   
: a. At least once per 7 days by: 1. Verifying the water level in the tank, and 2. Verifying the boron concentration of the water.* b. At least once per 24 hours by verifying the RWST temperature when the outside air temperature is less than 35°F . 3/4 5-7 I   
.EMERGENCY CORE COOLING SYSTEMS BASES .
.EMERGENCY CORE COOLING SYSTEMS BASES .
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The contained water volume limit includes an allowance for water not usable because of tank discharge line location or other physical characteristics
The contained water volume limit includes an allowance for water not usable because of tank discharge line location or other physical characteristics
* SALEM -UN IT 1 B 3/4 5-2
* SALEM -UN IT 1 B 3/4 5-2
* EMERGENCY CORE COOLING SYSTEMS 4.5.4 BORON INJECTION SYSTEM BORON INJECTION TANK LIMITING CONDITION FOR OPERATION 3.5.4. 1 The boron injection  
* EMERGENCY CORE COOLING SYSTEMS 4.5.4 BORON INJECTION SYSTEM BORON INJECTION TANK LIMITING CONDITION FOR OPERATION 3.5.4. 1 The boron injection
: a. A minimum contained volume of 900 b. Between 20,000 and 22,500 ppm of c. A minimum solution temperatur APPLICABILITY:
: a. A minimum contained volume of 900 b. Between 20,000 and 22,500 ppm of c. A minimum solution temperatur APPLICABILITY:
MODES l, 2 and 3. ACTION: le restore the tank to OPERABLE status d orated to a SHUTDOWN MARGIN equivalent hours; restore the tank to OPERABLE in HOT SHUTDOWN within the next 12 hours. 4.5.4. l The boron tank shall be demonstrated OPERABLE by: a. Verifying w ter level through a recirculation flow test at least once per 7 d y , b. Verifyin th boron concentration of the water in the tank at least once pe 7 days, and UNIT 2 3/4 S-9
MODES l, 2 and 3. ACTION: le restore the tank to OPERABLE status d orated to a SHUTDOWN MARGIN equivalent hours; restore the tank to OPERABLE in HOT SHUTDOWN within the next 12 hours. 4.5.4. l The boron tank shall be demonstrated OPERABLE by: a. Verifying w ter level through a recirculation flow test at least once per 7 d y , b. Verifyin th boron concentration of the water in the tank at least once pe 7 days, and UNIT 2 3/4 S-9
* EMERGENCY CORE COOLING SYSTEMS HEAT TRACING LiMITING CONDITION FOR OPERATION 3.5.4.2 At least two independent channels of heat racing shall be OPERABLE for the boron injection tank and for the heat tra d portions of the associated fl ow paths. APPLICABILITY:
* EMERGENCY CORE COOLING SYSTEMS HEAT TRACING LiMITING CONDITION FOR OPERATION 3.5.4.2 At least two independent channels of heat racing shall be OPERABLE for the boron injection tank and for the heat tra d portions of the associated fl ow paths. APPLICABILITY:
MODES l, 2 and 3. ACTION: With only one channel of heat tr the heat traced portion of an s continue for up to 30 da s provi verified to be greater t an otherwise, be in HOT SHU DO either the boron injection tank or on flow path OPERABLE, operation may tank and flow path temperatures are to 145°F at least once per 8 hours; 12 hours. r cing channel for the boron injection tank and associated onstrated OPERABLE:  
MODES l, 2 and 3. ACTION: With only one channel of heat tr the heat traced portion of an s continue for up to 30 da s provi verified to be greater t an otherwise, be in HOT SHU DO either the boron injection tank or on flow path OPERABLE, operation may tank and flow path temperatures are to 145°F at least once per 8 hours; 12 hours. r cing channel for the boron injection tank and associated onstrated OPERABLE:
: b. At east once per 24 hours by verifying the tank and flow path te eratures to be greater than or equal to 145°F. The tank t e shall be determined by measurement.
: b. At east once per 24 hours by verifying the tank and flow path te eratures to be greater than or equal to 145°F. The tank t e shall be determined by measurement.
The flow path temperature s all be determined by either measurement or recirculation flow ntil establishment of equilibrium temperatures within the tank . 3/4 5-10 EMERGENCY CORE COOLING SYSTEMS .FUELING WATER STORAGE TANK LIMITING CONDITION FOR OPERATION 3.5.4 The refueling water storage tank (RWST) shall be OPERABLE with: a. A contained volume of between 364,500 and 400,000 gallons of borated water, b. A boron concentration of between 2000 and 2200 ppm, and c. A minimum water temperature of 35°F. APPLICABILITY:
The flow path temperature s all be determined by either measurement or recirculation flow ntil establishment of equilibrium temperatures within the tank . 3/4 5-10 EMERGENCY CORE COOLING SYSTEMS .FUELING WATER STORAGE TANK LIMITING CONDITION FOR OPERATION 3.5.4 The refueling water storage tank (RWST) shall be OPERABLE with: a. A contained volume of between 364,500 and 400,000 gallons of borated water, b. A boron concentration of between 2000 and 2200 ppm, and c. A minimum water temperature of 35°F. APPLICABILITY:
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* 1. The saturation temperature corresponding to the pt'.rtial pressure of the contairment vapor is used in the calculation of condensing heat transfer to the passive heat sinks and the removal by ment fan coolers. 2. The Westinghouse containment model utilizes the analytical approaches described in References 6 and 60 to calculate the condensate removal from the condensate film. Justification of this model is provided in References 56, 59, 60, and 6. (For large breaks 100 percent revaporization of the condensate is used, and a calculated revaporization due *to convective heat flux is used for small breaks.) 3. The small steCITI line break containment analyses uti l1zed the nant TagC1ni correlation, and the large steCITI line break analyses utilized the Tagami correlation with an exponential  
* 1. The saturation temperature corresponding to the pt'.rtial pressure of the contairment vapor is used in the calculation of condensing heat transfer to the passive heat sinks and the removal by ment fan coolers. 2. The Westinghouse containment model utilizes the analytical approaches described in References 6 and 60 to calculate the condensate removal from the condensate film. Justification of this model is provided in References 56, 59, 60, and 6. (For large breaks 100 percent revaporization of the condensate is used, and a calculated revaporization due *to convective heat flux is used for small breaks.) 3. The small steCITI line break containment analyses uti l1zed the nant TagC1ni correlation, and the large steCITI line break analyses utilized the Tagami correlation with an exponential  
-to the stagnant TagC1ni correlation.
-to the stagnant TagC1ni correlation.
The details of these models are given in Reference  
The details of these models are given in Reference
: 38. Justification of the use of heat transfer coefficients has been provided in References 58, 59, and 61. [1:1] (f:.] A complete analysis of main steanline co ainment as been LrJJFTfl.A-r-1 perfonned using the MARVEL code and the Westing ouse . r-. .
: 38. Justification of the use of heat transfer coefficients has been provided in References 58, 59, and 61. [1:1] (f:.] A complete analysis of main steanline co ainment as been LrJJFTfl.A-r-1 perfonned using the MARVEL code and the Westing ouse . r-. .
* rment computer code, COCO, as described in and its references.
* rment computer code, COCO, as described in and its references.
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Also. since the feed tion valve is upstream of the regulator valve, failure of the regulator results in additional feed line volL1T1e which is not isolated from the stean generator.
Also. since the feed tion valve is upstream of the regulator valve, failure of the regulator results in additional feed line volL1T1e which is not isolated from the stean generator.
Thus, water in this portion of the lines can flash and enter into the stean generator.
Thus, water in this portion of the lines can flash and enter into the stean generator.
The only non-safety grade equipment in the main feed system W1ich is relied upon to tenninate the main feed flow to the stean generators are the main feedwater control valves. These valves are not seismic category I. Ho\!Ever, each valve receives dual, independent, safety grade trip:.elosed signals from the protection system following a stec111 line break. A1so. the valves are air-9perated fail-closed design. Since the assLITled break is inside contairment in a seismic category I pipe, it is not assuned to be i ni ti ated by a seismic event. Therefore, to ass1J11e a coincident sei smfc event with the hypothetic al pipe rupture is not required, and thus a seismic classification for the main feed SGS-UFSAR  
The only non-safety grade equipment in the main feed system W1ich is relied upon to tenninate the main feed flow to the stean generators are the main feedwater control valves. These valves are not seismic category I. Ho\!Ever, each valve receives dual, independent, safety grade trip:.elosed signals from the protection system following a stec111 line break. A1so. the valves are air-9perated fail-closed design. Since the assLITled break is inside contairment in a seismic category I pipe, it is not assuned to be i ni ti ated by a seismic event. Therefore, to ass1J11e a coincident sei smfc event with the hypothetic al pipe rupture is not required, and thus a seismic classification for the main feed SGS-UFSAR
: 15. 4-90 Revision O July 22. 1982   
: 15. 4-90 Revision O July 22. 1982   
*
*
* regulation valve is not necessary to insure closure following a
* regulation valve is not necessary to insure closure following a
li ne break inside contai r111ent. Because of the conservative nature of the transient calculations used for the 1971 Equipment Qualification Progran, the results of thfl Salem temperature transient calculatf on wf 11 fall under the peak transient calculated for the 1971 Equipment Qualification ProgrC111 and presented in Reference 60 (approximately 385.F). The pressure transient wf 11 fall below the design limits for the Salem 2 contail'lllent.
li ne break inside contai r111ent. Because of the conservative nature of the transient calculations used for the 1971 Equipment Qualification Progran, the results of thfl Salem temperature transient calculatf on wf 11 fall under the peak transient calculated for the 1971 Equipment Qualification ProgrC111 and presented in Reference 60 (approximately 385.F). The pressure transient wf 11 fall below the design limits for the Salem 2 contail'lllent.
Feedwater flow to the faulted steC111 generator from the main feed system is calculated using the hydraulic resistances of the system piping, head/flow curves for the main and the steC111 generator sure deczy .as calculated by the MARVEL code. In the calculations fonned to match these systems variables, a variety of assunptions are made to maximize the ca le ul ated flows. These f nc l ude: 1. No credit for extra pressure drop in the feed lines due to flashing of feedwater.  
Feedwater flow to the faulted steC111 generator from the main feed system is calculated using the hydraulic resistances of the system piping, head/flow curves for the main and the steC111 generator sure deczy .as calculated by the MARVEL code. In the calculations fonned to match these systems variables, a variety of assunptions are made to maximize the ca le ul ated flows. These f nc l ude: 1. No credit for extra pressure drop in the feed lines due to flashing of feedwater.
: 2. Feed regulator valve in the faulted loop f s full open. 3. Feed regulator valves in the intact loop do not change position prior to a trip signal.aREi elese iAstaRtly ef a sigAal te e lase. 4. All feed punps are running at maximun speed. 5. No credit is taken for flow redt.a:tion through the feed regulator or feed isolation valve until they are full closed. 6. Flow from the pllTlpS 11 nearly followf ng punp trf"p.
: 2. Feed regulator valve in the faulted loop f s full open. 3. Feed regulator valves in the intact loop do not change position prior to a trip signal.aREi elese iAstaRtly ef a sigAal te e lase. 4. All feed punps are running at maximun speed. 5. No credit is taken for flow redt.a:tion through the feed regulator or feed isolation valve until they are full closed. 6. Flow from the pllTlpS 11 nearly followf ng punp trf"p.
Calculation of feedwater flashing f s perfonned by the MAR'd:L code as described in Section 2.2.3 of WCAP For the Salem units, the . 4.1.r 1'101. SGS-UFSAR 15.4-91 Revision 0 .)11] v ?2 ] QQ2   
Calculation of feedwater flashing f s perfonned by the MAR'd:L code as described in Section 2.2.3 of WCAP For the Salem units, the . 4.1.r 1'101. SGS-UFSAR 15.4-91 Revision 0 .)11] v ?2 ] QQ2   
Line 98: Line 98:
by adding the piping mass to the faulted stean generator mass, arid by having dry steam bloMiowns.
by adding the piping mass to the faulted stean generator mass, arid by having dry steam bloMiowns.
the stean line inventory is included in the total bloMiown.
the stean line inventory is included in the total bloMiown.
Auxi 11 ary Feedwater Flow The Auxiliary Feedwater System fs actuated shortly after_the occurrence of *a stean line break. The mass addition to the faulted stean generator from the Auxi 11 ary Feed water System was conservatively detenni ned by using the fo 1 lowf ng assunptf ons. 1. The entire Auxf 11 ary Feedwater System was asst111ed to be actuated at the time of the break and f nstantaneously punpi ng at its maximun capacity. . 2. The affected stean generator was au1111d to be at atmospheric pressure.  
Auxi 11 ary Feedwater Flow The Auxiliary Feedwater System fs actuated shortly after_the occurrence of *a stean line break. The mass addition to the faulted stean generator from the Auxi 11 ary Feed water System was conservatively detenni ned by using the fo 1 lowf ng assunptf ons. 1. The entire Auxf 11 ary Feedwater System was asst111ed to be actuated at the time of the break and f nstantaneously punpi ng at its maximun capacity. . 2. The affected stean generator was au1111d to be at atmospheric pressure.
: 3. The intact stean generators assuned to be at the safety valve set pressure.  
: 3. The intact stean generators assuned to be at the safety valve set pressure.
: 4. Flow to the affected stean generator was fran the Auxiliary Feedwater System head curves. assunptions 2 and 3 above, and the system 11 ne re sf stances. The effects of flow* limiting devices were considered.  
: 4. Flow to the affected stean generator was fran the Auxiliary Feedwater System head curves. assunptions 2 and 3 above, and the system 11 ne re sf stances. The effects of flow* limiting devices were considered.
: 5. The flow to the faulted stean generator from the Auxi 11 ary Feed water System-was asst111ed to exist from the time of rupture until ment of the system was completed.  
: 5. The flow to the faulted stean generator from the Auxi 11 ary Feed water System-was asst111ed to exist from the time of rupture until ment of the system was completed.
: 6. The failure of auxi 11 ary feed water runout control was considered a.A <lY\.i &f r'M..u!etn11ate1y u i single o.f 1d a CN\J-1.o-:t of 'Z..040 jr -h> fu sf..ta.-
: 6. The failure of auxi 11 ary feed water runout control was considered a.A <lY\.i &f r'M..u!etn11ate1y u i single o.f 1d a CN\J-1.o-:t of 'Z..040 jr -h> fu sf..ta.-
SGS-UFSAR 15.4-93 ---*-----Revision O July 22, 1982   
SGS-UFSAR 15.4-93 ---*-----Revision O July 22, 1982   
*
*
* The a"alys'fs used the felle\IAAg arJM111aPy feeawateF flew Pates: la With rt1,.elft preteetieA a eeAstaRt awxi 11aFy feeEI fle\IJ of 1840 gpm to the faulted stesn ge"eraters  
* The a"alys'fs used the felle\IAAg arJM111aPy feeawateF flew Pates: la With rt1,.elft preteetieA a eeAstaRt awxi 11aFy feeEI fle\IJ of 1840 gpm to the faulted stesn ge"eraters
: 2. lwine ef P"WA&tff eeAt-l:"el was s1111t1lateEI  
: 2. lwine ef P"WA&tff eeAt-l:"el was s1111t1lateEI  
&y asst111Ag a ea,.sta"t al:IK111 aP'.)' feeElwater flew ef 2949 gp11 ta tt:le f abllteEI ste aR geAePateFa The flew rates 'WI! re he 1d ee"st ar1t freM time ef bl"e ak l::IAti 1 real1 gF1R1eRt1  
&y asst111Ag a ea,.sta"t al:IK111 aP'.)' feeElwater flew ef 2949 gp11 ta tt:le f abllteEI ste aR geAePateFa The flew rates 'WI! re he 1d ee"st ar1t freM time ef bl"e ak l::IAti 1 real1 gF1R1eRt1  
Line 115: Line 115:
Since a sufficient number of trains of instrumentation must be available for nonnal plant operation, steam generator instrumentation will be in operation at the time of the postulated event. Therefore, changes in steam generator pressure and steam flow will be detected as they occur. The only delay expected in transmitting the infonnation to the control room is the time required for the instrumentation to react to the changing conditions.
Since a sufficient number of trains of instrumentation must be available for nonnal plant operation, steam generator instrumentation will be in operation at the time of the postulated event. Therefore, changes in steam generator pressure and steam flow will be detected as they occur. The only delay expected in transmitting the infonnation to the control room is the time required for the instrumentation to react to the changing conditions.
This delay is expected to be no more than a few seconds. Failure of the auxiliary feedwater isolation valve to close has not been considered.
This delay is expected to be no more than a few seconds. Failure of the auxiliary feedwater isolation valve to close has not been considered.
The maximum auxiliary feedwater flow that can be delivered to a faulted steam been assumed in the analysis for ten minutes considered:  
The maximum auxiliary feedwater flow that can be delivered to a faulted steam been assumed in the analysis for ten minutes considered:
: 1) F'WRewt pPeteetieA 6f3el"a'  
: 1) F'WRewt pPeteetieA 6f3el"a'
: 2) failure of runout protection.
: 2) failure of runout protection.
Only after ten minutes the operator takes action to isolate auxiliary feedwater isolation valves fails to close, the operator can trip the two auxiliary feedwater pumps feeding broken steam generator until this valve or* another in the line is manually closed. The pump curves for the Auxiliary Feed pump are shown in Figure 15.4-93 (Steam Driven) and Figure 15.4-94 (Electrical Driven). A schematic of the Auxiliary Feed System is shown fn Figure 10.4-17
Only after ten minutes the operator takes action to isolate auxiliary feedwater isolation valves fails to close, the operator can trip the two auxiliary feedwater pumps feeding broken steam generator until this valve or* another in the line is manually closed. The pump curves for the Auxiliary Feed pump are shown in Figure 15.4-93 (Steam Driven) and Figure 15.4-94 (Electrical Driven). A schematic of the Auxiliary Feed System is shown fn Figure 10.4-17
Line 142: Line 142:
*1ariables are prov;ded in Figures 15.4-*97 through U . .
*1ariables are prov;ded in Figures 15.4-*97 through U . .
* W:J fw  
* W:J fw  
+N.. of tN lReference Sect;on 2.3 of WCAP-8822 for a complete d;scussion of this spHt break. .. SGS-UFSAR  
+N.. of tN lReference Sect;on 2.3 of WCAP-8822 for a complete d;scussion of this spHt break. .. SGS-UFSAR
: 15. 4-97 Rev;s;on 0 JU 1 Y 22 1 1982
: 15. 4-97 Rev;s;on 0 JU 1 Y 22 1 1982
* The large break case resulting in the calculated peak pressure has been ent;fied as the i*.4 ft2 break at 70 percent power. This case re lted in a peak pressure of 39.l psi g when dry steam bl owdowns are used. When this same case was reanalyzed utilizing blowdowns which include the effect of liquid carryover from the secondary  
* The large break case resulting in the calculated peak pressure has been ent;fied as the i*.4 ft2 break at 70 percent power. This case re lted in a peak pressure of 39.l psi g when dry steam bl owdowns are used. When this same case was reanalyzed utilizing blowdowns which include the effect of liquid carryover from the secondary
: side, ting eak pressures were 37. 7 and 37.2 using the Westi ngh se and NRC contai nt models respectively.
: side, ting eak pressures were 37. 7 and 37.2 using the Westi ngh se and NRC contai nt models respectively.
This indicates the over. 1 con-servatism of e Westinghouse containment model when used th dry steam, vs. usi n the expected mass and energy releases ch include the effect of entrai nt. Transients for the Westi nghous mode.1 with dry steam blowdowns are ovided in Figures 15.4-97 thro h 15.4-99. The case resulting  
This indicates the over. 1 con-servatism of e Westinghouse containment model when used th dry steam, vs. usi n the expected mass and energy releases ch include the effect of entrai nt. Transients for the Westi nghous mode.1 with dry steam blowdowns are ovided in Figures 15.4-97 thro h 15.4-99. The case resulting  
Line 158: Line 158:
**
**
model similar to that presented  
model similar to that presented  
*tn Reference  
*tn Reference
: 24. dfffe . es between the Westf nghouse then11l arialysf s model and t proposed N nterim model will be dfscussed and Justified.  
: 24. dfffe . es between the Westf nghouse then11l arialysf s model and t proposed N nterim model will be dfscussed and Justified.
: 1. 2. A conv
: 1. 2. A conv
* e heat transfer coefffcfent comparable to t by the NRC will be used. If necessary, sensftfvfty will be performed to j ustffy an.y model differences. 15.4.8.3 Subcompartrnent Pressure Analysts Reference b4 presents the containment subcmpartment pressure analysis usf ng an 18 node contaf nment model and the latest version of the TMD computer code. 15.4.8.4 Mf scell aneous Analysis 15.4.8.4.1 Minor Reactor Coolant Leakage The Hf Contaf rrnent Pressure sf gnal actuates engf neered safety features.
* e heat transfer coefffcfent comparable to t by the NRC will be used. If necessary, sensftfvfty will be performed to j ustffy an.y model differences. 15.4.8.3 Subcompartrnent Pressure Analysts Reference b4 presents the containment subcmpartment pressure analysis usf ng an 18 node contaf nment model and the latest version of the TMD computer code. 15.4.8.4 Mf scell aneous Analysis 15.4.8.4.1 Minor Reactor Coolant Leakage The Hf Contaf rrnent Pressure sf gnal actuates engf neered safety features.
Since the set point for this signal fs two psfg, the maximum containment pressure caused by leakage is restricted to thfs value. The containment response to such leakage would be a gradual pressure and temperature rise whfchjtould reach a pressure peak of slightly less* than two pounds gauge. At thf s point energy removal due to structural heat sinks and operating fan coolers would match the energy* addition due to the . . and other sources
Since the set point for this signal fs two psfg, the maximum containment pressure caused by leakage is restricted to thfs value. The containment response to such leakage would be a gradual pressure and temperature rise whfchjtould reach a pressure peak of slightly less* than two pounds gauge. At thf s point energy removal due to structural heat sinks and operating fan coolers would match the energy* addition due to the . . and other sources
* SGS-UFSAR 15.4-99 Revf sf on O July 22, 1982 REFERENCES FOR SECTION 15.4 1. "Acceptance Criteria for Emergency Core Cooling Systems for Light Water Cooled Noclear Power Reactors," lOCFRS0.46 and Appendix K of * .10CFR50.
* SGS-UFSAR 15.4-99 Revf sf on O July 22, 1982 REFERENCES FOR SECTION 15.4 1. "Acceptance Criteria for Emergency Core Cooling Systems for Light Water Cooled Noclear Power Reactors," lOCFRS0.46 and Appendix K of * .10CFR50.
Federal Register, Vol1111e 39, N1111ber 3, January 4, 1974. ' . 2. Bordelon, F. M., Massie, H. w. and Zordan T. A., "Westinghouse ECCS Evaluation Model -S11111J1ary, 11 WCAP-8339, July 1974. 3. Bordelon, F. M., et al ** "SATAN-VI Comprehensive Time Dependent Analysis of Loss of Coolant," WCAP-8302, June, 1974 (Proprietary) and WCAP-8306, June 1974 "(Non-P.roprietary).  
Federal Register, Vol1111e 39, N1111ber 3, January 4, 1974. ' . 2. Bordelon, F. M., Massie, H. w. and Zordan T. A., "Westinghouse ECCS Evaluation Model -S11111J1ary, 11 WCAP-8339, July 1974. 3. Bordelon, F. M., et al ** "SATAN-VI Comprehensive Time Dependent Analysis of Loss of Coolant," WCAP-8302, June, 1974 (Proprietary) and WCAP-8306, June 1974 "(Non-P.roprietary).
: 4. Bordelon, F. M., et al., 11 LOCTA-IV Loss of Coolant sient Analysis, 11 WCAP-8301, June 1974 (Proprietary) and WCAP-8305, June 1974 (Non-Proprietary).  
: 4. Bordelon, F. M., et al., 11 LOCTA-IV Loss of Coolant sient Analysis, 11 WCAP-8301, June 1974 (Proprietary) and WCAP-8305, June 1974 (Non-Proprietary).
: 5. Kelly R. D., et al., 11 Calculational Model for Core Reflooding After a Loss of Coolant Accident (WREFLOOD Code)," WCAP-8170, June 1974 (Proprietary) and WCAP-8171, June 1974 (Non-Proprietary)o  
: 5. Kelly R. D., et al., 11 Calculational Model for Core Reflooding After a Loss of Coolant Accident (WREFLOOD Code)," WCAP-8170, June 1974 (Proprietary) and WCAP-8171, June 1974 (Non-Proprietary)o
: 6. Bordelon, F. M. and Murphy, E.T., 11 Containnent Pressure Analysis Code (COCO)," WCAP-8327, June 1974 (Proprietary) and WCAP-8326, June 1974 (Non-Proprietary).  
: 6. Bordelon, F. M. and Murphy, E.T., 11 Containnent Pressure Analysis Code (COCO)," WCAP-8327, June 1974 (Proprietary) and WCAP-8326, June 1974 (Non-Proprietary).
: 7. Bordelon, F. M., et al., "Westinghouse ECCS Evaluation Model -plementary Infonnation, 11 WCAP-8471-P-A, April 1975 (Proprietary) and WCAP-8472-A, April 1975 (Non-Proprietary).  
: 7. Bordelon, F. M., et al., "Westinghouse ECCS Evaluation Model -plementary Infonnation, 11 WCAP-8471-P-A, April 1975 (Proprietary) and WCAP-8472-A, April 1975 (Non-Proprietary).
: 8. 11 Westi nghoi.se ECCS Evaluation Model -October 1975 Version, 11 WCAP-8622, November 1975 (Proprietary) and WCAP-8623, November 1975 (Non-Proprietary).  
: 8. 11 Westi nghoi.se ECCS Evaluation Model -October 1975 Version, 11 WCAP-8622, November 1975 (Proprietary) and WCAP-8623, November 1975 (Non-Proprietary).
: 9. Letter from C. Eicheldinger of Westinghouse Electric Corporation to D. B. Vassallo of the Noclear Regulatory Coamission.
: 9. Letter from C. Eicheldinger of Westinghouse Electric Corporation to D. B. Vassallo of the Noclear Regulatory Coamission.
Letter N1.111ber NS-CE-924, dated January 23, 1976. SGS-UFSAR 15.4-101 Revision O July 22, 1982   
Letter N1.111ber NS-CE-924, dated January 23, 1976. SGS-UFSAR 15.4-101 Revision O July 22, 1982   
* *
* *
* 10. Kelly, R. D., Thompson, C. M., et al., "Westinghouse Emergency Core Cooling System Evaluation Model for Analyzing Large LOCA's During Operation With One Loop Out of Service for Plants Without Loop lation Valves," WCAP-9166, February 1978. lL Eicheldinger, C., "Westinghouse ECCS Evaluation Model, February 1978 Version," WCAP-9220 (Proprietary Version), WCAP-9221 tary Version), February 1978. 12. Letter from T. M. Anderson of Westinghouse Electric Corporation to John Stolz of the Nuclear Regulatory Co11111ission, letter ntJ11ber NS-TMA-1830, June 16, 1978. 13. Letter from T. M. Anderson of Westinghouse Electric Corporation to John Stolz of the Nuclear Regulatory C0111T1ission, letter ntJ11ber NS-TMA-1834, June 20, 1978. 14. Letter from C. Eichelainger of Westinghouse Electric Corporation to V. Stello of the Nuclear Regulatory C011111ission.
* 10. Kelly, R. D., Thompson, C. M., et al., "Westinghouse Emergency Core Cooling System Evaluation Model for Analyzing Large LOCA's During Operation With One Loop Out of Service for Plants Without Loop lation Valves," WCAP-9166, February 1978. lL Eicheldinger, C., "Westinghouse ECCS Evaluation Model, February 1978 Version," WCAP-9220 (Proprietary Version), WCAP-9221 tary Version), February 1978. 12. Letter from T. M. Anderson of Westinghouse Electric Corporation to John Stolz of the Nuclear Regulatory Co11111ission, letter ntJ11ber NS-TMA-1830, June 16, 1978. 13. Letter from T. M. Anderson of Westinghouse Electric Corporation to John Stolz of the Nuclear Regulatory C0111T1ission, letter ntJ11ber NS-TMA-1834, June 20, 1978. 14. Letter from C. Eichelainger of Westinghouse Electric Corporation to V. Stello of the Nuclear Regulatory C011111ission.
Letter NtJ11ber NS-CE-1163, dated August 13, 1976. N 15. Beck, s. and Kemper, R. M., "Westinghouse ECCS Four-Loop Plant ( 17 x 17) Sensitivity Studies," WCAP-8865, October 19!6. 16. Salvatori, R., "Westinghouse ECCS -Plant Sensitivity Studies," WCAP-8340, July 1974 (Proprietary) and July 1974 Propri etary). 17. Johnson, w. J., Massie, H. w. and Thompson, C. M., "Westinghouse ECCS Loo'if>Plant (17 x 17) Sensitivity Studies," WCAP-8565, July 1975 (Proprietary) and WCAP-8S66, July 1975 (Non-Proprietary).  
Letter NtJ11ber NS-CE-1163, dated August 13, 1976. N 15. Beck, s. and Kemper, R. M., "Westinghouse ECCS Four-Loop Plant ( 17 x 17) Sensitivity Studies," WCAP-8865, October 19!6. 16. Salvatori, R., "Westinghouse ECCS -Plant Sensitivity Studies," WCAP-8340, July 1974 (Proprietary) and July 1974 Propri etary). 17. Johnson, w. J., Massie, H. w. and Thompson, C. M., "Westinghouse ECCS Loo'if>Plant (17 x 17) Sensitivity Studies," WCAP-8565, July 1975 (Proprietary) and WCAP-8S66, July 1975 (Non-Proprietary).
: 18. U.s.* Nuclear Regulatory Commission letter, D. G. Eisenhut to ities With Operati'ng Light Water Reactors, November 9, 1979
: 18. U.s.* Nuclear Regulatory Commission letter, D. G. Eisenhut to ities With Operati'ng Light Water Reactors, November 9, 1979
* SGS-UFSAR 15.4-102 Revision 0 July 22, 1982   
* SGS-UFSAR 15.4-102 Revision 0 July 22, 1982   
Line 181: Line 181:
* 20. Letter from T. M. Anderson of Westinghouse Electric Corporation to D. G. Eisenhut of the Nuclear Regulatory Co11111ission 1 letter ntJnber NS-TMA-2147 1 November 2 1 1979. 21. Letter from T. M. Anderson of Westinghouse Electric Corporation to D. G. Eisenhut of the Nuclear Regulatory Commission, letter nlJllber NS-TMA-2163 1 November 16 1 1979. 22. Letter from T. M. Anderson of Westinghouse Electric Corporation to D. G. Eisenhut of the Nuclear Regulatory C011111ission 1 letter nlJllber NS-TMA-2174 1 December 7 1 1979. 23. Letter from T. M. Anderson of Westinghouse Electric Corporation to Denise of the Nuclear Regulatory Comnission, letter nt1nber NS-TMA-2175 1 December 10 1 1979
* 20. Letter from T. M. Anderson of Westinghouse Electric Corporation to D. G. Eisenhut of the Nuclear Regulatory Co11111ission 1 letter ntJnber NS-TMA-2147 1 November 2 1 1979. 21. Letter from T. M. Anderson of Westinghouse Electric Corporation to D. G. Eisenhut of the Nuclear Regulatory Commission, letter nlJllber NS-TMA-2163 1 November 16 1 1979. 22. Letter from T. M. Anderson of Westinghouse Electric Corporation to D. G. Eisenhut of the Nuclear Regulatory C011111ission 1 letter nlJllber NS-TMA-2174 1 December 7 1 1979. 23. Letter from T. M. Anderson of Westinghouse Electric Corporation to Denise of the Nuclear Regulatory Comnission, letter nt1nber NS-TMA-2175 1 December 10 1 1979
* 24. Geets 1 J. M., "MARVEL -A Digital Computer Code for Transient sis of a Multi loop PWR System. 11 WCAP-7909 1 June 1972. 25. Moody 1 F. s., 11 Transacti ons of the ASME 1 Journal of Heat Transfer, 11 Figure 3 1 page 134 1 February 1965. 26. Bordelon, F. M., "Calculation of Flow Coastdown After Loss of tor Coolant Pt1np (PHOENIX Code)1 11 WCAP-7973 1 September 1972. 27. Burnett, T. W. T.1 Mcintyre.
* 24. Geets 1 J. M., "MARVEL -A Digital Computer Code for Transient sis of a Multi loop PWR System. 11 WCAP-7909 1 June 1972. 25. Moody 1 F. s., 11 Transacti ons of the ASME 1 Journal of Heat Transfer, 11 Figure 3 1 page 134 1 February 1965. 26. Bordelon, F. M., "Calculation of Flow Coastdown After Loss of tor Coolant Pt1np (PHOENIX Code)1 11 WCAP-7973 1 September 1972. 27. Burnett, T. W. T.1 Mcintyre.
C. J., Buker, J. C. and Rose, R. P., "LOFTRAN Code Description," WCAP-7907 1 June 1972. 28. Huni n 1 C. 1 "FACTRAN, A Fortran IV Code for Thenna 1 Transients in a U0 2 Fuel Rod 1 11 WCAP-7908 1 June 1972. 29. Burnett, T. w. T., "Reactor Protection System Diversity in Westing-* house Pressurized Water Reactors." WCAP-7306, Apri 1 1969. SGS-UFSAR 15.4-103 Revision O *July 22, 1982
C. J., Buker, J. C. and Rose, R. P., "LOFTRAN Code Description," WCAP-7907 1 June 1972. 28. Huni n 1 C. 1 "FACTRAN, A Fortran IV Code for Thenna 1 Transients in a U0 2 Fuel Rod 1 11 WCAP-7908 1 June 1972. 29. Burnett, T. w. T., "Reactor Protection System Diversity in Westing-* house Pressurized Water Reactors." WCAP-7306, Apri 1 1969. SGS-UFSAR 15.4-103 Revision O *July 22, 1982
: 30. Taxelius, T. G. (Ed), "Annual Report -Spert Project, 1968, September 1969," Idaho N11:lear Corporation IN-1370, June 1970.
: 30. Taxelius, T. G. (Ed), "Annual Report -Spert Project, 1968, September 1969," Idaho N11:lear Corporation IN-1370, June 1970.
* 31." Liimataninen, R. C. and Testa, F. J., "Studies in TREAT of Zirca-loy-2-Clad, U0 2-core Simulated Fuel Elements," ANL-7225, January -June 1966, p. 177, November 1966. 32. Risher, D. H., Jr., 11 An Evaluation of the Rod Ejection Accident in Westinghouse Pressurized Water Reactors Using Spatial Kinetics Methods,M WCAP-7588, Revision 1-A, January 1975. 33. Rf sher, D. H., Jr., and Barry, R. F., -A Multi-Dimensional Neutron Kinetics Computer Code," WCAP-7979-P-A, January 1975 prietary) and WCAP-8028-A, January 1975 (Non-Proprietary).  
* 31." Liimataninen, R. C. and Testa, F. J., "Studies in TREAT of Zirca-loy-2-Clad, U0 2-core Simulated Fuel Elements," ANL-7225, January -June 1966, p. 177, November 1966. 32. Risher, D. H., Jr., 11 An Evaluation of the Rod Ejection Accident in Westinghouse Pressurized Water Reactors Using Spatial Kinetics Methods,M WCAP-7588, Revision 1-A, January 1975. 33. Rf sher, D. H., Jr., and Barry, R. F., -A Multi-Dimensional Neutron Kinetics Computer Code," WCAP-7979-P-A, January 1975 prietary) and WCAP-8028-A, January 1975 (Non-Proprietary).
: 34. Barry, R. F., "LEOPARD -A Spectr1J11 Dependent Non-Spatial Depletion Code for the IBM-7094, 11 WCAP-3269-26, September 1963. 35. Bi shop, A. A., Sanberg, R. a. and Tong, L. s., "Forced Convection Heat Transfer at High Pressure After the Critical Heat Flux," ASME I . 65-HT-31, August 1965. 36. "Westinghouse Mass and Energy Re lease Datas for Contai ment Design, 11 WCAP-826.4 (Proprf etary) and WCAP-8312 (Non-Proprietary).  
: 34. Barry, R. F., "LEOPARD -A Spectr1J11 Dependent Non-Spatial Depletion Code for the IBM-7094, 11 WCAP-3269-26, September 1963. 35. Bi shop, A. A., Sanberg, R. a. and Tong, L. s., "Forced Convection Heat Transfer at High Pressure After the Critical Heat Flux," ASME I . 65-HT-31, August 1965. 36. "Westinghouse Mass and Energy Re lease Datas for Contai ment Design, 11 WCAP-826.4 (Proprf etary) and WCAP-8312 (Non-Proprietary).
: 37. Dittus, F. w., and Boelter, L. M. K., University of California (Berkely), Publs, Eng., &#xa3; 433 (1930). 38. Jens, w. H., and Lottes, P. A., "Analysts of Heat Transfer, Burnout, PresslJT'e D_rop, and Density Data for High Pressure*Water, 11 USAEC Report ANL-4627 (1951). SGS-UFSAR 15.4-104 Revision 0 July 22, 1982
: 37. Dittus, F. w., and Boelter, L. M. K., University of California (Berkely), Publs, Eng., &#xa3; 433 (1930). 38. Jens, w. H., and Lottes, P. A., "Analysts of Heat Transfer, Burnout, PresslJT'e D_rop, and Density Data for High Pressure*Water, 11 USAEC Report ANL-4627 (1951). SGS-UFSAR 15.4-104 Revision 0 July 22, 1982
* 39. Macbech, R. V., "Burnout Analysis, Pt. 2, The Basis Burn-out Curve," U. K. Report AEEW-R 167, Winfrith (1963). Also Pt. 3, "The Low-Velocity Burnout Regimes," AEEW-R 222 (1963); Pt. 4, "Application of Local Conditions Hypothesis to World Data for. Unifonnly Heated Round Tubes and Rectangular Channels,*
* 39. Macbech, R. V., "Burnout Analysis, Pt. 2, The Basis Burn-out Curve," U. K. Report AEEW-R 167, Winfrith (1963). Also Pt. 3, "The Low-Velocity Burnout Regimes," AEEW-R 222 (1963); Pt. 4, "Application of Local Conditions Hypothesis to World Data for. Unifonnly Heated Round Tubes and Rectangular Channels,*
AEEW-R 267 (1963). 40. Dougall, R. s., Rehsenow, w. M., Film Boiling on the Inside of Vertical Tubes with Upward Flow of Fluid at Low Quantities, MIT Report 9079-26. 41. EcEligot, D. M., Onnond, L.W., and Perkins, Jr., H. C., "Internal Low Reynolds -Nunber Turbulent and Transitional Gas Flow with Heat Transfer," nal of Heat Transfer, 88, 239-245 (May 1966). 42. W. H. 172. at Transmission, McGraw-Hill 3rd edition, 1954, p. 43. Cunningham, V. P., and Yeh, H. C., "Experiments and Void Correlation for PWR Small-Break LOCA Condition," Transactions of American Nuclear Society, Vol. 17, Nov. 1973, pp. 369-370. 44. lagC111i, Takaski, "Interim Report on Safety Assessments and Facilities Establishment Project in Japan for Period Ending June 196 5 ( N 0
AEEW-R 267 (1963). 40. Dougall, R. s., Rehsenow, w. M., Film Boiling on the Inside of Vertical Tubes with Upward Flow of Fluid at Low Quantities, MIT Report 9079-26. 41. EcEligot, D. M., Onnond, L.W., and Perkins, Jr., H. C., "Internal Low Reynolds -Nunber Turbulent and Transitional Gas Flow with Heat Transfer," nal of Heat Transfer, 88, 239-245 (May 1966). 42. W. H. 172. at Transmission, McGraw-Hill 3rd edition, 1954, p. 43. Cunningham, V. P., and Yeh, H. C., "Experiments and Void Correlation for PWR Small-Break LOCA Condition," Transactions of American Nuclear Society, Vol. 17, Nov. 1973, pp. 369-370. 44. lagC111i, Takaski, "Interim Report on Safety Assessments and Facilities Establishment Project in Japan for Period Ending June 196 5 ( N 0
* 1 ) II 45. Kolflat, A., and Chittenden, W. A., "A New Approach to the Design of Contairment Shells for Atomic Power Plants". Proc. of Amer. Power Conf.,_1957  
* 1 ) II 45. Kolflat, A., and Chittenden, W. A., "A New Approach to the Design of Contairment Shells for Atomic Power Plants". Proc. of Amer. Power Conf.,_1957
: p. 651-9. 46. McAdams, w. H., Heat Transmission , 3rd Edition, McGraw-Hill Book Co., Inc., New York (1954). 47. Standards of Tubular Exchanger Manufacturers Association SGS-UFSAR 15.4-105 Revision 0 Julv 22. 1982
: p. 651-9. 46. McAdams, w. H., Heat Transmission , 3rd Edition, McGraw-Hill Book Co., Inc., New York (1954). 47. Standards of Tubular Exchanger Manufacturers Association SGS-UFSAR 15.4-105 Revision 0 Julv 22. 1982
* 48. Eckert, E. R. G., and Drake, P. M. J., Heat and Mass  
* 48. Eckert, E. R. G., and Drake, P. M. J., Heat and Mass  
.* McGraw-Hill Book Co., Inc., New York (1959). 49. Eckert, E. and Gross, J., "Introduction to Heat and Mass Transfer", McGraw-Hill, 1963. 50. Kern, D. Q., Process Heat Transfer, McGraw-Hill Book Inc., New York ( 1950). 51. Chilton, T. H., and Colburn, A. P., "Mass Trarisfer (Absorption)
.* McGraw-Hill Book Co., Inc., New York (1959). 49. Eckert, E. and Gross, J., "Introduction to Heat and Mass Transfer", McGraw-Hill, 1963. 50. Kern, D. Q., Process Heat Transfer, McGraw-Hill Book Inc., New York ( 1950). 51. Chilton, T. H., and Colburn, A. P., "Mass Trarisfer (Absorption)
Coefficients Prediction from Data on Heat Transfer and Fluid Friction", Imd. Eng. Chem., 26, (1934),_ pp. 1183-87. 52. WCAP Topical Report -Reactor Contairment Fan Cooler Cooling Test Coil, w. L. Boettinger, July 1969. 53. S. Weinberg, Proc. Inst. Mech. Engr., 164, pp. 240-258, 1952 54. Ranz, w. and Marshall, w., Chem, Engr., Prog. 48, 3, pp. 141-146 and 48, 4, pp. 173-180, 1952. 55. Perry, J., "Chemical Engineers Handbook" 3rd Ed. McGraw-Hi 11, 1950. 56. Letter to Mr. D. B. Vassallo, Chief, Light Water Reactor Projects Branch 6, USNRC, From Mr. C. Eicheldinger, Manager, Nuclear Safety, Westinghouse Electric Corporation, Dated March 17, 1976 (NS-CE-992).  
Coefficients Prediction from Data on Heat Transfer and Fluid Friction", Imd. Eng. Chem., 26, (1934),_ pp. 1183-87. 52. WCAP Topical Report -Reactor Contairment Fan Cooler Cooling Test Coil, w. L. Boettinger, July 1969. 53. S. Weinberg, Proc. Inst. Mech. Engr., 164, pp. 240-258, 1952 54. Ranz, w. and Marshall, w., Chem, Engr., Prog. 48, 3, pp. 141-146 and 48, 4, pp. 173-180, 1952. 55. Perry, J., "Chemical Engineers Handbook" 3rd Ed. McGraw-Hi 11, 1950. 56. Letter to Mr. D. B. Vassallo, Chief, Light Water Reactor Projects Branch 6, USNRC, From Mr. C. Eicheldinger, Manager, Nuclear Safety, Westinghouse Electric Corporation, Dated March 17, 1976 (NS-CE-992).
: 57. Letter to Mr. D. B. Vassalo, Chief, Light Water Reactor Projects Branch 6, USNRC, from Mr. C. Eicheldinger, Manager, Nuclear Safety, Electric Corporation, Dated July 10, 1975 (NS-CE-692).  
: 57. Letter to Mr. D. B. Vassalo, Chief, Light Water Reactor Projects Branch 6, USNRC, from Mr. C. Eicheldinger, Manager, Nuclear Safety, Electric Corporation, Dated July 10, 1975 (NS-CE-692).
: 58. Letter to Mr. D. B. Vassalo, Chief, Light Water Reactor Projects Branch 6, USNRC, From Mr. C. Eicheldinger, Manager, Nuclear Safety, Westinghouse Electric Corporation, Dated April 7, 1976 (NS-CE-1021)
: 58. Letter to Mr. D. B. Vassalo, Chief, Light Water Reactor Projects Branch 6, USNRC, From Mr. C. Eicheldinger, Manager, Nuclear Safety, Westinghouse Electric Corporation, Dated April 7, 1976 (NS-CE-1021)
* SGS-UFSAR 15.4-106 Revision O July 22, 1982   
* SGS-UFSAR 15.4-106 Revision O July 22, 1982   
*
*
* 59. Letter to Mr. J. F. Stolz, Chief, Light Water Reactor Projects Branch 6, From Mr. C. Eicheldinger, Manager, Nuclear Safety, Westinghouse Electric Corporation, Dated August 27, 1976 60. ( NS-CE-1883).
* 59. Letter to Mr. J. F. Stolz, Chief, Light Water Reactor Projects Branch 6, From Mr. C. Eicheldinger, Manager, Nuclear Safety, Westinghouse Electric Corporation, Dated August 27, 1976 60. ( NS-CE-1883).
Hsieh, T., et. al., 11 Envirormental Qualification Instrt.ment Transmitter Temperature Transient Analysis, 11 WCAP-8936, February 1977 (Proprietary) and WCAP-8937, February 1977 (Non-proprietary).  
Hsieh, T., et. al., 11 Envirormental Qualification Instrt.ment Transmitter Temperature Transient Analysis, 11 WCAP-8936, February 1977 (Proprietary) and WCAP-8937, February 1977 (Non-proprietary).
: 61. Letter to John F. Stolz, Chief, Light Water Reactor Projects Branch 6, USNRC, from C. Eicheldinger, Manager, -Nuclear Safety Westinghouse Electric Corporation, Dated June 14, 1977. (NS-CE-1453).
: 61. Letter to John F. Stolz, Chief, Light Water Reactor Projects Branch 6, USNRC, from C. Eicheldinger, Manager, -Nuclear Safety Westinghouse Electric Corporation, Dated June 14, 1977. (NS-CE-1453).
ft.( f.(..f " L J..dd J . 62. Krise, R. C., Miranda, s .*
ft.( f.(..f " L J..dd J . 62. Krise, R. C., Miranda, s .*
A Bigital Code For Transient AnalJ si ! of a Leep PWR System, 11 WCAP 8843,' Nor;ember, 1977 (PP"ef3rietary) and WCAP 8844, Nor;ember, 1977 (Non p1oprietary}.  
A Bigital Code For Transient AnalJ si ! of a Leep PWR System, 11 WCAP 8843,' Nor;ember, 1977 (PP"ef3rietary) and WCAP 8844, Nor;ember, 1977 (Non p1oprietary}.
: 63. Land, R. E ** "Mass and Energy Releases Following a Steanline Rupture, 11 WCAP-8822, September, 1976 (Proprietary) and WCAP-8860, September, 1976 (Non-proprietary).  
: 63. Land, R. E ** "Mass and Energy Releases Following a Steanline Rupture, 11 WCAP-8822, September, 1976 (Proprietary) and WCAP-8860, September, 1976 (Non-proprietary).
: 64. 11 Eval uati on of the Reactor Coo 1 ant System Considering Subcompartment Pressurization Following a LOCA for Salem\.Units 1 and 2, 11 transmitted by PSEG letter, R. L. Mottle to O. 0. Parr, dated March 6, 1979
: 64. 11 Eval uati on of the Reactor Coo 1 ant System Considering Subcompartment Pressurization Following a LOCA for Salem\.Units 1 and 2, 11 transmitted by PSEG letter, R. L. Mottle to O. 0. Parr, dated March 6, 1979
* SGS*UFSAR 15.4-107 Revision O .l11lv '' _ lQQ..2_____   
* SGS*UFSAR 15.4-107 Revision O .l11lv '' _ lQQ..2_____   
Line 227: Line 227:
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Line 236: Line 236:
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Line 256: Line 256:
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Line 274: Line 274:
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Line 284: Line 284:
,;, Time (sec.) TABLE 15.4-28 Q.f44 Sheet 1 of 10 MASS AND ENERGY RELEASES FROM A FT2 SPLIT BREAK 3o AT rn PERCENT POWER (Worst Te111@eiaai1:1iae Case) Break Flow (lb/sec.)
,;, Time (sec.) TABLE 15.4-28 Q.f44 Sheet 1 of 10 MASS AND ENERGY RELEASES FROM A FT2 SPLIT BREAK 3o AT rn PERCENT POWER (Worst Te111@eiaai1:1iae Case) Break Flow (lb/sec.)
PR6PRIETAR'f RefeF te {5Q 311) "A13111ieatiert fe,. Witl:it:ieleiRg" Ra L. Mittl te Sla" 9. Par1 November 20, U78 ttd-NRC Af:lf31"9val letteP, Qlart Q, PaFF te Jani:ia1) 22, 1979 Energy Flow (million Btu/sec.)
PR6PRIETAR'f RefeF te {5Q 311) "A13111ieatiert fe,. Witl:it:ieleiRg" Ra L. Mittl te Sla" 9. Par1 November 20, U78 ttd-NRC Af:lf31"9val letteP, Qlart Q, PaFF te Jani:ia1) 22, 1979 Energy Flow (million Btu/sec.)
SGS-UFSAR Revision 0 July 22, 1982 Sheet 2 of 10 Break Flow Energy Flow Time Break Flow Energy Flow ec.J (lblsec. l !million Btu/sec.l  
SGS-UFSAR Revision 0 July 22, 1982 Sheet 2 of 10 Break Flow Energy Flow Time Break Flow Energy Flow ec.J (lblsec. l !million Btu/sec.l
{sec.l {lb/sec.l  
{sec.l {lb/sec.l
{million Btu/sec.)
{million Btu/sec.)
0.0000 0.0000 0.0000 J7.SU 1420. 1.104
0.0000 0.0000 0.0000 J7.SU 1420. 1.104
Line 299: Line 299:
* 1.417
* 1.417
* oo 1460. 1.751 71.00 1175
* oo 1460. 1.751 71.00 1175
* 1.413 33.50 1456. 1.746 11.50 1172. 1.410 34.00 1451. 1.741 72.00 1169. 1.406 34050 1447. 1.736 72.50 1166. 1.403 35.00 1443. 1.731 13.00 1163. 1.399 35.50 1439. 1.726 73.50 1160. 1.396 36.00 1434. 1.121 74.00 1157. 1.392 36.50 1430. 1.715 74.50 1154. 1.319 37.00 1425. 1.110 Sheet 3 of* 10 Break Flow Energy Flow Time Break Flow Energy Flow l blsec. l {million Btu/sec.l  
* 1.413 33.50 1456. 1.746 11.50 1172. 1.410 34.00 1451. 1.741 72.00 1169. 1.406 34050 1447. 1.736 72.50 1166. 1.403 35.00 1443. 1.731 13.00 1163. 1.399 35.50 1439. 1.726 73.50 1160. 1.396 36.00 1434. 1.121 74.00 1157. 1.392 36.50 1430. 1.715 74.50 1154. 1.319 37.00 1425. 1.110 Sheet 3 of* 10 Break Flow Energy Flow Time Break Flow Energy Flow l blsec. l {million Btu/sec.l
{sec. l {lb/sec.l  
{sec. l {lb/sec.l
{million Btu/sec.) 1151. 1cJl5 112.0 i7*.* 1.056 75 .. 50 1149. 1.382 112.5 166.1 1.044 76.00 1146. 1.378 113.0 157.Z 1.033 76 .. 1143. 1.375 113.S 141.0 1.021 11.00 1140. 1.31Z 114.0 139.1 1.011 114.,5 ll0.5 1.000 11.50 1137. 1.368 115.0 122.1 .9902 11.00 'i134. 1.365 ,15.5 114.0 .990S 1lo50 1131. 1.361 116.0 I06.Z .9710 19.00 1128. '93SI 198.6 .9618 79.50 1125. 1.354 116 .. S 191.2 .9529 I0.00 1123. 1.351 117.0 I0.50 1120. 1.348 l1o00 1117. 1.344 11.50 1114. 1.341 117.S 714.0 .9442 12.00 1111. 1.337 111.0 776.t .9357 az.so 1109. 1.334 111.S 110.t .t275 13.00 1106. 1.331 119.0 765.5 .9194 13.SO 1103. 1.327 119.S 151.9 .9116 14.00 1100. 1.324 120.0 HO. .9040 14.SO 1097. 1.321 120.S 744.5 .1966 IS.00 109'. 1.311 121.0 731.5 .1893 15.SO 1092. 1.314 121.s 732.6 .1822 16.00 1089. 1.311 12l.O 726.f .1753 16.SO 1086. 1.JOI 122.S 721.J .1685 11.00 1084. 1.305 123.0 115.t .1620
{million Btu/sec.) 1151. 1cJl5 112.0 i7*.* 1.056 75 .. 50 1149. 1.382 112.5 166.1 1.044 76.00 1146. 1.378 113.0 157.Z 1.033 76 .. 1143. 1.375 113.S 141.0 1.021 11.00 1140. 1.31Z 114.0 139.1 1.011 114.,5 ll0.5 1.000 11.50 1137. 1.368 115.0 122.1 .9902 11.00 'i134. 1.365 ,15.5 114.0 .990S 1lo50 1131. 1.361 116.0 I06.Z .9710 19.00 1128. '93SI 198.6 .9618 79.50 1125. 1.354 116 .. S 191.2 .9529 I0.00 1123. 1.351 117.0 I0.50 1120. 1.348 l1o00 1117. 1.344 11.50 1114. 1.341 117.S 714.0 .9442 12.00 1111. 1.337 111.0 776.t .9357 az.so 1109. 1.334 111.S 110.t .t275 13.00 1106. 1.331 119.0 765.5 .9194 13.SO 1103. 1.327 119.S 151.9 .9116 14.00 1100. 1.324 120.0 HO. .9040 14.SO 1097. 1.321 120.S 744.5 .1966 IS.00 109'. 1.311 121.0 731.5 .1893 15.SO 1092. 1.314 121.s 732.6 .1822 16.00 1089. 1.311 12l.O 726.f .1753 16.SO 1086. 1.JOI 122.S 721.J .1685 11.00 1084. 1.305 123.0 115.t .1620
* 11.so 1081. 1.301 123.S 110.5 .1555 11 .. 00 1071. 1.291 124e0 105.i .1492 II.SO 107,. t.m *24.5 100. .1431 . . 19.00 1073. t.Z92 125.0 695.J .1371 -1010. 1.m 125.S t90.5 .1313 1068. 1.285 126.0 615.1 .12S6 1065. 1.212 126.S 611.1 .l200 1062. 1.219 127.0 676.6 .1146 '1.SO 1060. 1.276 127.5 672.2 .I093 J2.00 1057. 1.273 128.0 661.0 .I041 92.SO 1055. 1.210 128.5 663.I .7990 93.00 1052. 1.267 129.0 659.7 .1941 93.SO 1049. 1.263 129.S 655.7 .7893 . 94.00 1047. 1.260 130 .. 0 651.1 .7146 94.SO 1044. 1.257 130.5 641.0 .7800 95.00 1042. 1.254 131.0 644 .. J .;1755 95.50 1039. 1.251 131.5 640.1 .7111 96.00 1037. 1.248 132.0 637.Z .7669 96.50 1034. 1.245 132.5 w.a .7627 97.00 1032. 1.;242 133.0 630.5 .7Sl7 133.5 6Z7.2 .7548 97.50 10Zt. 1.ZJ9 134.0 6Z4.1 .7510 91.00 1027. 1.236 134.5 621.0 .7472 91.50 1024. 1.2JJ 135.0 611.0 .7436 99.00 1022. 1.230 135.5 615.1 .7401 99.50 1019. 1.221 136.0 612.Z .7367 100.0 1011. -1.224 136.5 609.5 .7333 100.5 1014. : 1.221 137.0 606.1 .7301 101.0 1012. 1.211 101.s 1009. 1.215 117.5 604.2 .7269 102.0 1007. . 1.212 138.0 601.6 .7238 102.S 1004. 1.209 131.5 599.1 .1208 103.0 1002. 1.206 139.0 596.7 .7179 103.S 999.4 1.ZOJ 139.5 594.4 .7151 104.0 996.7 1.200 140.0 192.1 .7123 104.S 994.S 1.191 140.5 "*' .1096 105.0 "'*' 1.1M 141.0 511.1 .1010 105.5 919.7 1.192 141.5 515 ** .1045 106.0 917.1 1.119 142.0 sas.* .1020 9-' 915.0 1.116 142.5 511.6 .6996 g 912.4 1.113 143.0 519.7 .6913 ..... 1.191 143.5 577.9 .6950 969.7 1.161 144.0 516.0 .6928 !)8.5 956.S 1.152 144.5 574.J .6901 .09.0 94:S.I 1.131 145.0 572.6 .6186 1"9.5 931.6 1.122 145.S 510.9 .6166 110.0 "'*' 1.108 146.0 569.J .6847 110.S 90l.J 1.094 146.5 567.7 .6127 111.0 197.4 1.0l1 147.0 566.Z .6809  
* 11.so 1081. 1.301 123.S 110.5 .1555 11 .. 00 1071. 1.291 124e0 105.i .1492 II.SO 107,. t.m *24.5 100. .1431 . . 19.00 1073. t.Z92 125.0 695.J .1371 -1010. 1.m 125.S t90.5 .1313 1068. 1.285 126.0 615.1 .12S6 1065. 1.212 126.S 611.1 .l200 1062. 1.219 127.0 676.6 .1146 '1.SO 1060. 1.276 127.5 672.2 .I093 J2.00 1057. 1.273 128.0 661.0 .I041 92.SO 1055. 1.210 128.5 663.I .7990 93.00 1052. 1.267 129.0 659.7 .1941 93.SO 1049. 1.263 129.S 655.7 .7893 . 94.00 1047. 1.260 130 .. 0 651.1 .7146 94.SO 1044. 1.257 130.5 641.0 .7800 95.00 1042. 1.254 131.0 644 .. J .;1755 95.50 1039. 1.251 131.5 640.1 .7111 96.00 1037. 1.248 132.0 637.Z .7669 96.50 1034. 1.245 132.5 w.a .7627 97.00 1032. 1.;242 133.0 630.5 .7Sl7 133.5 6Z7.2 .7548 97.50 10Zt. 1.ZJ9 134.0 6Z4.1 .7510 91.00 1027. 1.236 134.5 621.0 .7472 91.50 1024. 1.2JJ 135.0 611.0 .7436 99.00 1022. 1.230 135.5 615.1 .7401 99.50 1019. 1.221 136.0 612.Z .7367 100.0 1011. -1.224 136.5 609.5 .7333 100.5 1014. : 1.221 137.0 606.1 .7301 101.0 1012. 1.211 101.s 1009. 1.215 117.5 604.2 .7269 102.0 1007. . 1.212 138.0 601.6 .7238 102.S 1004. 1.209 131.5 599.1 .1208 103.0 1002. 1.206 139.0 596.7 .7179 103.S 999.4 1.ZOJ 139.5 594.4 .7151 104.0 996.7 1.200 140.0 192.1 .7123 104.S 994.S 1.191 140.5 "*' .1096 105.0 "'*' 1.1M 141.0 511.1 .1010 105.5 919.7 1.192 141.5 515 ** .1045 106.0 917.1 1.119 142.0 sas.* .1020 9-' 915.0 1.116 142.5 511.6 .6996 g 912.4 1.113 143.0 519.7 .6913 ..... 1.191 143.5 577.9 .6950 969.7 1.161 144.0 516.0 .6928 !)8.5 956.S 1.152 144.5 574.J .6901 .09.0 94:S.I 1.131 145.0 572.6 .6186 1"9.5 931.6 1.122 145.S 510.9 .6166 110.0 "'*' 1.108 146.0 569.J .6847 110.S 90l.J 1.094 146.5 567.7 .6127 111.0 197.4 1.0l1 147.0 566.Z .6809  
..... 1.061 147.5 564.7 .6191 Sheet 4 of 10 Break Flow Energy Flow Time Break Flow Energy Flow lb/sec.) (million  
..... 1.061 147.5 564.7 .6191 Sheet 4 of 10 Break Flow Energy Flow Time Break Flow Energy Flow lb/sec.) (million
{lbLsec. {million Btu/sec. 141.0 563.Z .6m 115.0 515.Z .61'2 148.5 =*I .6156 115.5 514.f .6119 149.0 .4 .6740 116.0 514.1 .6115 149.5 559.1 .6723 116.S 514.4 .6112 150.0 557.1 .6108 111.0 514.Z .6119 150.S 556.5 .6692 111.s 51J.f .6176 151.0 555.J .6671 111.0 I"*' .6173 151.5 554.1 .6663 181.5 1J.4 .6110 152.0 553.0 .6649 11900 513.Z .6167 152 .. 5 551.1 .'635 119.5 512.t .6164 153.0 550.7 .6622 190.0 512.1 .6161 153.5 549.6 .6609 190.S 512.5 .6158 154.0 548.6 .6596 '91 .. 0 512.2 .6156 154.5 547.6 .6514 '91.S 112.0 .6153 155.0 546.6 .6572 192.0 511.I .6150 155.5 545.6 .6560 192.5 511.5 .6141 156.0 544.7 .6549 193.0 511.J' .6145 156.5 543.1 .6531 '93.5 511.1 .6142 157.0 542.9 .6527 194.0 510.f -.6140 194.5 510.7 .6137 157.5 542.0 .'517 195.0 510.5 .6135 195.5 510.J .6132 151.0 541.Z ** S06 196.0 510.1 .6130 151.5 m*' .6496 196.5 509.9 .6127 159.0 .s .6417 191.0 509.7 .6125 159.5 ** .6411 160.0 531.0 *""' . 160.5 537.2 .6459 '97.5 509 .. 5 .6122 161.0 536=5 .6450 19'.0 509.J .6120 1.5 "5.1 .. 6441 191.5 509.1 .. 6111
{lbLsec. {million Btu/sec. 141.0 563.Z .6m 115.0 515.Z .61'2 148.5 =*I .6156 115.5 514.f .6119 149.0 .4 .6740 116.0 514.1 .6115 149.5 559.1 .6723 116.S 514.4 .6112 150.0 557.1 .6108 111.0 514.Z .6119 150.S 556.5 .6692 111.s 51J.f .6176 151.0 555.J .6671 111.0 I"*' .6173 151.5 554.1 .6663 181.5 1J.4 .6110 152.0 553.0 .6649 11900 513.Z .6167 152 .. 5 551.1 .'635 119.5 512.t .6164 153.0 550.7 .6622 190.0 512.1 .6161 153.5 549.6 .6609 190.S 512.5 .6158 154.0 548.6 .6596 '91 .. 0 512.2 .6156 154.5 547.6 .6514 '91.S 112.0 .6153 155.0 546.6 .6572 192.0 511.I .6150 155.5 545.6 .6560 192.5 511.5 .6141 156.0 544.7 .6549 193.0 511.J' .6145 156.5 543.1 .6531 '93.5 511.1 .6142 157.0 542.9 .6527 194.0 510.f -.6140 194.5 510.7 .6137 157.5 542.0 .'517 195.0 510.5 .6135 195.5 510.J .6132 151.0 541.Z ** S06 196.0 510.1 .6130 151.5 m*' .6496 196.5 509.9 .6127 159.0 .s .6417 191.0 509.7 .6125 159.5 ** .6411 160.0 531.0 *""' . 160.5 537.2 .6459 '97.5 509 .. 5 .6122 161.0 536=5 .6450 19'.0 509.J .6120 1.5 "5.1 .. 6441 191.5 509.1 .. 6111
* 0 535.1 .6433 1".o SOl.9 .6115. 5 r* .6425 1".5 SOl.7 .61'3 .o 13.1 .6417 200.0 =*' .6111 SJ.1 .6409 200.5 .J .6108 '4.0 SZ.5 .'401 201.0 SOl.1 .6106 .64.5 131.* .6394 201.5 507.9 .6104 165.0 31.S .6316 202.0 507.1 .6102 165.5 530.7 .6319 202.5 131.6 .6099 166.0 530.1 .6372 203.0 7.4 .6091 166.5 529.6 .'366 203.5 507.Z .6095 167.0 529., .6359 204.0 507.0 .6093 167.S sza. .6352 204.5 506.9 *'&deg;" 161.0 5Z1.t .6346 205.0 5(-C.7 .at 161.5 527.4 .634() 205.5 .6086 169.0 526.t .6334 206.0 506.S .6084 169.S 526.4 .6321 206.S 506.Z .6082 170.0  
* 0 535.1 .6433 1".o SOl.9 .6115. 5 r* .6425 1".5 SOl.7 .61'3 .o 13.1 .6417 200.0 =*' .6111 SJ.1 .6409 200.5 .J .6108 '4.0 SZ.5 .'401 201.0 SOl.1 .6106 .64.5 131.* .6394 201.5 507.9 .6104 165.0 31.S .6316 202.0 507.1 .6102 165.5 530.7 .6319 202.5 131.6 .6099 166.0 530.1 .6372 203.0 7.4 .6091 166.5 529.6 .'366 203.5 507.Z .6095 167.0 529., .6359 204.0 507.0 .6093 167.S sza. .6352 204.5 506.9 *'&deg;" 161.0 5Z1.t .6346 205.0 5(-C.7 .at 161.5 527.4 .634() 205.5 .6086 169.0 526.t .6334 206.0 506.S .6084 169.S 526.4 .6321 206.S 506.Z .6082 170.0  
.6322 207.0 506.0 .ao 170.S 525. .6316 207.S 505.1 .t071 111.0 525.0 .6311 208.0 181*6 .6076 171.5 524.6 .6305 208.5 .5 .6074 172.0 524.1 .6300 209.0 505.J .6072 172.5 523.7 .6295
.6322 207.0 506.0 .ao 170.S 525. .6316 207.S 505.1 .t071 111.0 525.0 .6311 208.0 181*6 .6076 171.5 524.6 .6305 208.5 .5 .6074 172.0 524.1 .6300 209.0 505.J .6072 172.5 523.7 .6295
* 209e5 50Sa1 .6010 1?3.0 523.J -.6290 210.0 505.0 .6068 173.5 522.9 .6285 210.s 504.1 .6066 174.0 522.5 : .6280 211.0 504.1 .6064 174.S nz.1 .6275 211.5 SOtt.5 .6062 175.0 521.1 .6270 212.0 504.J .6060 175.5 521.J .6265 212.s 504.2 .60SI 176.0 520.9 .6261 213.0 504.0 .6056 176.5 520.5 .6257 213.5 503.1 .* 6054 111.0 520.2 .6252 214.0 503.7 .60S2 214.5 503.5 .6050 117.5 519.1 .6241 215.0 503.4 .6048 215.5 503.2 .6046 111.0 519.5 .6244 216.0 503.1 .6045 41*' 519.1 216.5 502.9 .6043 .o Ill.I .623 211.0 502.1 .6041 .5 "*' .6231 .o 11.1 .6221  
* 209e5 50Sa1 .6010 1?3.0 523.J -.6290 210.0 505.0 .6068 173.5 522.9 .6285 210.s 504.1 .6066 174.0 522.5 : .6280 211.0 504.1 .6064 174.S nz.1 .6275 211.5 SOtt.5 .6062 175.0 521.1 .6270 212.0 504.J .6060 175.5 521.J .6265 212.s 504.2 .60SI 176.0 520.9 .6261 213.0 504.0 .6056 176.5 520.5 .6257 213.5 503.1 .* 6054 111.0 520.2 .6252 214.0 503.7 .60S2 214.5 503.5 .6050 117.5 519.1 .6241 215.0 503.4 .6048 215.5 503.2 .6046 111.0 519.5 .6244 216.0 503.1 .6045 41*' 519.1 216.5 502.9 .6043 .o Ill.I .623 211.0 502.1 .6041 .5 "*' .6231 .o 11.1 .6221
: 11. .6224 111.0 511.S .6220 111.S 111.z .6216 112.0 "*' .6213 112.S 516.6 .6209 113.0 116.J .6205 113.S 16.0 .'202 114.0 s1s.1 .6199 , .... & .,. . .. ,.
: 11. .6224 111.0 511.S .6220 111.S 111.z .6216 112.0 "*' .6213 112.S 516.6 .6209 113.0 116.J .6205 113.S 16.0 .'202 114.0 s1s.1 .6199 , .... & .,. . .. ,.
Sheet 5 of 10 Break Flow Energy Flow Time Break Flow Energy Flow lb/sec.) (million Btu/sec.) (sec.) (lb/sec.)  
Sheet 5 of 10 Break Flow Energy Flow Time Break Flow Energy Flow lb/sec.) (million Btu/sec.) (sec.) (lb/sec.)
{million Btu/sec.)
{million Btu/sec.)
211.s 502.6 .6039 Z55.0 491.4 .5903 502.4 .6037 255.5 491.2 *.5901 211.0 502 .. J .6035 256.0 491.1 .5899 211.s 50Z.'i .6033 256.5 490.9 .5891 219.0 502.0 .6031 257.0 490.I .5196 219.5 .6029 220.0 501.I 220.s 501.7 .6021 H1.5 490.6 .5194 221.0 501.5 .6026 2n.o 490.5 .Sl92 221.s 501.s .6024 zsa.5 490.3 .5'90 222.0 501.Z .6022 H9.0 490.2 .SM9 222.5. 501.0 .6020 259.5 4t0.D .SM7 223.0 500.9 .6011 260.0 m** .SNS 223.5 500.1 .6017 260.5 .7 .SM3 224.0 500.6 .6015 261.0 "'*' .SM1 224.5 500.4 .6013 261.S 419.4 .HIO 225.0 500.3 .6011 2.z.o 4".S .Sl71 225.5 500.1 .6009 262.S 419.1 .Sl76 226.0 500.0 .6007 263.0 4".0 .Sl74 226.5 499.I .6006 263.5 411.1 .Sl72 227.0 499.7 .6004 2'4.0 411.7 .Sl11 227.5 499.5 .6002 264.S 411.5 .5169 221.0 499.4 .6000 H5.0 411.4 .5167 221.5 499.2 .5991 265.S 411.Z .5165 229.0 499.1 .5996 266.0 "'*' .5163 229.5 491.9 .599S 2o6.5 411.0 .5162 230.0 498.I .5993 267.0 417.1 .5'60 230.5 491.6 .5991 267.5 417 .. 7 .5158 231.0 491.5 .5919 261.0 417.5 .5156. 31.5 491 .. 3 .5917 268.5 417.4 .5154 .o 491.2 .5916 269.0 417.Z .5153 .5 . 491.0 .5914 269.5 417.1 .Sl51 .o 497.9 .5912 210.0 416.t .5149 233.5 491.1 .5980 210.s 416.I .5147 234.0 497.6 .5971 211.0 416.6 .Sl45 234.5 497.4 .5971 211.s 416.5 .5143 235.0 497.3 .5975 212.0 416.J .5142 235.5 491.Z .5973 272.5 416.Z .Sl40 236.0 497.0 2n.o 486.0 .5131 236.5 496.9 213.S 415.9 .5136 237.0 496.7 274.0 415.7 .Sl34 274.5 415.6 .5133 237.S 496.6 .5966 275.0 415.4 .5131 238.0 496.4 .5964 275.5 415.S .5129 211.s 496.3 .5962 276.0 415.1 .Sll1 239.0 496.1 .5960 276.5 415.0 .5125 239.5 496.0 .5959 211.0 484.1 .5124 240.0 495.I .5957 240.5 495.7 .5955 zn.s 414.7 .5122 241.0 495.5 .5953 Z71.0 414.5 .Sl20 241.5 495.4 .5952 Z71.S 414.,4 .H11 242.0 49S.Z .5950 279.0 414.2 .5116 242.5 495.1 -.5941 279.5 414.1 .5115 zu.o 494.9 .5946 ZIO.O 413.t .Sl13 243.5 494.I : .5944 2ao.5 413.I .5111 244.0 494.6 .5943 211.0 413.6 .5809 244.5 494.5 .5941 211.s 413.5 .5807 245.0 494.S .5939 212.0 413.J .5806 245.5 494.2 .5937 21z.5 413.Z .SI04 24'.0 494.0 .5935 213.0 413.0 .saoz 246.5 493.9 .5934 213.5 412.t .saoo 247.0 493.7 .5932 214.0 . 412.7 .5198 247.S 493.6 .5930 214.5 W"' .5196 241.0 493.4 .5921 215.0 .4 .5m 241.5 493.J .5926 215.5 412.J .5193 --0 493.2 .5925 216.0 412.1 .5191 .5 491.0 .5923 216.5 412-a .5719 .o 492.9 .5921 211.0 411. .5717 .5 492.7 .5919 211.s 411.7 .5716 lS1.0 492.6 .5917 211.0 411.5 .5714 251.5 492.4 .5916 211.S 411.4 .5712 252.0 492.3 .5914 219.0 411.2 .5710 252.5 492.1 .5912 219.5 411.1 .5nt 253.0 492.0 .5910 290.0 480.t .sn1 *253.5 491.I .5908 290.S 4'0.1 .sns 254.0 491.7 .5901 291.0 480.7 .sm 491.5 .5905  
211.s 502.6 .6039 Z55.0 491.4 .5903 502.4 .6037 255.5 491.2 *.5901 211.0 502 .. J .6035 256.0 491.1 .5899 211.s 50Z.'i .6033 256.5 490.9 .5891 219.0 502.0 .6031 257.0 490.I .5196 219.5 .6029 220.0 501.I 220.s 501.7 .6021 H1.5 490.6 .5194 221.0 501.5 .6026 2n.o 490.5 .Sl92 221.s 501.s .6024 zsa.5 490.3 .5'90 222.0 501.Z .6022 H9.0 490.2 .SM9 222.5. 501.0 .6020 259.5 4t0.D .SM7 223.0 500.9 .6011 260.0 m** .SNS 223.5 500.1 .6017 260.5 .7 .SM3 224.0 500.6 .6015 261.0 "'*' .SM1 224.5 500.4 .6013 261.S 419.4 .HIO 225.0 500.3 .6011 2.z.o 4".S .Sl71 225.5 500.1 .6009 262.S 419.1 .Sl76 226.0 500.0 .6007 263.0 4".0 .Sl74 226.5 499.I .6006 263.5 411.1 .Sl72 227.0 499.7 .6004 2'4.0 411.7 .Sl11 227.5 499.5 .6002 264.S 411.5 .5169 221.0 499.4 .6000 H5.0 411.4 .5167 221.5 499.2 .5991 265.S 411.Z .5165 229.0 499.1 .5996 266.0 "'*' .5163 229.5 491.9 .599S 2o6.5 411.0 .5162 230.0 498.I .5993 267.0 417.1 .5'60 230.5 491.6 .5991 267.5 417 .. 7 .5158 231.0 491.5 .5919 261.0 417.5 .5156. 31.5 491 .. 3 .5917 268.5 417.4 .5154 .o 491.2 .5916 269.0 417.Z .5153 .5 . 491.0 .5914 269.5 417.1 .Sl51 .o 497.9 .5912 210.0 416.t .5149 233.5 491.1 .5980 210.s 416.I .5147 234.0 497.6 .5971 211.0 416.6 .Sl45 234.5 497.4 .5971 211.s 416.5 .5143 235.0 497.3 .5975 212.0 416.J .5142 235.5 491.Z .5973 272.5 416.Z .Sl40 236.0 497.0 2n.o 486.0 .5131 236.5 496.9 213.S 415.9 .5136 237.0 496.7 274.0 415.7 .Sl34 274.5 415.6 .5133 237.S 496.6 .5966 275.0 415.4 .5131 238.0 496.4 .5964 275.5 415.S .5129 211.s 496.3 .5962 276.0 415.1 .Sll1 239.0 496.1 .5960 276.5 415.0 .5125 239.5 496.0 .5959 211.0 484.1 .5124 240.0 495.I .5957 240.5 495.7 .5955 zn.s 414.7 .5122 241.0 495.5 .5953 Z71.0 414.5 .Sl20 241.5 495.4 .5952 Z71.S 414.,4 .H11 242.0 49S.Z .5950 279.0 414.2 .5116 242.5 495.1 -.5941 279.5 414.1 .5115 zu.o 494.9 .5946 ZIO.O 413.t .Sl13 243.5 494.I : .5944 2ao.5 413.I .5111 244.0 494.6 .5943 211.0 413.6 .5809 244.5 494.5 .5941 211.s 413.5 .5807 245.0 494.S .5939 212.0 413.J .5806 245.5 494.2 .5937 21z.5 413.Z .SI04 24'.0 494.0 .5935 213.0 413.0 .saoz 246.5 493.9 .5934 213.5 412.t .saoo 247.0 493.7 .5932 214.0 . 412.7 .5198 247.S 493.6 .5930 214.5 W"' .5196 241.0 493.4 .5921 215.0 .4 .5m 241.5 493.J .5926 215.5 412.J .5193 --0 493.2 .5925 216.0 412.1 .5191 .5 491.0 .5923 216.5 412-a .5719 .o 492.9 .5921 211.0 411. .5717 .5 492.7 .5919 211.s 411.7 .5716 lS1.0 492.6 .5917 211.0 411.5 .5714 251.5 492.4 .5916 211.S 411.4 .5712 252.0 492.3 .5914 219.0 411.2 .5710 252.5 492.1 .5912 219.5 411.1 .5nt 253.0 492.0 .5910 290.0 480.t .sn1 *253.5 491.I .5908 290.S 4'0.1 .sns 254.0 491.7 .5901 291.0 480.7 .sm 491.5 .5905  
Line 339: Line 339:
* 2994. 2840. 2696. 2515. 2311
* 2994. 2840. 2696. 2515. 2311
* 2131. 1971. 1129. 1701. 1587. 1483. 1389. 1304. 1226. 1154. 1089. 1021. 1005. 986.0 968.0 9S0.7 934.2 911.3 903.1 888.5 174.5 161.0 148.0 835.5 123.5 111.9 eoo.a 790.0 779.5 769.3 777.2 778.0 778.5 778.8 778.I 778.6 778.2 777.6 776.I 775.9 2.760 2.667 2.569 2.476 2.387 2.3()2 z.221 2.143 2.,070 1 .. 995 1.895 1.812 1.737 1.661 1.605 1.547 1.493 1.443 1.396 1.352 1.310 1.271 1.235 1.210 1.187 1.165 1.144 1.124 1. 105 1.087 1.069 1.052 1.036 1.ozo 1.oos .9902 .9762 .9627 .9496 .9369 .9247 .9342 .9352 .9358 .9361 .9361 .9358 .9353 .9346 .9337 .9326 47.50 737.9 *::::l 41.00 736.0 .1842 41.50 134.0 *8811 49.00 732.0 :1794 49.50 730.0 8770 50.00 121.0 *,,46 50.50 726.0 *1122 51.00 724.1 .8698 51.50 122.1 .8674 52.00 720.1 .1650 52.SO 718.2 *1627 53.00 716.J .8604 53.so 714.4 *1581 54.oo 112.s *8558 54.so 110.6 *8535 5s.oo 1oe.1 *1512 SS.SO 706.9 *14 90 56.00 705. 1 .1468 56.50 703.3 .1446 57 .00 701.S :14 24 57.50 58.00 58.50 59.00 59.50 60.00 60.50 61.00 61.50 62.00 62.50 63.00 63.50 64.00 64.SO 65.00 65.50 66.00 66.50 67.00 67.50 68.00 68.50 69.00 69.50 70.00 70.50 71.00 71.50 72.00 72.50 73.00 73.50 74.00 74.50 699.7 697.9 696.2 694.5 692.7 691.0 689.4 687.7 686.1 6&4.4 6&2.1 6t1.2 679.7 678.1 676.6 675.1 673.6 672.1 670.6 669.2 667.7 666.] 664.9 663.5 662.1 660.8 659.4 658.1 656.1 655.5 654.3 653.0 651.7 650.5  
* 2131. 1971. 1129. 1701. 1587. 1483. 1389. 1304. 1226. 1154. 1089. 1021. 1005. 986.0 968.0 9S0.7 934.2 911.3 903.1 888.5 174.5 161.0 148.0 835.5 123.5 111.9 eoo.a 790.0 779.5 769.3 777.2 778.0 778.5 778.8 778.I 778.6 778.2 777.6 776.I 775.9 2.760 2.667 2.569 2.476 2.387 2.3()2 z.221 2.143 2.,070 1 .. 995 1.895 1.812 1.737 1.661 1.605 1.547 1.493 1.443 1.396 1.352 1.310 1.271 1.235 1.210 1.187 1.165 1.144 1.124 1. 105 1.087 1.069 1.052 1.036 1.ozo 1.oos .9902 .9762 .9627 .9496 .9369 .9247 .9342 .9352 .9358 .9361 .9361 .9358 .9353 .9346 .9337 .9326 47.50 737.9 *::::l 41.00 736.0 .1842 41.50 134.0 *8811 49.00 732.0 :1794 49.50 730.0 8770 50.00 121.0 *,,46 50.50 726.0 *1122 51.00 724.1 .8698 51.50 122.1 .8674 52.00 720.1 .1650 52.SO 718.2 *1627 53.00 716.J .8604 53.so 714.4 *1581 54.oo 112.s *8558 54.so 110.6 *8535 5s.oo 1oe.1 *1512 SS.SO 706.9 *14 90 56.00 705. 1 .1468 56.50 703.3 .1446 57 .00 701.S :14 24 57.50 58.00 58.50 59.00 59.50 60.00 60.50 61.00 61.50 62.00 62.50 63.00 63.50 64.00 64.SO 65.00 65.50 66.00 66.50 67.00 67.50 68.00 68.50 69.00 69.50 70.00 70.50 71.00 71.50 72.00 72.50 73.00 73.50 74.00 74.50 699.7 697.9 696.2 694.5 692.7 691.0 689.4 687.7 686.1 6&4.4 6&2.1 6t1.2 679.7 678.1 676.6 675.1 673.6 672.1 670.6 669.2 667.7 666.] 664.9 663.5 662.1 660.8 659.4 658.1 656.1 655.5 654.3 653.0 651.7 650.5  
.1403 .1381 .1360 .1339 .8311 .am .1277 .1257 .1237 .8217 .1198 .1179 .1160 .1141 .11zz .810lt .1086 .8068 .1050 .8033 .8015 .7998 .1'911 .7964 .7947 .7931 *.7914 .7198 .7882 .7166 .7152 .7136 .7821 .7806 .7791 Sheet 3 of 10 Break Flow Energy Flow Time Break Flow Energy Flow lb/sec.) {million Btu/sec.}  
.1403 .1381 .1360 .1339 .8311 .am .1277 .1257 .1237 .8217 .1198 .1179 .1160 .1141 .11zz .810lt .1086 .8068 .1050 .8033 .8015 .7998 .1'911 .7964 .7947 .7931 *.7914 .7198 .7882 .7166 .7152 .7136 .7821 .7806 .7791 Sheet 3 of 10 Break Flow Energy Flow Time Break Flow Energy Flow lb/sec.) {million Btu/sec.}
{sec.} {lb/sec.)  
{sec.} {lb/sec.)
{million Btu/sec.)
{million Btu/sec.)
15.00 i4i:o .7716 111.0 595.Z .7136 .7761 111.5 594.1 .7131 75.50 646 .. I .17.47 112 .. 0 594.5 .7127 76.00 .645.6 .n 33 112.S 594.1 .7123 76.50 644.4 113.0 593.7 .7118 77.00 643.3 113.,S 593.4 .7114 114.0 593.0 .,7109 77.50 642.1 .7704 114.5 592.7 .7105 71.00 641.0 .7690 115.0 592.3 .7101 71.50 639.1 .7677 115 .. 5 592.0 .7097 79.00 638.7 .7663 116.0 591.6 .7092 79.50 637.6 .7650 116.5 591.3 .70M 10.00 636.5 .7637 111.0 590.9 .7084 10.50 635.5 .7624 11.00 634.4 .7611 11.50 633.3 .7598 117 .5 590.6 .7080 12.00 632.3 .7586 118.0 590.3 .,7076 12.50 631.3 .7573 118.5 589.9 .7072 13.00 630.3 .7561 119.0 589.6 .7068 13.50 6l9.3 .7549 119.5 589.3 .7064 84.00 628.3 .7537 120.0 518.9 .7060 14.50 627.4 .7526 120.S 588.6 .70S6 IS.00 626.4* .7514 121 .o 588.3 .70S2 15.SO 625.5 .7503 121 .5 588.0 .700 . 16.00 624.6 .7492 122.0 517 .. 7 .7044 86.50 623.7 .* 7481 122.5 587.3 .7041 17.00 622.8 .7470 123.0 587 .. 0 .7037 17.50 621.9 .7460 123.S 586 .. 7 .7033 N.00 621.1 124.0 586.4 .7029 . 18.50 620 .. :S .7440 124.S 586.1 .7026 41 619.4 .7430 125.0 585 .. 1 .7022 . 618.6 .7420 125.5 585.5 .7018 617.9 .7410 126.0  
15.00 i4i:o .7716 111.0 595.Z .7136 .7761 111.5 594.1 .7131 75.50 646 .. I .17.47 112 .. 0 594.5 .7127 76.00 .645.6 .n 33 112.S 594.1 .7123 76.50 644.4 113.0 593.7 .7118 77.00 643.3 113.,S 593.4 .7114 114.0 593.0 .,7109 77.50 642.1 .7704 114.5 592.7 .7105 71.00 641.0 .7690 115.0 592.3 .7101 71.50 639.1 .7677 115 .. 5 592.0 .7097 79.00 638.7 .7663 116.0 591.6 .7092 79.50 637.6 .7650 116.5 591.3 .70M 10.00 636.5 .7637 111.0 590.9 .7084 10.50 635.5 .7624 11.00 634.4 .7611 11.50 633.3 .7598 117 .5 590.6 .7080 12.00 632.3 .7586 118.0 590.3 .,7076 12.50 631.3 .7573 118.5 589.9 .7072 13.00 630.3 .7561 119.0 589.6 .7068 13.50 6l9.3 .7549 119.5 589.3 .7064 84.00 628.3 .7537 120.0 518.9 .7060 14.50 627.4 .7526 120.S 588.6 .70S6 IS.00 626.4* .7514 121 .o 588.3 .70S2 15.SO 625.5 .7503 121 .5 588.0 .700 . 16.00 624.6 .7492 122.0 517 .. 7 .7044 86.50 623.7 .* 7481 122.5 587.3 .7041 17.00 622.8 .7470 123.0 587 .. 0 .7037 17.50 621.9 .7460 123.S 586 .. 7 .7033 N.00 621.1 124.0 586.4 .7029 . 18.50 620 .. :S .7440 124.S 586.1 .7026 41 619.4 .7430 125.0 585 .. 1 .7022 . 618.6 .7420 125.5 585.5 .7018 617.9 .7410 126.0  
.7015 0 617.1 .7401 126.5 584.9 .7011 , .oo 616.3 .7392 127.0 584.6 .7007 11 .so 615.6 .7383 127 .5 584.3 .7004 92.00 614.9 .7374 128.0 584.0 .7000 92.50 614.2 .7366 128.5 583.7 .6997 93.00 613.S .7357 129.0 583.4 .6993 93.50 612.8 .7349 129.5 583.1 .6990 94.00 612.1 .7341 130.0 582.9 .6986 94.SO 611.5 .. 7333 *130.s 582.6 .6983 95.00. 610.8 .7325 131.0 512.3 .6979 95.50 610.2 .7311 131 .s 582.0 .6976 96.00 609.6 .7310 132.0 581.7 .6972 96.50 609.0 .730Z 132.S 581.4 .6969 97.00 608.4 .. 7295 133.0 581.2 .6966 133.5 580.9 .6962 134.0 sao.6 97.50 607.1 .7218 134.5 580.3 .6955 98.00 607.2 .7211 135.0 580.1 .6952 98.50 6()6.6 .1274 135.S 579.8 .6949 99.00 606.1 -.7267 136.0 579.5 .6946 99.SO 60S.5 .7261 136.5 579.2 .6942 : 137.0 579.0 .6939 100.0 60S.O .7254 100.S '&deg;"*4 .7248 101 .o 603.9 .7241 137.5 571.7 .6936 101.5 603.4 .7235 138.0 578.4 .6933 102.0 602.9 .7229 138.5 571.2 .6929 102.5 602.4 .7223 139.0 577.9 .6926 103;.0 601.9 .7217 139.S 577.6 .6923 103.5 601.4 *.1211 140.0 577., .6920 104.0 601.0 .7206 140.5 577.1 .6916 104.5 600.5 .7200 141.0 576.9 .6913 105.0 600.1 .7195 141.5 576.6 .6910 --5 599.6 .7190 142.0 576.S .6907 .o 599.2 .7114 142.5 576.1 .6904 .5 598.8 .7179 143.0 575.1 .6901 . .o 59&.4 .7174 143.5 575.6 .6898 07.5 598.0 .7169 . 144.0 575.3 .689S 108.0 597.6 .7164 144.5 575.0 .6891 108.5 597.2 .7159 145.0 574.I .6888 109.0 596.I .7155 145.5 574.5 .6&85 109.5 596.4 .7150 146.0 574.J .6182 110.0 596.0 .7145 146.5 574.0 .6879 110.5 595.6 .7141 147.0 57S.I .6876 147.S 573.$ a617J Sheet 4 of 10 Break Flow Energy Flow Time Break Flow Energy Flow lb/sec.) {million Btulsec.}  
.7015 0 617.1 .7401 126.5 584.9 .7011 , .oo 616.3 .7392 127.0 584.6 .7007 11 .so 615.6 .7383 127 .5 584.3 .7004 92.00 614.9 .7374 128.0 584.0 .7000 92.50 614.2 .7366 128.5 583.7 .6997 93.00 613.S .7357 129.0 583.4 .6993 93.50 612.8 .7349 129.5 583.1 .6990 94.00 612.1 .7341 130.0 582.9 .6986 94.SO 611.5 .. 7333 *130.s 582.6 .6983 95.00. 610.8 .7325 131.0 512.3 .6979 95.50 610.2 .7311 131 .s 582.0 .6976 96.00 609.6 .7310 132.0 581.7 .6972 96.50 609.0 .730Z 132.S 581.4 .6969 97.00 608.4 .. 7295 133.0 581.2 .6966 133.5 580.9 .6962 134.0 sao.6 97.50 607.1 .7218 134.5 580.3 .6955 98.00 607.2 .7211 135.0 580.1 .6952 98.50 6()6.6 .1274 135.S 579.8 .6949 99.00 606.1 -.7267 136.0 579.5 .6946 99.SO 60S.5 .7261 136.5 579.2 .6942 : 137.0 579.0 .6939 100.0 60S.O .7254 100.S '&deg;"*4 .7248 101 .o 603.9 .7241 137.5 571.7 .6936 101.5 603.4 .7235 138.0 578.4 .6933 102.0 602.9 .7229 138.5 571.2 .6929 102.5 602.4 .7223 139.0 577.9 .6926 103;.0 601.9 .7217 139.S 577.6 .6923 103.5 601.4 *.1211 140.0 577., .6920 104.0 601.0 .7206 140.5 577.1 .6916 104.5 600.5 .7200 141.0 576.9 .6913 105.0 600.1 .7195 141.5 576.6 .6910 --5 599.6 .7190 142.0 576.S .6907 .o 599.2 .7114 142.5 576.1 .6904 .5 598.8 .7179 143.0 575.1 .6901 . .o 59&.4 .7174 143.5 575.6 .6898 07.5 598.0 .7169 . 144.0 575.3 .689S 108.0 597.6 .7164 144.5 575.0 .6891 108.5 597.2 .7159 145.0 574.I .6888 109.0 596.I .7155 145.5 574.5 .6&85 109.5 596.4 .7150 146.0 574.J .6182 110.0 596.0 .7145 146.5 574.0 .6879 110.5 595.6 .7141 147.0 57S.I .6876 147.S 573.$ a617J Sheet 4 of 10 Break Flow Energy Flow Time Break Flow Energy Flow lb/sec.) {million Btulsec.}
{sec.} {lblsec.)  
{sec.} {lblsec.)
{million Btu/sec.) .o 573.:S .6170 185.5 556.3 .6664 -.-.5 573.0 .6167 186.0 556.1 .6661 149.0 572.I .6164 186.S 555.1 .6659 149.5 572.5 .6161 187.0 555.6 .6656 150.0 572.J .6158 187.5 555.4 .6654 150.5 572.1 .6155 188.0 555.2 .6651 151 .. 0 571.I .6152 188.5 555.0 .6648 151 .. 5 571.6 .6849 18900 554.1 .6646 152.0 571 .. J .6146 189.5 554.6 .,6643 152.S 571.1 .6843 190.0 554.4 .6641 153.0 570.8 .6841 190.5 554.Z .6638 153.5 570.6 .6138 191.0 553.9 .6636 154.0 570 .. 4 .6135 191 .5 553.7 .6633 154.5 570.1 .6132 192.0 553.5 .6631 155.0 569.9 .6829 192.5 553.3 .6621 155.5 569.7 .6126 19300 553.1 .662S 156.0 569.4 .6123* 193.5 552.9 .6623 156.5 569.2 .6120 194.0 552.7 .6620 157.0 561.9 .6117 194.5 552.5 .6611 195.0 552.3 .6615 157.5 561.7 .6115 195.5 552.1 .6613 196.0 551.9 .6610 158.0 561.5 .6112 196.5 551.6 .6608 158.5 561.Z .6809 197.0 551.4 .6605 159.0 561.0 .6806 159.5 567.1 .6803 160.0 567.5 .6800 160.5 567.J .6798 197.5 551.Z .6603 161.0 567.1 .6795 199.0 551.0 .6600 161.5 566.9 .. 6792 199.5 550.1 .6598 162.0 566.6 .6719 199.0 550.6 .,6S9S 162.5 566.4 .6717 199.5 550.4 .6593 .a* 566.Z 200.0 550.2 .5 565.9 .6714 200.5 550.0 .6590 .6711 .6588 .o 565.7 .6771 201.0 549.1 .6585 64.5 565.o5 .6775 201.5 549.6 .6513 165.0 565.3 .6773 202.0 549.4 .6580 165.5 565.0 .6770 202.5 549.Z .6571 166.0 564.8 .6767 203.0 549.0 .6575 166.5 564.6 .6765 203.5 54'.7 .6573 167.0 564.4 204.0 541.5 167.5 564.1 .6762 204.5 544.3 .6570 161.0 563.9 .6759 205.0 541.1 .6561 161.5 .. 563.7 .6756 205.5 547.9 .6565 169.0 563.5 .67S4 206.0 547.7 .6563 169.5 563.Z .6751 206.5 547.5 .6560 .6741 .6558 170.0 563.0 .6746 207.0 547.J .6555 170.S 562.1 207.5 547.1 171.0 562.6 .6743 2oe.o 546.9 .6553 .6740 .6550 171.5 562.J .6737 208.5 546.7 .6541 172.0 562.1 .6735 209.0 546.5 .6545 172.5 561.9 .6132 209.5 546.3 .6543 173.0 561.7 .6729 210.0 546.1 .6540 17305 561.5 .6727 210 .. 5 545.9 .6538 174.0 561.Z -.6724 211.0 545.7 .6536 174.S 561.0 : .6721 211.5 545.S .6533 175.0 560.8 .6719 . _212.0 545.3 .6531 175.5 560.6 -.6716 212.5 545.1 .6528 176.0 560.4 .6713 213.0 544.9 .6526 176.5 560.Z .6711 213.5 544.7 .6523 177.0 559.9 .6108 214.0 544.S .6521 214.5 544.3 .6518 177.5 559.7 .'706 215.0 544.1 .6516 179.0 559.5 .6703 215.5 543.9 .6514 179.5 559.3 .6700 216.0 543.7 .. 6511 179.0 559.1 .6698 216.5 543.5 .6509 179.5 558.1 .6695 217.0 543.3 .6506 -558.6 .669Z 558.4 .6690 551.2 .6617 .5 558.0 .6615 12.0 557.1 .6612 .e2.5 557.6 .6679 19J.O 19J.S 557.3 .6677 194.0 557.1 .6674 184.5 556.9 .6672 1es.o 556.7 .6669 556.S .6666 Sheet 5 of 10 Break Flow Energy Flow Time Break Flow Energy Flow lb sec. mi 11 ion Btu /sec. sec. lb/sec. million Btu/sec. 217.5 543.1 .6504 c53.5 5Z9.0 .6334 218.0 542.9 .6501 254.0 521.1 .6331 218.5 542.7 .6499 C?54.5 521.6 .6329 219.0 542.5 .6496 528.4 .6327 219.5 542.3 .6494 255.5 528.3 .6324 220.0 542.1 .6492 256.0 sza.1 .6322 220.5 co6489 256.5 527.9 .6320 221.0 541 .. 7 .6487 257.0 527.7 .6317 221.5 541.5 .64&4 222.0 541.3 .64&2 222.5 541.1 .6480 257.5 527.5 .6315 223.0 54().9 .6477 Z5a.o 527.J .6313 223.5 540.7 .6475 258.5 527.1 .6311 224.0 540.5 .6472 259.0 526.9 .6308 224.5 540 .. J .6470 259.5 526.7 .6306 225.0 540.1 .6467 260.0 526.6 .6304 225.5 539.9 .6465 260.5 526.4 .* 6301 226.0 539.7 .6463 261.0 526.Z .6299 226.5 539.5 .6460 261.5 526.0 .6297 227.0 539.3 .6453 262.0 525.1 .6295 227.5 539.1 .. 6455 262.5 525.6 .6292 228.0 538.9 .6453 263.0 525.4 .6290 228.5 538.7 .6451 263.5 szs.z .6288 229.0 538.5 .6448 264.0 525.1 .62&6 229.5 538.3 .. 6446 264 .5 524.9 .6l83 . 230.0 538.1 .6444 265.0 524.7 .6281 230.5 537.9 .6441 265.5 524.5 .6279 231.0 537.7 .6439 266.0 524.3 .6277 . 231.5 537.S
{million Btu/sec.) .o 573.:S .6170 185.5 556.3 .6664 -.-.5 573.0 .6167 186.0 556.1 .6661 149.0 572.I .6164 186.S 555.1 .6659 149.5 572.5 .6161 187.0 555.6 .6656 150.0 572.J .6158 187.5 555.4 .6654 150.5 572.1 .6155 188.0 555.2 .6651 151 .. 0 571.I .6152 188.5 555.0 .6648 151 .. 5 571.6 .6849 18900 554.1 .6646 152.0 571 .. J .6146 189.5 554.6 .,6643 152.S 571.1 .6843 190.0 554.4 .6641 153.0 570.8 .6841 190.5 554.Z .6638 153.5 570.6 .6138 191.0 553.9 .6636 154.0 570 .. 4 .6135 191 .5 553.7 .6633 154.5 570.1 .6132 192.0 553.5 .6631 155.0 569.9 .6829 192.5 553.3 .6621 155.5 569.7 .6126 19300 553.1 .662S 156.0 569.4 .6123* 193.5 552.9 .6623 156.5 569.2 .6120 194.0 552.7 .6620 157.0 561.9 .6117 194.5 552.5 .6611 195.0 552.3 .6615 157.5 561.7 .6115 195.5 552.1 .6613 196.0 551.9 .6610 158.0 561.5 .6112 196.5 551.6 .6608 158.5 561.Z .6809 197.0 551.4 .6605 159.0 561.0 .6806 159.5 567.1 .6803 160.0 567.5 .6800 160.5 567.J .6798 197.5 551.Z .6603 161.0 567.1 .6795 199.0 551.0 .6600 161.5 566.9 .. 6792 199.5 550.1 .6598 162.0 566.6 .6719 199.0 550.6 .,6S9S 162.5 566.4 .6717 199.5 550.4 .6593 .a* 566.Z 200.0 550.2 .5 565.9 .6714 200.5 550.0 .6590 .6711 .6588 .o 565.7 .6771 201.0 549.1 .6585 64.5 565.o5 .6775 201.5 549.6 .6513 165.0 565.3 .6773 202.0 549.4 .6580 165.5 565.0 .6770 202.5 549.Z .6571 166.0 564.8 .6767 203.0 549.0 .6575 166.5 564.6 .6765 203.5 54'.7 .6573 167.0 564.4 204.0 541.5 167.5 564.1 .6762 204.5 544.3 .6570 161.0 563.9 .6759 205.0 541.1 .6561 161.5 .. 563.7 .6756 205.5 547.9 .6565 169.0 563.5 .67S4 206.0 547.7 .6563 169.5 563.Z .6751 206.5 547.5 .6560 .6741 .6558 170.0 563.0 .6746 207.0 547.J .6555 170.S 562.1 207.5 547.1 171.0 562.6 .6743 2oe.o 546.9 .6553 .6740 .6550 171.5 562.J .6737 208.5 546.7 .6541 172.0 562.1 .6735 209.0 546.5 .6545 172.5 561.9 .6132 209.5 546.3 .6543 173.0 561.7 .6729 210.0 546.1 .6540 17305 561.5 .6727 210 .. 5 545.9 .6538 174.0 561.Z -.6724 211.0 545.7 .6536 174.S 561.0 : .6721 211.5 545.S .6533 175.0 560.8 .6719 . _212.0 545.3 .6531 175.5 560.6 -.6716 212.5 545.1 .6528 176.0 560.4 .6713 213.0 544.9 .6526 176.5 560.Z .6711 213.5 544.7 .6523 177.0 559.9 .6108 214.0 544.S .6521 214.5 544.3 .6518 177.5 559.7 .'706 215.0 544.1 .6516 179.0 559.5 .6703 215.5 543.9 .6514 179.5 559.3 .6700 216.0 543.7 .. 6511 179.0 559.1 .6698 216.5 543.5 .6509 179.5 558.1 .6695 217.0 543.3 .6506 -558.6 .669Z 558.4 .6690 551.2 .6617 .5 558.0 .6615 12.0 557.1 .6612 .e2.5 557.6 .6679 19J.O 19J.S 557.3 .6677 194.0 557.1 .6674 184.5 556.9 .6672 1es.o 556.7 .6669 556.S .6666 Sheet 5 of 10 Break Flow Energy Flow Time Break Flow Energy Flow lb sec. mi 11 ion Btu /sec. sec. lb/sec. million Btu/sec. 217.5 543.1 .6504 c53.5 5Z9.0 .6334 218.0 542.9 .6501 254.0 521.1 .6331 218.5 542.7 .6499 C?54.5 521.6 .6329 219.0 542.5 .6496 528.4 .6327 219.5 542.3 .6494 255.5 528.3 .6324 220.0 542.1 .6492 256.0 sza.1 .6322 220.5 co6489 256.5 527.9 .6320 221.0 541 .. 7 .6487 257.0 527.7 .6317 221.5 541.5 .64&4 222.0 541.3 .64&2 222.5 541.1 .6480 257.5 527.5 .6315 223.0 54().9 .6477 Z5a.o 527.J .6313 223.5 540.7 .6475 258.5 527.1 .6311 224.0 540.5 .6472 259.0 526.9 .6308 224.5 540 .. J .6470 259.5 526.7 .6306 225.0 540.1 .6467 260.0 526.6 .6304 225.5 539.9 .6465 260.5 526.4 .* 6301 226.0 539.7 .6463 261.0 526.Z .6299 226.5 539.5 .6460 261.5 526.0 .6297 227.0 539.3 .6453 262.0 525.1 .6295 227.5 539.1 .. 6455 262.5 525.6 .6292 228.0 538.9 .6453 263.0 525.4 .6290 228.5 538.7 .6451 263.5 szs.z .6288 229.0 538.5 .6448 264.0 525.1 .62&6 229.5 538.3 .. 6446 264 .5 524.9 .6l83 . 230.0 538.1 .6444 265.0 524.7 .6281 230.5 537.9 .6441 265.5 524.5 .6279 231.0 537.7 .6439 266.0 524.3 .6277 . 231.5 537.S
* 6436 524.1 .6274 , 0 537.3 .6434 2t-7 .o 523.9 .6272 537.1 .6432 267.5 523.I .6270 536.9 .6429 263.0 523.6 .6268 .5 536.7 .6427 268.5 523.4 .6265 '4.0 536.5 .6425 523.Z .6263 5 536.3 .6422 .5 523.0 .6261 536. 1 .6420 270.0 522.I .6259 23S.5 535.9 .6417 270.5 522.6 .62S6 236.0 535.7 .6415 271 .o 522.5 .6254 236.5 535.6 .6413 271.5 522.J .6252 237.0 535.4 .. 6410 272.0 522.1 .6250 272.5 521.9 .6247 535.2 .6408 273.0 521.7 .6245 237.S 535.0 273.5 521.5 .6243 233.0 534.8 .6406 274.0 521.3 .6241 233. 5 534.6 .6403 274.5 521.2 .6238 239.0 534.4 .6401 275.0 521.0 .6236 239.5 .6399 275.5 520.8 .623' 240.0 534.2 .6396 276.0 520 .. 6 .623' 240.5 534.0 .6394 276.5 520.4 .623( 241.0 533.8 .6392 277.0 520.2 .622i 533.6 241.5 533.4 .6389 21.2.0 533.2 .6387 242.5 533.0 .6385 277.5 520. 1 .6Z25 243.0 .6382 278.0 519.9 243.5 532.9 .6380 278.5 519.7 .6223 244.0 532.7 .6378 279.0 519.5 .6221 244.5 532.S .6375 279.5 519.3 .6218 245.0 532.3 .6373 280.0 519.2 .6216 245.5 532.1 .6371 280.5 519.0 .6214 246.0 531.9 .6361 211.0 518.8 .6212 246.5 531.7 .6366 281.5 518.6 .6210 247.0 531.5 .6364 282.0 518.5 .6209 . 247.5 531.3 .6361 282.5 518.3 .6206 248.0 531.1 .6359 283.0 511.1 .6204 241.5 530.9 .6357 283.5 517.9 .6202 530.7 .6354 284.0 517.1 .6199 530.S .6352 284.5 517.6 .6197 530.4 .6350 28s.o 517.4 .619S .5 530.Z .6347 285.5 517.2 .6193 i .O 530.0 .6345 286.0 517.1 .6191 _.,,1.s 529.1 .6343 286.5 516.9 .6189 252.0 529.6 .6340 287.0 516.7 .6186 252.5 529.4 .6331 287.5 516.5 .06184 253.0  
* 6436 524.1 .6274 , 0 537.3 .6434 2t-7 .o 523.9 .6272 537.1 .6432 267.5 523.I .6270 536.9 .6429 263.0 523.6 .6268 .5 536.7 .6427 268.5 523.4 .6265 '4.0 536.5 .6425 523.Z .6263 5 536.3 .6422 .5 523.0 .6261 536. 1 .6420 270.0 522.I .6259 23S.5 535.9 .6417 270.5 522.6 .62S6 236.0 535.7 .6415 271 .o 522.5 .6254 236.5 535.6 .6413 271.5 522.J .6252 237.0 535.4 .. 6410 272.0 522.1 .6250 272.5 521.9 .6247 535.2 .6408 273.0 521.7 .6245 237.S 535.0 273.5 521.5 .6243 233.0 534.8 .6406 274.0 521.3 .6241 233. 5 534.6 .6403 274.5 521.2 .6238 239.0 534.4 .6401 275.0 521.0 .6236 239.5 .6399 275.5 520.8 .623' 240.0 534.2 .6396 276.0 520 .. 6 .623' 240.5 534.0 .6394 276.5 520.4 .623( 241.0 533.8 .6392 277.0 520.2 .622i 533.6 241.5 533.4 .6389 21.2.0 533.2 .6387 242.5 533.0 .6385 277.5 520. 1 .6Z25 243.0 .6382 278.0 519.9 243.5 532.9 .6380 278.5 519.7 .6223 244.0 532.7 .6378 279.0 519.5 .6221 244.5 532.S .6375 279.5 519.3 .6218 245.0 532.3 .6373 280.0 519.2 .6216 245.5 532.1 .6371 280.5 519.0 .6214 246.0 531.9 .6361 211.0 518.8 .6212 246.5 531.7 .6366 281.5 518.6 .6210 247.0 531.5 .6364 282.0 518.5 .6209 . 247.5 531.3 .6361 282.5 518.3 .6206 248.0 531.1 .6359 283.0 511.1 .6204 241.5 530.9 .6357 283.5 517.9 .6202 530.7 .6354 284.0 517.1 .6199 530.S .6352 284.5 517.6 .6197 530.4 .6350 28s.o 517.4 .619S .5 530.Z .6347 285.5 517.2 .6193 i .O 530.0 .6345 286.0 517.1 .6191 _.,,1.s 529.1 .6343 286.5 516.9 .6189 252.0 529.6 .6340 287.0 516.7 .6186 252.5 529.4 .6331 287.5 516.5 .06184 253.0  
Line 355: Line 355:
* 6114 336.5 498.1 .5967 * . 5 510.7 .6112 499.6 .5965 .o . 5i0.6 .6110 s 491.4 .5963 .5 510.4 .61oe 31.0.0 499.Z .5960 '05.0 510.2 .6106 491.1 .S9S& JS.5 510.0 .6103 341.0 497.9 .S9S6 ..106.0 509.9 .6101 341.5 497.7 .S9S4 306.5 509.7 .6099 342.0 497oS .S9S2 307.0 5CYI. S .6'197 342.5 497.4 .59SO 307.5  
* 6114 336.5 498.1 .5967 * . 5 510.7 .6112 499.6 .5965 .o . 5i0.6 .6110 s 491.4 .5963 .5 510.4 .61oe 31.0.0 499.Z .5960 '05.0 510.2 .6106 491.1 .S9S& JS.5 510.0 .6103 341.0 497.9 .S9S6 ..106.0 509.9 .6101 341.5 497.7 .S9S4 306.5 509.7 .6099 342.0 497oS .S9S2 307.0 5CYI. S .6'197 342.5 497.4 .59SO 307.5  
.609S 343.0 497.2 .5948 308.0  
.609S 343.0 497.2 .5948 308.0  
.6'193 343.5 497.0 .5946 3oe.s 509.0 .6'191 344.0 496.9 .5944 309.0 508.8 .6089 344.5 496.7 .5942 309.S 508.6 .6087 345.0 496.5 .5940 310.0 5CMS.5 .6085 345.5 496.4 .5938 310.5 506.3 .6082 346.0 496.Z .5936 311 .o 5oe.1 .6080 346.5 496.0 .5934 3,, .s 507.9 .6078 347.0 495.9 .5932 507.8 .6076 347.5 495.7 .5930 312.5 507.6 .6074 348.0 495.5 .5928 313.0 507.4 .6072 34!.5 495.4 .5926 313.5 . 507 .3 .6070 349.0 49S.2 .5924 314.0 507.1 .6068 349.5 49S.O .5922 3l4.5 506.9 .6066 350.0 494.,9 .5920 315.0 506.7 .6064 350.5 494.7 .5911 315.5 506.6 .6062 351 .o 494.5 .5916 316.0 506.4 .6060 351.5 494.4 .5914 316.5 506.2 .6058 352.0 49".2 .5912 317.0 506., .6056 352.5 494.0 .5910 353.0 493.9 .5909 353.5 493.7 .5906 3H.5 505.9 .6053 354.0 493.6 .5904 311.0 505.7 .6051. 354.5 493.4 .5902 318.5 SOS.6 .6049 355.0 493.2 .5900 319.0 505.4 .6047 355.5 493.1 .5898 319.S sos.z .6045 356.0 492.9 .S896 o.o 505.0 .6043 356.5 492.7 .5894 .5 504.9 .6041 357.0 492.6 .5192 .a. 504.7 .60'9 -* .s 504.5 .6037 u.o 504.4 .6035 ,22.S 504.Z .6033 323.0 504.0 .6031 323.S 503.1 .6028 324.0 503.7 .6026 324.5 503.5 .6024 325.0 503.J .6022 325.S 503.1 .6020 Sheet 7 of 10 Time Break Flow Energy Flow Time Break Flow Energy Flow lb/sec.} {million Btulsec.}  
.6'193 343.5 497.0 .5946 3oe.s 509.0 .6'191 344.0 496.9 .5944 309.0 508.8 .6089 344.5 496.7 .5942 309.S 508.6 .6087 345.0 496.5 .5940 310.0 5CMS.5 .6085 345.5 496.4 .5938 310.5 506.3 .6082 346.0 496.Z .5936 311 .o 5oe.1 .6080 346.5 496.0 .5934 3,, .s 507.9 .6078 347.0 495.9 .5932 507.8 .6076 347.5 495.7 .5930 312.5 507.6 .6074 348.0 495.5 .5928 313.0 507.4 .6072 34!.5 495.4 .5926 313.5 . 507 .3 .6070 349.0 49S.2 .5924 314.0 507.1 .6068 349.5 49S.O .5922 3l4.5 506.9 .6066 350.0 494.,9 .5920 315.0 506.7 .6064 350.5 494.7 .5911 315.5 506.6 .6062 351 .o 494.5 .5916 316.0 506.4 .6060 351.5 494.4 .5914 316.5 506.2 .6058 352.0 49".2 .5912 317.0 506., .6056 352.5 494.0 .5910 353.0 493.9 .5909 353.5 493.7 .5906 3H.5 505.9 .6053 354.0 493.6 .5904 311.0 505.7 .6051. 354.5 493.4 .5902 318.5 SOS.6 .6049 355.0 493.2 .5900 319.0 505.4 .6047 355.5 493.1 .5898 319.S sos.z .6045 356.0 492.9 .S896 o.o 505.0 .6043 356.5 492.7 .5894 .5 504.9 .6041 357.0 492.6 .5192 .a. 504.7 .60'9 -* .s 504.5 .6037 u.o 504.4 .6035 ,22.S 504.Z .6033 323.0 504.0 .6031 323.S 503.1 .6028 324.0 503.7 .6026 324.5 503.5 .6024 325.0 503.J .6022 325.S 503.1 .6020 Sheet 7 of 10 Time Break Flow Energy Flow Time Break Flow Energy Flow lb/sec.} {million Btulsec.}
{sec* l {lb/  
{sec* l {lb/
{million Btu/sec.) .s 492.4 .5890 .
{million Btu/sec.) .s 492.4 .5890 .
478.5 39S.5 476.I .5700 351.0 492.2 .SW 396.0 474.8 .S6'7 351.5 492.1 .Sl86 39o.5 472.7 .S651 359.0 . 491 .* 9 .5884 397.0 470.5 .S62S 359.5 491.7 .seaz 360.0 491.6 .HaO 360.5 491.4 .5171 468 .. l 361 .o 491.2 .5176 397.5 .5591' 361.5 491.1 .5174 398.0 465.1 .5568 362.0 490.9 .5172 398.S 463.3 .5537 362.5 490.1 .5170 399.0 460.7 .5505 363.0 490.6 .5168 . 399.5 45'.0 .5473 363.5 490.4 .5166 . 400.0 455.1 .5438 364.0 490.3 .5164 400.5 452 .. Z .S403 364.5 490.1 .S862 401.0 449.Z .5367 365.0 419.9 .5860 401.5 446.2 .5330 365.5 419.1 .5158 402.0 443.0 .5292 36600 489.6 .51S6 402.5 439.1 .5252 366.5 419.4 .5154 403.0 436.5 .5213 367.0 489.3 .5152 403.5 433.2 '.5172 367.5 489.1 .5150 404.0 429.7 .5131 368.0 419.0 .5&44 404.5 426.J .soea 368.5 488.8 .5146 405.0 422.7 .5046 369.0 418.6 .5144 405.5 419.1 .5002 369.5 416.S .5142 406.0 415.5 .49SI 370.0 418.! .Sl40 406.S 411.I .4913 , 370.S 418.1 .5138 407.0 408.1 .4868 371.0 418.0 .5136 407.5 404.J .4822 371 .5 . 487.8
478.5 39S.5 476.I .5700 351.0 492.2 .SW 396.0 474.8 .S6'7 351.5 492.1 .Sl86 39o.5 472.7 .S651 359.0 . 491 .* 9 .5884 397.0 470.5 .S62S 359.5 491.7 .seaz 360.0 491.6 .HaO 360.5 491.4 .5171 468 .. l 361 .o 491.2 .5176 397.5 .5591' 361.5 491.1 .5174 398.0 465.1 .5568 362.0 490.9 .5172 398.S 463.3 .5537 362.5 490.1 .5170 399.0 460.7 .5505 363.0 490.6 .5168 . 399.5 45'.0 .5473 363.5 490.4 .5166 . 400.0 455.1 .5438 364.0 490.3 .5164 400.5 452 .. Z .S403 364.5 490.1 .S862 401.0 449.Z .5367 365.0 419.9 .5860 401.5 446.2 .5330 365.5 419.1 .5158 402.0 443.0 .5292 36600 489.6 .51S6 402.5 439.1 .5252 366.5 419.4 .5154 403.0 436.5 .5213 367.0 489.3 .5152 403.5 433.2 '.5172 367.5 489.1 .5150 404.0 429.7 .5131 368.0 419.0 .5&44 404.5 426.J .soea 368.5 488.8 .5146 405.0 422.7 .5046 369.0 418.6 .5144 405.5 419.1 .5002 369.5 416.S .5142 406.0 415.5 .49SI 370.0 418.! .Sl40 406.S 411.I .4913 , 370.S 418.1 .5138 407.0 408.1 .4868 371.0 418.0 .5136 407.5 404.J .4822 371 .5 . 487.8
Line 370: Line 370:
* Z11 .5 .Z498 598.5 21105 .2497 S69.0 z11.s .Z498 599.0 211.5 .2497 S69.5 211.s .2498 599.5 211.5 .2497 570.0 211.s .2498 600.0 211.5 .2497 570.5 211.s .2499 571QO 211 .. s .Z498 s11.s Z11 .5 .2498 57Z.0 211.s .2499 572.5 tn .s .2499 511.0 211.s .2498 573.5 2'11 .s .2499 574.0 211.s .2498 574.5 211.s .2499 575.0 211.s .2499 575.5 211.s .2499 576.0 211.5 .2498 576.5 211 .s .2499 577.0 211.s .2498 211.5 .2498 .2497 577 .5 211.s .2497 578.0 211.s .2491 578.5 211.5 .2497 579.0 Z-11 .5 .2497 579.5 211.5 .2497 c*o  
* Z11 .5 .Z498 598.5 21105 .2497 S69.0 z11.s .Z498 599.0 211.5 .2497 S69.5 211.s .2498 599.5 211.5 .2497 570.0 211.s .2498 600.0 211.5 .2497 570.5 211.s .2499 571QO 211 .. s .Z498 s11.s Z11 .5 .2498 57Z.0 211.s .2499 572.5 tn .s .2499 511.0 211.s .2498 573.5 2'11 .s .2499 574.0 211.s .2498 574.5 211.s .2499 575.0 211.s .2499 575.5 211.s .2499 576.0 211.5 .2498 576.5 211 .s .2499 577.0 211.s .2498 211.5 .2498 .2497 577 .5 211.s .2497 578.0 211.s .2491 578.5 211.5 .2497 579.0 Z-11 .5 .2497 579.5 211.5 .2497 c*o  
.2497 0.5" 211.5 .2497 .o 211.s .2497 1e5 I 211 .5 02497 582 .* 0 211.s 02497 582.5 211.s .2497 583.0 211.s .2497 583.5 211.s .2497 584.0 . 211 .s .2497 584.5 211.s .2497 585.0 211.s .2497 585.5 211.5 .2497 586.0 211.s .2497 586.5 211.s .2497 587.0 211.s .2497 587.5 211.5 .2497 588.0 211 .s .2497 588.5 211.s .2497 589.0 211a5 .2497 589.5 211.5 .2497 590.0 211.5 .2497 590.5 211.5 .2497 591.0 211.5 -.2497 591.5 211.s : .2497 592.0 211.s .2497 592.5 211.s .2497 593.0 211.s .2497 593.5 211 .s .2497 594.0 211.s .2497 594.5 211.s .2497 59S.O 211.s .2497 595.5 211.s .2497 596.0 211.5 .2497 596.5 211.s 597.0 *   
.2497 0.5" 211.5 .2497 .o 211.s .2497 1e5 I 211 .5 02497 582 .* 0 211.s 02497 582.5 211.s .2497 583.0 211.s .2497 583.5 211.s .2497 584.0 . 211 .s .2497 584.5 211.s .2497 585.0 211.s .2497 585.5 211.5 .2497 586.0 211.s .2497 586.5 211.s .2497 587.0 211.s .2497 587.5 211.5 .2497 588.0 211 .s .2497 588.5 211.s .2497 589.0 211a5 .2497 589.5 211.5 .2497 590.0 211.5 .2497 590.5 211.5 .2497 591.0 211.5 -.2497 591.5 211.s : .2497 592.0 211.s .2497 592.5 211.s .2497 593.0 211.s .2497 593.5 211 .s .2497 594.0 211.s .2497 594.5 211.s .2497 59S.O 211.s .2497 595.5 211.s .2497 596.0 211.5 .2497 596.5 211.s 597.0 *   
**:: * ..... ! ..... *,::  
**:: * ..... ! ..... *,::
:::}::-:  
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:* .. *-..  
:* .. *-..
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:-::*i:*:*
:;_.y *. =;:-: :-.t :::.-J .... :;:.* ;-.::;: ..... .... : :* : "':" \J::  
:;_.y *. =;:-: :-.t :::.-J .... :;:.* ;-.::;: ..... .... : :* : "':" \J::  
*;:j:.: ... I:: :*' . l*": .. !*;: . J: ... : ; . : i *:. .. .. /* I.. : i . ;::; :: .. ::. "i ... :::x.:* ":*! :: ... :y:::  
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Line 379: Line 379:
* 1 .,.., _ : * :
* 1 .,.., _ : * :
* r* 1 ! ' . I . . . . . .
* r* 1 ! ' . I . . . . . .
alculated F1cw Flow Used 1n.Ana1ysis  
alculated F1cw Flow Used 1n.Ana1ysis
:-:::y-. ; . : :-: I: , 4 * ! -<*:-*  
:-:::y-. ; . : :-: I: , 4 * ! -<*:-*  
..  
..  
-: i-:: .. , :-* --F1cw d in Analysis ...  
-: i-:: .. , :-* --F1cw d in Analysis ...
: .  
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:.: .. j ::; . ' . : -** * * * * * **J... -***: 1: ' ** 1 -.  
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Line 473: Line 473:
* 15.2.13 ACCIDENTAL DEPRESSURIZATION OF THE MAIN STEAM SYSTEM 15.2.13.l IDENTIFICATION OF CAUSES AND ACCIDENT DESCRIPTION The most severe core cond1t1ons result1ng from an acc1dental depressur1zation of the Ma1n Steam System are assoc1ated w1th an 1nadvertent opening of a single steam dump, relief or safety valve. The analyses performed assuming a rupture of a main steam p1pe are g1ven 1n Section 15.4.3. The steam release as a consequence of this acc1dent results 1n an initial increase in steam flow which during the accident as the steam pressure falls. The energy removal from the Reactor Coolant System causes a reduction of coolant temperature and pressure.
* 15.2.13 ACCIDENTAL DEPRESSURIZATION OF THE MAIN STEAM SYSTEM 15.2.13.l IDENTIFICATION OF CAUSES AND ACCIDENT DESCRIPTION The most severe core cond1t1ons result1ng from an acc1dental depressur1zation of the Ma1n Steam System are assoc1ated w1th an 1nadvertent opening of a single steam dump, relief or safety valve. The analyses performed assuming a rupture of a main steam p1pe are g1ven 1n Section 15.4.3. The steam release as a consequence of this acc1dent results 1n an initial increase in steam flow which during the accident as the steam pressure falls. The energy removal from the Reactor Coolant System causes a reduction of coolant temperature and pressure.
In the presence of a negative moderator temperature coefficient, the cooldown results in a reduction of core shutdown margin. The analysis is perfcrmed to demonstrate that the following criterion is satisfied:
In the presence of a negative moderator temperature coefficient, the cooldown results in a reduction of core shutdown margin. The analysis is perfcrmed to demonstrate that the following criterion is satisfied:
Assuming a stuck rod cluster control assembly, with or without offsite power, and assuming a single failure in the Engineered Safety Features there will be no coasequential fuel damage after reactor trip for a steam release equivalent to the spurious opening, with failure to close, of the largest of any single steam dump, relief or safety valve. This criterion is satisfied by verifying the DNB design basis is met. The following systems provide the necessary protection against an accidental depressurization of the Main Steam System: l. Safety injection System actuation from any of the following:  
Assuming a stuck rod cluster control assembly, with or without offsite power, and assuming a single failure in the Engineered Safety Features there will be no coasequential fuel damage after reactor trip for a steam release equivalent to the spurious opening, with failure to close, of the largest of any single steam dump, relief or safety valve. This criterion is satisfied by verifying the DNB design basis is met. The following systems provide the necessary protection against an accidental depressurization of the Main Steam System: l. Safety injection System actuation from any of the following:
: 2. a. Two out of three channels of low pressurizer pressure, b. High differential pressure signals between steam lines. The overpower reactor trips (neutron flux and AT) and the reactor trip occurring 1n conjunction with receipt of the safety injection signal . sa.s -u  
: 2. a. Two out of three channels of low pressurizer pressure, b. High differential pressure signals between steam lines. The overpower reactor trips (neutron flux and AT) and the reactor trip occurring 1n conjunction with receipt of the safety injection signal . sa.s -u  
&929Q.1e1e1eees   
&929Q.1e1e1eees   
Line 479: Line 479:
* 3. Redundant 1solat1on of the ma1n feedwater 11nes: Susta1ned high feedwater flow would cause additional cooldown.
* 3. Redundant 1solat1on of the ma1n feedwater 11nes: Susta1ned high feedwater flow would cause additional cooldown.
Therefore, 1n addition to the normal control act1on wh1ch will close the main feedwater valves following reactor tr1p, a safety injection signal w111 rap1dly close all feedwater  
Therefore, 1n addition to the normal control act1on wh1ch will close the main feedwater valves following reactor tr1p, a safety injection signal w111 rap1dly close all feedwater  
-control valves, tr1p the main feedwater pumps, and close the back up feedwater isolation valves. 15.2.13.2 METHOD OF ANALYSIS The follow1ng analyses of a secondary system steam release are for th1 s section.*  
-control valves, tr1p the main feedwater pumps, and close the back up feedwater isolation valves. 15.2.13.2 METHOD OF ANALYSIS The follow1ng analyses of a secondary system steam release are for th1 s section.*
: 1. A full plant digital computer simulation, LOFTRAN (Ref. 4), is used to determine Reactor Coolant System temperature and pressure during cooldown.  
: 1. A full plant digital computer simulation, LOFTRAN (Ref. 4), is used to determine Reactor Coolant System temperature and pressure during cooldown.
: 2. An analysis to determine that there is no consequential fuel damage . . The following conditions are assumed to exist at the time of a secondary system steam release: 1. End of life shutdown margin at no load, equilibrium xenon conditions, and with the most reactive assembly stuck in its fully withdrawn positiori.
: 2. An analysis to determine that there is no consequential fuel damage . . The following conditions are assumed to exist at the time of a secondary system steam release: 1. End of life shutdown margin at no load, equilibrium xenon conditions, and with the most reactive assembly stuck in its fully withdrawn positiori.
Operation of rod cluster control assembly banks during core-burnup is restricted in such a way that addition of positive reactivity in a secondary system break accident will not lead to a more adverse condition than the case analyzed.  
Operation of rod cluster control assembly banks during core-burnup is restricted in such a way that addition of positive reactivity in a secondary system break accident will not lead to a more adverse condition than the case analyzed.
: 2. A negative moderator coefficient corresponding to the end of life rodded -core with most reactive rod cluster control assembly in the fully withdrawn positi.on.
: 2. A negative moderator coefficient corresponding to the end of life rodded -core with most reactive rod cluster control assembly in the fully withdrawn positi.on.
The variation of the coefficient with temperature and pressure is included.
The variation of the coefficient with temperature and pressure is included.
Line 509: Line 509:
* System providing sufficient negative reactivity to maintain t well below criticality.
* System providing sufficient negative reactivity to maintain t well below criticality.
The reactivity transient for the 15.2-43 and 15.2-44 is more severe than tha f a rater safety or relief valve which is t inated by stedm line differe *a1 r dump valve which is terminated by low p The transient is quite conservative with ct to cooldown, 1nce no credit is taken for the energy stored in the s em meta than that of the fuel iler steam generators.
The reactivity transient for the 15.2-43 and 15.2-44 is more severe than tha f a rater safety or relief valve which is t inated by stedm line differe *a1 r dump valve which is terminated by low p The transient is quite conservative with ct to cooldown, 1nce no credit is taken for the energy stored in the s em meta than that of the fuel iler steam generators.
Si nee the occurs over a stored energy cool down. 15.2.13.4 minutes, the neglected effect in the The ana has shown that the criteria stated earlier in this isfied. Since the reactor does not return to critical the 1lity of a DNBR less than l.3u does not exist. 15.2.14 SPUIUOUS uPEAATIUN OF THt:: SAFETY INJECTION AT POwEK 15.2.14.1 Identification of Causes Spurious SIS operation at power could be caused by operator error or a false electrical actuating signal. A spurious signal in any of the followin':;1 channels could cause this incident.  
Si nee the occurs over a stored energy cool down. 15.2.13.4 minutes, the neglected effect in the The ana has shown that the criteria stated earlier in this isfied. Since the reactor does not return to critical the 1lity of a DNBR less than l.3u does not exist. 15.2.14 SPUIUOUS uPEAATIUN OF THt:: SAFETY INJECTION AT POwEK 15.2.14.1 Identification of Causes Spurious SIS operation at power could be caused by operator error or a false electrical actuating signal. A spurious signal in any of the followin':;1 channels could cause this incident.
: l. rli gh coritai n_ment i->ressure  
: l. rli gh coritai n_ment i->ressure
: 2. rligh steam line differential pressure 3.
: 2. rligh steam line differential pressure 3.
steam line flow and low average coolant temperature or low steam line pressure
steam line flow and low average coolant temperature or low steam line pressure
Line 516: Line 516:
* TAaLE 15.2-1 (Sheet 1 of 10) TIME SEQUENCE OF EVENTS FOR CONDITION II EVENTS. Accident
* TAaLE 15.2-1 (Sheet 1 of 10) TIME SEQUENCE OF EVENTS FOR CONDITION II EVENTS. Accident
* 11(' A !" ** Witndrawal from a Subcriti cal Condition SGS-UFSAR Event Initiation of uncontro11ed rod withdrawal 7.5 x 10-4 AK/sec. reactivity insertion rate from la-13 of nominal power Power range hi neutron flux low setpoint reached Peak nuclear power occurs Rods begin to fall into core Peak heat flux occurs Peak average fuel temperature.
* 11(' A !" ** Witndrawal from a Subcriti cal Condition SGS-UFSAR Event Initiation of uncontro11ed rod withdrawal 7.5 x 10-4 AK/sec. reactivity insertion rate from la-13 of nominal power Power range hi neutron flux low setpoint reached Peak nuclear power occurs Rods begin to fall into core Peak heat flux occurs Peak average fuel temperature.
occurs Peak average clad temperature occurs Peak average coolant ture occurs ; Time (sec. ) a.a 6.9 7.a 7.5 7.a 8.2 a.a 9.2 Revision a July 22, 19a2 Sheet 9 of 10 Time Break Flow Energy Flow Time Flow Energy Flow ,c. ) {lblsec.}  
occurs Peak average clad temperature occurs Peak average coolant ture occurs ; Time (sec. ) a.a 6.9 7.a 7.5 7.a 8.2 a.a 9.2 Revision a July 22, 19a2 Sheet 9 of 10 Time Break Flow Energy Flow Time Flow Energy Flow ,c. ) {lblsec.}
{million Btu/sec.}  
{million Btu/sec.}
{sec. } {lb/sec.}  
{sec. } {lb/sec.}
{mi 11 ion Btu/sec.)
{mi 11 ion Btu/sec.)
1.0 422.5 .506i , .... o 41J.5 .4959 511.5 422.4 .S067 541.5 413.4 .4951 512.0 422.J .5065 549.0 41J.J .4957 512.5 422.2 .5064 549.5 413.Z .4955 513.0 422.0 .5063 550.0 413.1 .4954 513.5 421.9 .S061 550.5 412.9 .4952 514.0 421.1 .5060 551.0 412.1 .4951 5H.5 421.7 .sose 551.5 412.7 .4949 515.0 421.5 .5057 552.0 412.6 .4948 51505 421.4 .5055 552.5 412.5 .4946 516.0 421.3 .5054 553.0 412.3 .4945 516.5 421.2 .5052 553.5 412eZ .4943 517.0 421.1 .5051 554.0 412.1 .4942 554.5 412.0 .4941 517.5 420.9 .5049 555.0 411.9 .4939 555.5 511.0 420.I .5()41 556.0 411.7 .4938 511.5 420.7 .5046 556.S 411.6 .4936 519.0 420.6 .5045 557.0 411.S .4935 519.5 420.4 .5043 411.4 .4933 520.0 420.J .5042 520.5 420.Z .504() 557.5 411.J .4932 521.0 420.1 .5039 551.0 411.1 .4930 521.5 420.0 .5037 551.5 411.0 .4929 522.0 419.I .5036 559.0 410.9 .4927 522.5 419.7 .5034 559.5 410.1 .492.ti . 523.0 419.6 .5033 560.0 410.7 .4925 523.5 419.S .5031 560.5 410.S .4923 524.0 419.4 .5030 561.0 410.4 .. 4922 . 524.5 419.Z .5021 561.5 410.J .4920 525.0 419. 1 .5027 562.0 '10oZ .4919 41*5 419.0 .5026 562.5 410.1 .4917 .o 411.9 .5024 563.0 409.9 .4916 .5 411.7 .5023 563.5 409.1 .4914 .o 411.6 .5021 564.0 :g:.1 ;.4913 )27.5 411.5 .5020 564.5 .6 .4911 528.0 418.4 .5011 565.0 409.S .4910 528.5 411.3 .5017 565.5 409.J .4909 529.0 411.1 .5015 566.0 409.2 .4907 529.5 418.0 .5014 566.5 409.1 .4906 530.0 417.9 .5012 567.0 409.0 .4904 530.5 417.1 .5011 567.5 408.9 .4903 531.0 417.7 .5009 561.0 408.7 .4901 531.5 417.5 .sooa 561.5 408.6 .4900 532.0 417.4 .5006 569.0 408.S .4198 532.5 417.3 .SOOS 569.5 408.4 .4197 533.0 417.2 .5003 570.0 408.J .489S 533.5 417.0 .5002 570.5 408.1 .4194 534.0 416.9 .5001 571.0 408.0 .4193 534.5 416.8 .4999 571.5 407.9 .4191 535.0 416.7 .4991 572.0 407.1 .4190 535.5 416.6 .4996 572.5 407.7 .. 4118 536.0 416.le .4995 573.0 407.S .4887 536.5 416.3 -.4993 573.5 407.4 .4885 537.0 416.Z : .4992 574.0 407.J .4184 574.5 407.2 .4182 537.5 416.1 -.499() 575.0 407.1 .4881 5ll.O 416.0 .4989 575.5 406.9 .418() 531.5 415.I .4917 576.0 406.1 .4878 539.0 415.7 .49U 576.5 406.7 .4877 539.5 415.6 .4984 577.0 406.6 .4875 540.0 415.5 .4983 540.5 415.J .4981 577.5 406.5 541.0 415.2 .498() .4874 541.5 415.1 .4979 571.0 406.4 .4172 542.0 415.0 .4977 571.5 406.Z .4171 _.5 414.9 .4976 519.0 406.1 .4169 .o 414.7 .4974 579.5 406.0 .4168 .5 414.6 .4973 580.o 405.9 *4167 4.0 414.5 .4971 580.5 405.1 .4165 ,44.5 414.4 .4970 511.0 405.6 .4864 545.0 414.3 .4968 511.5 405.5 .4862 545.5 414.1 .4967 512.0 405.4 .4161 546.0 414.0 .4965 512.5 405.3 .4159 546.5 413.9 .4964 513.0 405.Z .4151 547.0 413.1 .4962 513.5 405.0 .4156 547.S 413.1 .4961 584.0 404.9 .4155 -. --584.5 404.1 .4154 --* -.   
1.0 422.5 .506i , .... o 41J.5 .4959 511.5 422.4 .S067 541.5 413.4 .4951 512.0 422.J .5065 549.0 41J.J .4957 512.5 422.2 .5064 549.5 413.Z .4955 513.0 422.0 .5063 550.0 413.1 .4954 513.5 421.9 .S061 550.5 412.9 .4952 514.0 421.1 .5060 551.0 412.1 .4951 5H.5 421.7 .sose 551.5 412.7 .4949 515.0 421.5 .5057 552.0 412.6 .4948 51505 421.4 .5055 552.5 412.5 .4946 516.0 421.3 .5054 553.0 412.3 .4945 516.5 421.2 .5052 553.5 412eZ .4943 517.0 421.1 .5051 554.0 412.1 .4942 554.5 412.0 .4941 517.5 420.9 .5049 555.0 411.9 .4939 555.5 511.0 420.I .5()41 556.0 411.7 .4938 511.5 420.7 .5046 556.S 411.6 .4936 519.0 420.6 .5045 557.0 411.S .4935 519.5 420.4 .5043 411.4 .4933 520.0 420.J .5042 520.5 420.Z .504() 557.5 411.J .4932 521.0 420.1 .5039 551.0 411.1 .4930 521.5 420.0 .5037 551.5 411.0 .4929 522.0 419.I .5036 559.0 410.9 .4927 522.5 419.7 .5034 559.5 410.1 .492.ti . 523.0 419.6 .5033 560.0 410.7 .4925 523.5 419.S .5031 560.5 410.S .4923 524.0 419.4 .5030 561.0 410.4 .. 4922 . 524.5 419.Z .5021 561.5 410.J .4920 525.0 419. 1 .5027 562.0 '10oZ .4919 41*5 419.0 .5026 562.5 410.1 .4917 .o 411.9 .5024 563.0 409.9 .4916 .5 411.7 .5023 563.5 409.1 .4914 .o 411.6 .5021 564.0 :g:.1 ;.4913 )27.5 411.5 .5020 564.5 .6 .4911 528.0 418.4 .5011 565.0 409.S .4910 528.5 411.3 .5017 565.5 409.J .4909 529.0 411.1 .5015 566.0 409.2 .4907 529.5 418.0 .5014 566.5 409.1 .4906 530.0 417.9 .5012 567.0 409.0 .4904 530.5 417.1 .5011 567.5 408.9 .4903 531.0 417.7 .5009 561.0 408.7 .4901 531.5 417.5 .sooa 561.5 408.6 .4900 532.0 417.4 .5006 569.0 408.S .4198 532.5 417.3 .SOOS 569.5 408.4 .4197 533.0 417.2 .5003 570.0 408.J .489S 533.5 417.0 .5002 570.5 408.1 .4194 534.0 416.9 .5001 571.0 408.0 .4193 534.5 416.8 .4999 571.5 407.9 .4191 535.0 416.7 .4991 572.0 407.1 .4190 535.5 416.6 .4996 572.5 407.7 .. 4118 536.0 416.le .4995 573.0 407.S .4887 536.5 416.3 -.4993 573.5 407.4 .4885 537.0 416.Z : .4992 574.0 407.J .4184 574.5 407.2 .4182 537.5 416.1 -.499() 575.0 407.1 .4881 5ll.O 416.0 .4989 575.5 406.9 .418() 531.5 415.I .4917 576.0 406.1 .4878 539.0 415.7 .49U 576.5 406.7 .4877 539.5 415.6 .4984 577.0 406.6 .4875 540.0 415.5 .4983 540.5 415.J .4981 577.5 406.5 541.0 415.2 .498() .4874 541.5 415.1 .4979 571.0 406.4 .4172 542.0 415.0 .4977 571.5 406.Z .4171 _.5 414.9 .4976 519.0 406.1 .4169 .o 414.7 .4974 579.5 406.0 .4168 .5 414.6 .4973 580.o 405.9 *4167 4.0 414.5 .4971 580.5 405.1 .4165 ,44.5 414.4 .4970 511.0 405.6 .4864 545.0 414.3 .4968 511.5 405.5 .4862 545.5 414.1 .4967 512.0 405.4 .4161 546.0 414.0 .4965 512.5 405.3 .4159 546.5 413.9 .4964 513.0 405.Z .4151 547.0 413.1 .4962 513.5 405.0 .4156 547.S 413.1 .4961 584.0 404.9 .4155 -. --584.5 404.1 .4154 --* -.   
-Sheet 10 of 10 Time Break Flow Energy Flow {sec.} {lblsec.}  
-Sheet 10 of 10 Time Break Flow Energy Flow {sec.} {lblsec.}
{million Btu/sec.)  
{million Btu/sec.)  
** u 4()1..1 .usz oS 404.6 .4151 .o 404.4 .4149 586.5 404.J .uu 517.0 404.z .4146 517.5 4()4.1 .4145 511.0 404.0 .4143 518.S 403.9 .4142 589.0 403.1 .4141 519.5 403.6 .4839 590 .. 0 403.5 .4831 590.5 403.4 .4836 591.0 403.3 .4135 591.5 403.1 .4133 592.0 403.0 .4832 592.5 402.9 .4831 593.0 402.8 .41l9 593.5 402.1 .4828 594.0 402.S .4126 594.5 402.4 .4125 595.0 402.3 .4123 595.5 402.2 .4122 596.0 402.1 .4820 596.5 40Ze0 .4819 597.0 401.I .4811 597.5 401 * ., .4816 599.0 401.6 .4115 599.5 401.S .4113 599.0 401.4 .4112 599.5 401.2 .4110 .o. 401.1 .4809
** u 4()1..1 .usz oS 404.6 .4151 .o 404.4 .4149 586.5 404.J .uu 517.0 404.z .4146 517.5 4()4.1 .4145 511.0 404.0 .4143 518.S 403.9 .4142 589.0 403.1 .4141 519.5 403.6 .4839 590 .. 0 403.5 .4831 590.5 403.4 .4836 591.0 403.3 .4135 591.5 403.1 .4133 592.0 403.0 .4832 592.5 402.9 .4831 593.0 402.8 .41l9 593.5 402.1 .4828 594.0 402.S .4126 594.5 402.4 .4125 595.0 402.3 .4123 595.5 402.2 .4122 596.0 402.1 .4820 596.5 40Ze0 .4819 597.0 401.I .4811 597.5 401 * ., .4816 599.0 401.6 .4115 599.5 401.S .4113 599.0 401.4 .4112 599.5 401.2 .4110 .o. 401.1 .4809
Line 537: Line 537:
* 2.751 17.00 575.3 .6929
* 2.751 17.00 575.3 .6929
* oo 2291
* oo 2291
* Z.740 17.50 574.1 .6915 3.50 2289. 2.730 18.00 572.9 .6900 34.00 22ao. 2.719 18.50 571.7 .6816 34e50 2271. 2.709 89.00 570.5 .6872 35a00 2262. Z.699 89.50 569.4 .68S& 35.50 2252. Z.687 90.00 568.2 .6844 36.00 2243. 2.676 36.50 2233. 2.665 *31.00 2224. 2.654 Sheet 3 of 9 Time Break Flow Energy Flow. Time. .Break.Flow . Energy.Flow lb/sec.} {million Btu/sec.}  
* Z.740 17.50 574.1 .6915 3.50 2289. 2.730 18.00 572.9 .6900 34.00 22ao. 2.719 18.50 571.7 .6816 34e50 2271. 2.709 89.00 570.5 .6872 35a00 2262. Z.699 89.50 569.4 .68S& 35.50 2252. Z.687 90.00 568.2 .6844 36.00 2243. 2.676 36.50 2233. 2.665 *31.00 2224. 2.654 Sheet 3 of 9 Time Break Flow Energy Flow. Time. .Break.Flow . Energy.Flow lb/sec.} {million Btu/sec.}
{sec.} Pb/sec.} {million 0 567., .6130 127.5 506.1 .61&deg;' 91.00 566.0 .6117 121.0 506.Z 91.50 564.9 *"&deg;' 121.5 505.6 .6099 9Z.OO . 563.1 .6190 1Z9.0 505.0 .6082 56Z.7 .6m 1Z9.5 506.4 .6075 93.00 56,., .6764 130.0 503.1 .6068 93.50 560.6 .6752 130.5 503.Z .6061 94.00 559.5 .6739 131.0 502.6 .6053 94.50 551.5 .6727 131.5 502.0 .6046 9S.OO 557.4 .6714 132.0 501.4 .6039 95.50 556.4 .6702 13Z .. S 500.9 .6032 96 .. 00 555.4 .6690 133.0 500.] .602S 96.50 554.4 .6678 133.5 499.7 .6019 97.00 553.4 .6666 134.0 499.1 .6012 134.,S 498.6 .6005 135.0 498.0 .5998 97.50 552.5 .6654 135.5 497.5 .5991 98.00 551.5 .6643 136.0 496.9 .5994 550.5 -.6631 136.5 496.S .5971 98.50 -137.0 99.00 549.6 .6620 495.1 .5971 99.50 541.7 .6608 100.0 547.7 .6597 137.S 4".Z 100.5 546.1 .6586 .5964 101 .o 545.9 .6575 131.0 494.7 .59SS 101 .5 545.0 .6564 131.5 494.1 .m1 102.0 544.1 .6554 139.0 49J.6 .5945 102.5 543.Z .6543 U9.5 493.1 .5931 103.0 542.3 .6532 140.0 49Z.5 .59JZ 103.5  
{sec.} Pb/sec.} {million 0 567., .6130 127.5 506.1 .61&deg;' 91.00 566.0 .6117 121.0 506.Z 91.50 564.9 *"&deg;' 121.5 505.6 .6099 9Z.OO . 563.1 .6190 1Z9.0 505.0 .6082 56Z.7 .6m 1Z9.5 506.4 .6075 93.00 56,., .6764 130.0 503.1 .6068 93.50 560.6 .6752 130.5 503.Z .6061 94.00 559.5 .6739 131.0 502.6 .6053 94.50 551.5 .6727 131.5 502.0 .6046 9S.OO 557.4 .6714 132.0 501.4 .6039 95.50 556.4 .6702 13Z .. S 500.9 .6032 96 .. 00 555.4 .6690 133.0 500.] .602S 96.50 554.4 .6678 133.5 499.7 .6019 97.00 553.4 .6666 134.0 499.1 .6012 134.,S 498.6 .6005 135.0 498.0 .5998 97.50 552.5 .6654 135.5 497.5 .5991 98.00 551.5 .6643 136.0 496.9 .5994 550.5 -.6631 136.5 496.S .5971 98.50 -137.0 99.00 549.6 .6620 495.1 .5971 99.50 541.7 .6608 100.0 547.7 .6597 137.S 4".Z 100.5 546.1 .6586 .5964 101 .o 545.9 .6575 131.0 494.7 .59SS 101 .5 545.0 .6564 131.5 494.1 .m1 102.0 544.1 .6554 139.0 49J.6 .5945 102.5 543.Z .6543 U9.5 493.1 .5931 103.0 542.3 .6532 140.0 49Z.5 .59JZ 103.5  
.652"2 140.5 492.u .59ZS 104.0 540 .. 6 .6512 141.0 491.5 *"'' . 5. 539.& .6501 141.5 490.9 .S91S 0 538.9 .6491 142.0 490.4 .5906 s 538.1 .6481 142.5 419.9 .S900 .o 537.Z .6471 143.0 .e9.4 .5894 06.S 536.4 .6461 143.5 418.I .5887 107.0 535.6 .6451 144.0 488.] .sae1 107.S 534.1 .6441 144.5 417.1 .5875 108.0 534.0 .6432 145.0 417.J .5869 108.5 533.2 .6422 145.5 416.1 .5863 109.0 53Z .. 4 .6412 146.0 416.J .5856 109.S 531.6 .6403 146.5 415.1 .5850 110.0 530.1 .6394 147.0 415.3 .5144 110.5 530.0 .6314 147.5 414.1 .5831 111.0 5Z9.3 .6375 141.0 414.3 .Sill 111.5 528.5 .6366 141.5 413.1 .sa.Z6 112.0 527.1 .6357 149.0 413.3 .5820 112.5, 527.0 .6341 149.5 412.1 .5114 113.0 526.3 .6339 150.0 412.S .SIOI 113.5 525.5 .6330 150.5 411.8 .5802 114.0 524.1 .6321 151.0 411.3 .5797 114.5 524.1 .6312 151.5 480.1 .51'91 115.0 523.4 .6304 152.0 480.4 .5715 115.5 522.6 .6295 152.5 479.,9 .sm 116.0 521.9 -.6286 153".0 419.4 .5m 116.S 521.2 .6271 153.5 471.9 . .5761 117 .. 0 520.5 .6269 154.0 471.4 .5762 154.5 471.0 .5756 155.0 477.5 .5750 117.5 519.1 .6261 155.5 477.0 .5745 11100 .519.1 .6HJ 156.0 476.6 .5739 111.5 511.4 .6244 ,56.5 476.1 .5733 119.0 517.1 .6236 157.0 475.6 .5728 119.5 517.1 .6221 157.S 475.Z .5722 120.0 516.4 .6220 'il0.5 515.7 .6212 1Slo0 474.1 .5717 1 .o 515. 1 .6204 151.5 474.z* _,,,, .5 514.4 .6196 159.0 473.1 .5706 .o 513.1 .6111 159.5 473.S .5700 .5 513.1 .6180 160.0 47Z.9 .5695 12].0 512.5 .617Z 160.5 472.4 .5689 12].5 511.I .6164 161.0 472.0 .5684 124.0 511.Z .6157 161.5 471.5 .5671 124.5 510.5 .6149 162.0 471 .. 1 .5673 125.0 S09.9 .6141 162.5 470.6 .5667 125.S 509.J .6134 163.0 470.Z .5662 126.0 509.7 .61Z6 163.S 469.7 .5657 126.5 508.0 .6,19 164.0 469.3 .565' 127.0 501.4 _.,,, 164.5 461.1 .5646 165.0 461.4 .5641 Sheet 4 of 9 Break Flow Energy Flow Time Break Flow Energy Flow lb sec. mi 11 ion Btu sec. sec . lb/sec. million Btu/sec.) .s 461.0
.652"2 140.5 492.u .59ZS 104.0 540 .. 6 .6512 141.0 491.5 *"'' . 5. 539.& .6501 141.5 490.9 .S91S 0 538.9 .6491 142.0 490.4 .5906 s 538.1 .6481 142.5 419.9 .S900 .o 537.Z .6471 143.0 .e9.4 .5894 06.S 536.4 .6461 143.5 418.I .5887 107.0 535.6 .6451 144.0 488.] .sae1 107.S 534.1 .6441 144.5 417.1 .5875 108.0 534.0 .6432 145.0 417.J .5869 108.5 533.2 .6422 145.5 416.1 .5863 109.0 53Z .. 4 .6412 146.0 416.J .5856 109.S 531.6 .6403 146.5 415.1 .5850 110.0 530.1 .6394 147.0 415.3 .5144 110.5 530.0 .6314 147.5 414.1 .5831 111.0 5Z9.3 .6375 141.0 414.3 .Sill 111.5 528.5 .6366 141.5 413.1 .sa.Z6 112.0 527.1 .6357 149.0 413.3 .5820 112.5, 527.0 .6341 149.5 412.1 .5114 113.0 526.3 .6339 150.0 412.S .SIOI 113.5 525.5 .6330 150.5 411.8 .5802 114.0 524.1 .6321 151.0 411.3 .5797 114.5 524.1 .6312 151.5 480.1 .51'91 115.0 523.4 .6304 152.0 480.4 .5715 115.5 522.6 .6295 152.5 479.,9 .sm 116.0 521.9 -.6286 153".0 419.4 .5m 116.S 521.2 .6271 153.5 471.9 . .5761 117 .. 0 520.5 .6269 154.0 471.4 .5762 154.5 471.0 .5756 155.0 477.5 .5750 117.5 519.1 .6261 155.5 477.0 .5745 11100 .519.1 .6HJ 156.0 476.6 .5739 111.5 511.4 .6244 ,56.5 476.1 .5733 119.0 517.1 .6236 157.0 475.6 .5728 119.5 517.1 .6221 157.S 475.Z .5722 120.0 516.4 .6220 'il0.5 515.7 .6212 1Slo0 474.1 .5717 1 .o 515. 1 .6204 151.5 474.z* _,,,, .5 514.4 .6196 159.0 473.1 .5706 .o 513.1 .6111 159.5 473.S .5700 .5 513.1 .6180 160.0 47Z.9 .5695 12].0 512.5 .617Z 160.5 472.4 .5689 12].5 511.I .6164 161.0 472.0 .5684 124.0 511.Z .6157 161.5 471.5 .5671 124.5 510.5 .6149 162.0 471 .. 1 .5673 125.0 S09.9 .6141 162.5 470.6 .5667 125.S 509.J .6134 163.0 470.Z .5662 126.0 509.7 .61Z6 163.S 469.7 .5657 126.5 508.0 .6,19 164.0 469.3 .565' 127.0 501.4 _.,,, 164.5 461.1 .5646 165.0 461.4 .5641 Sheet 4 of 9 Break Flow Energy Flow Time Break Flow Energy Flow lb sec. mi 11 ion Btu sec. sec . lb/sec. million Btu/sec.) .s 461.0
* 5635 z02.s 431.6 .5l80 166.0 461.5 .5630 Z03.0 431.Z .5276 166.5 . 467.1 .5625 203 .. S 437.8 .5271 167.0 466.7 .5619 204.0 437.5 .5267 167.S 466.Z .5614 204.5 437.1 .5263 168.0 465.8 .5609 205.0 436.1 .52sa 161.5 465.4 .5604 205.5 436.4 .5254 169.0 464.9 .5599 206.0 436.0 .5250 169.5 464.5 .5593 206.5 435.7 .5245 170.0 464.1 .ssaa 207.0 435.3 .5241 170.5 463.7 .5583 207.5 435.0 .5237 171 .. 0 463.Z .5578 2oe.o 434.6 .5232 171.5 w.1 .5573 209.5 434.3 .5zza 17Z.O W.4 .5561 209.0 433.9 .5224 17Z.5 w.o .5563 209.5 433.5 .5219 173 .. 0 461.5 .55sa 210.0 433.2 .5215 173.5 461.1 .5553 210.s 432.1 .5211 174.0 460 .. 7 .. 5548 211.0 432.5 .5207 174.5 460.J .5543 211.5 432.1 .5202 11s.o 459.9 .5531 212.0 431.I .5198 175.5 459.5 .5533 212.5 431.4 .5194 176.0 459.1 .ss2a 213.0 431.1 .5190 176.S 458.6 .55l3 213.5 430.7 .5185 177.0 458.2 .5511 214.0 430.4 .5181 214.5 430.0 .517-1 215.0 429.7 .5173 11705 457.1 .5513 215.5 429.4 .5169 216.0 429.1 .5165 111.0 457.4 .55oe* 216.5 421.a .5162 171 .. 5 457.0 .5503 211 .. 0 428.S .5158 O* 456.6 .5491 456.2 .5493 455.8 .5481 .5 455.4 .5413 217.S 428.1 .5154 1.0 455.0 .5471 21a.o 427.8 .5150 1151 .5 454.6 .5474 211.5 427.5 .5146 112.0 454.Z .5469 219.0 427.2 .5143 112.5 453.1 .5464 219.5 426.9 .5139 113.0 453.4 .S459 220.0 426.6 .5135 11305 453.0 .5454 220.5 426 .. 3 .5132 114.0 452.6 .5450 221.0 426.0 .5121 114.5 452.Z .5445 221.5 425.7 .5124 115.0 451.I .5440 222.0 425.4 .5120 115.5 451.4 .5435 222.5 425.0 .5117 116 .. 0 451.0 .5431 223.0 424.7 .5113 116 .. 5 450.6 .5426 223.5 424.4 .5109 111.0 450.Z .5421 224 .. 0 424.1 .5105 187 .. S 449.9 .S416 224.5 423.1 .5102 181.0 449.5 .541Z 225.0 423.5 .5cm 181.5 449.1 .5407 225.5 423.2 .5094 189.0 441.7 .540Z 226.0 422.9 .5091 189.5 441.J .5398 226.5 422.6 .5057 190.0 447.9 -*.5393 221.0 422.3 .sou 190.S 447.5 .5389 227.S 422.0 .5079 191.0 447.Z .5384 221.0 421.7 .5076 191.S 446.I .5379 221.s 421.4 .5072 192.0 446.4 -.5375 229.0 421.0 .5068 192.S 446.0 .5370 229.5 420.7 .5065 193.0 445.6 .5365 230.0 420.4 .5061 193.S 445.J .5361 230.5 420.1 .5057 194.0 444.9 .5356 231.0 419.I .5053 194.5 444.5 .5352 231.5 419.5 .5050 195.0 444.1 .5347 232.0 419.Z .5046 195.5 443.7 .5343 232.5 411.9 .5042 196.0 443.4 .5331 233.0 411.6 .5039 196.5 443.0 .5334 233.5 411.3 .5035 0 442.6 .5329 234.0 411.0 .5031 234.5 417.7 .* 5026 .5 442.3 .5325 235.0 417.4 .5024 18.0 441.9 .S320 235.5 417.1 .S020. 198.5 441.5 .5316 236.0 416.I .5016 199.0 441.1 .5311 236.5 416.5 .son 199.5 440.1 .5307 237.0 416.2 .5009 200.0 440.4 .5302 200.5 440.0 .5298 201 .o 439.7 .5293 201.5 439.J .5289 202.0 438.9 .5215 Sheet 5 of 9 Break Flow Energy Flow Time Break Flow Fl ow lb/sec.) {million  
* 5635 z02.s 431.6 .5l80 166.0 461.5 .5630 Z03.0 431.Z .5276 166.5 . 467.1 .5625 203 .. S 437.8 .5271 167.0 466.7 .5619 204.0 437.5 .5267 167.S 466.Z .5614 204.5 437.1 .5263 168.0 465.8 .5609 205.0 436.1 .52sa 161.5 465.4 .5604 205.5 436.4 .5254 169.0 464.9 .5599 206.0 436.0 .5250 169.5 464.5 .5593 206.5 435.7 .5245 170.0 464.1 .ssaa 207.0 435.3 .5241 170.5 463.7 .5583 207.5 435.0 .5237 171 .. 0 463.Z .5578 2oe.o 434.6 .5232 171.5 w.1 .5573 209.5 434.3 .5zza 17Z.O W.4 .5561 209.0 433.9 .5224 17Z.5 w.o .5563 209.5 433.5 .5219 173 .. 0 461.5 .55sa 210.0 433.2 .5215 173.5 461.1 .5553 210.s 432.1 .5211 174.0 460 .. 7 .. 5548 211.0 432.5 .5207 174.5 460.J .5543 211.5 432.1 .5202 11s.o 459.9 .5531 212.0 431.I .5198 175.5 459.5 .5533 212.5 431.4 .5194 176.0 459.1 .ss2a 213.0 431.1 .5190 176.S 458.6 .55l3 213.5 430.7 .5185 177.0 458.2 .5511 214.0 430.4 .5181 214.5 430.0 .517-1 215.0 429.7 .5173 11705 457.1 .5513 215.5 429.4 .5169 216.0 429.1 .5165 111.0 457.4 .55oe* 216.5 421.a .5162 171 .. 5 457.0 .5503 211 .. 0 428.S .5158 O* 456.6 .5491 456.2 .5493 455.8 .5481 .5 455.4 .5413 217.S 428.1 .5154 1.0 455.0 .5471 21a.o 427.8 .5150 1151 .5 454.6 .5474 211.5 427.5 .5146 112.0 454.Z .5469 219.0 427.2 .5143 112.5 453.1 .5464 219.5 426.9 .5139 113.0 453.4 .S459 220.0 426.6 .5135 11305 453.0 .5454 220.5 426 .. 3 .5132 114.0 452.6 .5450 221.0 426.0 .5121 114.5 452.Z .5445 221.5 425.7 .5124 115.0 451.I .5440 222.0 425.4 .5120 115.5 451.4 .5435 222.5 425.0 .5117 116 .. 0 451.0 .5431 223.0 424.7 .5113 116 .. 5 450.6 .5426 223.5 424.4 .5109 111.0 450.Z .5421 224 .. 0 424.1 .5105 187 .. S 449.9 .S416 224.5 423.1 .5102 181.0 449.5 .541Z 225.0 423.5 .5cm 181.5 449.1 .5407 225.5 423.2 .5094 189.0 441.7 .540Z 226.0 422.9 .5091 189.5 441.J .5398 226.5 422.6 .5057 190.0 447.9 -*.5393 221.0 422.3 .sou 190.S 447.5 .5389 227.S 422.0 .5079 191.0 447.Z .5384 221.0 421.7 .5076 191.S 446.I .5379 221.s 421.4 .5072 192.0 446.4 -.5375 229.0 421.0 .5068 192.S 446.0 .5370 229.5 420.7 .5065 193.0 445.6 .5365 230.0 420.4 .5061 193.S 445.J .5361 230.5 420.1 .5057 194.0 444.9 .5356 231.0 419.I .5053 194.5 444.5 .5352 231.5 419.5 .5050 195.0 444.1 .5347 232.0 419.Z .5046 195.5 443.7 .5343 232.5 411.9 .5042 196.0 443.4 .5331 233.0 411.6 .5039 196.5 443.0 .5334 233.5 411.3 .5035 0 442.6 .5329 234.0 411.0 .5031 234.5 417.7 .* 5026 .5 442.3 .5325 235.0 417.4 .5024 18.0 441.9 .S320 235.5 417.1 .S020. 198.5 441.5 .5316 236.0 416.I .5016 199.0 441.1 .5311 236.5 416.5 .son 199.5 440.1 .5307 237.0 416.2 .5009 200.0 440.4 .5302 200.5 440.0 .5298 201 .o 439.7 .5293 201.5 439.J .5289 202.0 438.9 .5215 Sheet 5 of 9 Break Flow Energy Flow Time Break Flow Fl ow lb/sec.) {million
{sec.} {1 b/sec. {million Btu/sec.)
{sec.} {1 b/sec. {million Btu/sec.)
Z37.5 415.t .5005 z15.o 393.J .4733 ne.o 415.5 .5002 Z75.5 393.0 .4729 Z38.5 415.Z .4998 276.0 392.7 .4725 Z39.0 414.9 .4"4 Z76.5 392.4 .4722 Z39.5 414.6 .4"1 211.0 392.1 .4711 Z40.0 414.J .4917 Z40.5 614.0 .4913 Z41.0 413.7 .4990 Z41.5 41J.4 .4976 Z77.5 J91.I .4715 Z42o0 41J., .497Z Z71.0 J91.5 .4711 242.5 412.1 .'969 Z71.5 . J91.2 .4708 243.0 412.5 .4965 279.0 390.9 .4704 Z4J.,5 412.2 .4961 279.5 390.6 .4701 244.0 411.9 .4951 zao.o J90.4 .4697 z,4.5 4,1.6 .4954 210.s J90.1 .4694 245.0 4n.J .4950 za1.o 389.8 .4690 245.S 4n.o .4947 211.5 389.5 .4687 Z46.0 .. ,0.7 .4943 212.0 389.2 .4683 Z46.5  
Z37.5 415.t .5005 z15.o 393.J .4733 ne.o 415.5 .5002 Z75.5 393.0 .4729 Z38.5 415.Z .4998 276.0 392.7 .4725 Z39.0 414.9 .4"4 Z76.5 392.4 .4722 Z39.5 414.6 .4"1 211.0 392.1 .4711 Z40.0 414.J .4917 Z40.5 614.0 .4913 Z41.0 413.7 .4990 Z41.5 41J.4 .4976 Z77.5 J91.I .4715 Z42o0 41J., .497Z Z71.0 J91.5 .4711 242.5 412.1 .'969 Z71.5 . J91.2 .4708 243.0 412.5 .4965 279.0 390.9 .4704 Z4J.,5 412.2 .4961 279.5 390.6 .4701 244.0 411.9 .4951 zao.o J90.4 .4697 z,4.5 4,1.6 .4954 210.s J90.1 .4694 245.0 4n.J .4950 za1.o 389.8 .4690 245.S 4n.o .4947 211.5 389.5 .4687 Z46.0 .. ,0.7 .4943 212.0 389.2 .4683 Z46.5  
Line 582: Line 582:
* Charging pumps begin borated water Low pressure trip point T1me (sec.) 0 22.1 24.0 0 172 214 0 . reached 64 Rods begin to drop 66 14202., I .04 1.03 . a: 1.02 0 r-u < la.. z 1.0 I 0 .... I-< u .... ...I 1.00 CL .... I-...I ::) :E 0.99 0.98 0.97 .........  
* Charging pumps begin borated water Low pressure trip point T1me (sec.) 0 22.1 24.0 0 172 214 0 . reached 64 Rods begin to drop 66 14202., I .04 1.03 . a: 1.02 0 r-u < la.. z 1.0 I 0 .... I-< u .... ...I 1.00 CL .... I-...I ::) :E 0.99 0.98 0.97 .........  
-
-
200 250 300 350 400 450 500 550 CORE AVERAGE TEMPERATURE  
200 250 300 350 400 450 500 550 CORE AVERAGE TEMPERATURE
(*F) PUBLIC SERVICE ELECTRIC AND GAS COMPANY Vari*tion of KEFF with Core Temperature SALEM NUCLEAR GENERATING STATION Updated FSAR Figure 15.2*41 *
(*F) PUBLIC SERVICE ELECTRIC AND GAS COMPANY Vari*tion of KEFF with Core Temperature SALEM NUCLEAR GENERATING STATION Updated FSAR Figure 15.2*41 *
* 2t+OO 2200 2000 1800 1600 -411: I ijQO Cl) ""' ex 1200 ;:) Cl) Cl) ""' ex Cl) 1000 (,,.) ex 800 600 200 0 -0 100 200 300 t+OO 500 600 700 SAFETY INJECTION FLOW
* 2t+OO 2200 2000 1800 1600 -411: I ijQO Cl) ""' ex 1200 ;:) Cl) Cl) ""' ex Cl) 1000 (,,.) ex 800 600 200 0 -0 100 200 300 t+OO 500 600 700 SAFETY INJECTION FLOW
Line 592: Line 592:
* 15.4.2 MAJOR SECONDARY SYSTEM PIPE RUPTURE 15.4.2.1 IDENTIFICATION OF CAUSES AND ACCIDENT DESCRIPTION The steam release arising from a rupture of a main steam pipe would result in an initial increase in steam flow which decreases during the .accident as the steam pressure falls. The removal from the Reactor Coolant System causes a reduction of coolant temperature and pressure.
* 15.4.2 MAJOR SECONDARY SYSTEM PIPE RUPTURE 15.4.2.1 IDENTIFICATION OF CAUSES AND ACCIDENT DESCRIPTION The steam release arising from a rupture of a main steam pipe would result in an initial increase in steam flow which decreases during the .accident as the steam pressure falls. The removal from the Reactor Coolant System causes a reduction of coolant temperature and pressure.
In the presence of a negative moderator temperature coefficient, the cooldown results in a reduction of core shutdown margin. If the most reactive rod cluster control assembly is assumed stuck in its fully withdrawn position after reactor trip, there is an increased possibility that the core will become critical and return to power. A return to power following a steam pipe rupture is a potential problem mainly because of the high power peaking factors which exist assuming the most reactive rod cluster control assembly to be stuck in its fully withdrawn position.
In the presence of a negative moderator temperature coefficient, the cooldown results in a reduction of core shutdown margin. If the most reactive rod cluster control assembly is assumed stuck in its fully withdrawn position after reactor trip, there is an increased possibility that the core will become critical and return to power. A return to power following a steam pipe rupture is a potential problem mainly because of the high power peaking factors which exist assuming the most reactive rod cluster control assembly to be stuck in its fully withdrawn position.
The core is ultimately shutdown by the boric acid injection delivered by the Safety Injection System. The analysis of a main steam pipe rupture is performed to demonstrate that the following criteria are satisfied:  
The core is ultimately shutdown by the boric acid injection delivered by the Safety Injection System. The analysis of a main steam pipe rupture is performed to demonstrate that the following criteria are satisfied:
: 1. Assuming a stuck rod cluster control assembly, with or without offsite power, and assuming a single failure in the engineered safeguards there is no consequential damage to the primary system and the core remains in place and intact. 2. Energy release to containment from the worst steam pipe break does not cause failure of the containment structure.
: 1. Assuming a stuck rod cluster control assembly, with or without offsite power, and assuming a single failure in the engineered safeguards there is no consequential damage to the primary system and the core remains in place and intact. 2. Energy release to containment from the worst steam pipe break does not cause failure of the containment structure.
Although DNB and possible clad perforation following*
Although DNB and possible clad perforation following*
Line 605: Line 605:
* Fast-act1ng valves are prov1ded 1n each steam line that will fully w1thin 7 seconds of a signal to close (including instrumentation delays). For breaks downstream of the isolation valves, closure of all valves would completely terminate the blowdown.
* Fast-act1ng valves are prov1ded 1n each steam line that will fully w1thin 7 seconds of a signal to close (including instrumentation delays). For breaks downstream of the isolation valves, closure of all valves would completely terminate the blowdown.
For any break, in any location, no more than one steam generator would blowdown even if one of 'the 1solat1on valves fails to close. A description of steam line isolation is included in Chapter 10. Steam flow 1s measured by monitoring dynam1c head in nozzles inside the steam pipes. The nozzles which are of considerably smaller diameter than the main steam pipe are located inside the containment near the steam generators and also serve to limit the maximum steam flow for any break further downstream.
For any break, in any location, no more than one steam generator would blowdown even if one of 'the 1solat1on valves fails to close. A description of steam line isolation is included in Chapter 10. Steam flow 1s measured by monitoring dynam1c head in nozzles inside the steam pipes. The nozzles which are of considerably smaller diameter than the main steam pipe are located inside the containment near the steam generators and also serve to limit the maximum steam flow for any break further downstream.
15.4.2.2 METHOD OF ANALYSIS The analysis of the steam pipe rupture has been performed to determine:  
15.4.2.2 METHOD OF ANALYSIS The analysis of the steam pipe rupture has been performed to determine:
: l. The core heat flux and Reactor Coolant System temperature and pressure resulting from the cooldown following the steam line break. The LOFTRAN[2?] code has been used. 2. The thermal and hydraulic behavior of the core following a steam line break. A detailed thermal and hydraulic digital-computer code, THINC, has J been used to determine if DNB occurs for the core conditions computed in (l) above. The following conditions were assumed to exist at the time of a main steam line break. ace i de_nt. l. End of life shutdown margin at no load, equilibrium xenon conditions, and the most reactive assembly stuck in its fully withdrawn position:
: l. The core heat flux and Reactor Coolant System temperature and pressure resulting from the cooldown following the steam line break. The LOFTRAN[2?] code has been used. 2. The thermal and hydraulic behavior of the core following a steam line break. A detailed thermal and hydraulic digital-computer code, THINC, has J been used to determine if DNB occurs for the core conditions computed in (l) above. The following conditions were assumed to exist at the time of a main steam line break. ace i de_nt. l. End of life shutdown margin at no load, equilibrium xenon conditions, and the most reactive assembly stuck in its fully withdrawn position:
Operation of the control rod banks during core burnup is restricted in such a way that addition of posit1ve reactivity in a steam line break accident will not lead to a more adverse condition than the case analyzed.
Operation of the control rod banks during core burnup is restricted in such a way that addition of posit1ve reactivity in a steam line break accident will not lead to a more adverse condition than the case analyzed.
Line 616: Line 616:
The keff versus temperature at 1000 psi corresponding to the negative moderator temperature coefficient used is shown in Figure 15.4-48. The effect of power generat1on in the core on over-all reactivity is shown in Figure 15.4-49. The core properties associated with the sector nearest the affected steam generator and those associated with the remaining sector were conservatively combined to obtain average core properties for reactivity feedback calculations.
The keff versus temperature at 1000 psi corresponding to the negative moderator temperature coefficient used is shown in Figure 15.4-48. The effect of power generat1on in the core on over-all reactivity is shown in Figure 15.4-49. The core properties associated with the sector nearest the affected steam generator and those associated with the remaining sector were conservatively combined to obtain average core properties for reactivity feedback calculations.
Further, it was conservatively assumed that the core power distribution was uniform. These two conditions cause underprediction of the reactivity feedback in the high power region near the stuck rod. To verify the conservatism of this method, the reactivity as well as the power distribution was checked. These core analyses considered the Doppler reactivity from the high fuel temperature near the stuck RCCA, moderator feedback from the high water enthalpy near the stuck RCCA, power redistribut1on and nonuniform core inlet temperature effects. For cases in which steam generation occurs in the high flux regions of the core, the effect of void formation was also included.
Further, it was conservatively assumed that the core power distribution was uniform. These two conditions cause underprediction of the reactivity feedback in the high power region near the stuck rod. To verify the conservatism of this method, the reactivity as well as the power distribution was checked. These core analyses considered the Doppler reactivity from the high fuel temperature near the stuck RCCA, moderator feedback from the high water enthalpy near the stuck RCCA, power redistribut1on and nonuniform core inlet temperature effects. For cases in which steam generation occurs in the high flux regions of the core, the effect of void formation was also included.
It was determined that the reactivity employed in the kinetics analysis was always larger than the reactivity calculated for all cases. These results verified conservatism; i.e., underprediction of negative reactivity feedback from power generation.  
It was determined that the reactivity employed in the kinetics analysis was always larger than the reactivity calculated for all cases. These results verified conservatism; i.e., underprediction of negative reactivity feedback from power generation.
: 3. Minimum capability for injection of boric acid (2,000 ppm) solution corresponding to the most restrictive single failure in the safety injection 9'YStem. This corresponds to the flow delivered by one charging pump delivering its full flow to the cold leg header. Low concentration boric acid (<2,000 ppm) must be purged from the safety injection lines downstream of the Refueling Water Storage Tank prior to the delivery of boric acid to the reactor coolant loops. This effect has been allowed for in the analysis by assuming the lines to contain unborated water. The modeling of the Safety Injection System in LOFTRAN is described in Reference  
: 3. Minimum capability for injection of boric acid (2,000 ppm) solution corresponding to the most restrictive single failure in the safety injection 9'YStem. This corresponds to the flow delivered by one charging pump delivering its full flow to the cold leg header. Low concentration boric acid (<2,000 ppm) must be purged from the safety injection lines downstream of the Refueling Water Storage Tank prior to the delivery of boric acid to the reactor coolant loops. This effect has been allowed for in the analysis by assuming the lines to contain unborated water. The modeling of the Safety Injection System in LOFTRAN is described in Reference
: 27. S.GS-U\:.SAfl....
: 27. S.GS-U\:.SAfl....
15"*4-15
15"*4-15
Line 623: Line 623:
After the generation of the safety injection signal (appropriate delays for instrumentation.
After the generation of the safety injection signal (appropriate delays for instrumentation.
logic and signal transport included), the appropriate valves begin to operate and the high head injection pump starts. In an additional 12 sec, the valves are assumed to be in their final position and the pump is assumed to be at full speed. The volume containing the unborated water is purged before the 2,000 ppm boron reaches the core. This delay, described above, is inherently 1ricluded in the modeling.
logic and signal transport included), the appropriate valves begin to operate and the high head injection pump starts. In an additional 12 sec, the valves are assumed to be in their final position and the pump is assumed to be at full speed. The volume containing the unborated water is purged before the 2,000 ppm boron reaches the core. This delay, described above, is inherently 1ricluded in the modeling.
* In cases where offsite power is not available, a 12-sec delay is assumed to start the diesels and to load the necessary safety injection equipment onto them. 4. Four combinations of break sizes and initial plant conditions have been considered in determining the core power and Reactor Coolant System transients:  
* In cases where offsite power is not available, a 12-sec delay is assumed to start the diesels and to load the necessary safety injection equipment onto them. 4. Four combinations of break sizes and initial plant conditions have been considered in determining the core power and Reactor Coolant System transients:
: 5. a. Complete severance of a pipe outside the containment, downstream of the steam flow measuring nozzle, with the plant initially at no load conditions, full reactor coolant flow with offsite power available.  
: 5. a. Complete severance of a pipe outside the containment, downstream of the steam flow measuring nozzle, with the plant initially at no load conditions, full reactor coolant flow with offsite power available.
: b. Complete severance of a pipe inside the containment at the outlet of the steam generator with the plant initially at no load conditions with offsite power available.  
: b. Complete severance of a pipe inside the containment at the outlet of the steam generator with the plant initially at no load conditions with offsite power available.
: c. Case (a) above with loss of offsite power simultaneous with the initiation of the safety injection signal. Loss of offsite power results-in coolant pump coastdown.  
: c. Case (a) above with loss of offsite power simultaneous with the initiation of the safety injection signal. Loss of offsite power results-in coolant pump coastdown.
: d. Case tb) above with the loss of offstte power simultaneous with the initiation of the safety injection signal. Power peaking factors corresponding to one stuck RCCA and non uniform core inlet coolant temperatures are determined at end of core life. The coldest core inlet temperatures are assumed to occur in the sector with the stuck rod. The power peaking factors account for the effect of the UFSA'-.. -e92ee .1 e/01eees . \5*4-'2.0   
: d. Case tb) above with the loss of offstte power simultaneous with the initiation of the safety injection signal. Power peaking factors corresponding to one stuck RCCA and non uniform core inlet coolant temperatures are determined at end of core life. The coldest core inlet temperatures are assumed to occur in the sector with the stuck rod. The power peaking factors account for the effect of the UFSA'-.. -e92ee .1 e/01eees . \5*4-'2.0   
* ** local void in the region of the stuck control assembly during return to power phase following the steam line break. This void in conjunction with the large negative moderator coefficient partially offsets the effect of the stuck assembly.
* ** local void in the region of the stuck control assembly during return to power phase following the steam line break. This void in conjunction with the large negative moderator coefficient partially offsets the effect of the stuck assembly.
Line 655: Line 655:
8929Q:19/97988S IS-* 4-2.4
8929Q:19/97988S IS-* 4-2.4
* 2. Off-s1te power 1s lost, main steam condensers are not ava11able for steam dump. 3. Eight hours after the accident the Residual Heat Removal System starts operation to cool down the plant. 4. The primary to secondary leakage is evenly d1str1buted in the three non-defective steam generators.
* 2. Off-s1te power 1s lost, main steam condensers are not ava11able for steam dump. 3. Eight hours after the accident the Residual Heat Removal System starts operation to cool down the plant. 4. The primary to secondary leakage is evenly d1str1buted in the three non-defective steam generators.
no tube leakage in the defective steam generator.  
no tube leakage in the defective steam generator.
: 5. Defective fuel is l percent. 6. After eight hours following the accident.
: 5. Defective fuel is l percent. 6. After eight hours following the accident.
no steam and activity are released to the environment.  
no steam and activity are released to the environment.
: 7. No air ejector release and no steam generator blowdown during the accident.  
: 7. No air ejector release and no steam generator blowdown during the accident.
: 8. No noble gas is dissolved in the steam generator water. amount of iodine/unit mass steam = 0 1 9. The iodine partition factor amount of 1odine/unit mass liquid . in steam generators  
: 8. No noble gas is dissolved in the steam generator water. amount of iodine/unit mass steam = 0 1 9. The iodine partition factor amount of 1odine/unit mass liquid . in steam generators
: 10. The atmosphere dispersion factors (x/Q) at site boundary and low population zone are as listed in Table 15.4-9. The breathing rate is 3.47 x 10-4 m 3/sec for 0-8 hours. 11. In the affected steam generator, all the water boils off and releases through the break inmediately after the accident.
: 10. The atmosphere dispersion factors (x/Q) at site boundary and low population zone are as listed in Table 15.4-9. The breathing rate is 3.47 x 10-4 m 3/sec for 0-8 hours. 11. In the affected steam generator, all the water boils off and releases through the break inmediately after the accident.
One tenth of the iodines in the is released to the environment.  
One tenth of the iodines in the is released to the environment.
: 12. The primary pressure remains constant at 2235 psig for 0-2 hour and decreases linearly to atmosphere from 2235 psig during the period 2-B hour . sc...s.
: 12. The primary pressure remains constant at 2235 psig for 0-2 hour and decreases linearly to atmosphere from 2235 psig during the period 2-B hour . sc...s.
8929Q.lBIB78BB'  
8929Q.lBIB78BB'  
\S'*4-25"
\S'*4-25"
* STEAM LINE BREAK STEAM RELEASE Mass release from defect1ve S.G. lbs Steam release from non-defect1ve S.G.'s lbs Feedwater Flow to 3 non-defect1ve S.G.'s lbs Mass of reactor coolant transferred 1nto 3 non-defective S.G.'s lbs for a primary to secondary leak rate of l gpm, lbm 0-2 Hours 95.000 424,000 433,000 719 2-8 Hours 0 1,188,000 1,300,000  
* STEAM LINE BREAK STEAM RELEASE Mass release from defect1ve S.G. lbs Steam release from non-defect1ve S.G.'s lbs Feedwater Flow to 3 non-defect1ve S.G.'s lbs Mass of reactor coolant transferred 1nto 3 non-defective S.G.'s lbs for a primary to secondary leak rate of l gpm, lbm 0-2 Hours 95.000 424,000 433,000 719 2-8 Hours 0 1,188,000 1,300,000
: 2. 510 Us1ng the above assumpt1ons, the thyro1d 1nhalat1on exposure was calculated to be 2.1 rem at the m1n1mum exclus1on d1stance (1270 meters) and 0.37 rem at the 5 m1le low populat1on zone rad1us. Us1ng the conservat1ve calculational models presented 1n Safety Gu1de 4, the whole body doses were calculated to be 0.0067 rem at the m1nimum exclus1on d1stance and 0.0014 .rem at the low population zone radius . Sc:-...s-8929Q:19/Q7988S  
: 2. 510 Us1ng the above assumpt1ons, the thyro1d 1nhalat1on exposure was calculated to be 2.1 rem at the m1n1mum exclus1on d1stance (1270 meters) and 0.37 rem at the 5 m1le low populat1on zone rad1us. Us1ng the conservat1ve calculational models presented 1n Safety Gu1de 4, the whole body doses were calculated to be 0.0067 rem at the m1nimum exclus1on d1stance and 0.0014 .rem at the low population zone radius . Sc:-...s-8929Q:19/Q7988S  
\5"-4-2.(,
\5"-4-2.(,
TABLE 15.4-1 (Sheet 1 of 3) TIME SEQUENCE OF EVENTS FOR CONDIT ION IV EVENTS Accident Major Reactor Coo 1 ant System Pipe Ruptures Double-Ended Cold Leg Guillotine  
TABLE 15.4-1 (Sheet 1 of 3) TIME SEQUENCE OF EVENTS FOR CONDIT ION IV EVENTS Accident Major Reactor Coo 1 ant System Pipe Ruptures Double-Ended Cold Leg Guillotine
: 1. { C 0 = 1.0) 2. (.c 0 = o.8) 3. ( C 0 = O. 6) SGS-UFSAR Event Start Reactor trip signal Safety injection signal AccLmulator injection End of B Bottom of core recovery Accllllulators empty Pllllp i nj ecti on End of bypass Start Reactor trip signal* Safety injection signal Accllllulator injection End of 8 . Bottom of core recovery Ace llllU l ators empty Pllllp injection End of bypass Start Reactor trip si gna 1 Safety injection signal Ace IJ11U l ator injection Time{ Seconds) 0.0 1.65 0.86 14.1 28.1 . 40.34 51.15 25.86 25.4 o.o 1.66 0.92 14.6 28.8 40.95 51.6 25.92 26.0 0.0 1.66 1.03 16.8 Revision 0 July 22, 1982 . -
: 1. { C 0 = 1.0) 2. (.c 0 = o.8) 3. ( C 0 = O. 6) SGS-UFSAR Event Start Reactor trip signal Safety injection signal AccLmulator injection End of B Bottom of core recovery Accllllulators empty Pllllp i nj ecti on End of bypass Start Reactor trip signal* Safety injection signal Accllllulator injection End of 8 . Bottom of core recovery Ace llllU l ators empty Pllllp injection End of bypass Start Reactor trip si gna 1 Safety injection signal Ace IJ11U l ator injection Time{ Seconds) 0.0 1.65 0.86 14.1 28.1 . 40.34 51.15 25.86 25.4 o.o 1.66 0.92 14.6 28.8 40.95 51.6 25.92 26.0 0.0 1.66 1.03 16.8 Revision 0 July 22, 1982 . -
* TABLE 15.4-1 (Sheet 2 of 3) TIME SEQUENCE OF EVENTS FOR CONDITION rv* t:VErHS Accident Rupture of main feedwater pipe SGS-UFSAR Event End of B lo\l<<iown Bottom of core recovery Accurn ... lators empty P1J11p injection  
* TABLE 15.4-1 (Sheet 2 of 3) TIME SEQUENCE OF EVENTS FOR CONDITION rv* t:VErHS Accident Rupture of main feedwater pipe SGS-UFSAR Event End of B lo\l<<iown Bottom of core recovery Accurn ... lators empty P1J11p injection  
Line 675: Line 675:
Affected steam generate'.
Affected steam generate'.
liquid discharge; low level coincident with feed/steam flow mismatch in other steam generators; Time( Seconds) J0.46 42.5 53.64 26.03 27.51 o.oo 11.0 reactor trip setpoi nts reached. 18. 5 Reactor trip occurs 20. 5 Peak steam relief from pressurizer safety valves Pressurizer fills Bulk boiliny oegins in reactor cool ant fluid 22.5 527 876 Re vision 0 July 22, 1982 TABLE 15.4-1 (Sheet 3 of 3) TIME SEQUENCE OF EVENTS FOR CONDITION IV EVENTS Accident Event Time (Seconds)
liquid discharge; low level coincident with feed/steam flow mismatch in other steam generators; Time( Seconds) J0.46 42.5 53.64 26.03 27.51 o.oo 11.0 reactor trip setpoi nts reached. 18. 5 Reactor trip occurs 20. 5 Peak steam relief from pressurizer safety valves Pressurizer fills Bulk boiliny oegins in reactor cool ant fluid 22.5 527 876 Re vision 0 July 22, 1982 TABLE 15.4-1 (Sheet 3 of 3) TIME SEQUENCE OF EVENTS FOR CONDITION IV EVENTS Accident Event Time (Seconds)
Core decay heat decreases to auxiliary feedwater heat removal capacity 2100 Major Secondary System Pipe Rupture  
Core decay heat decreases to auxiliary feedwater heat removal capacity 2100 Major Secondary System Pipe Rupture
: 1. Case a Steam line ruptures 0 Criticality attained 40 Pressurizer empty 13 2,000 ppm boron reaches loops 27
: 1. Case a Steam line ruptures 0 Criticality attained 40 Pressurizer empty 13 2,000 ppm boron reaches loops 27
* 2 . Case b Steam line ruptures 0 Criticality attained 24 Pressurizer empty 13 2,000 ppm boron reaches loops 27 3. Case C Steam line ruptures 0 Criticality attained 49 Pressurizer empty 14 2,000 ppm boron reaches loops 33 4. Case d Steam line ruptures 0 Criticality attained 28 Pressurizer empty 15 2,000 ppm boron reaches loops 34 8920Q:l0/070885 CORC: PARAf'ETERS USED IN ST&#xa3;AM BREAK DNB ANALYSIS Case a Time Point Parameter 2 3 5 Unit 1 Unit 2 Unit 1 Unit 2 Unit 1 Unit 2 Reactor Vessel inlet temperature to sector connected to affected steam generator  
* 2 . Case b Steam line ruptures 0 Criticality attained 24 Pressurizer empty 13 2,000 ppm boron reaches loops 27 3. Case C Steam line ruptures 0 Criticality attained 49 Pressurizer empty 14 2,000 ppm boron reaches loops 33 4. Case d Steam line ruptures 0 Criticality attained 28 Pressurizer empty 15 2,000 ppm boron reaches loops 34 8920Q:l0/070885 CORC: PARAf'ETERS USED IN ST&#xa3;AM BREAK DNB ANALYSIS Case a Time Point Parameter 2 3 5 Unit 1 Unit 2 Unit 1 Unit 2 Unit 1 Unit 2 Reactor Vessel inlet temperature to sector connected to affected steam generator  
Line 692: Line 692:
* TABLE 15.4-9 ATMOSPHERIC DISPERSION FACTORS AND BREATHING RATES Distance, m Atmospheric Df spersfon Factors, X/Q (sec/m 3) 1270 8052 Time Perf od, hr a -a 8 -24 24 -720 SGS-UFSAR 1785Q:l a -2 hrs 2 -24 hrs 1 .. 5 days 5.0 x 10-4 2.5 x 10-4 4.25 x 10-6 4.0 x 10-5 2.0 x 10-5 Breathing Rates, m /sec 3.47 x io-4 1.75 x 10 -4 2.32 x 10-4 5 -30 days 2.53 x 10-6 9.6 x 10-8 Revis ion l 22, 1983 14202.3 1.04 1.03 :.: . a: I .02 0 .... u < IL z I .0 I 0 ..... .... < u ..... _J 1.00 a. * ..... t-_J :::> ::i 0.99 0.98  
* TABLE 15.4-9 ATMOSPHERIC DISPERSION FACTORS AND BREATHING RATES Distance, m Atmospheric Df spersfon Factors, X/Q (sec/m 3) 1270 8052 Time Perf od, hr a -a 8 -24 24 -720 SGS-UFSAR 1785Q:l a -2 hrs 2 -24 hrs 1 .. 5 days 5.0 x 10-4 2.5 x 10-4 4.25 x 10-6 4.0 x 10-5 2.0 x 10-5 Breathing Rates, m /sec 3.47 x io-4 1.75 x 10 -4 2.32 x 10-4 5 -30 days 2.53 x 10-6 9.6 x 10-8 Revis ion l 22, 1983 14202.3 1.04 1.03 :.: . a: I .02 0 .... u < IL z I .0 I 0 ..... .... < u ..... _J 1.00 a. * ..... t-_J :::> ::i 0.99 0.98  
.......
.......
200 250 300 350 400 450 500 550 CORE AVERAGE TEMPERATURE  
200 250 300 350 400 450 500 550 CORE AVERAGE TEMPERATURE
(*F) PUBLIC SERVICE ELECTRIC AND GAS COMPANY Variation of KEFF with Core Temperature SALEM NUCLEAR GENERATING STATION
(*F) PUBLIC SERVICE ELECTRIC AND GAS COMPANY Variation of KEFF with Core Temperature SALEM NUCLEAR GENERATING STATION
* Updated FSAR Figure 15.4-48   
* Updated FSAR Figure 15.4-48   
Line 716: Line 716:
* 2000 u Q,, -c -en w I-Q,,
* 2000 u Q,, -c -en w I-Q,,
1000 ....I 0 0 u 1-....I % ><O II ....I :::i % w ....I en ao Q. WO I-.....1-w w % a: u.. ::w 0 u %
1000 ....I 0 0 u 1-....I % ><O II ....I :::i % w ....I en ao Q. WO I-.....1-w w % a: u.. ::w 0 u %
a:w 0 Q,, I-w u-cnu a: w Q,, 0 600 500 2.5 2.0 I. 5 1.0 -2.5 0 INITIAL STEAM FLOW IS I I 53 LBS/SEC FROM FAULTED STEAM GENERATO (ANO 29BL4 LBS/ SEC FROM INTACT STEAM G ERATORS) 20.000 PPM BORON REACHES LOOPS AT 35 S 25 50 75 I 00 125 I SO 175 TIME (SECOHOS)  
a:w 0 Q,, I-w u-cnu a: w Q,, 0 600 500 2.5 2.0 I. 5 1.0 -2.5 0 INITIAL STEAM FLOW IS I I 53 LBS/SEC FROM FAULTED STEAM GENERATO (ANO 29BL4 LBS/ SEC FROM INTACT STEAM G ERATORS) 20.000 PPM BORON REACHES LOOPS AT 35 S 25 50 75 I 00 125 I SO 175 TIME (SECOHOS)
:DE.. LE:.IE. u fL.E PUBLIC SERVICE ELECTRIC AND GAS COMPANY SALEM NUCLEAR GENERATING STATION Transient Response to Steam Line Break at Exit of Steam Generator With Safety Injection and Without Offsite Power (Case d) -Unit 1 Updated FSAR Jiii9wre 15 4 5S   
:DE.. LE:.IE. u fL.E PUBLIC SERVICE ELECTRIC AND GAS COMPANY SALEM NUCLEAR GENERATING STATION Transient Response to Steam Line Break at Exit of Steam Generator With Safety Injection and Without Offsite Power (Case d) -Unit 1 Updated FSAR Jiii9wre 15 4 5S   
*
*

Revision as of 17:30, 25 April 2019

Proposed Tech Specs Re Boron Injection Tank & Contained Vol, Boron Concentration & Temp & Heat Tracing of Tank & Associated Piping
ML18092A888
Person / Time
Site: Salem  PSEG icon.png
Issue date: 10/25/1985
From:
Public Service Enterprise Group
To:
Shared Package
ML18092A887 List:
References
NUDOCS 8511010226
Download: ML18092A888 (157)


Text

ACTION: With the status wi MARGIN eq the tank within t ec on ank inoperable, restore the tank to OPERABLE or e in HOT STANDBY and borated to a SHUTDOWN en to l 6k/k at 200°F within the next 6 hours6.944444e-5 days <br />0.00167 hours <br />9.920635e-6 weeks <br />2.283e-6 months <br />; restore E BLE atus within the next 7 days.or be in HOT SHUTDOWN n t 12 h rs.* 4.5.4.l The oron injection tank shall be demonstrated OPERABLE by: a. V rifying the water level through a recirculation flow test t least once per 7 days, b. Verifying the boron concentration of the water in the tank at least once per 7 days, and Verifying the water temperature at least once per 24 hours2.777778e-4 days <br />0.00667 hours <br />3.968254e-5 weeks <br />9.132e-6 months <br />. Effective 5:55 P.M.

12, 1979 and expiring at 11 :55 A.M., January 13, 1979 the following ACTION statement is applicable:

With the boron injection tank inoperable, restore the tank to OPERABLE status within 1 hour1.157407e-5 days <br />2.777778e-4 hours <br />1.653439e-6 weeks <br />3.805e-7 months <br /> or be 1n HOT atid borated to a SHUTDOWN MARGIN equivalent to ii 6k/k at 2Q0°F within the next 24 hours2.777778e-4 days <br />0.00667 hours <br />3.968254e-5 weeks <br />9.132e-6 months <br />; restore th2 tank to OPERABLE status within the next 7 days or be in HOT SHUTDOWN within the next 12 hours1.388889e-4 days <br />0.00333 hours <br />1.984127e-5 weeks <br />4.566e-6 months <br />.

  • SALEM -UNIT l 3/4 5-7 Amendment No, 15 -
  • '
  • EMERGENCY CORE COOLING SYS'1EMS HEA i TAAC ING LIMITING CONDITION FOR OPERATION 3.5.4.2 At least two independent channels of heat acing shall be OPERJl.BLE for the boron injection tank and for the eat traced portions of the associated flow paths. APPLICABILITY:

MODES l, 2 and 3. ACTION: With only one channel of heat tra ing on ither the boron injection tank or on the heat traced portion f an as o iated flow path OPERABLE, operation may continue for up 3 d y provided the tank and flow path temperatures are verified to b at least once per 8 hours9.259259e-5 days <br />0.00222 hours <br />1.322751e-5 weeks <br />3.044e-6 months <br />; otherwise, be in HOT SHUT OWN wi 2 hours2.314815e-5 days <br />5.555556e-4 hours <br />3.306878e-6 weeks <br />7.61e-7 months <br />. 4.5.4.2 Each heat tracing hannel for the boron injection tank and associated flow path shall e demonstrated OPERABLE:

a. At least once p r 31 days by energizing each heat tracing channel, and b. At least once per 24 hours2.777778e-4 days <br />0.00667 hours <br />3.968254e-5 weeks <br />9.132e-6 months <br /> by verifying the tank and flow path tempera ures to be .!. 14S*F. The tank temperature shall be de nriined by measurement.

The flow path temperature shall be de enriined by either measurement or recirculation flow until esta ishment of equilibrium temperatures within the tank.

  • SALEM -UNIT l 3/4 5
  • . EMERGENCY CORE COOLING SYSTEMS REFUELING wATER STORAGE TANK LIMITING CONDITION FOR OPERATION 3.5.4 The refueling water storage tank (RWST) shall be OPERABLE with: a. A contained volume of between 364 1 500 and 400,000 gallons of borated water, b. A boron concentration of between-2000 and 2200 ppm, and c. A minimum water temperature of 35°F. APPLICABILITY:

MODES 1, 2, 3 and 4. ACTION: With the refueling water storage tank inoperable, restore the tank to OPERABLE status within 1 hour1.157407e-5 days <br />2.777778e-4 hours <br />1.653439e-6 weeks <br />3.805e-7 months <br /> or be in at least HOT STANDBY within 6 hours6.944444e-5 days <br />0.00167 hours <br />9.920635e-6 weeks <br />2.283e-6 months <br /> and in COLO SHUTDOWN within the following 30 hours3.472222e-4 days <br />0.00833 hours <br />4.960317e-5 weeks <br />1.1415e-5 months <br />. SURVEILLANCE REQUIREMENTS 4.5.4 The RWST shall be demonstrated OPERABLE:

a. At least once per 7 days by: 1. Verifying the water level in the tank, and 2. Verifying the boron concentration of the water.* b. At least once per 24 hours2.777778e-4 days <br />0.00667 hours <br />3.968254e-5 weeks <br />9.132e-6 months <br /> by verifying the RWST temperature when the outside air temperature is less than 35°F . 3/4 5-7 I

.EMERGENCY CORE COOLING SYSTEMS BASES .

  • 3/4.5.4 REFUELING WATER STORAGE TANK The OPERABILITY of the RWST as part of the ECCS ensures that a sufficient supply of borated water is available for injection by the ECCS in the event of a LOCA. The limits on minimum volume and boron concentration ensure .that 1) sufficient water is available within containment to permit recirculation cooling flow to the core, and 2) the reactor will remain subcritical in the cold condition following mixing of the RWST and the RCS water volumes with all control rods inserted except for the rnst reactive control assembly.

These assumptions are consistent with the LOCA analyses.

In addition, the OPERABILITY of the RWST as part of the ECCS ensures that sufficient negative reactivity is injected into the core to counteract any positive increase in reactivity caused by RCS cooldown.

RCS cooldown can be caused by inadvertent depressuri.zation, a loss-of-cool ant accident or a steamline rupture.

  • The limits on contained water volume and boron concentration of the RWST also ensure a pH value of between 8.5 and 11.0 for the solution recirculated within containment after a LOCA. This pH band minimizes the evolution of iodine and minimizes the effect of chloride and caustic stress corrosion on rrechanical systems and components.

The contained water volume limit includes an allowance for water not usable because of tank discharge line location or other physical characteristics

  • SALEM -UN IT 1 B 3/4 5-2
a. A minimum contained volume of 900 b. Between 20,000 and 22,500 ppm of c. A minimum solution temperatur APPLICABILITY:

MODES l, 2 and 3. ACTION: le restore the tank to OPERABLE status d orated to a SHUTDOWN MARGIN equivalent hours; restore the tank to OPERABLE in HOT SHUTDOWN within the next 12 hours1.388889e-4 days <br />0.00333 hours <br />1.984127e-5 weeks <br />4.566e-6 months <br />. 4.5.4. l The boron tank shall be demonstrated OPERABLE by: a. Verifying w ter level through a recirculation flow test at least once per 7 d y , b. Verifyin th boron concentration of the water in the tank at least once pe 7 days, and UNIT 2 3/4 S-9

  • EMERGENCY CORE COOLING SYSTEMS HEAT TRACING LiMITING CONDITION FOR OPERATION 3.5.4.2 At least two independent channels of heat racing shall be OPERABLE for the boron injection tank and for the heat tra d portions of the associated fl ow paths. APPLICABILITY:

MODES l, 2 and 3. ACTION: With only one channel of heat tr the heat traced portion of an s continue for up to 30 da s provi verified to be greater t an otherwise, be in HOT SHU DO either the boron injection tank or on flow path OPERABLE, operation may tank and flow path temperatures are to 145°F at least once per 8 hours9.259259e-5 days <br />0.00222 hours <br />1.322751e-5 weeks <br />3.044e-6 months <br />; 12 hours1.388889e-4 days <br />0.00333 hours <br />1.984127e-5 weeks <br />4.566e-6 months <br />. r cing channel for the boron injection tank and associated onstrated OPERABLE:

b. At east once per 24 hours2.777778e-4 days <br />0.00667 hours <br />3.968254e-5 weeks <br />9.132e-6 months <br /> by verifying the tank and flow path te eratures to be greater than or equal to 145°F. The tank t e shall be determined by measurement.

The flow path temperature s all be determined by either measurement or recirculation flow ntil establishment of equilibrium temperatures within the tank . 3/4 5-10 EMERGENCY CORE COOLING SYSTEMS .FUELING WATER STORAGE TANK LIMITING CONDITION FOR OPERATION 3.5.4 The refueling water storage tank (RWST) shall be OPERABLE with: a. A contained volume of between 364,500 and 400,000 gallons of borated water, b. A boron concentration of between 2000 and 2200 ppm, and c. A minimum water temperature of 35°F. APPLICABILITY:

MODES l, 2, 3 and 4. ACTION: With the refueling water storage tank inoperable, restore the tank to OPERABLE status within l hour or be in at least HOT STANDBY within 6 hours6.944444e-5 days <br />0.00167 hours <br />9.920635e-6 weeks <br />2.283e-6 months <br /> and in COLD SHUTDOWN within the following 30 hours3.472222e-4 days <br />0.00833 hours <br />4.960317e-5 weeks <br />1.1415e-5 months <br />. SURVEILLANCE REQUIREMENTS 4.5.4 The RWST shall be demonstrated OPERABLE:

  • a. At least once per 7 days by: 1. Verifying the water level in the tank, and 2. Verifying the boron concentration of the water. b. At least*once per 24*hours by verifying the RWST temperature when the outside air temperature is less than 35°F . SALEM -UNIT 2 I 3/4 5-9 I

With the RCS temperature below 350°F, one OPERABLE ECCS subsystem is acceptable without single fail.ure consideration on the basis of the stable reactivity condition of the reactor and the limited core cooling requirements.

The limitation for a maximum of one safety injection pump to be OPERABLE and the Surveillance Requirement to verify all safety injection lumps except the allowed OPERABLE safety injection pump to be inoperable below 312°F provides assurance that a mass addition pressure transient can be relieved by the o per at i o n o f a s i n g 1 e PO PS re 1 i e f v a 1 ve

  • The Surveillance Requirelfents provided to ensure OPERABILITY of each component ensures that at a minimum, the assumptions used in the safety analyses are ITEt and that subsystem OPERABILITY is maintained.

Surveillance requirements for throttle valve position stops and flow balance testing provide assurance that proper ECCS flows will be maintained in the event of a LOCA. Maintenance of proper flow resistance and pressure drop in the piping system to each injection point is necessary to: 1) prevent total pump flow from exceeding runout conditions when the system is in its minimum resistance configuration, 2) provide the proper flow split between injection points in accordance with the assumptions used in the ECCS-LOCA analyses, and 3) provide an acceptable level of total ECCS flow to all injection points equal to or above that assumed in the ECCS-LOCA analyses.

3/4.5.4 REFUELING WA.TER STORAGE TANK The OPERABILITY of the RWST as part of the ECCS ensures that a sufficient supply of borated water is available for injection by the ECCS in the event of a LOCA. The limits on RWST minimum volume and boron concentration ensure that 1) sufficient water is available within containment to permit *recirculation cooling flow to the core, and 2) the reactor will remain subcritical in the cold condition following mixing of the RWST and the RCS water volumes with al 1 control rods inserted except for the rrost reactive control assembly.

These assumptions are consistent with the LOCA analyses.

In addition, the OPERABILITY of the RWST as part of the ECCS ensures that sufficient negative reactivity is injected into the core to counteract any positive increase in reactivity caused by RCS cooldown.

RCS cooldown can be caused by inadvertent depressurization, a loss-of-coolant acc*ident or a steam-1 i ne rupture

  • The 1 imits on contained water volume and boron concentration of the RWST al so ensure a pH value of between 8.5 and 11.0 for the solution recirculated within containment after a LOCA. This pH band minimizes the evolution of iodine and minimizes the effect of chloride and caustic stress corrosion on ITEchanical systems and components.

The contained water volume limit includes an allowance for water not usable because of tank discharge line location or other physical characteristics.

SALEM -UNIT 2 B 3/4 5-2 r-0 I c.J 1.11 00 00 ¢ cl . t) Vl _, -z J) -t-v I.!) "" c:l. 4: L1 \-U-V7 'Z .;, *.11 c( ! IJ) :i: tJ} rl.. tJ J 4: < ,,., ,_ t-1.!J <( Q.. "'2. :J -I .J Cl r t.!J -:/. IJJ fi. r V'.l t.

  • been sho'-fl on similar plants to less severe than the double ended hot ----. -. ---*-. . .. . -. * --.. *
  • leg break. Cold leg breaks, on the other hand are lower both in the blowown peak and in the reflood pressure rise. Thus an analysis of smaller punp suction breaks is representative of the spectrun of. break sizes. For these analyses it was assuned that the single failure occurred on a diesel ge_nerator such that one punp and two fan coolers f af led to operate. Figures 15.4-86 and 15.4-87 give the contail'lllent pressure transients for several break sf zes and locations for the de sf gn basis case. Additio.nal margin cases assuning entrainnent continues up to the 10 foot core level analyzed wf th results presented f n Figures 15.4-88 and 15.4-89. The peak pressures .for these cases are s1Jmtarf zed in Table 15.4-22. Structural heat transfer.coefficients as a function of time are cated in Figure 15.4-90
  • The DEPS results are shown in Figure 15.4-91. This transient results in the highest peak pressure of 45 psig. 15. 4. 8. 2 Ste an line Breaks 15.4.8.2.1 Analytical Methods 'Jarietis eentaimient models ha*1e been titilized te a"aly!e steMt break;" Sa le111 P 1 a.. t * .stu.-.:b""

The 111a;ier'ity e:f the A"al,ses perfonned utilized the Westinghouse con-tail'lllent model developed for the IEEE-323-1971 Equipment Qualification progran. These models and their justification (experimental .and ical) are detailed in References 56 through 60. Some major points of the model are as follows: SGS-UFSAR 15.4-88 Revision 0 July 22, 1982

  • *
  • 1. The saturation temperature corresponding to the pt'.rtial pressure of the contairment vapor is used in the calculation of condensing heat transfer to the passive heat sinks and the removal by ment fan coolers. 2. The Westinghouse containment model utilizes the analytical approaches described in References 6 and 60 to calculate the condensate removal from the condensate film. Justification of this model is provided in References 56, 59, 60, and 6. (For large breaks 100 percent revaporization of the condensate is used, and a calculated revaporization due *to convective heat flux is used for small breaks.) 3. The small steCITI line break containment analyses uti l1zed the nant TagC1ni correlation, and the large steCITI line break analyses utilized the Tagami correlation with an exponential

-to the stagnant TagC1ni correlation.

The details of these models are given in Reference

38. Justification of the use of heat transfer coefficients has been provided in References 58, 59, and 61. [1:1] (f:.] A complete analysis of main steanline co ainment as been LrJJFTfl.A-r-1 perfonned using the MARVEL code and the Westing ouse . r-. .
  • rment computer code, COCO, as described in and its references.

All blowdown calculations wfth the code done asslllling the coolant pllllps running, (i.e. offsite po-..er available) bee ause this increases the primary-to-secondary heat ,.... trans\ fer and therefore maintains higher blo\ldown flow rates (Ref. -Section 3..1.7 of WCAP-8822E 63 l). Although this is inconsistent wfth the timfis assuned in containment fan cooler and initiations, Wiere loss of offsite po-..er is asslllled, the combined effect is extra conservatism in the calculated containnent conditions.

15.4.8.2.2 Mass and Energy Releases Several failures can be postulated Wiich \ttOuld impair the performance of various stea11 break protection systems and therefore

\ttOUld change the

  • --.. * * (. fv\S I t\, .u;1. net ener re leases from a r14>tured 1f ne. Three different s1 ng le f ai 1-or each break condition These .ere,( 1) failure of "IMJI __ ..,. a main feed valve; 2) failure of main stec111 1 solation valve; and 3) failure of auxiliary feedwater runou protection Feedwater Flow
" o.

There are two valves in each main feedwater line wnich serve to isolate main feed flow following a stec111 line break. One is the main feed regulator valve W1ich receives dual, separate train trip signals from the plant protection system on any safety injection signal and closes within five seconds of receipt. of this signal. The second is the feed line isolation valve W1ich also receives dual. separate train trip sf gnal s from the protection system fo llowf ng a safety injection signal. This valve closes within 30 seconds. Additionally, the main feed punps receive dual, separate train trip signals from the protection system following a stec111 line break. Thus. the worst failure in this system is* a failure of the main regulator valve to close. This results in an additional 25 seconds during W1ich feedwater from the condensate feed may be added to the steam generator.

Also. since the feed tion valve is upstream of the regulator valve, failure of the regulator results in additional feed line volL1T1e which is not isolated from the stean generator.

Thus, water in this portion of the lines can flash and enter into the stean generator.

The only non-safety grade equipment in the main feed system W1ich is relied upon to tenninate the main feed flow to the stean generators are the main feedwater control valves. These valves are not seismic category I. Ho\!Ever, each valve receives dual, independent, safety grade trip:.elosed signals from the protection system following a stec111 line break. A1so. the valves are air-9perated fail-closed design. Since the assLITled break is inside contairment in a seismic category I pipe, it is not assuned to be i ni ti ated by a seismic event. Therefore, to ass1J11e a coincident sei smfc event with the hypothetic al pipe rupture is not required, and thus a seismic classification for the main feed SGS-UFSAR

15. 4-90 Revision O July 22. 1982
  • regulation valve is not necessary to insure closure following a

li ne break inside contai r111ent. Because of the conservative nature of the transient calculations used for the 1971 Equipment Qualification Progran, the results of thfl Salem temperature transient calculatf on wf 11 fall under the peak transient calculated for the 1971 Equipment Qualification ProgrC111 and presented in Reference 60 (approximately 385.F). The pressure transient wf 11 fall below the design limits for the Salem 2 contail'lllent.

Feedwater flow to the faulted steC111 generator from the main feed system is calculated using the hydraulic resistances of the system piping, head/flow curves for the main and the steC111 generator sure deczy .as calculated by the MARVEL code. In the calculations fonned to match these systems variables, a variety of assunptions are made to maximize the ca le ul ated flows. These f nc l ude: 1. No credit for extra pressure drop in the feed lines due to flashing of feedwater.

2. Feed regulator valve in the faulted loop f s full open. 3. Feed regulator valves in the intact loop do not change position prior to a trip signal.aREi elese iAstaRtly ef a sigAal te e lase. 4. All feed punps are running at maximun speed. 5. No credit is taken for flow redt.a:tion through the feed regulator or feed isolation valve until they are full closed. 6. Flow from the pllTlpS 11 nearly followf ng punp trf"p.

Calculation of feedwater flashing f s perfonned by the MAR'd:L code as described in Section 2.2.3 of WCAP For the Salem units, the . 4.1.r 1'101. SGS-UFSAR 15.4-91 Revision 0 .)11] v ?2 ] QQ2

  • --* *
  • maximun volune of rm1solated feed lines is 328.2 ft3 without a feed regulator valve fai'Jure, and increases to 868.5 ft3 with a feed lator valve failure. (See Teele 4 of WSAP B84J).f'62t The feedwater flew as a ft1rietfe" ef tf1t1e fs l'P'ese,.teel f" Ffgtft"e 15.4 92. Main Ste an I so 1 ati on . Since all main stean isolation valves have closing times of no more than five seconds, failure of one of these valves affects only the volune of the main stean and turbine stean piping htlich cannot be isolated from the pipe r14>ture.

4 ef W6i\.? 8822Eii1 and Table 15.4-23 shows the mass in the stean lines with and without an isolation valve failure at the four levels considered in the analyses.

Stean contained in the unisolated portions of the stec111 lines and bine plant considered in the contairment analyses in t"'10 For the large double-ended ruptures, stean in the unisolated steam lines is released to the contairment as part of the reverse flow. This is plished by having the reverse flow begin at the time of the break at the Moody critical flow rate for stean as established by the cross-sectional area of the stean line and the initial stec111 pressure.

The flow is held constant at this rate for a time period sufficient to purge the entire unisolated portion of the stean lines. Enthalpy of the flow is also held constant at the initial stean enthalpy.

Following the period of constant flow representing purging of flow from the intact stean generators, as calculated by f¥cRVEL, is added to the con-tai rment and continues until stean line isolation is complete.

When considering the split r14>tures, stec111 in the steam lines is inc 1 uded in the an a ly si s *by addi ng the tot a 1 *mass in the 11 ne s to the . initial mass of stean in the faulted stean generator.

This is necessary because, unlike double-ended ruptures, the total break area for a split is unchanged by steam line isolation; only the source of the blowdown effluent is changed. Thus, stec111 flow from the piping in the intact SGS-UFSAR 15.4-92 Revision O July 22, 1982

  • loops is indistinguishable fran steam leaving the faulted stean generator.

by adding the piping mass to the faulted stean generator mass, arid by having dry steam bloMiowns.

the stean line inventory is included in the total bloMiown.

Auxi 11 ary Feedwater Flow The Auxiliary Feedwater System fs actuated shortly after_the occurrence of *a stean line break. The mass addition to the faulted stean generator from the Auxi 11 ary Feed water System was conservatively detenni ned by using the fo 1 lowf ng assunptf ons. 1. The entire Auxf 11 ary Feedwater System was asst111ed to be actuated at the time of the break and f nstantaneously punpi ng at its maximun capacity. . 2. The affected stean generator was au1111d to be at atmospheric pressure.

3. The intact stean generators assuned to be at the safety valve set pressure.
4. Flow to the affected stean generator was fran the Auxiliary Feedwater System head curves. assunptions 2 and 3 above, and the system 11 ne re sf stances. The effects of flow* limiting devices were considered.
5. The flow to the faulted stean generator from the Auxi 11 ary Feed water System-was asst111ed to exist from the time of rupture until ment of the system was completed.
6. The failure of auxi 11 ary feed water runout control was considered a.A <lY\.i &f r'M..u!etn11ate1y u i single o.f 1d a CN\J-1.o-:t of 'Z..040 jr -h> fu sf..ta.-

SGS-UFSAR 15.4-93 ---*-----Revision O July 22, 1982

  • The a"alys'fs used the felle\IAAg arJM111aPy feeawateF flew Pates: la With rt1,.elft preteetieA a eeAstaRt awxi 11aFy feeEI fle\IJ of 1840 gpm to the faulted stesn ge"eraters
2. lwine ef P"WA&tff eeAt-l:"el was s1111t1lateEI

&y asst111Ag a ea,.sta"t al:IK111 aP'.)' feeElwater flew ef 2949 gp11 ta tt:le f abllteEI ste aR geAePateFa The flew rates 'WI! re he 1d ee"st ar1t freM time ef bl"e ak l::IAti 1 real1 gF1R1eRt1

'*'1 et:! was at te A Mi r11:fte s. In the ana1ysf sJ the auxi 11 ary feedwater flow to the faulted stean generator was ass1J11ed to exist frcm the time of the r1.4>ture until rea-lf g1111ent of the system was ccmp leted. The Auxf 1f ary Feed water System f s manually realigned by the operator after 10 minutes. Therefore, the analysis asst.mes maxfmt.m auxf lf ary feedwater flow to a depressurf zed stean generator forvfull 10 mf nutes. 4. In the event a postulated maf n stean lf ne break occurs, aux111 ary water to the affected stean generator must be tennf nated manually.

Present de sf gn crf terf a al lows ten mf nute s for the operator to recognf ze the postulated event and perfonn the necessary actf ons. Hohever, the operator f s expected to tennfnate auxiliary feedwater flow to the affected steC111 generator f n much less time due to the anount of Class lE fndfcatfon provided to monitor plant conditions.

The f nfonnatfon avaf lab le to alert the operator of the need to f so late auxiliary feedwater to the affected stean generator fs mounted on the control console fn the control room. The pressure f n each stean gen-erator and by t'-0 independent channels of fnstru-mentatf on. A Tso, a bank of pen recorders f ndf c ates stean and feed water flows for each stean generator; thf s al lows contra l roan operator to readf ly vf ew and compare the stean flow of one stean generator to the others. SGS-UFSAR 15.4-94 Revision O July 22, 1982 )

  • **
  • The suction and discharge pressures of each auxiliary feedwater pump are indicated on the control console. The auxiliary feedwater flow. tions for each steam generator are mounted on the control counsole next to each other, allowing the operator to easily view and compare flows. In addition to the above mentioned indications, high steam flow, low steam pressure, and steam-feed fl ow deviation condi tfons for each steam generator are alarmed on the main control console in the control room. Alanns for these conditions are also provided on the overhead annunciator.

Since a sufficient number of trains of instrumentation must be available for nonnal plant operation, steam generator instrumentation will be in operation at the time of the postulated event. Therefore, changes in steam generator pressure and steam flow will be detected as they occur. The only delay expected in transmitting the infonnation to the control room is the time required for the instrumentation to react to the changing conditions.

This delay is expected to be no more than a few seconds. Failure of the auxiliary feedwater isolation valve to close has not been considered.

The maximum auxiliary feedwater flow that can be delivered to a faulted steam been assumed in the analysis for ten minutes considered:

1) F'WRewt pPeteetieA 6f3el"a'
2) failure of runout protection.

Only after ten minutes the operator takes action to isolate auxiliary feedwater isolation valves fails to close, the operator can trip the two auxiliary feedwater pumps feeding broken steam generator until this valve or* another in the line is manually closed. The pump curves for the Auxiliary Feed pump are shown in Figure 15.4-93 (Steam Driven) and Figure 15.4-94 (Electrical Driven). A schematic of the Auxiliary Feed System is shown fn Figure 10.4-17

  • SGS-UFSAR 1750Q:l 15.4-95 Revision 1 July 22, 1983
  • *
  • 15.4.8.2.3 Heat Sinks The worst effect of a contair111ent safeguards failure is the loss of a spray pump which reduces containment spray flow by 50 percent. In al 1 analyses, the times ass1111ed for of contair111ent spra1s and fan coolers are 59 and 35 seconds re spec ti vely following the appropriate initiating trip signal. These times are based on the a loss of offsfte power and the delays are consistent with Technical ification limits. The delay time for spray delivery includes the time required for the spray pumps to reach full speed and the tfme required to fill the sprai headers and piping. The saturation temperature corresponding to the partial pressure of the vapor in the contairment is conservatively assumed for the temperature in the calculation of condensing heat transfer to the passive heat sinks. This temperature is also conservatively assu111ned for the latiQn of heat removal by the containment fan Gaolers
  • Parameters for the Sprays and Fan Coolers are presented in Table 15.4-24. The parameters for the Passive Heat Sinks are presented in Table 15.4-25. The Fan Cooler heat removal rate as a function of contairment ture is presented in Figure 15.4-96. 15.4.8.2.4 Results +w .. ( 7..q) A total of fit.P't;'

eight (48) different blowdowns covering fouI_power five. r1Vl. levels different break sizes were evaluated.*

The iRP'ee break sizes considered at each power level (0, 30 1 70 and 102 percent of . nominal) WIF8 i fwll S9W91e eASeQ FY,tWPe Y,StPeam ef tAe Steam l;ne*) flew restrietar, a fwll dewble e"ded dewAstreaffi ef tAe ,er H"e flew restrietar and the largest split rupture that will not-result in generation of a steam line isolation signal from the primary plant .. ,:* . * ... * .*; -' SGS-UFSAR 15.4-96 Revision O July 22, 1982 r.i r* c.t w/

_JuJf. ,J cJUl).'f.Jj

    • -**---*--*

-*-------*-*--

-no(

protection equipment:T"" In the analys;s of the eft;rd (split) break, reactor trip, feed line isolation and steam line isolation are generated by high pressure signals. Additienally, all blewdewns 1 __

  • each b.rreeaak.

c i ti .* four di f.ferent $i ngl e.

ures were C0\1..S i c.{42 rc,4' (Ar\l'ZllAl'\.M f . li'\ "'

ijated. These were 1.1' safeguards train, * * (2) failure of a ma;n feed f valve, (3) fa;lure of a ma;n steam holation valve, and (4) failure of the auxiliary feedwater runout protect;on equipment.

WCAP=8822 ptovides conta;nment

n;tial (See Taele lia4 28), aAS* ;QAtaiAmeAt aAd pFe&&wFe' fFQm ill ;i&e& ;eA=
  • sieeree are preseAtee iA Table 15.4 27 aleAg with peFtiAeAt trips, trip aAe siAgle failijres assee1atee with eaeh. Alse shewA 1A Taele 15.4-27 ate add;tional entr;es. These shew the resijlts ef aAalyses
  • ef tAe weFst aAa pressijre traAsieAts as aRalyzea witR tRe ceca code modi f; ed to conform to the NRC i nteri111 eentai MeAt e\lal ijati eA aAe the resijlts ef the werst pressijre traRsieRt iR1t1ated a eAeed rijptijre wheA aAalyzed asstlflling e"trail'll'fte"t
n the blowdown as speeified in Seetie" 3.2.2 f6r WCAP 8822.t§ai These haYe eeeR pFe'fi ded feP ee1R13arheA ef Westi Agl
teyse aRa mu: eeRta1 AmeRt 111eael s aAd feF effeets eR peak preSSijl"e fre111 eRtra1Aed meistYre WRi&R is te ee iR large BFeaK elewdewRSa As eaA ee* &eeR fpe111 the taele, tl:te feP aA;Y ease ijS1Ag tl:te WestiRg ReYse meael is 42.8 aAe the feP aAy ease YS1Ag the medel is aaa,6°F, Mass and energy releases for the worst cases are prov;ded in Table 15.4-28 thru 15.4-30. Graphical results sRswiA§ eeRtaiRmeRt aR& etl:tel" pertirtent
  • 1ariables are prov;ded in Figures 15.4-*97 through U . .
  • W:J fw

+N.. of tN lReference Sect;on 2.3 of WCAP-8822 for a complete d;scussion of this spHt break. .. SGS-UFSAR

15. 4-97 Rev;s;on 0 JU 1 Y 22 1 1982
  • The large break case resulting in the calculated peak pressure has been ent;fied as the i*.4 ft2 break at 70 percent power. This case re lted in a peak pressure of 39.l psi g when dry steam bl owdowns are used. When this same case was reanalyzed utilizing blowdowns which include the effect of liquid carryover from the secondary
side, ting eak pressures were 37. 7 and 37.2 using the Westi ngh se and NRC contai nt models respectively.

This indicates the over. 1 con-servatism of e Westinghouse containment model when used th dry steam, vs. usi n the expected mass and energy releases ch include the effect of entrai nt. Transients for the Westi nghous mode.1 with dry steam blowdowns are ovided in Figures 15.4-97 thro h 15.4-99. The case resulting

nth calculated peak pressu has been identified as the .86 ttf. break at 1 for the small breaks percent power. The resulting peak pressure for is case was 4 reanalyzed*

utilizing the NRC c psig. When this case was del, and the same mass and pressure was found to be 43.0

  • psig. The transients for the Westi use model are provided in Figures 15.4-100 through 15.4-102.

Similar nsients for the case which used the NII: model are provided in Fig es l 4-103 through 15.4-105.

The case resulting in the cal lated peak te erature has been identi-fied as the 0.908 ft2brea at 70 percent powe This case resulted in a peak temperature of 3.5 *F. When this sam case was analyzed with the NRC containment mo l a peak temperature of 34 °F was calculated.

These results verify hat the Westinghouse and NRC m els yield similar results. Transi en s for both of these cases have been Figures 15.4-106 hrough 15.4-108.

An evaluati of the safety related instrumentation will show confo ance with the requirements of IEEE-223-1971.

alua-be performed by comparing the containment equipment tes *c_on-* versus the calculated containment accident environnents pre-vi o ly discussed.

If a thennal analysis is necessary Westinghouse w l SGS-UFSAR Revision 0 July 22, 1982

model similar to that presented

  • tn Reference
24. dfffe . es between the Westf nghouse then11l arialysf s model and t proposed N nterim model will be dfscussed and Justified.
1. 2. A conv
  • e heat transfer coefffcfent comparable to t by the NRC will be used. If necessary, sensftfvfty will be performed to j ustffy an.y model differences. 15.4.8.3 Subcompartrnent Pressure Analysts Reference b4 presents the containment subcmpartment pressure analysis usf ng an 18 node contaf nment model and the latest version of the TMD computer code. 15.4.8.4 Mf scell aneous Analysis 15.4.8.4.1 Minor Reactor Coolant Leakage The Hf Contaf rrnent Pressure sf gnal actuates engf neered safety features.

Since the set point for this signal fs two psfg, the maximum containment pressure caused by leakage is restricted to thfs value. The containment response to such leakage would be a gradual pressure and temperature rise whfchjtould reach a pressure peak of slightly less* than two pounds gauge. At thf s point energy removal due to structural heat sinks and operating fan coolers would match the energy* addition due to the . . and other sources

  • SGS-UFSAR 15.4-99 Revf sf on O July 22, 1982 REFERENCES FOR SECTION 15.4 1. "Acceptance Criteria for Emergency Core Cooling Systems for Light Water Cooled Noclear Power Reactors," lOCFRS0.46 and Appendix K of * .10CFR50.

Federal Register, Vol1111e 39, N1111ber 3, January 4, 1974. ' . 2. Bordelon, F. M., Massie, H. w. and Zordan T. A., "Westinghouse ECCS Evaluation Model -S11111J1ary, 11 WCAP-8339, July 1974. 3. Bordelon, F. M., et al ** "SATAN-VI Comprehensive Time Dependent Analysis of Loss of Coolant," WCAP-8302, June, 1974 (Proprietary) and WCAP-8306, June 1974 "(Non-P.roprietary).

4. Bordelon, F. M., et al., 11 LOCTA-IV Loss of Coolant sient Analysis, 11 WCAP-8301, June 1974 (Proprietary) and WCAP-8305, June 1974 (Non-Proprietary).
5. Kelly R. D., et al., 11 Calculational Model for Core Reflooding After a Loss of Coolant Accident (WREFLOOD Code)," WCAP-8170, June 1974 (Proprietary) and WCAP-8171, June 1974 (Non-Proprietary)o
6. Bordelon, F. M. and Murphy, E.T., 11 Containnent Pressure Analysis Code (COCO)," WCAP-8327, June 1974 (Proprietary) and WCAP-8326, June 1974 (Non-Proprietary).
7. Bordelon, F. M., et al., "Westinghouse ECCS Evaluation Model -plementary Infonnation, 11 WCAP-8471-P-A, April 1975 (Proprietary) and WCAP-8472-A, April 1975 (Non-Proprietary).
8. 11 Westi nghoi.se ECCS Evaluation Model -October 1975 Version, 11 WCAP-8622, November 1975 (Proprietary) and WCAP-8623, November 1975 (Non-Proprietary).
9. Letter from C. Eicheldinger of Westinghouse Electric Corporation to D. B. Vassallo of the Noclear Regulatory Coamission.

Letter N1.111ber NS-CE-924, dated January 23, 1976. SGS-UFSAR 15.4-101 Revision O July 22, 1982

  • *
  • 10. Kelly, R. D., Thompson, C. M., et al., "Westinghouse Emergency Core Cooling System Evaluation Model for Analyzing Large LOCA's During Operation With One Loop Out of Service for Plants Without Loop lation Valves," WCAP-9166, February 1978. lL Eicheldinger, C., "Westinghouse ECCS Evaluation Model, February 1978 Version," WCAP-9220 (Proprietary Version), WCAP-9221 tary Version), February 1978. 12. Letter from T. M. Anderson of Westinghouse Electric Corporation to John Stolz of the Nuclear Regulatory Co11111ission, letter ntJ11ber NS-TMA-1830, June 16, 1978. 13. Letter from T. M. Anderson of Westinghouse Electric Corporation to John Stolz of the Nuclear Regulatory C0111T1ission, letter ntJ11ber NS-TMA-1834, June 20, 1978. 14. Letter from C. Eichelainger of Westinghouse Electric Corporation to V. Stello of the Nuclear Regulatory C011111ission.

Letter NtJ11ber NS-CE-1163, dated August 13, 1976. N 15. Beck, s. and Kemper, R. M., "Westinghouse ECCS Four-Loop Plant ( 17 x 17) Sensitivity Studies," WCAP-8865, October 19!6. 16. Salvatori, R., "Westinghouse ECCS -Plant Sensitivity Studies," WCAP-8340, July 1974 (Proprietary) and July 1974 Propri etary). 17. Johnson, w. J., Massie, H. w. and Thompson, C. M., "Westinghouse ECCS Loo'if>Plant (17 x 17) Sensitivity Studies," WCAP-8565, July 1975 (Proprietary) and WCAP-8S66, July 1975 (Non-Proprietary).

18. U.s.* Nuclear Regulatory Commission letter, D. G. Eisenhut to ities With Operati'ng Light Water Reactors, November 9, 1979
  • SGS-UFSAR 15.4-102 Revision 0 July 22, 1982
  • 19. NUREG-0630 1 (Draft) D. A.1 Meyer, R. 0.1 November 8 1 1979 1 Cladding and for LOCA Analysis
  • 20. Letter from T. M. Anderson of Westinghouse Electric Corporation to D. G. Eisenhut of the Nuclear Regulatory Co11111ission 1 letter ntJnber NS-TMA-2147 1 November 2 1 1979. 21. Letter from T. M. Anderson of Westinghouse Electric Corporation to D. G. Eisenhut of the Nuclear Regulatory Commission, letter nlJllber NS-TMA-2163 1 November 16 1 1979. 22. Letter from T. M. Anderson of Westinghouse Electric Corporation to D. G. Eisenhut of the Nuclear Regulatory C011111ission 1 letter nlJllber NS-TMA-2174 1 December 7 1 1979. 23. Letter from T. M. Anderson of Westinghouse Electric Corporation to Denise of the Nuclear Regulatory Comnission, letter nt1nber NS-TMA-2175 1 December 10 1 1979
  • 24. Geets 1 J. M., "MARVEL -A Digital Computer Code for Transient sis of a Multi loop PWR System. 11 WCAP-7909 1 June 1972. 25. Moody 1 F. s., 11 Transacti ons of the ASME 1 Journal of Heat Transfer, 11 Figure 3 1 page 134 1 February 1965. 26. Bordelon, F. M., "Calculation of Flow Coastdown After Loss of tor Coolant Pt1np (PHOENIX Code)1 11 WCAP-7973 1 September 1972. 27. Burnett, T. W. T.1 Mcintyre.

C. J., Buker, J. C. and Rose, R. P., "LOFTRAN Code Description," WCAP-7907 1 June 1972. 28. Huni n 1 C. 1 "FACTRAN, A Fortran IV Code for Thenna 1 Transients in a U0 2 Fuel Rod 1 11 WCAP-7908 1 June 1972. 29. Burnett, T. w. T., "Reactor Protection System Diversity in Westing-* house Pressurized Water Reactors." WCAP-7306, Apri 1 1969. SGS-UFSAR 15.4-103 Revision O *July 22, 1982

30. Taxelius, T. G. (Ed), "Annual Report -Spert Project, 1968, September 1969," Idaho N11:lear Corporation IN-1370, June 1970.
  • 31." Liimataninen, R. C. and Testa, F. J., "Studies in TREAT of Zirca-loy-2-Clad, U0 2-core Simulated Fuel Elements," ANL-7225, January -June 1966, p. 177, November 1966. 32. Risher, D. H., Jr., 11 An Evaluation of the Rod Ejection Accident in Westinghouse Pressurized Water Reactors Using Spatial Kinetics Methods,M WCAP-7588, Revision 1-A, January 1975. 33. Rf sher, D. H., Jr., and Barry, R. F., -A Multi-Dimensional Neutron Kinetics Computer Code," WCAP-7979-P-A, January 1975 prietary) and WCAP-8028-A, January 1975 (Non-Proprietary).
34. Barry, R. F., "LEOPARD -A Spectr1J11 Dependent Non-Spatial Depletion Code for the IBM-7094, 11 WCAP-3269-26, September 1963. 35. Bi shop, A. A., Sanberg, R. a. and Tong, L. s., "Forced Convection Heat Transfer at High Pressure After the Critical Heat Flux," ASME I . 65-HT-31, August 1965. 36. "Westinghouse Mass and Energy Re lease Datas for Contai ment Design, 11 WCAP-826.4 (Proprf etary) and WCAP-8312 (Non-Proprietary).
37. Dittus, F. w., and Boelter, L. M. K., University of California (Berkely), Publs, Eng., £ 433 (1930). 38. Jens, w. H., and Lottes, P. A., "Analysts of Heat Transfer, Burnout, PresslJT'e D_rop, and Density Data for High Pressure*Water, 11 USAEC Report ANL-4627 (1951). SGS-UFSAR 15.4-104 Revision 0 July 22, 1982
  • 39. Macbech, R. V., "Burnout Analysis, Pt. 2, The Basis Burn-out Curve," U. K. Report AEEW-R 167, Winfrith (1963). Also Pt. 3, "The Low-Velocity Burnout Regimes," AEEW-R 222 (1963); Pt. 4, "Application of Local Conditions Hypothesis to World Data for. Unifonnly Heated Round Tubes and Rectangular Channels,*

AEEW-R 267 (1963). 40. Dougall, R. s., Rehsenow, w. M., Film Boiling on the Inside of Vertical Tubes with Upward Flow of Fluid at Low Quantities, MIT Report 9079-26. 41. EcEligot, D. M., Onnond, L.W., and Perkins, Jr., H. C., "Internal Low Reynolds -Nunber Turbulent and Transitional Gas Flow with Heat Transfer," nal of Heat Transfer, 88, 239-245 (May 1966). 42. W. H. 172. at Transmission, McGraw-Hill 3rd edition, 1954, p. 43. Cunningham, V. P., and Yeh, H. C., "Experiments and Void Correlation for PWR Small-Break LOCA Condition," Transactions of American Nuclear Society, Vol. 17, Nov. 1973, pp. 369-370. 44. lagC111i, Takaski, "Interim Report on Safety Assessments and Facilities Establishment Project in Japan for Period Ending June 196 5 ( N 0

  • 1 ) II 45. Kolflat, A., and Chittenden, W. A., "A New Approach to the Design of Contairment Shells for Atomic Power Plants". Proc. of Amer. Power Conf.,_1957
p. 651-9. 46. McAdams, w. H., Heat Transmission , 3rd Edition, McGraw-Hill Book Co., Inc., New York (1954). 47. Standards of Tubular Exchanger Manufacturers Association SGS-UFSAR 15.4-105 Revision 0 Julv 22. 1982
  • 48. Eckert, E. R. G., and Drake, P. M. J., Heat and Mass

.* McGraw-Hill Book Co., Inc., New York (1959). 49. Eckert, E. and Gross, J., "Introduction to Heat and Mass Transfer", McGraw-Hill, 1963. 50. Kern, D. Q., Process Heat Transfer, McGraw-Hill Book Inc., New York ( 1950). 51. Chilton, T. H., and Colburn, A. P., "Mass Trarisfer (Absorption)

Coefficients Prediction from Data on Heat Transfer and Fluid Friction", Imd. Eng. Chem., 26, (1934),_ pp. 1183-87. 52. WCAP Topical Report -Reactor Contairment Fan Cooler Cooling Test Coil, w. L. Boettinger, July 1969. 53. S. Weinberg, Proc. Inst. Mech. Engr., 164, pp. 240-258, 1952 54. Ranz, w. and Marshall, w., Chem, Engr., Prog. 48, 3, pp. 141-146 and 48, 4, pp. 173-180, 1952. 55. Perry, J., "Chemical Engineers Handbook" 3rd Ed. McGraw-Hi 11, 1950. 56. Letter to Mr. D. B. Vassallo, Chief, Light Water Reactor Projects Branch 6, USNRC, From Mr. C. Eicheldinger, Manager, Nuclear Safety, Westinghouse Electric Corporation, Dated March 17, 1976 (NS-CE-992).

57. Letter to Mr. D. B. Vassalo, Chief, Light Water Reactor Projects Branch 6, USNRC, from Mr. C. Eicheldinger, Manager, Nuclear Safety, Electric Corporation, Dated July 10, 1975 (NS-CE-692).
58. Letter to Mr. D. B. Vassalo, Chief, Light Water Reactor Projects Branch 6, USNRC, From Mr. C. Eicheldinger, Manager, Nuclear Safety, Westinghouse Electric Corporation, Dated April 7, 1976 (NS-CE-1021)
  • SGS-UFSAR 15.4-106 Revision O July 22, 1982
  • 59. Letter to Mr. J. F. Stolz, Chief, Light Water Reactor Projects Branch 6, From Mr. C. Eicheldinger, Manager, Nuclear Safety, Westinghouse Electric Corporation, Dated August 27, 1976 60. ( NS-CE-1883).

Hsieh, T., et. al., 11 Envirormental Qualification Instrt.ment Transmitter Temperature Transient Analysis, 11 WCAP-8936, February 1977 (Proprietary) and WCAP-8937, February 1977 (Non-proprietary).

61. Letter to John F. Stolz, Chief, Light Water Reactor Projects Branch 6, USNRC, from C. Eicheldinger, Manager, -Nuclear Safety Westinghouse Electric Corporation, Dated June 14, 1977. (NS-CE-1453).

ft.( f.(..f " L J..dd J . 62. Krise, R. C., Miranda, s .*

A Bigital Code For Transient AnalJ si ! of a Leep PWR System, 11 WCAP 8843,' Nor;ember, 1977 (PP"ef3rietary) and WCAP 8844, Nor;ember, 1977 (Non p1oprietary}.

63. Land, R. E ** "Mass and Energy Releases Following a Steanline Rupture, 11 WCAP-8822, September, 1976 (Proprietary) and WCAP-8860, September, 1976 (Non-proprietary).
64. 11 Eval uati on of the Reactor Coo 1 ant System Considering Subcompartment Pressurization Following a LOCA for Salem\.Units 1 and 2, 11 transmitted by PSEG letter, R. L. Mottle to O. 0. Parr, dated March 6, 1979
  • SGS*UFSAR 15.4-107 Revision O .l11lv _ lQQ..2_____
  • ... .. -tt
  • TABLE 15.4-23 (Sheet 1 of 2) EFFECTS OF SINGLE FAILURES ON CONTAINf'ENT ANALYSES I. MAIN STEAM ISOLATION VALVES* -F Break Area Forward Reverse 1.4 4.25 1.4 4.25 1.4 4.25 1.4 4.25 4.25 1.4 4.25 1.4 4.25 1.4 4.25 1. 4 Power Percent 102 70 30 0 182 . 70 30 0 Piping Slowdown Duration of (lb/sec) Piping Slowdown (sec)* No Ms!v MSIV Failure Failure 7047 o .140 z.sg1 8.136 2.532 0 I 13" 'Lo .f.S4 7595 B.137 2.541 O *fl 1 Z..S'SD 8377 B.137 2.556 o. o 1 9002 e.1ae 2.s6e 2315 0.414 7. 786 2495 8.416 7.736 2752 0.418 7.780 2957 0.420 7.817 Steam Mass (lb) No MSIV MSIV Failure Failure qg.,r 1&,3LJ *9" 17,846 */O 34 11, z.4.t. l&3& 19, 302 11+K g 21,409 12.JS' Z.L, '113 23,115 959 :i-7,848 1838 19, 382" 1151 21, 489 1243 23, 115 li\U"u.Jc.4'
  • Failure of main stea)line isolation valve iAePeses the unisolatable steam line volume from 542 t3 to 10,083 f II MAIN FEED LINE ISOLATION VALVE Maximum Unisolatable Feed Line Volume Without MFIV Failure Maximum Unisolatable Feed Line Volume With MFIV Failure Closing Ti.me of Feed Regulation Valve Closing Time of Feed Isolation Valve SGS-UFSAR f = 328. 2 l = 868. 5 = <5.0 sec. = <30.0 sec
  • Revision O July 22, 1982
  • TABLE (Sheet 2 of 2) III. AUXILIARY FEED SYSTEM RUNOUT PROTECTION FAILURE Ma>t'f111tm1 i'.tutil h ry Feed Flew W'f Maximum Auxiliary Feed Flow With Runout Protection Failure SGS-UFSAR

= 1840 gpm = 2040 gpm Revision O July 22 1 1982

  • TABLE 15.4-24 SPRAY SYSTEM Number of Spray Trains Number of Spray Trains Operating fn Minimum Safeguards Analysis NwlfleeF ef SpFa:y TPaiRs OpePatiRg iA MaMiA11:iHR SafegyaPfis ARalysis Spray Fl ow Rate per Spray Train FAN COOLERS Number of Fan Coolers Number of Fan Coolers Operating in Minimum Safeguards Analysis HwA19eP ef 'eeleFs iA 2 1 2 2600 gpm 5 3 na:1tillH:llR SafegyaFfis ARalysis 4 I System Spray Fan Coolers SGS-UFSAR INITIATION TIMES/SETPOINTS Containment Setpoint used 26.7 psig 7.9 psig Delay After Setpoint (sec) 59. 35. Revision 0 July 22. 1982
  • Wall (ft2::> No. Area layer 1 45169 1 2 3 4 2 14206 1 2 3 4 3 29249 1 2 3 4 -*4 11611 1 2 3 5 6806 1 2 3 4 6 9424 1 2 3 7 31660 1 2 3 8 13279 1 2 3 9 47590 . 1 2
  • in contact with sump * '!i . *"t** .*:.;.; *: SGS-UFSAR TABLE 15.4-25 (Sheet 1 of 2) PASSIVE HEAT SINK Thennal Cond.

hickness '8tff-/HR-FT-*F B"M Paint 0.000625 0.083 Steel 0.03125 27.0 Concrete 0.5 0.92 Concrete 4.0 0.92 Insulation 0.2083 0.024 Steel 0.03125 27.0 Concrete 0.5 0.92 Concrete 4.0 0.92 Paint 0.000625 0.083 Steel 0.04167 27.0 Cone rete 0.5 0.92 Cone rete 3.0 0.92 Paint 0.0015 0.083 Concrete 0.5 0.92 Concrete 3.0 0.92 Paint 0.0015 0.083 Cone rete 0.5 0.92 Concrete 0.5 0.92 Concrete 0.5 0.92 Paint 0.0015 0.083 Concrete 0.5 0.92 Concrete 1.21 0.92 Paint 0.00117 0.083 Cone rete

  • Oe5 . 0.92 Concrete 1.0 0.92 Stainless 0.01773 8.0 Steel Concrete Oe5 0.92 Concrete 1.4 0.92 Paint 0.000625 0.083 Steel 0.011 27.0 Volumetric Heat Capacity . BTU /FT 3_ °F 39.6 58.8 22.6 22.6 3.94 58.8 22.6 22.6 39.6 58.8 -22. 6 22.6 39.6 22.6 22.6 39.6 22.6 22.6 22.6 39.6 22.6 22.6 39.6 22.6 22.6 53.6 22.6 22.6 39.6 58.8 Revision O July 22, 1982
  • Wall ( ft!2;; No. Are Layer 10 76741 1 2 11 19348 1 2 12 9330 . l 2 13 7452 1 2 14 3218 1 *.2 _15 1553 l
  • 2 16 43740 1 2 17 4272 1 18 53745 1 2 19 11244 l 2 20 2989 l 2 * -, SGS-UFSAR TABLE 15.4-25 (Sheet 2 of 2) PASSIVE HEAT SINK Composition hickness Paint 0.000625 Steel 0.02102 Paint 0.000625 Steel 0.0437 Paint 0.000625 Steel 0.611 Paint 0.000625 Steel 0.086 Paint 0.000625 Steel 0.1112 Paint 0.000625 *Steel 0.217 Paint 0.000625 Steel 0.0052 Stainless 0.0329 Steel Paint 0.000625 Steel 0.0211 Paint 0.000625 Steel 0.0379 Paint 0.000625 Steel 0.15806 Volumetric Thennal Heat Cond.

Capacity BTU/FT3-*F 0.083 27.0 0.083 27.0 0.083 27.0 0.083 27.0 0.083 27.0 0.083 27.0 0.083 7.0 8.0 0.083 27.0 0.083 21.0 27.0 27.0 39.6 58.8 39.6 58.8 39.6 58.8 .39.6 58.8 . 39. 6 58.8 39.6 58.8 39.6 58.8 53.6 39.6 58.8 39.6 58.8 39.6 58.8 Revision 0 July 22, 1982

  • * * .. TABLE 15.4-26 CONTAINMENT INITIAL CONDITIONS FOR MSLB Containment Design Pressure Containment Volume Initial Containment Pressure Initial Air Partial Pressure Initial Steam Partial Pressure Initial Containmen.t Temperature Refueling Water Storage Tank Inventory Service Water Temperature SGS-UFSAR 47 psig 2,620,000 ft3 0.3 psig *14.7 psia O. 3 psia 350,000 gal as* Revision 0 July 22, 1982
        • ----****----****----****-----.;..,;...;..:..:..:..:..

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,;, Time (sec.) TABLE 15.4-28 Q.f44 Sheet 1 of 10 MASS AND ENERGY RELEASES FROM A FT2 SPLIT BREAK 3o AT rn PERCENT POWER (Worst Te111@eiaai1:1iae Case) Break Flow (lb/sec.)

PR6PRIETAR'f RefeF te {5Q 311) "A13111ieatiert fe,. Witl:it:ieleiRg" Ra L. Mittl te Sla" 9. Par1 November 20, U78 ttd-NRC Af:lf31"9val letteP, Qlart Q, PaFF te Jani:ia1) 22, 1979 Energy Flow (million Btu/sec.)

SGS-UFSAR Revision 0 July 22, 1982 Sheet 2 of 10 Break Flow Energy Flow Time Break Flow Energy Flow ec.J (lblsec. l !million Btu/sec.l

{sec.l {lb/sec.l

{million Btu/sec.)

0.0000 0.0000 0.0000 J7.SU 1420. 1.104

  • sooo 1741. z.oeo sa.oo 1416
  • 1.699 1.000 174'. z.oeo SI.SO 1411. 1.693 1.SOO 1121. Z.065 39.00 1406. 1.611 2.000 1711. 2.053 39.50 1401. 1.612 2.500 1708. Z.041 40.00 1396. 1.676 3.000 1691. z .. 030 40.50 1392. 1.670 3.500 1611. z.011 41.00 1387D 1.665 4.000 1671. Z.007 41.50 1382. 1.659 4.500 1669. 1.995 42.00 1377. 1.653 59000 1659. 1.914 42.50 1372. 1.647 5.500 1650. 1.'74 43.00 1367. 1.642 6.000 1641. 1.963 43.50 1362. 1.636 6.500 1633. 1.'54 44.00 . 1357. 1.630 1.000 1625. 1.'44 44.50 1352. 1.624 1.500 1617. 1.tJ5 45.00 1348. 1.619 1.000 1608. 1.9ZS 45.50 1343. 1.613 1.500 1602. 1.917 46.00 1338. . 1 .607 9.000 1594. 1.909 46.50 1333. 1.601 9.500 1517. 1.199 47.00 1321. 1.595 10.00 1519. 1.191 47.50 1323. 1.590 10.SO '1572. 1.112 48.00 1319. 1.514 11.00 1565. 1.174 48.50 1314. 1.571 11.50 1551. 1.166 49.00 1309. 1.573 12.00 155Z. 1.151 49.50 1304. 1.567 12.50 1545. 1.151 50.00 1Z99. 1.561 13.00 1539. 1.143 50.50 129S. 1.556 13.50 1533. 1.136 51.00 1290. 1.550 . 14.00 1526. 1.129 51.50 1217
  • 1.546
  • 4.50 1520. 1.122 52.00 1217
  • 1.546 5.00. 1515. 1.115 52.50 1215. 1.544 5.50 1509. 1.aoe 53.00 1213. 1.542 6.00 1503. 1.801 53.50 1280. 1.539 16.50 1498. 1.795 54.00 1271. 1.536 17.00 1493. 1.190 54.50 1275. 1.533 55.00 1272. 1.529 17.50 1417. 1.112 55.50 1269. 1.526 56.00 1267. 1.522 18.00 1413. 1.111 56.50 1264. 1.519 18.50 1417. 1.110 57.00 1261. 1.516 19.00 1473. 1.766 19.50 1467. 1.759 !;;
  • so 1251. 1.512 20.00 1463. 1.754 51.00 1255. 1.509 20.50 1459. 1.749 58.50 1252. 1.505 21.00 1454. 1.744 59.00 1249. 1.502 21.50 1448. 1.736 59.50 1246. 1.498 22.00 1443. 1.731 60.00 1243. 1.494 22.50 1475. 1.768 60.50 1240. 1.491 23.00 1476. 1.769 61.00 1237. 1.417 23.50 1411. 1.176 61.50 1234. 1.413 24.00 1412. 1.111 62.00 1231. 1.480 24.50 1413 .. 1.771 6l.50 1221. 1.476 25.00 1414. -1.719 63.00 1224. . 1.472 25.50 1414. 1.780 63.50 1221. 1.469 26.00 1415. : . 1.711 64.00 1211. 1.465 26.50 1485. 1.711 64.50 1215. 1.461 21.00 1485. 1.711 65.00 1212. 1.457 21.so 1485. 1.711 65.50 1209. 1.454 21.00 1485. 1 .. 711 66.00 1206. 1.450 21.so 1414. 1.780 66.50 1203. 1.446 29.00 1413. 1.779 67.00 11"* 1.443 29.SO 1412. 1.717 67.50 1196. 1.439 30.00 1480. 1.774 61.00 1193. 1.435 :so.so 1477. 1.771 68.50 1190. 1.431 31.00 1474. 1.768 69.00 1117. 1.421 e-50 1471. 1.764 69.50 1114. 1.424
  • oo 1467. 1.760 10.00 1111
  • 1.421
  • so 1463. 1.755 70.50 1171
  • 1.417
  • oo 1460. 1.751 71.00 1175
  • 1.413 33.50 1456. 1.746 11.50 1172. 1.410 34.00 1451. 1.741 72.00 1169. 1.406 34050 1447. 1.736 72.50 1166. 1.403 35.00 1443. 1.731 13.00 1163. 1.399 35.50 1439. 1.726 73.50 1160. 1.396 36.00 1434. 1.121 74.00 1157. 1.392 36.50 1430. 1.715 74.50 1154. 1.319 37.00 1425. 1.110 Sheet 3 of* 10 Break Flow Energy Flow Time Break Flow Energy Flow l blsec. l {million Btu/sec.l

{sec. l {lb/sec.l

{million Btu/sec.) 1151. 1cJl5 112.0 i7*.* 1.056 75 .. 50 1149. 1.382 112.5 166.1 1.044 76.00 1146. 1.378 113.0 157.Z 1.033 76 .. 1143. 1.375 113.S 141.0 1.021 11.00 1140. 1.31Z 114.0 139.1 1.011 114.,5 ll0.5 1.000 11.50 1137. 1.368 115.0 122.1 .9902 11.00 'i134. 1.365 ,15.5 114.0 .990S 1lo50 1131. 1.361 116.0 I06.Z .9710 19.00 1128. '93SI 198.6 .9618 79.50 1125. 1.354 116 .. S 191.2 .9529 I0.00 1123. 1.351 117.0 I0.50 1120. 1.348 l1o00 1117. 1.344 11.50 1114. 1.341 117.S 714.0 .9442 12.00 1111. 1.337 111.0 776.t .9357 az.so 1109. 1.334 111.S 110.t .t275 13.00 1106. 1.331 119.0 765.5 .9194 13.SO 1103. 1.327 119.S 151.9 .9116 14.00 1100. 1.324 120.0 HO. .9040 14.SO 1097. 1.321 120.S 744.5 .1966 IS.00 109'. 1.311 121.0 731.5 .1893 15.SO 1092. 1.314 121.s 732.6 .1822 16.00 1089. 1.311 12l.O 726.f .1753 16.SO 1086. 1.JOI 122.S 721.J .1685 11.00 1084. 1.305 123.0 115.t .1620

  • 11.so 1081. 1.301 123.S 110.5 .1555 11 .. 00 1071. 1.291 124e0 105.i .1492 II.SO 107,. t.m *24.5 100. .1431 . . 19.00 1073. t.Z92 125.0 695.J .1371 -1010. 1.m 125.S t90.5 .1313 1068. 1.285 126.0 615.1 .12S6 1065. 1.212 126.S 611.1 .l200 1062. 1.219 127.0 676.6 .1146 '1.SO 1060. 1.276 127.5 672.2 .I093 J2.00 1057. 1.273 128.0 661.0 .I041 92.SO 1055. 1.210 128.5 663.I .7990 93.00 1052. 1.267 129.0 659.7 .1941 93.SO 1049. 1.263 129.S 655.7 .7893 . 94.00 1047. 1.260 130 .. 0 651.1 .7146 94.SO 1044. 1.257 130.5 641.0 .7800 95.00 1042. 1.254 131.0 644 .. J .;1755 95.50 1039. 1.251 131.5 640.1 .7111 96.00 1037. 1.248 132.0 637.Z .7669 96.50 1034. 1.245 132.5 w.a .7627 97.00 1032. 1.;242 133.0 630.5 .7Sl7 133.5 6Z7.2 .7548 97.50 10Zt. 1.ZJ9 134.0 6Z4.1 .7510 91.00 1027. 1.236 134.5 621.0 .7472 91.50 1024. 1.2JJ 135.0 611.0 .7436 99.00 1022. 1.230 135.5 615.1 .7401 99.50 1019. 1.221 136.0 612.Z .7367 100.0 1011. -1.224 136.5 609.5 .7333 100.5 1014. : 1.221 137.0 606.1 .7301 101.0 1012. 1.211 101.s 1009. 1.215 117.5 604.2 .7269 102.0 1007. . 1.212 138.0 601.6 .7238 102.S 1004. 1.209 131.5 599.1 .1208 103.0 1002. 1.206 139.0 596.7 .7179 103.S 999.4 1.ZOJ 139.5 594.4 .7151 104.0 996.7 1.200 140.0 192.1 .7123 104.S 994.S 1.191 140.5 "*' .1096 105.0 "'*' 1.1M 141.0 511.1 .1010 105.5 919.7 1.192 141.5 515 ** .1045 106.0 917.1 1.119 142.0 sas.* .1020 9-' 915.0 1.116 142.5 511.6 .6996 g 912.4 1.113 143.0 519.7 .6913 ..... 1.191 143.5 577.9 .6950 969.7 1.161 144.0 516.0 .6928 !)8.5 956.S 1.152 144.5 574.J .6901 .09.0 94:S.I 1.131 145.0 572.6 .6186 1"9.5 931.6 1.122 145.S 510.9 .6166 110.0 "'*' 1.108 146.0 569.J .6847 110.S 90l.J 1.094 146.5 567.7 .6127 111.0 197.4 1.0l1 147.0 566.Z .6809

..... 1.061 147.5 564.7 .6191 Sheet 4 of 10 Break Flow Energy Flow Time Break Flow Energy Flow lb/sec.) (million

{lbLsec. {million Btu/sec. 141.0 563.Z .6m 115.0 515.Z .61'2 148.5 =*I .6156 115.5 514.f .6119 149.0 .4 .6740 116.0 514.1 .6115 149.5 559.1 .6723 116.S 514.4 .6112 150.0 557.1 .6108 111.0 514.Z .6119 150.S 556.5 .6692 111.s 51J.f .6176 151.0 555.J .6671 111.0 I"*' .6173 151.5 554.1 .6663 181.5 1J.4 .6110 152.0 553.0 .6649 11900 513.Z .6167 152 .. 5 551.1 .'635 119.5 512.t .6164 153.0 550.7 .6622 190.0 512.1 .6161 153.5 549.6 .6609 190.S 512.5 .6158 154.0 548.6 .6596 '91 .. 0 512.2 .6156 154.5 547.6 .6514 '91.S 112.0 .6153 155.0 546.6 .6572 192.0 511.I .6150 155.5 545.6 .6560 192.5 511.5 .6141 156.0 544.7 .6549 193.0 511.J' .6145 156.5 543.1 .6531 '93.5 511.1 .6142 157.0 542.9 .6527 194.0 510.f -.6140 194.5 510.7 .6137 157.5 542.0 .'517 195.0 510.5 .6135 195.5 510.J .6132 151.0 541.Z ** S06 196.0 510.1 .6130 151.5 m*' .6496 196.5 509.9 .6127 159.0 .s .6417 191.0 509.7 .6125 159.5 ** .6411 160.0 531.0 *""' . 160.5 537.2 .6459 '97.5 509 .. 5 .6122 161.0 536=5 .6450 19'.0 509.J .6120 1.5 "5.1 .. 6441 191.5 509.1 .. 6111

  • 0 535.1 .6433 1".o SOl.9 .6115. 5 r* .6425 1".5 SOl.7 .61'3 .o 13.1 .6417 200.0 =*' .6111 SJ.1 .6409 200.5 .J .6108 '4.0 SZ.5 .'401 201.0 SOl.1 .6106 .64.5 131.* .6394 201.5 507.9 .6104 165.0 31.S .6316 202.0 507.1 .6102 165.5 530.7 .6319 202.5 131.6 .6099 166.0 530.1 .6372 203.0 7.4 .6091 166.5 529.6 .'366 203.5 507.Z .6095 167.0 529., .6359 204.0 507.0 .6093 167.S sza. .6352 204.5 506.9 *'°" 161.0 5Z1.t .6346 205.0 5(-C.7 .at 161.5 527.4 .634() 205.5 .6086 169.0 526.t .6334 206.0 506.S .6084 169.S 526.4 .6321 206.S 506.Z .6082 170.0

.6322 207.0 506.0 .ao 170.S 525. .6316 207.S 505.1 .t071 111.0 525.0 .6311 208.0 181*6 .6076 171.5 524.6 .6305 208.5 .5 .6074 172.0 524.1 .6300 209.0 505.J .6072 172.5 523.7 .6295

  • 209e5 50Sa1 .6010 1?3.0 523.J -.6290 210.0 505.0 .6068 173.5 522.9 .6285 210.s 504.1 .6066 174.0 522.5 : .6280 211.0 504.1 .6064 174.S nz.1 .6275 211.5 SOtt.5 .6062 175.0 521.1 .6270 212.0 504.J .6060 175.5 521.J .6265 212.s 504.2 .60SI 176.0 520.9 .6261 213.0 504.0 .6056 176.5 520.5 .6257 213.5 503.1 .* 6054 111.0 520.2 .6252 214.0 503.7 .60S2 214.5 503.5 .6050 117.5 519.1 .6241 215.0 503.4 .6048 215.5 503.2 .6046 111.0 519.5 .6244 216.0 503.1 .6045 41*' 519.1 216.5 502.9 .6043 .o Ill.I .623 211.0 502.1 .6041 .5 "*' .6231 .o 11.1 .6221
11. .6224 111.0 511.S .6220 111.S 111.z .6216 112.0 "*' .6213 112.S 516.6 .6209 113.0 116.J .6205 113.S 16.0 .'202 114.0 s1s.1 .6199 , .... & .,. . .. ,.

Sheet 5 of 10 Break Flow Energy Flow Time Break Flow Energy Flow lb/sec.) (million Btu/sec.) (sec.) (lb/sec.)

{million Btu/sec.)

211.s 502.6 .6039 Z55.0 491.4 .5903 502.4 .6037 255.5 491.2 *.5901 211.0 502 .. J .6035 256.0 491.1 .5899 211.s 50Z.'i .6033 256.5 490.9 .5891 219.0 502.0 .6031 257.0 490.I .5196 219.5 .6029 220.0 501.I 220.s 501.7 .6021 H1.5 490.6 .5194 221.0 501.5 .6026 2n.o 490.5 .Sl92 221.s 501.s .6024 zsa.5 490.3 .5'90 222.0 501.Z .6022 H9.0 490.2 .SM9 222.5. 501.0 .6020 259.5 4t0.D .SM7 223.0 500.9 .6011 260.0 m** .SNS 223.5 500.1 .6017 260.5 .7 .SM3 224.0 500.6 .6015 261.0 "'*' .SM1 224.5 500.4 .6013 261.S 419.4 .HIO 225.0 500.3 .6011 2.z.o 4".S .Sl71 225.5 500.1 .6009 262.S 419.1 .Sl76 226.0 500.0 .6007 263.0 4".0 .Sl74 226.5 499.I .6006 263.5 411.1 .Sl72 227.0 499.7 .6004 2'4.0 411.7 .Sl11 227.5 499.5 .6002 264.S 411.5 .5169 221.0 499.4 .6000 H5.0 411.4 .5167 221.5 499.2 .5991 265.S 411.Z .5165 229.0 499.1 .5996 266.0 "'*' .5163 229.5 491.9 .599S 2o6.5 411.0 .5162 230.0 498.I .5993 267.0 417.1 .5'60 230.5 491.6 .5991 267.5 417 .. 7 .5158 231.0 491.5 .5919 261.0 417.5 .5156. 31.5 491 .. 3 .5917 268.5 417.4 .5154 .o 491.2 .5916 269.0 417.Z .5153 .5 . 491.0 .5914 269.5 417.1 .Sl51 .o 497.9 .5912 210.0 416.t .5149 233.5 491.1 .5980 210.s 416.I .5147 234.0 497.6 .5971 211.0 416.6 .Sl45 234.5 497.4 .5971 211.s 416.5 .5143 235.0 497.3 .5975 212.0 416.J .5142 235.5 491.Z .5973 272.5 416.Z .Sl40 236.0 497.0 2n.o 486.0 .5131 236.5 496.9 213.S 415.9 .5136 237.0 496.7 274.0 415.7 .Sl34 274.5 415.6 .5133 237.S 496.6 .5966 275.0 415.4 .5131 238.0 496.4 .5964 275.5 415.S .5129 211.s 496.3 .5962 276.0 415.1 .Sll1 239.0 496.1 .5960 276.5 415.0 .5125 239.5 496.0 .5959 211.0 484.1 .5124 240.0 495.I .5957 240.5 495.7 .5955 zn.s 414.7 .5122 241.0 495.5 .5953 Z71.0 414.5 .Sl20 241.5 495.4 .5952 Z71.S 414.,4 .H11 242.0 49S.Z .5950 279.0 414.2 .5116 242.5 495.1 -.5941 279.5 414.1 .5115 zu.o 494.9 .5946 ZIO.O 413.t .Sl13 243.5 494.I : .5944 2ao.5 413.I .5111 244.0 494.6 .5943 211.0 413.6 .5809 244.5 494.5 .5941 211.s 413.5 .5807 245.0 494.S .5939 212.0 413.J .5806 245.5 494.2 .5937 21z.5 413.Z .SI04 24'.0 494.0 .5935 213.0 413.0 .saoz 246.5 493.9 .5934 213.5 412.t .saoo 247.0 493.7 .5932 214.0 . 412.7 .5198 247.S 493.6 .5930 214.5 W"' .5196 241.0 493.4 .5921 215.0 .4 .5m 241.5 493.J .5926 215.5 412.J .5193 --0 493.2 .5925 216.0 412.1 .5191 .5 491.0 .5923 216.5 412-a .5719 .o 492.9 .5921 211.0 411. .5717 .5 492.7 .5919 211.s 411.7 .5716 lS1.0 492.6 .5917 211.0 411.5 .5714 251.5 492.4 .5916 211.S 411.4 .5712 252.0 492.3 .5914 219.0 411.2 .5710 252.5 492.1 .5912 219.5 411.1 .5nt 253.0 492.0 .5910 290.0 480.t .sn1 *253.5 491.I .5908 290.S 4'0.1 .sns 254.0 491.7 .5901 291.0 480.7 .sm 491.5 .5905

£M\.5 .5ll1 Sheet 6 of 10 Break Flow Energy Flow Time Break Flow Energy Flow lb sec. mill ion Btu sec. sec. lb/sec. million Btu/sec.)

2.0 4'0.4 329.0 469.7 .564() 292.5 4'0.2 .5761 329.S 469.6 .5639 293.0 "°*' .5766 330.0 469.4 .5637 293.5 . 479.9 .5764 330.5 469.J .5635 ZM.O 479.1 .5162 n1.o 469.1 .,5634 294 .. 5 479.6 .5761 331.5 469.0 .S6l2 m.o 479 .* 5 .5759 332.0 461.9 .5630 295 .. 5 419.3 .5757 332.5 468.1 .5628 296.0 479.Z .5755 333.0 468.6 .5627 296.5 479.0 .5753 333.5 468.4 .5625 297.0 471.9 .5752 334.0 468 .. 3 .5623 334.5 468.Z .5622 297.5 471.7 .5750 335.0 468.0 .5620 471.6 335.5 46709 .5611 291.0 411.4 .5741 336.0 467.7 .5617 298.5 471.J .5746 336.5 467.6 .5615 299.0 471.1 .5745 337.0 467.5 .5613 299.5 .5743 300.0 471.0 .5741 300.5 417.9 .5739 337.5 467.3 .5612 301.0 477.7 .5737 331.0 467.Z .5610 301.S 477.6 .5736 331.5 467 .. 0 .S60t 302.0 471.4 .5734 339.0 466.9 .5606 302.5 477.J .5732 339.5 466.I .5605 303.0 477.t .5730 340.0 466.6 .5603 303.5 477.0 .5729 340.5 466.5 .56e1 . 304.0 476.I .5727 341.0 466.4 .5600 304.S 476.7 .572' 341.5 466.2 .5598 JOS.O 476.5 .5723 J42 .. 0 466.1 .,5596. . '°'*s

.5722 342.5 465.9 .559S .. o 476.J .5720 343.0 465.1 .5593 .5 476. 1 .5711 343.5 465.7 .5591 .o 476.0 .5716 344.0 465.S .5590 .5 475.1 .5715 344.5 465.4 .5511 JOl.O 475.7 .5713 345.0 465.Z .5586 JOe.5 475.5 .5711 S45.S 465.1 .5sa5 309.0 475.4 .5709 346.0 465.0 .5583 309.5 475.2 .5708 346.S 464.8 .5511 310.0 475.t .5706 347.0 464.7 .5580 310.5 475.0 .5704 347.5 464.6 .5578 311.0 474.1 .5702 341.0 464.4 .5576 311.5 414.1 .5101 341.5 464.J .5575 312.0 414.S .5699 349.0 464.t .5573 312.5 474.4 .5697 349.5 464.0 .5571 313.0 474.Z .5695 351).0 463.9 .5570 313.5 474.1 .5694 350 .. 5 463.7 .5568 314.0 474.0 .5692 351.0 463.6 .5566 314.5 473.1 .5690 351.5 463.5 .5565 315.0 473.7 .5611 352.0 463.3 .5563 315.5 473.5 .5687 352.5

  • 463.Z .5561 316.0 473.4 .5685 353.0 463.0 .* 5560 316.5 473.2 .5683 353.5 462.9 .5551 317 .. 0 473.1 .5612 354.0 462.8 .5556 354.5 462.6 .5555 317.S 473.0 *.5680 355.0 462.5 .5553 31&.0 472.1 .5671 355.5 462.4 .5551* 318.S 472.7 .5676 356.0 462.2 .5550 319.0 472.5 .5675 356.5 462.1 .5548 319.5 472.4 .5673 357.0 462.0 .5547 320.0 472.2 .S671 320.5 472.1 .S670 357.5 .H45 321.0 472.0 .5661 '"*' 321.5 471.1 .5666 JSl.O 4'1.7 .5543 322.0 411.7 .5664 351.S 4'1.6 .5542 322.5 471.5 .5663 359.0 "'** .5540 471.4 .5661 359.S 461.J .5531 471.J .S659 360.0 461.t .553'." 471.1 .5658 360.S 461.0 .5535 5 471.0 .5656 J61.0 4'0.t .5533 i25.0 410.1 .5654 J61.S . 4'0.1 .5532 $25.S 470.7 .S652 J62.0 4'0.6 .5530 326.0 470.6 .S651 J62.S ::8*' .5521 326.5 470.4 .5649 J63.0 ;.55"' 327.0 410.J .5647 J63.5 4'0.J .55i.S 327.S 410.1 .5646 364.0 .552] ne.o 410.0 .5644 364.S 459*1 .5522 328.5 469.1 .5642 565.0 459:: .5520 -.

Sheet 7 of 10 Break Flow Energy Flow Time Break Flow Energy Flow (million_

BtuLsec.) (sec.} (lb/sec.} (million Btu/sec.)

,_, '"*' *"" 44f.7 .5398 .o 45'.t .5517 403.5 449.6 .5396 .5 45'.4 .5515 449.4 .5395 367.0 459.J '514 .0..,5 449.J .5393 367.S 459.1 *'"1? 605.0 44f .Z .5392 . 361.0 45'.0 605.5 449.1 .5390 361.5 451.I .. 5509 606.0 441.f .5389 369.0 451.1 .5507 606.t 441.1 .5317 369.5 451.6 .5506 .01.0 441.7 .5315 310.0 451.4 .5504 .01.s 441.5 .5314 370.5 451.3 .5502 609.0 441.4 .5312 371.0 451.2 .5501 a.s 441.J. .5311 371.5 451.0 .5499 609.0 441.1 .5319 372.0 457.t .5497 609.S 441.0 .5371 372.5 451.1 .5496 410.0 447.f .5376 373.0 457.6 .5494 410.5 447.1 .5374 373.5 457.5 .5493 411.0 447.6 .5373 374 .. 0 457.4 .5491 411.S 447.5 .5371 374.S 457.2 .5419 412.0 447.4 .5310 375.0 457.1 .Ma 412.S 447.Z .5361 375.5 457.0 .5486 *1S.O 447.1 .5367 376.0 456.I .5484 413.5 447.0 .5365 376.S 456.7 .5483 414.0 446.9 .5363 377.0 456 .. 6 .5411 414.S 446.7 .5362 415.0 446.6 .5360 . 317.5 456.4 .5480 415.5 446.5 .5319 416 .. 0 446.J .5357 *371.0 456.3 .5471 416.S 446.Z .5356 371.5 456.2 .5476 417.0 44601 .53S4 379.0 456.0 .5475-319 .. 5 455.9 .5473 380.0 455.S .5411 .s 455.6 .5470 417.5 445.f .5352

.5461 411.0 445.1 .5351 .5 455.4 .5467 411.S 445 .. 7 .5349 .o 455.2 .5465 419.0 445.6 .5348 .sa2.5 455.1 .5463 419.5 445.4 .5346 313.0 455.0 .5462 420.0 445.J .5345 313.5 454., 420.5 445.Z .5343 314.0 454. .5459 421.0 445.0 .5341 314.5 454.6 .5457 421.5 444.9 .5340 315.0 454.4 .5455 422.0 444.1 .5338 315.5 454.J .54S4 422.5 444.7 .5337 316.0 454.Z .5452 423.0 444.S .5335 316.5 454.0 .5451 423.5 444.4 .5334 317.0 453.9 .5449 424.0 444.3 .5332 317.5 453.1 .5447 424.5 444.1 .5331 388.0 453.6 .5446 425.0 444.0 .5329 388.5 453.5 .5444 425.5 443.9 .5327 389.0 453.4 .5443 426.0 443.1 .5326 453.3 .5441 426.5 443.6 .5324 390.0 453.1 .5439 427.0 443.5 .5323 390.5 -.53.0 .5431 427.5 443.4 .5321 ,91.0 452.f .5436 421.0 443.2 .5320 J91.,5 452 .. 7 -.5435 421.5 443.1 .5318 392.0 452.6 .5433 429.0 443.0 .5317 392.5 452.S .5431 429.5 442.9 .5315 393.0 452.3 .5430 442.7 .5313 393.5 452.Z .5428 430 .. 5 442.6 .5312 394.0 l.SZ.1 .5427 431.0 442.5 .5310 394.5 451.t .5425 431.5 442.4. .5309 395.0 451.I .5423 432.0 442.2 .5307 451.7 .5422 442.1 .5306 396.0 451.5 .5420 433.0 442.0 .5304 396.5 451.4 .5419 433.5 441.a .5303 391.0 451.3 .5417 ,!,.O 441.1 .5302 . 441.7 .5300 41*' 451.1 .5415 ' J. (, 441.S .5299 .o 451.0 .5414 e35.S 441.4 .5297 .s 450.9 .5412 .. 36.0 441.J .5296 .o 450.1 .5411 436.5 441.1 .5294 J99.5 450.6 .5409 437.0 441.0 .5293 400.0 450.S .540* 400.5 450.4 .5406 401.0 450.2 .5404 401.S 450.1 .5403 450.0 .5401 602.S 449.1 .5400 Sheet 8 of 10 Time Break Flow Energy Flow Time Break Flow Energy Flow lb/sec.) (million Btu/sec.)

_ (sec.) (lb/sec.) (million Btu/sec.)

.5 440.9 .5291 475.0 431.4 .5176 31.0 440.I .5289 475.5 431.3 .5175 431.5 440.6 .5211 476.0 431.Z .5173 439.0 440.5 .5216 476.5 431.0 .s112 439.5 440.4 .5285 417.0 430.9 .5170 440.0 440.Z .5213 440.5 440.1 .5212 441.0 440.0 .5210 .. 5 4J0el .5169 441.5 439.9 .5279 471.0 430.7 .5167 442.0 439.7 .52n 471.5 430 .. 5 .5166 442.5 439.6 .5276 479.0 430.4 .5164 443.0 439.5 .5274 479.5 430.3 .5163 443.5 439.4 .5272 480.0 430.Z .5161 444.0 439.Z .5271 480.5 430.1 .5160 444.5 439.1 .5269 411.0 429.9 .s1se 445.0 439.0 .5268 411.5 429.I .5157 445.5 438.1 .5266 412.0 429.7 .5155 446.0 431.7 .5265 W.5 429.6 .5154 446.5 431.6 .5263 413.0 429.4 .5152 447.0 431.5 .5262 413.5 429.3 .5151 447.5 431.3 .5260 414.0 429.Z .5149 441.0 431.Z .!i259 484 .. 5 429.1 .5141 441 .. 5 438.1 .5257 415.0 421.9 .5146 449.0 438.0 .5255 415.5 421.1 .5145 449.5 437.1 .5254 416.0 421.7 .5143 450.0 437.7 .5252 416.5 421.6 .5142 450.5 437.6 .5251 417.0 421.4 .5140 451.0 437.4 .5249 -87.5 421.J .5139 451.5 437.3 .5248 411.0 421 .. Z .51J7 452.0 437.Z .5246 418.5 421.1 .5136 452.5 437.1 .5245 489.0 427.9 .5134 .o 436.9 .5243 489.5 427.1 .5133 .5 436.1 .5242 490.0 427.7 .5131 .o 436.7 .5240 490.5 427.6 .5130 4.5 436.6 .5239 491.0 427.4 .5121 455.0 436.4 .5237 491.5 427.S .5127 455.5 436.3 .5236 492.0 427.2 .5125 456.0 436.2 .5234 492.5 427.1 .5124 456.5 436.1 .5233 493.0 427.0 .5122 457.0 435.9 .5231 493.5 426.I .5121 494.0 426.7 .5119 457.S 435.1 .5229 494.5 426.6 .5111 451.0 435.7 .5221 49S.O 426.5 .5116 458.S 435.6 .5226 495.5 426.3 .5115 459.0 435.4 .5225 496.0 426.Z .5113 459.5 435.3 .5223 496.5 426.1 .5112 460.0 435.2 .5222 497.0 426.0 .5110 460.S 435.1 .5220 461.0 434.9 .5219 461.S 434.1 .5217 497.5 425.1 .5109 462.0 434.7 .5216 491.0 425.7 .5107 46l.S 434.5 .5214 491.5 425.6 .5106 463.0 434 .. tt -.521J 499.0 425.5 .5104 w.s 434.3 : .5211 499.5 425.4 .5103 464.0 434.Z .5210 -500.0 425.Z .5101 464.5 434.0 .5208 500.5 425.1 .5100 465.0 433.9 -.5207 501.0 425.0 .5098 465.5 433.1 .5205 501.5 424.9 .5097 466*0 433.7 .5204 502.0 424.7 .S09S 466.5 433.5 .5202 502.5 424.6 .S094 467.0 433.4 . .5201 503.0 424.5 .5092 467.5 433.3 .5199 503.5 424.4 .5091 461.0 433.Z .5197 504.0 424.? .5089 461.5 433.0 .5196 504.5 424.1 .soaa 469.0 432.9 .5194 505.0 424.0 .5086 469.S 432.1 .5193 505.5 423.9 .5085 432.7 .5191 506.0 423.1 .5083 432.5 .5190 506.5 423.6 .5082 .o 432.4 .5111 507.0 423.5 .5080 .5 432.3 .5117 507.5 423.4 .5079 472.0 432.2 .5185 508.0 423.3 .5077 472.5 432.0 .5184 509.5 423.1 .5076 473.0 431.9 .5112 509.0 423.0 .5074 473.5 431.1 .5111 509.5 422.9 .5073 474.0 431.7 .5119 510.0 422.1 .5071 474.5 431.5 .5171 510.i 422.6 .5070

  • Time (sec.) Sheet 1 of 10 TABLE 15. 4-30 AT MASS AND ENERGY RELEASES FROM A 1. 4 FT2 de 1 AT 78 PERCEIH POWER (Including Entrained Moisture Effects) Break Fl ow ( 1 b/sec.) PROPRIETARY
  • RefeF te (5Q Jll) fe F Wi tl:ll:lel eiRg" R, b. Mittl te Ola" 9. Pa11 Novembe1 20, 1978 -af4fJ-NRb Ai;ii;iFeval letteP, QlaA Q, PaFF ta JarnJa 'fY 22, 1979 Energy Flow (million Btu/sec.)

SGS-UFSAR Revision 0 July 22, 1982 Sheet 2 of 10 Time Break Flow Energy Flow Time Break Flow Energy Flow (lb/sec.) (million Btu/sec.) (sec.) (lb/sec.) (million Btu/sec.)

000 11899 14.179 37.50 774.I 9*13 *

  • 14 84 38.00 773.6
  • 2.552 14945.
  • 9 38.SO 772.3 3 052 . 14917. 14 .530. 39.00 770.8 3°552 14517 13.977 39*50 769*2 0 92LS *
  • 6 40.00 767 .5 *
  • 4.052 14279. 13. 07 40.50 . 765.8 4.552 13959. 13.224 41.00 764.0 :9181 5.552 13208. 12.469 :}:l,8

.915a 6.552 12495.. 11.753 42.SO 751.2 7 552 113 er 11. 104 43.00 756.2

  • _..7
  • l.O. 43 50 754 2 8.552 11252. 10.527 44:00 1sz:1 .9063 9.552 10656. 9.986 44.50 750.1 *:8ff 11 052 9658 9.197 45.00 741.1 *-9 o o 8 958 45.50 746 0 0 oVYV 11.552 9357.
  • 46.00 744.0 .8964 11 602 4422 3 .028 46.50 742.o *!?'°15 *
  • 47.00 740.0 * ., ... 12.00 12.50 . , ... 00 . 14.50 -* oo 17.50 18.00 18.50 19.00 19.50 20.00 20.50 21 .oo 21.50 22.00 22.50 23.00 23.50 24.00 24.50 25.00 25.50 26.00 26.50 27.00 . 27.SO 28.00 2e.50* 29.00 29.50 30.00 30.SO 31 .oo. -1.50 .,,4.00 34.50 35.00 35.SO 36.00 36.-50 37.00 41Z1. 3921. 3717
  • 3518. -3332. 3158
  • 2994. 2840. 2696. 2515. 2311
  • 2131. 1971. 1129. 1701. 1587. 1483. 1389. 1304. 1226. 1154. 1089. 1021. 1005. 986.0 968.0 9S0.7 934.2 911.3 903.1 888.5 174.5 161.0 148.0 835.5 123.5 111.9 eoo.a 790.0 779.5 769.3 777.2 778.0 778.5 778.8 778.I 778.6 778.2 777.6 776.I 775.9 2.760 2.667 2.569 2.476 2.387 2.3()2 z.221 2.143 2.,070 1 .. 995 1.895 1.812 1.737 1.661 1.605 1.547 1.493 1.443 1.396 1.352 1.310 1.271 1.235 1.210 1.187 1.165 1.144 1.124 1. 105 1.087 1.069 1.052 1.036 1.ozo 1.oos .9902 .9762 .9627 .9496 .9369 .9247 .9342 .9352 .9358 .9361 .9361 .9358 .9353 .9346 .9337 .9326 47.50 737.9 *::::l 41.00 736.0 .1842 41.50 134.0 *8811 49.00 732.0 :1794 49.50 730.0 8770 50.00 121.0 *,,46 50.50 726.0 *1122 51.00 724.1 .8698 51.50 122.1 .8674 52.00 720.1 .1650 52.SO 718.2 *1627 53.00 716.J .8604 53.so 714.4 *1581 54.oo 112.s *8558 54.so 110.6 *8535 5s.oo 1oe.1 *1512 SS.SO 706.9 *14 90 56.00 705. 1 .1468 56.50 703.3 .1446 57 .00 701.S :14 24 57.50 58.00 58.50 59.00 59.50 60.00 60.50 61.00 61.50 62.00 62.50 63.00 63.50 64.00 64.SO 65.00 65.50 66.00 66.50 67.00 67.50 68.00 68.50 69.00 69.50 70.00 70.50 71.00 71.50 72.00 72.50 73.00 73.50 74.00 74.50 699.7 697.9 696.2 694.5 692.7 691.0 689.4 687.7 686.1 6&4.4 6&2.1 6t1.2 679.7 678.1 676.6 675.1 673.6 672.1 670.6 669.2 667.7 666.] 664.9 663.5 662.1 660.8 659.4 658.1 656.1 655.5 654.3 653.0 651.7 650.5

.1403 .1381 .1360 .1339 .8311 .am .1277 .1257 .1237 .8217 .1198 .1179 .1160 .1141 .11zz .810lt .1086 .8068 .1050 .8033 .8015 .7998 .1'911 .7964 .7947 .7931 *.7914 .7198 .7882 .7166 .7152 .7136 .7821 .7806 .7791 Sheet 3 of 10 Break Flow Energy Flow Time Break Flow Energy Flow lb/sec.) {million Btu/sec.}

{sec.} {lb/sec.)

{million Btu/sec.)

15.00 i4i:o .7716 111.0 595.Z .7136 .7761 111.5 594.1 .7131 75.50 646 .. I .17.47 112 .. 0 594.5 .7127 76.00 .645.6 .n 33 112.S 594.1 .7123 76.50 644.4 113.0 593.7 .7118 77.00 643.3 113.,S 593.4 .7114 114.0 593.0 .,7109 77.50 642.1 .7704 114.5 592.7 .7105 71.00 641.0 .7690 115.0 592.3 .7101 71.50 639.1 .7677 115 .. 5 592.0 .7097 79.00 638.7 .7663 116.0 591.6 .7092 79.50 637.6 .7650 116.5 591.3 .70M 10.00 636.5 .7637 111.0 590.9 .7084 10.50 635.5 .7624 11.00 634.4 .7611 11.50 633.3 .7598 117 .5 590.6 .7080 12.00 632.3 .7586 118.0 590.3 .,7076 12.50 631.3 .7573 118.5 589.9 .7072 13.00 630.3 .7561 119.0 589.6 .7068 13.50 6l9.3 .7549 119.5 589.3 .7064 84.00 628.3 .7537 120.0 518.9 .7060 14.50 627.4 .7526 120.S 588.6 .70S6 IS.00 626.4* .7514 121 .o 588.3 .70S2 15.SO 625.5 .7503 121 .5 588.0 .700 . 16.00 624.6 .7492 122.0 517 .. 7 .7044 86.50 623.7 .* 7481 122.5 587.3 .7041 17.00 622.8 .7470 123.0 587 .. 0 .7037 17.50 621.9 .7460 123.S 586 .. 7 .7033 N.00 621.1 124.0 586.4 .7029 . 18.50 620 .. :S .7440 124.S 586.1 .7026 41 619.4 .7430 125.0 585 .. 1 .7022 . 618.6 .7420 125.5 585.5 .7018 617.9 .7410 126.0

.7015 0 617.1 .7401 126.5 584.9 .7011 , .oo 616.3 .7392 127.0 584.6 .7007 11 .so 615.6 .7383 127 .5 584.3 .7004 92.00 614.9 .7374 128.0 584.0 .7000 92.50 614.2 .7366 128.5 583.7 .6997 93.00 613.S .7357 129.0 583.4 .6993 93.50 612.8 .7349 129.5 583.1 .6990 94.00 612.1 .7341 130.0 582.9 .6986 94.SO 611.5 .. 7333 *130.s 582.6 .6983 95.00. 610.8 .7325 131.0 512.3 .6979 95.50 610.2 .7311 131 .s 582.0 .6976 96.00 609.6 .7310 132.0 581.7 .6972 96.50 609.0 .730Z 132.S 581.4 .6969 97.00 608.4 .. 7295 133.0 581.2 .6966 133.5 580.9 .6962 134.0 sao.6 97.50 607.1 .7218 134.5 580.3 .6955 98.00 607.2 .7211 135.0 580.1 .6952 98.50 6()6.6 .1274 135.S 579.8 .6949 99.00 606.1 -.7267 136.0 579.5 .6946 99.SO 60S.5 .7261 136.5 579.2 .6942 : 137.0 579.0 .6939 100.0 60S.O .7254 100.S '°"*4 .7248 101 .o 603.9 .7241 137.5 571.7 .6936 101.5 603.4 .7235 138.0 578.4 .6933 102.0 602.9 .7229 138.5 571.2 .6929 102.5 602.4 .7223 139.0 577.9 .6926 103;.0 601.9 .7217 139.S 577.6 .6923 103.5 601.4 *.1211 140.0 577., .6920 104.0 601.0 .7206 140.5 577.1 .6916 104.5 600.5 .7200 141.0 576.9 .6913 105.0 600.1 .7195 141.5 576.6 .6910 --5 599.6 .7190 142.0 576.S .6907 .o 599.2 .7114 142.5 576.1 .6904 .5 598.8 .7179 143.0 575.1 .6901 . .o 59&.4 .7174 143.5 575.6 .6898 07.5 598.0 .7169 . 144.0 575.3 .689S 108.0 597.6 .7164 144.5 575.0 .6891 108.5 597.2 .7159 145.0 574.I .6888 109.0 596.I .7155 145.5 574.5 .6&85 109.5 596.4 .7150 146.0 574.J .6182 110.0 596.0 .7145 146.5 574.0 .6879 110.5 595.6 .7141 147.0 57S.I .6876 147.S 573.$ a617J Sheet 4 of 10 Break Flow Energy Flow Time Break Flow Energy Flow lb/sec.) {million Btulsec.}

{sec.} {lblsec.)

{million Btu/sec.) .o 573.:S .6170 185.5 556.3 .6664 -.-.5 573.0 .6167 186.0 556.1 .6661 149.0 572.I .6164 186.S 555.1 .6659 149.5 572.5 .6161 187.0 555.6 .6656 150.0 572.J .6158 187.5 555.4 .6654 150.5 572.1 .6155 188.0 555.2 .6651 151 .. 0 571.I .6152 188.5 555.0 .6648 151 .. 5 571.6 .6849 18900 554.1 .6646 152.0 571 .. J .6146 189.5 554.6 .,6643 152.S 571.1 .6843 190.0 554.4 .6641 153.0 570.8 .6841 190.5 554.Z .6638 153.5 570.6 .6138 191.0 553.9 .6636 154.0 570 .. 4 .6135 191 .5 553.7 .6633 154.5 570.1 .6132 192.0 553.5 .6631 155.0 569.9 .6829 192.5 553.3 .6621 155.5 569.7 .6126 19300 553.1 .662S 156.0 569.4 .6123* 193.5 552.9 .6623 156.5 569.2 .6120 194.0 552.7 .6620 157.0 561.9 .6117 194.5 552.5 .6611 195.0 552.3 .6615 157.5 561.7 .6115 195.5 552.1 .6613 196.0 551.9 .6610 158.0 561.5 .6112 196.5 551.6 .6608 158.5 561.Z .6809 197.0 551.4 .6605 159.0 561.0 .6806 159.5 567.1 .6803 160.0 567.5 .6800 160.5 567.J .6798 197.5 551.Z .6603 161.0 567.1 .6795 199.0 551.0 .6600 161.5 566.9 .. 6792 199.5 550.1 .6598 162.0 566.6 .6719 199.0 550.6 .,6S9S 162.5 566.4 .6717 199.5 550.4 .6593 .a* 566.Z 200.0 550.2 .5 565.9 .6714 200.5 550.0 .6590 .6711 .6588 .o 565.7 .6771 201.0 549.1 .6585 64.5 565.o5 .6775 201.5 549.6 .6513 165.0 565.3 .6773 202.0 549.4 .6580 165.5 565.0 .6770 202.5 549.Z .6571 166.0 564.8 .6767 203.0 549.0 .6575 166.5 564.6 .6765 203.5 54'.7 .6573 167.0 564.4 204.0 541.5 167.5 564.1 .6762 204.5 544.3 .6570 161.0 563.9 .6759 205.0 541.1 .6561 161.5 .. 563.7 .6756 205.5 547.9 .6565 169.0 563.5 .67S4 206.0 547.7 .6563 169.5 563.Z .6751 206.5 547.5 .6560 .6741 .6558 170.0 563.0 .6746 207.0 547.J .6555 170.S 562.1 207.5 547.1 171.0 562.6 .6743 2oe.o 546.9 .6553 .6740 .6550 171.5 562.J .6737 208.5 546.7 .6541 172.0 562.1 .6735 209.0 546.5 .6545 172.5 561.9 .6132 209.5 546.3 .6543 173.0 561.7 .6729 210.0 546.1 .6540 17305 561.5 .6727 210 .. 5 545.9 .6538 174.0 561.Z -.6724 211.0 545.7 .6536 174.S 561.0 : .6721 211.5 545.S .6533 175.0 560.8 .6719 . _212.0 545.3 .6531 175.5 560.6 -.6716 212.5 545.1 .6528 176.0 560.4 .6713 213.0 544.9 .6526 176.5 560.Z .6711 213.5 544.7 .6523 177.0 559.9 .6108 214.0 544.S .6521 214.5 544.3 .6518 177.5 559.7 .'706 215.0 544.1 .6516 179.0 559.5 .6703 215.5 543.9 .6514 179.5 559.3 .6700 216.0 543.7 .. 6511 179.0 559.1 .6698 216.5 543.5 .6509 179.5 558.1 .6695 217.0 543.3 .6506 -558.6 .669Z 558.4 .6690 551.2 .6617 .5 558.0 .6615 12.0 557.1 .6612 .e2.5 557.6 .6679 19J.O 19J.S 557.3 .6677 194.0 557.1 .6674 184.5 556.9 .6672 1es.o 556.7 .6669 556.S .6666 Sheet 5 of 10 Break Flow Energy Flow Time Break Flow Energy Flow lb sec. mi 11 ion Btu /sec. sec. lb/sec. million Btu/sec. 217.5 543.1 .6504 c53.5 5Z9.0 .6334 218.0 542.9 .6501 254.0 521.1 .6331 218.5 542.7 .6499 C?54.5 521.6 .6329 219.0 542.5 .6496 528.4 .6327 219.5 542.3 .6494 255.5 528.3 .6324 220.0 542.1 .6492 256.0 sza.1 .6322 220.5 co6489 256.5 527.9 .6320 221.0 541 .. 7 .6487 257.0 527.7 .6317 221.5 541.5 .64&4 222.0 541.3 .64&2 222.5 541.1 .6480 257.5 527.5 .6315 223.0 54().9 .6477 Z5a.o 527.J .6313 223.5 540.7 .6475 258.5 527.1 .6311 224.0 540.5 .6472 259.0 526.9 .6308 224.5 540 .. J .6470 259.5 526.7 .6306 225.0 540.1 .6467 260.0 526.6 .6304 225.5 539.9 .6465 260.5 526.4 .* 6301 226.0 539.7 .6463 261.0 526.Z .6299 226.5 539.5 .6460 261.5 526.0 .6297 227.0 539.3 .6453 262.0 525.1 .6295 227.5 539.1 .. 6455 262.5 525.6 .6292 228.0 538.9 .6453 263.0 525.4 .6290 228.5 538.7 .6451 263.5 szs.z .6288 229.0 538.5 .6448 264.0 525.1 .62&6 229.5 538.3 .. 6446 264 .5 524.9 .6l83 . 230.0 538.1 .6444 265.0 524.7 .6281 230.5 537.9 .6441 265.5 524.5 .6279 231.0 537.7 .6439 266.0 524.3 .6277 . 231.5 537.S

  • 6436 524.1 .6274 , 0 537.3 .6434 2t-7 .o 523.9 .6272 537.1 .6432 267.5 523.I .6270 536.9 .6429 263.0 523.6 .6268 .5 536.7 .6427 268.5 523.4 .6265 '4.0 536.5 .6425 523.Z .6263 5 536.3 .6422 .5 523.0 .6261 536. 1 .6420 270.0 522.I .6259 23S.5 535.9 .6417 270.5 522.6 .62S6 236.0 535.7 .6415 271 .o 522.5 .6254 236.5 535.6 .6413 271.5 522.J .6252 237.0 535.4 .. 6410 272.0 522.1 .6250 272.5 521.9 .6247 535.2 .6408 273.0 521.7 .6245 237.S 535.0 273.5 521.5 .6243 233.0 534.8 .6406 274.0 521.3 .6241 233. 5 534.6 .6403 274.5 521.2 .6238 239.0 534.4 .6401 275.0 521.0 .6236 239.5 .6399 275.5 520.8 .623' 240.0 534.2 .6396 276.0 520 .. 6 .623' 240.5 534.0 .6394 276.5 520.4 .623( 241.0 533.8 .6392 277.0 520.2 .622i 533.6 241.5 533.4 .6389 21.2.0 533.2 .6387 242.5 533.0 .6385 277.5 520. 1 .6Z25 243.0 .6382 278.0 519.9 243.5 532.9 .6380 278.5 519.7 .6223 244.0 532.7 .6378 279.0 519.5 .6221 244.5 532.S .6375 279.5 519.3 .6218 245.0 532.3 .6373 280.0 519.2 .6216 245.5 532.1 .6371 280.5 519.0 .6214 246.0 531.9 .6361 211.0 518.8 .6212 246.5 531.7 .6366 281.5 518.6 .6210 247.0 531.5 .6364 282.0 518.5 .6209 . 247.5 531.3 .6361 282.5 518.3 .6206 248.0 531.1 .6359 283.0 511.1 .6204 241.5 530.9 .6357 283.5 517.9 .6202 530.7 .6354 284.0 517.1 .6199 530.S .6352 284.5 517.6 .6197 530.4 .6350 28s.o 517.4 .619S .5 530.Z .6347 285.5 517.2 .6193 i .O 530.0 .6345 286.0 517.1 .6191 _.,,1.s 529.1 .6343 286.5 516.9 .6189 252.0 529.6 .6340 287.0 516.7 .6186 252.5 529.4 .6331 287.5 516.5 .06184 253.0

.6336 288.0 516.3 .6182 288.S 516.2 .6180 .6171 289.0 516.0 .6176 289.5 515.1 .... ., ..

Sheet 6 of 10 Break Flow Energy Flow nme Break Flow Energy Flow lb/sec. mil lion Btu sec. sec. lb/sec. million Btu/sec.)

l90.U 515.6 .6171 326.0 503.0 .6018 . 290.,S 515.4 .6169 3Z6.S 50Z.I .6016 291.0 515.3 .6167 327.0 502.6 .6014 291.s 515.1 .6165 3Z7.S 502.4 .6012

  • 292.0 514.9 .6163 328.0 502.3 .6010 292.S 514.7 .6160 328.S 502.1 .6007 293.0 514.5 .6158 32900 501.9 .6005 293.5 514.4 .6156 329.S 501.1 .6003 294.0 514.2 .6154 330.0 501.6 .6001 294.S 514.0 .6152 330.S 501.4 .5999 m.o 513.8 .6149 331.0 501.3 .5997 295.S 513.6 .6147 331.S 501.1 .599S Z96.0 513.4 .6145 33Z.O 500.9 .5993 *Z96.5 513.3 .6143 332.S 500.7 .5991 297.0 513. 1 .6140 333.0 500.6 .5989 333.S 500.4 .5967 334.0 500.2 .5995 297 .s 512.9 .6138 334.5 500.1 .5993 298.0 512.7 .6136 335.0 499.9 .5911 298.S 512.5
  • 6134 335.5 499.7 .5979 . 299.0 512.3 .6132 336.0 499.6 .5977 299.5 512.2 .6129 336.5 499.4 .5975 300.0 512.0 .6127 337.0 499.2 .5973 300.5 511.I .6125 I 301.0 511.6 .6123 301.5 511.4 .6121 302.0

.6111 Jp .5 499.1 .5971 302.S 511.1 .6116 Q 491.9 .5969 03.0 510.9

  • 6114 336.5 498.1 .5967 * . 5 510.7 .6112 499.6 .5965 .o . 5i0.6 .6110 s 491.4 .5963 .5 510.4 .61oe 31.0.0 499.Z .5960 '05.0 510.2 .6106 491.1 .S9S& JS.5 510.0 .6103 341.0 497.9 .S9S6 ..106.0 509.9 .6101 341.5 497.7 .S9S4 306.5 509.7 .6099 342.0 497oS .S9S2 307.0 5CYI. S .6'197 342.5 497.4 .59SO 307.5

.609S 343.0 497.2 .5948 308.0

.6'193 343.5 497.0 .5946 3oe.s 509.0 .6'191 344.0 496.9 .5944 309.0 508.8 .6089 344.5 496.7 .5942 309.S 508.6 .6087 345.0 496.5 .5940 310.0 5CMS.5 .6085 345.5 496.4 .5938 310.5 506.3 .6082 346.0 496.Z .5936 311 .o 5oe.1 .6080 346.5 496.0 .5934 3,, .s 507.9 .6078 347.0 495.9 .5932 507.8 .6076 347.5 495.7 .5930 312.5 507.6 .6074 348.0 495.5 .5928 313.0 507.4 .6072 34!.5 495.4 .5926 313.5 . 507 .3 .6070 349.0 49S.2 .5924 314.0 507.1 .6068 349.5 49S.O .5922 3l4.5 506.9 .6066 350.0 494.,9 .5920 315.0 506.7 .6064 350.5 494.7 .5911 315.5 506.6 .6062 351 .o 494.5 .5916 316.0 506.4 .6060 351.5 494.4 .5914 316.5 506.2 .6058 352.0 49".2 .5912 317.0 506., .6056 352.5 494.0 .5910 353.0 493.9 .5909 353.5 493.7 .5906 3H.5 505.9 .6053 354.0 493.6 .5904 311.0 505.7 .6051. 354.5 493.4 .5902 318.5 SOS.6 .6049 355.0 493.2 .5900 319.0 505.4 .6047 355.5 493.1 .5898 319.S sos.z .6045 356.0 492.9 .S896 o.o 505.0 .6043 356.5 492.7 .5894 .5 504.9 .6041 357.0 492.6 .5192 .a. 504.7 .60'9 -* .s 504.5 .6037 u.o 504.4 .6035 ,22.S 504.Z .6033 323.0 504.0 .6031 323.S 503.1 .6028 324.0 503.7 .6026 324.5 503.5 .6024 325.0 503.J .6022 325.S 503.1 .6020 Sheet 7 of 10 Time Break Flow Energy Flow Time Break Flow Energy Flow lb/sec.} {million Btulsec.}

{sec* l {lb/

{million Btu/sec.) .s 492.4 .5890 .

478.5 39S.5 476.I .5700 351.0 492.2 .SW 396.0 474.8 .S6'7 351.5 492.1 .Sl86 39o.5 472.7 .S651 359.0 . 491 .* 9 .5884 397.0 470.5 .S62S 359.5 491.7 .seaz 360.0 491.6 .HaO 360.5 491.4 .5171 468 .. l 361 .o 491.2 .5176 397.5 .5591' 361.5 491.1 .5174 398.0 465.1 .5568 362.0 490.9 .5172 398.S 463.3 .5537 362.5 490.1 .5170 399.0 460.7 .5505 363.0 490.6 .5168 . 399.5 45'.0 .5473 363.5 490.4 .5166 . 400.0 455.1 .5438 364.0 490.3 .5164 400.5 452 .. Z .S403 364.5 490.1 .S862 401.0 449.Z .5367 365.0 419.9 .5860 401.5 446.2 .5330 365.5 419.1 .5158 402.0 443.0 .5292 36600 489.6 .51S6 402.5 439.1 .5252 366.5 419.4 .5154 403.0 436.5 .5213 367.0 489.3 .5152 403.5 433.2 '.5172 367.5 489.1 .5150 404.0 429.7 .5131 368.0 419.0 .5&44 404.5 426.J .soea 368.5 488.8 .5146 405.0 422.7 .5046 369.0 418.6 .5144 405.5 419.1 .5002 369.5 416.S .5142 406.0 415.5 .49SI 370.0 418.! .Sl40 406.S 411.I .4913 , 370.S 418.1 .5138 407.0 408.1 .4868 371.0 418.0 .5136 407.5 404.J .4822 371 .5 . 487.8

  • 5134 408.0 400.4 .4776 * . 372.0 487.7 .. 5832 408.5 J96.S .4721 .5 487.5 .5130 409.0 J92.6 .4681 0 417.J .5129 409.5 311.6 .4633 5 487.2 .5127 410.0 314.6 .45&4 .o 487.0 .5125 410.5 JI0.6 .4S35 14.5 416.1 .5823 411.0 376.5 .4486 fS.O 416.7 .5121 411.5 372.4 .4436 375.5 416.5 .5119 412.0 368.3 .4386 376.0 .a6.4 .5817 412.5 364.1 .4336 376.5 I .5815 413.0 359.9 .4216 377.0
  • i&.O .5813 413.5 355.1 .4235 41400 351.6 .4185 485.9 414.S 347.4 .4134 377. 5 .5811 415.0 343.Z .4084 371.0 485.6 .5aoa 415.5 339.1 .4033 378.5 485.4 .5106 416.0 334.9 .3993 379.0 485.3 .5804 416.5 330.8 .3933 379.S 485.1 .5802 417.0 326.6 .3884 380.0 485.0 .5800 380.S 484.8 .5798 381 .o 484.7 .5796 417.S 322.6 .3"835 381.5 484.5 .5794 418.0 318.5 .3716 332.0 484.3 .5792 418.S 31406 .37!9 332.5 484.2 .5790 419.0 310.6 .3690 333.0 484.0 -.5788 419.S )06.7 .3644 333.5 483.9 : .5787 420.0 )02.9 .3599 334.0 483.7 .5785 420.5 299.Z .* lSSZ 334.5 483.5 .5783 421.0 295.5 .3508 335.0 483.4 .5781 421.5 291.I .3463 . 335.5 483.2 .5779 422.0 218.2 .3421 366.0. 4U.1 .5777 422.5 284.9 .3379 336.5 482.9 .5775 423.0 ll1.4 .3338 337.0 482.8 .5773 423.5 278.2 .)299 387.5 482.6 .5771 424.0 275.0 .3261 388.0 442.4 .5769 424.5 271.9 .3224 388.5 482.3 .5767 42500 268.9 .31M 389.0 482.1 .5765 425.5 266.0 .3153 -5 482.0 .5763 426.0 Z63.S .3120 0 481.8 .5762 426.5 260.6 .3088 5 481.6 .5760 427.0 481.5 zsa.o .3057 , .o 481.3 .5758 427.5 25S.6 .3027 ,, .5 481.2 .57S6 428.0 253.2 .592.0 .5754 428.5 ZS0.9 .2971 392.5 441.0 .5752 429.0 393.0 440.a .5750 429.5 248.I .2945 393.5 480.7 .5748 430.0 246.7 .29Z1 394.0 440.5 .5746 430.5 244.7 .2897 394.5 479.9 .5738 242.9 .2874

Sheet 8 of 10 Breo:k Flow Energy Flow Time Break Flow Energy Flow lb sec. mi 11 ion Btu sec. sec *. lb sec. million Btu/sec.)

4 1.0 241.1 .2153 46700 Z12.4 .zsoe 431.5 ZJ9.4 .2133 467.S 212.4 .2508 432.0 Z37.I .2113 468.0 21Z.4 .lsoe 432.5 Z36.J .2795 468.S 212.J .lSOS 433.0 234.I .2778 469.0 212.3 .2507 433.S 233.,5 .2761 469.5 212.3 .2507 4J4.0 232.2 .2746 470.0 21Z.3 .2507 4J4.5 231.0 .2731 470c5 Z12o3 .2S06 435c0 229.I .2111 471.0 212.2 .2506 43S.5 228.7 .2705 471.5 212.2 .2S06 436.0 227.7 .2692 472.0 z12.2 .2506 436.5 Zl6.8 .2681 472.5 212.2 .2S06 437.0 22S.9 .2670 473.0 211.z .2SOS 473.5 212.1 .2505 474.0 212.1 .2SOS 437.5 zzs.o .2660 474.5 2,2.1 .2sos 475.,0 .250S 431.0 224.2 .2650 47S.5 212.1 .2504 431.5 223.5 .2641 476.0 212.1 .2S04 439.0 222.1 .2633 476.5 212. 1 .2504 439.S 222.1 .2625 477.0 212.0 .lS04 440.0 221.s .2617 212.9 440.S 220.9 .2610 441.0 220.4 .2604 477.5 212.0 .2504 441.5 219.S .2598 478.0 212.0 .2504 . 442.0 219.4 .2592 478.5 212.0 .2503 442.5 211.9 .2517 479.0 212.0 .2503 443.0 211.5 .2sa2 479.5 212.0 .2503 443.5 218.1 .2577 480.0 212.0 .2503 444.0 217.8 .2572 480.S 212.0

  • 2503 . ... 5 !17.4 .2568 481.0 211.9 .2SOJ 0. 217.1 .2565 481.5 211.9 .2503 5 216.I .2561 482.0 211 .9 .2502 .o 216.5 .2558 482.5 211 .9 *.2s02 \46.5 216.2 .25S4 483.0 211.9 .2502 47.0 216.0 .2551 483.5 211.9 .2502 447.S Z15.8 .2549 484.0 211 .9 .2502 448.0 21s.s .ZS46 484.5 211.9 .2502 448.5 215.J .2544 415.0 211 .9 .2502 449.0 21s.2 .ZS41 485.5 211.9 .2502 449.5 215.0 .2539 486.0 211.a .2502 450.0 214.8 .2537 486.5 211.a .2502 450.S 214.7 .2535 417.0 211.a .2501 451.0 214.5 .2534 417.5 211.a .. 2501 451.5 214.4 .zs:sz 483.0 211.8 .2501 452.0 214.2 .2530 488.S 211.a .2so1 452.S 214.1 .2529 419.0 211.1 .2501 453.0 214.0 .2527 419.5 211.a .2501 453.5 213.9 .2526 491).0 211.1 .2501 454.0 213.8 .2525 490.5 211.1 .2501 454.5 213.7 .2524 491.0 211.a .2501 455.0 213.6 .2523 491.5 211.a .2soi 455.5 213.5 .2522 492.0 211.a .2501 4S6.0 213.4 .. 2521 492.5 211 ** .2501 456.5 213.4 .2520 493.0 211.a .2so1 457.0 213.3 .ZS19 493.5 211.7 .2500 494.0 211.1 457.5 213.2 .2518 494.S 211.1 .2500 458.0 213.2 02517 495.0 211.1 .2500 458.5 Z13.1 .. 2511 495.5 211.1 .2500 459.0 Z13.0 .2516 496.0 211.7 .2500 459.5 Z13.0 .2515 211.1 .2500 460.0 212.9 .2515 491.0 211.7 .2soo 460.5 212.9 .2514 461.0 212.1 .2513 461.5 212.1 .2513 41 212.7 .2512 212.7 .2512 212.7 .2511 212.6 .2511 .>4.0 212.6 .zs11 212.6 .2S10 465.0 212.5 .zs10 465.5 212.5 .2509 466.0 212.5 .2509 466.5 2,2.4 Sheet 9 of 10 Time Break Flow Energy Flow Time Break Flow Energy Flow ) (lb/sec.) (million Btu/sec.) (sec.) (lb/sec.) (million Btu/sec.)

.5 Z11.7 .2500 533.0 z11.s .Z491 1.0 211.7 .2500 533.S Z11.5 .Z491 491.5 Z11.7 .2500 534.0 Z11.S .Z491 499.0 . Z11.7 .Z500 534.5 211.s .Z491 499.5 211.7 .zsoo 535.0 211.s .Z498 500.0 Z11.7 .2500 535.5 211.s .2491 500.5 211.7 .zsoo 536.0 211.s .2491 501.0 Z11.7 .zsoo 536.5 211.s .. 2499 501.5 Z11.7 .zsoo 537.0 211.s .Z499 502.0 211.7 .2500 502.5 Z11.7 .2499 .2499 503.0 211.7 .2499 5]7c5 211.5 503.5 Z11.7 .2499 5ll.O 211.5 e2498 504.0 Z11.7 .2499 5ll.5 211.5 .249t 504.5 211.7 .2499 539.0 211.5 .2491 50S.O Z11.7 .2499 559e5 211.5 .2498 505.5 211.6 .2499 540.0 z11.s .2491 Z11.6 .2499 540.5 211.5 .2498 506.5 211.6 .2499 541.0 211.5 .Z491 507.0 211.6 .2499 541.,5 z11.s .2491 507.5 Z11.6 .Z499 542.0 211.s .Z498 508.0 Z11.6 .Z499 542.5 211.s .2498 508.5 Z11.6 .2499 543.0 211.s .2499 509.0 211.6 .2499 543.5 211.s .2498 509.5 211.6 .2499 544.0 211.s .2491 510.0 211.6 .2499 544.,5 211.5. .2491 510.5 211.6 .2499 545.0 211.5 .2491 511.0 211.6 .2499 545.5 211.s .2491 511.5 211.6 .2499 546 .. 0 21105 .2491 -512.0 211.6 .2499 5'16.5 211.5 .2498

  • 512.5 Z11.6 .2499 547 .. 0 211 .. 5 .Z491 --0 211.6 .2499 547.5 211.5 .2491 .5 211.6 .2499 541.0 211.5 .2499 .o 211.6 .2499 548.5 211.s .2491 .5 211.6 .2499 549.0 211.s .2491 115.0 211 .. 6 .2499 549.5 211.5 .2491 ;15.5. 211.6 .2499 550.0 Z11.5 .2498 516.0 211.6 .2499 550.5 211 .s .2499 516.5 211.6 .2499 551.0 Z11.5 .2491 517.0 211.6 .2499 551.5 211 .s .2499 552.0 Z11 .5 .Z491 552.5 211.s .Z491 517.5 211.6 .2499 553.0 Z11.5 .2491 511.0 211 .6 .2491 553.5 211.5 .Z491 511.5 211.6 .2491 554.0 211.5 .2491 519.0 211.6 .2498 554.5 211.5 .2491 519.5 Z11.6 .2491 555.0 211.5 .2491 520.0 211.6 .2498 555.5 211.5 .2491 520.5 211.6 .2491 556.0 211 .5 .Z498 521 .o 211.6 .2491 556.5 Z11.5 .2491 521.5 211.6 .2491 557.0 211.5 .2491 522.0 211.6 .2491 522.5 211.6 .2491 Sl3.0 211.6 -.2496 557.5 211 .s .2498 523.5 211.6 : .2491 551.0 z11.s .2491 524.0 Z11.6 .2491 551.S 211.s .2 .. 9& 524.5 211.6 .2491 559.0 z11.s .2491 525.0 Z11.6 .2491 559.5 211.5 .2491 525.5 211.6 .2491 560.0 211.s .2498 526.0 211.6 .2491 560.5 211.s .2491 526.S 211.6 .2491 561.0 211.5 .2491 527.0 211.6 .2491 561.5 211.5 .2498 527.5 211.6 .2491 562.0 Z11.5 .2491 528.0 211.6 .2491 562.5 211.s .2491 521.5 211.6 .2491 563 .. 0 Z't1 .5 .2491 529 .. 0 211.6 .2499 563.5 211.s .2491 211.6 .2498 564.0 211.s .2491 211.6 .2499 564.5 z11.s .2498 211.6 .2491 565.0 211.5 .2491 .o 211.6 .2499 565.5 211.s .2491 .n.5 211.6 .2498 566.0 211.s .2498 >32.0 211.6 .2491 566.5 211.5 .2491 211.5 .2491 -

Sheet 10 o.f 10 Time Break Flow Energy Flow Time Break Flow Energy Flow lb/sec.) (million Btu/sec.) (sec.) (lb/sec.)

_(million Btu/sec.) .u 111.s .Z491 567.5 z11.s .Z498 597.5 211.5 .2497 568.0 Z11.5 .Z491 598.0 211.5 .2497 568.5

  • Z11 .5 .Z498 598.5 21105 .2497 S69.0 z11.s .Z498 599.0 211.5 .2497 S69.5 211.s .2498 599.5 211.5 .2497 570.0 211.s .2498 600.0 211.5 .2497 570.5 211.s .2499 571QO 211 .. s .Z498 s11.s Z11 .5 .2498 57Z.0 211.s .2499 572.5 tn .s .2499 511.0 211.s .2498 573.5 2'11 .s .2499 574.0 211.s .2498 574.5 211.s .2499 575.0 211.s .2499 575.5 211.s .2499 576.0 211.5 .2498 576.5 211 .s .2499 577.0 211.s .2498 211.5 .2498 .2497 577 .5 211.s .2497 578.0 211.s .2491 578.5 211.5 .2497 579.0 Z-11 .5 .2497 579.5 211.5 .2497 c*o

.2497 0.5" 211.5 .2497 .o 211.s .2497 1e5 I 211 .5 02497 582 .* 0 211.s 02497 582.5 211.s .2497 583.0 211.s .2497 583.5 211.s .2497 584.0 . 211 .s .2497 584.5 211.s .2497 585.0 211.s .2497 585.5 211.5 .2497 586.0 211.s .2497 586.5 211.s .2497 587.0 211.s .2497 587.5 211.5 .2497 588.0 211 .s .2497 588.5 211.s .2497 589.0 211a5 .2497 589.5 211.5 .2497 590.0 211.5 .2497 590.5 211.5 .2497 591.0 211.5 -.2497 591.5 211.s : .2497 592.0 211.s .2497 592.5 211.s .2497 593.0 211.s .2497 593.5 211 .s .2497 594.0 211.s .2497 594.5 211.s .2497 59S.O 211.s .2497 595.5 211.s .2497 596.0 211.5 .2497 596.5 211.s 597.0 *

    • * ..... ! ..... *,::
}::-:
  • .. *-..
-::*i:*:*
_.y *. =;
-: :-.t :::.-J .... :;:.* ;-.::;: ..... .... : :* : "':" \J::
  • j
    .: ... I:: :*' . l*": .. !*;: . J: ... : ; . : i *:. .. .. /* I.. : i . ;::; :: .. ::. "i ... :::x.:* ":*! :: ... :y:::

... *Timi:a l'lf1Hi-1 I l . /i*. **:.;r.-.... -.... .. .. * **' : .. , .. *. * .. T ..... :-.. "' Pressure Tr1*p : f* "11111 0 * * *** **** r*** * -o o -I .... :. ,1 .. :.1*:** ... *=/ *' ... ,-r .. 1 1 . .., *= *.:: *r . ..; A ** , *., **

  • 1 .,.., _ : * :
  • r* 1 ! ' . I . . . . . .

alculated F1cw Flow Used 1n.Ana1ysis

-:::y-. ; . : :-: I: , 4 * ! -<*:-*

..

-: i-:: .. , :-* --F1cw d in Analysis ...

.
.: .. j ::; . ' . : -** * * * * * **J... -***: 1: ' ** 1 -.

.... -:-! *.

  • 1* ':'". * .. *** .1 * .;:: **

=1: :: * :* *:'...rl'::: . ! . . I . I ..

.... 'I * ,.. ':J". I . "' : . i 7'-. : : . : .

J ... l. :I I. * . . ! : I I*

  • I : : 1 TIME (sec.) * * : 1
  • Revis1on l... " July 22,
  • 0 41c SERVICE ELECTRIC AND GAS COMPANY NUCLEAR GENERATING STATION Feedwater Flow to the Faulted Steam Generator I Updated FSAR -1..'o,l.Nlt..

.___._._.

_____ _. __

_____

f'1ya1 e 15.4 Si------

  • 4500 ... w 4000 w LL. z 0 3500 <( w ::c _, <( ... . 3000 0 ... 2500 2000 0 *-* 20 1-10 w Wa: LL. w -c:c . 400 800 1200 GALLONS PER MINUTE PUBLIC SERVICE ELECTRIC AND GAS COMPANY SALEM NUCLEAR GENERATING STATION 1600 2000 Revision 0 July 22,
  • 1982 I -0 1500 1000 500 Q.. LL. zo A. ::c FULL CAPACITY AUXILIARY BOILER FEED Pump Curves for Auxiliary Feed Pump/Steam Driven Updated FSAR figure 15.4-93 90 80 70 60 50 40 30 20 10 0 ** ::E a: u a: w A. > u z w u LL. LL. w --------------------------
  • 3500 I-w w 3000 IL z c .2500 w J: ...J I-2000 0 I-1500 0 %PUMP Eff.

'\.O s\\P @S\l 200 400 600 GALLONS PER MINUTE PUBLIC SERVICE ELECTRIC AND GAS COMPANY SALEM NUCLEAR GENERATING STATION 800 40 20 0 1000 1/2 CAPACITY AUXILIARY BOILER FEED I-w i}i . 0.. z Z-0.. :c 600 400 200 Revision 0 July 22, 1982 Pump Curves

  • Auxiliary Feed Pump/Electrical Driven FSAR figure 15 4 !'!-< L_ _________________

__JL_ ________________

._ *--*---* 90 80 70 2: a: 60 u a: w A. > 50 u z w u IL 40 IL w 30 20 10 0

  • Figure 15.4-95 (Intentionally Deleted) Revision 1 July 22. 1983 -
  • 0 ..,. ... -0 0 ... \ \ \ 0 co \ 1 \ 0 N (.llNn/\:IH/n.l.8 gOL) 3.l.'IH 1\f/\OW3H .l'f3H Q N N Q Q N 0 CCI -Q "' ... Q ..,. -Q N -I!. w cc => I-< cc w CL. :E w I-I-z w :E z <C I-z 0 (J R.evi si on O July 22, 198t! PUBLIC SERVICE ELECTRIC AND GAS COMPANY Fan Cooler Heat Removal Rate SALEM NUCLEAR GENERATING STATION Updated FSAR Figure 15.4-96 _j
  • Q = IC SERVICE ELECTRIC AND GAS COMPANY SALEM NUCLEAR GENERATING STATION ('11Sd)
Q 8 -Q Q = 8 .... Q Q co Q Q in Q Q .., Q Q M Q Q N Q Q -Containment Pressure Transient 1.4 FT2 DE Break en c z 0 (.) LI.I LI.I t-70% Power Minimum Safeguards Westinghouse Mode 1 Upd*ted FSAR ) I I p 0 1982 FIGURE 15.4-97 1.4ft 2 DER. HOT ZERO POWER 40.0 --V> c.. -Ll.J 30.0 0
: :::::> V> V> Ll.J 0:: c.. I-z: Ll.J 2:
  • z: -20.0 ct I-z: 0 u TIME (SECONDS)
  • 0 Q Q 0 PUBLIC SERVICE ELECTRIC AND GAS COMPANY SALEM NUCLEAR GENERATING STATION Q 0 N 0 0 ... c 0 cc Q 0 ""' Q Q in Q 0 Q Q Q 0 *N Q Q ... Cf) 0 z 0 (,J w w I-Containment Temperature Transient 1.4 FT2 DE Break 70% Power Minimum Safeguards Westinghouse Mode 1 Updated FSAR Figure 15.4-98 FIGURE 15.4-98
  • 1.4 ft 2 DER, HOT ZERO POWER 300.o,........--------------------------------------------------------------------------------

200.0 -LL.. 0 -UJ 0:: => I-. 0:: UJ 0.. :::E: UJ I-l 00. 0 0.o,__ ______ _._ ______

TIME (SECONDS) in ""' .-Cl in .-in N .-Cl Cl .-Cl in Cl Cl co Cl Cl ""' Cl Cl in Cl Cl "" Cl Cl C") Cl Cl N Cl Cl .-*-U) 0 z 0 (.,) w w :E I-(:lo -z.l:I -HH/n.lB) .lN3101:1:1300 H3::1SN'iH.l .l'i3H BLIC SERVICE ELECTRIC AND GAS COMPANY SALEM NUCLEAR GENERATING STATION Containment Heat Transfer Coefficient 1.4 FT2 DE Break 70% Power Minimum Safeguards Westinghouse Mode 1 Updated FSAR Figure 15.4-99 FIGURE 15.4-99 SPLIT BREAK, 30 PERCENT POWER

  • *0.000 '"' V'l ...., 30.000 a: :::> "" "" ...., .... 2iJ.OOO z ...., ::E z c .... 10.000 z 0 C.J 0.0 0 0 0 000 0 0 0 0 0 0 0 000 0 0 000 0 0 00 0 0 0 000 0 0 coo 0 0 000 0 0 0 0 . . . .
  • w 0 -0 0 000 0 0 000 0 0 00 . *
  • 0
  • 0 0 0 coo C'l.I P'.' in ..... 0 0 0 00 . . . .
  • 0 0 0 00 0 0 0 000 . . .. . . . .
  • 0 0 0 000 0 0 000 0 0 oo 0 0 0 00 -"" ('I') in ..... -"" ('I') in ..... -"" ('I') in ..... -1\.1 ('I') in" -TIME <SECONDS)
  • ------**-----------

0 co Q IC Q ..,. Q N 0 0 a> 0 0 co 0 0 .... 0 0 IC Q 0 in 0 0 ..,. 0 0 C"') 0 0 N 0 0 .-Q -en

  • c 2 0 (.) w w I-('11Sd) 3i::lnSS31::1d PUBLIC SERVICE ELECTRIC AND GAS COMPANY SALEM NUCLEAR GENERATING STATION w Containment Pressure Transient 0.860 FT2 Split Break 102% Power Minimum Safeguards Westinghouse Mode 1 Updated FSAR Figure 15.4-100
  • 300.0 I I 200.0 100.*0
  • FIGURE 15. 4-100 SPLIT BREAK, 30 PERCENT POWER TIME (SECONDS) t I I I.
  • *
  • 0 0 0 0 M PUBLIC SERVICE ELECTRIC AND GAS COMPANY SALEM NUCLEAR GENERATING STATION 0 0 N 0 0 ... 0 0 CD 0 0 ""' 0 0 co 0 0 in 8 0 0 M 0 0 N 0 0 ... Containment Temperature Transient 0.860 FT2 Split Break c;; .. c z 0 tJ LU !!? LU :E I-102% Power Minimum Safeguards Westinghouse Mode 1 Updated FSAR FIGURE 15.4-101 0.6 DER BREAK, HOT FULL POWER W/0 ENTRAINMENT 40.0 30.0 --Vl . c.. -LI.I c::: :::::> Vl Vl LI.I 20.0 0:: 0. I-z: LI.I :::i:: z: -ct I-z: 0 u i a.a i o:i. TI ME (SECONDS)
  • 0 0 0 co 0 ca 0 N 0 0 0 a) 0 0 co 0 0 r.. 0 0 ca 0 0 in 0 0 0 0 M 0 0 N 0 0 .-<n 0 z 0 (.) LI.I LI.I :E I-(:f 0 --l::lH/n.18) .lN31:>1:f:f30:>

l::l3:fSN\tl::l.l

.1'13H PUBLIC SERVICE ELECTRIC AND GAS COMPANY SALEM NUCLEAR GENERATING STATION Containment Heat Transfer Coefficient 0.860 FT2 Split Break 102% Power Minimum Safeguards Westinghouse Mode 1 Updated FSAR Figure 15.4-102

  • -LI.. 0 -40 30 FIGURE 15. 4-102 0.6 DER BREAK, HOT FULL POWER W/0 ENTRAINMENT 1..1..1 c::: ::::> 20 c::: 1..1..1 a. :::&: 1..1..1 I-10 0.0 ....... .......

10-1 -. TIME (SECONDS)

  • ... Cl CIO Cl N Cl Cl .... Cl Cl co Cl Q in Cl Cl .., Cl Cl C") Cl Cl N Cl Cl ... en c z 0 (.) w w I-("ISd) , PUBLIC SERVICE ELECTRIC AND GAS COMPANY I
  • SALEM NUCLEAR GENERATING STATION Containment Pressure Transient for 0.860 FT2 Split Break at 102% Power with Minimum Safeguards (NRC Model) -_ _... --
  • a.: w .... z 0 .... <( cc ::::> .... <( en *
  • 0 Cl 0 Cl N PUBLIC SERVICE ELECTRIC AND GAS COMPANY SALEM NUCLEAR GENERATING STATION g -0 Cl Cl Cl -Cl 0 .... 0 0 cg 0 Cl in 0 Cl Cl 0 p) 0 0 N Ci) c z 0 (J w !!? w i= Containment Temperature for 0.860 FT2 Split Break at 102% Power with Minimum Safeguards (NRC Model) Updated FSAR 1)ELe;c Fi 11 1m 1S.4 194
  • g N in "" ... Cl in ... in N Cl Cl ... in "" in N Cl Cl "". Cl Cl IO en Cl Q Cl z in 0 CJ w w Cl :E Cl 'Iii' I-g Cl Cl N Cl -z*H -

J.'13H PUBLIC SERVICE ELECTRIC AND GAS COMPANY SALEM NUCLEAR GENERATING STATION Containment Heat Coefficient for 0.860 FT2 Split Break at 102% Power with Minimum Safeguards (NRC Model) ___________________

Fig '5 4 'PS

  • Q c:o ('lflSd) 31:inSS31:id Q N 0 0 in 0 0 "O:I' 0 0 M g N 0 0 -. iii' c 2 0 (,.) w w I-PUBLIC SERVICE ELECTRIC AND GAS COMPANY SALEM NUCLEAR GENERATING STATION* Containment Pressure Transient 0.908 FT2 Split Break 70% Power Minimum Safeguards Westinghouse Mode 1
  • * * *g N = c ... = = co = c ..... = c co = = in = = ""' = c N = c ... c;; c . 2 0 u w w I-(:lo) 3.l:!n.l'1H3dW3.l PUBLIC SERVICE ELECTRIC AND GAS COMPANY SALEM NUCLEAR GENERATING STATION Containment Temperature Transient 0.908 FT2 Split Break 70% Power Minimum Safe uards Westinghouse Mode 1 Updated FSAR ()Q.ete; Figa;e 1i:119r
  • * * ... 0 = e N Cl Q Q = Q Cl ..... g co Q 0 in 8 0 Q M Q 0 N c;; c 2 0 (.) w !1 w I-(:fo -z.1:1 -t:!Htn.18)

.1N31:>1:f:f30:>

H3:fSNVt:l.1.1V3H PUBLIC SERVICE ELECTRIC AND GAS COMPANY SALEM NUCLEAR GENERATING STATION Containment Heat Transfer Coefficient 0.908 FT2 Split Break 70% Power Minimum Safeguards Westinghouse Mode 1 Upd*ted FSAR OE\ETE Fi11u:e 1&:1198

  • PUBLIC SERVICE ELECTRIC AND GAS COMPANY SALEM NUCLEAR GENERATING STATION ('11Sdl Q N Q f6 g ID 0 Q 0 Q (") 0 0 N Q Q ... c;; 0 z 0 u w !!? w :!: I-Containment Pressure Transient for 0.908 FT2 Split Break at 70% Power with Minimum Safeguards (NRC Model) Updated FSAR DE1£TE' Fig 16 t 1Qi
  • 0 0 U) ::; w .... z 0 .... < a: :> .... < en *
  • 0 Q g C"'I 0 0 N PUBLIC SERVICE ELECTRIC AND GAS COMPANY --------L

_ ___::_:SALEM NUCLEAR GENERATING STATION 0 g -0 0 0) 0 0 co 0 0 U) 0 0 8 C"'I 0 en c z 0 (,) w !!! w :E Revision July 22, Containment Temperature Transient for 0.908 FT2 Split Break at 70% Power with Minimum Safeguards (NRC Model) __ _1'1101 e 1 1 **

  • 0 in -in N -0 0 -0 in 0 0 0 0 -0 0 ..... 0 0 ID 0 0 in 0 0 0 0 M 0 0 N iii c z 0 (,J w w :! I-(:1 0 -zl.:I -'=IH/nl.8) l.N3101::1::1300

'=!3::1SN'V'=ll.

l.'V3H PUBLIC SERVICE ELECTRIC AND GAS COMPANY SALEM NUCLEAR GENERATING STATION Containment Heat Transfer Coefficient for 0.908 FT2 Split Break at 70% Power with Minimum Safeguards (NRC Model) -;* 1A.1cM1

\5"2* \3 \\.liE.


  • 15.2.12.l Results Figure 15.2-38 illustrates the flux transient following the accident.

Reactor trip on overtemperature occurs as shown in Figure 15.2-38. The pressure decay transient following the accident is given in Figure 15.2-39. The resulting DNBR never goe*s below 1.30 as shown in Figure 15.2-40. 15.2.12.4 Conclusions The pressurizer low pressure and the overtemperature Reactor tion System signals provide adequate protection against this accident, and the minimum DNBR remains in excess of 1.30. 15.2.13 ACCIDENTAL DEPRESSURIZATION OF THE MAIN STEAM SYSTEM Identification of Causes and Accident Description ere core conditions resulting from an accidental ization of the ain Steam System are associated with an ina opening of a sing steam dump, assuming a upture of a main steam pipe 15.\)' The steam release as a consequ ce of s accident results in an . initial increase in steam flow whi decreases during the accident as the steam p-ressure.falls.

The ergy emoval from the Reactor Coolant System causes a reduction coolant temp ature and pressure.

In the derator temperature oefficient, the cooldown results in a reduc *on of core shutdown margin. is performed to demonstrate that the ing criterion is satisf" d: Assumi-ng a stuck rod cluster control assembly nd a single f

  • ure in the Engineered Safety Features there will SGS-UFSAR 15.2-49 Revision 0 July 22, 1982
  • *
  • 15.2.13 ACCIDENTAL DEPRESSURIZATION OF THE MAIN STEAM SYSTEM 15.2.13.l IDENTIFICATION OF CAUSES AND ACCIDENT DESCRIPTION The most severe core cond1t1ons result1ng from an acc1dental depressur1zation of the Ma1n Steam System are assoc1ated w1th an 1nadvertent opening of a single steam dump, relief or safety valve. The analyses performed assuming a rupture of a main steam p1pe are g1ven 1n Section 15.4.3. The steam release as a consequence of this acc1dent results 1n an initial increase in steam flow which during the accident as the steam pressure falls. The energy removal from the Reactor Coolant System causes a reduction of coolant temperature and pressure.

In the presence of a negative moderator temperature coefficient, the cooldown results in a reduction of core shutdown margin. The analysis is perfcrmed to demonstrate that the following criterion is satisfied:

Assuming a stuck rod cluster control assembly, with or without offsite power, and assuming a single failure in the Engineered Safety Features there will be no coasequential fuel damage after reactor trip for a steam release equivalent to the spurious opening, with failure to close, of the largest of any single steam dump, relief or safety valve. This criterion is satisfied by verifying the DNB design basis is met. The following systems provide the necessary protection against an accidental depressurization of the Main Steam System: l. Safety injection System actuation from any of the following:

2. a. Two out of three channels of low pressurizer pressure, b. High differential pressure signals between steam lines. The overpower reactor trips (neutron flux and AT) and the reactor trip occurring 1n conjunction with receipt of the safety injection signal . sa.s -u

&929Q.1e1e1eees

  • 3. Redundant 1solat1on of the ma1n feedwater 11nes: Susta1ned high feedwater flow would cause additional cooldown.

Therefore, 1n addition to the normal control act1on wh1ch will close the main feedwater valves following reactor tr1p, a safety injection signal w111 rap1dly close all feedwater

-control valves, tr1p the main feedwater pumps, and close the back up feedwater isolation valves. 15.2.13.2 METHOD OF ANALYSIS The follow1ng analyses of a secondary system steam release are for th1 s section.*

1. A full plant digital computer simulation, LOFTRAN (Ref. 4), is used to determine Reactor Coolant System temperature and pressure during cooldown.
2. An analysis to determine that there is no consequential fuel damage . . The following conditions are assumed to exist at the time of a secondary system steam release: 1. End of life shutdown margin at no load, equilibrium xenon conditions, and with the most reactive assembly stuck in its fully withdrawn positiori.

Operation of rod cluster control assembly banks during core-burnup is restricted in such a way that addition of positive reactivity in a secondary system break accident will not lead to a more adverse condition than the case analyzed.

2. A negative moderator coefficient corresponding to the end of life rodded -core with most reactive rod cluster control assembly in the fully withdrawn positi.on.

The variation of the coefficient with temperature and pressure is included.

The keff versus temperature at 1000 psi corresponding to the negative moderator temperature coefficient used plus the Doppler temperature effect is shown in Figure 15.2-41 . S G -U i=

8929Q;l9/979885 15*2 -

  • 3. Minimum capability for injection of high concentration boric acid solution corresponding to the most single failure in the Safety Injection System. The injection curve used is shown in Figure 15.2-42. Th1s corresponds to the flow delivered by one charging pump delivering its full contents to the cold leg header. No credit has been taken for the low concentration boric acid which must be swept from the safety injection lines downstream of the Refueling Water Storage Tank (RWST) prior to the delivery of boric acid (2,000 ppm) to the reactor coolant loops. 4. The case studied is an initial total steam flow of 228 lbs/second at 1015 psia from one steam generator with offsite power available.

This is the maximum capacity of any single steam dump or safety valve. Initial hot shutdown conditions at time zero are assumed since this represents the most pessimistic initial condition.

Should the reactor be just critical or* operating at power at the of a steam release, the reactor will be tripped by the normal overpower protection signals when power level reaches a trip point. Following a trip at power the Reactor Coolant System contains more stored energy than at no load, the average coolant temperature is higher than at no load and there is appreciable energy stored in the fuel. Thus. the additional stored energy is removed via the cooldown caused by the steam line .break before the no load conditions of Reactor Coolant System temperature and shutdown margin assumed in the analyses are reached. After the additional stored energy has been removed, the cooldown and reactivity insertions proceed in the same manner as in the analysis which assumes no load condition at time zero. However, since the initial ste.am generator water inventory is greatest at no load, the magnitude and of the Reactor Coolant System cooldown are less for steam line breaks occurring at power. 5. In computing the steam flow the Moody Curve for fl/D = O is used. 6. Perfect moisture separation in the steam generator is assumed. SGS-

.19f97988S

  • 15.2.13.3 RESULTS The results presented are a conservat1ve 1nd1cat1on of the events which would occur assum1ng a secondary system steam release s1nce 1t 1s postulated that all of the cond1t1ons descr1bed above occur s1multaneously.

F1gure 15.2-43 shows the trans1ent ar1s1ng as the result of a steam release hav1ng an 1n1t1al steam flow of 228 lbs/second at 1015 ps1a w1th steam release from one safety valve.

  • The assumed steam release 1s typ1cal of the capac1ty of any s1ngle steam dump or safety valve. In th1s case safety 1nject1on is 1nitiated automat1cally by low pressurizer pressure.

Operation of one centrifugal charging pump 1s considered.

Boron solut1on at 2,000 ppm enters the Reactor Coolant System providing suff1c1ent negat1ve reactivity to assure no fuel damage. A DNB analysis was performed for this case and the minimum u DNBR was above the 11m1t val1e of 1.3. The react1v1ty transient for the case shown 1n F1gure 15.2-43 1s more severe than that of a failed steam generator safety or relief valve Which is terminated by steam line differential pressure, or a failed condenser dump valve which is terminated by low pre1surtzer pressure.

The transient 1s quite conservative w1th respect to cooldown.

s1nce no credit 1s taken for the energy stored in the system metal other than that of the fuel elements or the energy stored in the other steam generators.

the trans1ent occurs over a period of about ten minutes, the neglected stored energy 1s 11kely to have a s1gn1ficant effect in slow1ng the cooldown.

15.2.

13.4 CONCLUSION

S The analys1s has shown that the cr1ter1a stated earl1er 1n th1s section is sat1sf1ed s1nt"e a DNBR less than 1.30 does not occur. SGS-UFS'Afl..

8929Q.1B/67ll85

\S.2.-5'"2.

  • *
  • System providing sufficient negative reactivity to maintain t well below criticality.

The reactivity transient for the 15.2-43 and 15.2-44 is more severe than tha f a rater safety or relief valve which is t inated by stedm line differe *a1 r dump valve which is terminated by low p The transient is quite conservative with ct to cooldown, 1nce no credit is taken for the energy stored in the s em meta than that of the fuel iler steam generators.

Si nee the occurs over a stored energy cool down. 15.2.13.4 minutes, the neglected effect in the The ana has shown that the criteria stated earlier in this isfied. Since the reactor does not return to critical the 1lity of a DNBR less than l.3u does not exist. 15.2.14 SPUIUOUS uPEAATIUN OF THt:: SAFETY INJECTION AT POwEK 15.2.14.1 Identification of Causes Spurious SIS operation at power could be caused by operator error or a false electrical actuating signal. A spurious signal in any of the followin':;1 channels could cause this incident.

l. rli gh coritai n_ment i->ressure
2. rligh steam line differential pressure 3.

steam line flow and low average coolant temperature or low steam line pressure

  • SGS-LJFSAK lti.2-5J Re vision u July 22, 1982
  • TAaLE 15.2-1 (Sheet 1 of 10) TIME SEQUENCE OF EVENTS FOR CONDITION II EVENTS. Accident
  • 11(' A !" ** Witndrawal from a Subcriti cal Condition SGS-UFSAR Event Initiation of uncontro11ed rod withdrawal 7.5 x 10-4 AK/sec. reactivity insertion rate from la-13 of nominal power Power range hi neutron flux low setpoint reached Peak nuclear power occurs Rods begin to fall into core Peak heat flux occurs Peak average fuel temperature.

occurs Peak average clad temperature occurs Peak average coolant ture occurs ; Time (sec. ) a.a 6.9 7.a 7.5 7.a 8.2 a.a 9.2 Revision a July 22, 19a2 Sheet 9 of 10 Time Break Flow Energy Flow Time Flow Energy Flow ,c. ) {lblsec.}

{million Btu/sec.}

{sec. } {lb/sec.}

{mi 11 ion Btu/sec.)

1.0 422.5 .506i , .... o 41J.5 .4959 511.5 422.4 .S067 541.5 413.4 .4951 512.0 422.J .5065 549.0 41J.J .4957 512.5 422.2 .5064 549.5 413.Z .4955 513.0 422.0 .5063 550.0 413.1 .4954 513.5 421.9 .S061 550.5 412.9 .4952 514.0 421.1 .5060 551.0 412.1 .4951 5H.5 421.7 .sose 551.5 412.7 .4949 515.0 421.5 .5057 552.0 412.6 .4948 51505 421.4 .5055 552.5 412.5 .4946 516.0 421.3 .5054 553.0 412.3 .4945 516.5 421.2 .5052 553.5 412eZ .4943 517.0 421.1 .5051 554.0 412.1 .4942 554.5 412.0 .4941 517.5 420.9 .5049 555.0 411.9 .4939 555.5 511.0 420.I .5()41 556.0 411.7 .4938 511.5 420.7 .5046 556.S 411.6 .4936 519.0 420.6 .5045 557.0 411.S .4935 519.5 420.4 .5043 411.4 .4933 520.0 420.J .5042 520.5 420.Z .504() 557.5 411.J .4932 521.0 420.1 .5039 551.0 411.1 .4930 521.5 420.0 .5037 551.5 411.0 .4929 522.0 419.I .5036 559.0 410.9 .4927 522.5 419.7 .5034 559.5 410.1 .492.ti . 523.0 419.6 .5033 560.0 410.7 .4925 523.5 419.S .5031 560.5 410.S .4923 524.0 419.4 .5030 561.0 410.4 .. 4922 . 524.5 419.Z .5021 561.5 410.J .4920 525.0 419. 1 .5027 562.0 '10oZ .4919 41*5 419.0 .5026 562.5 410.1 .4917 .o 411.9 .5024 563.0 409.9 .4916 .5 411.7 .5023 563.5 409.1 .4914 .o 411.6 .5021 564.0 :g:.1 ;.4913 )27.5 411.5 .5020 564.5 .6 .4911 528.0 418.4 .5011 565.0 409.S .4910 528.5 411.3 .5017 565.5 409.J .4909 529.0 411.1 .5015 566.0 409.2 .4907 529.5 418.0 .5014 566.5 409.1 .4906 530.0 417.9 .5012 567.0 409.0 .4904 530.5 417.1 .5011 567.5 408.9 .4903 531.0 417.7 .5009 561.0 408.7 .4901 531.5 417.5 .sooa 561.5 408.6 .4900 532.0 417.4 .5006 569.0 408.S .4198 532.5 417.3 .SOOS 569.5 408.4 .4197 533.0 417.2 .5003 570.0 408.J .489S 533.5 417.0 .5002 570.5 408.1 .4194 534.0 416.9 .5001 571.0 408.0 .4193 534.5 416.8 .4999 571.5 407.9 .4191 535.0 416.7 .4991 572.0 407.1 .4190 535.5 416.6 .4996 572.5 407.7 .. 4118 536.0 416.le .4995 573.0 407.S .4887 536.5 416.3 -.4993 573.5 407.4 .4885 537.0 416.Z : .4992 574.0 407.J .4184 574.5 407.2 .4182 537.5 416.1 -.499() 575.0 407.1 .4881 5ll.O 416.0 .4989 575.5 406.9 .418() 531.5 415.I .4917 576.0 406.1 .4878 539.0 415.7 .49U 576.5 406.7 .4877 539.5 415.6 .4984 577.0 406.6 .4875 540.0 415.5 .4983 540.5 415.J .4981 577.5 406.5 541.0 415.2 .498() .4874 541.5 415.1 .4979 571.0 406.4 .4172 542.0 415.0 .4977 571.5 406.Z .4171 _.5 414.9 .4976 519.0 406.1 .4169 .o 414.7 .4974 579.5 406.0 .4168 .5 414.6 .4973 580.o 405.9 *4167 4.0 414.5 .4971 580.5 405.1 .4165 ,44.5 414.4 .4970 511.0 405.6 .4864 545.0 414.3 .4968 511.5 405.5 .4862 545.5 414.1 .4967 512.0 405.4 .4161 546.0 414.0 .4965 512.5 405.3 .4159 546.5 413.9 .4964 513.0 405.Z .4151 547.0 413.1 .4962 513.5 405.0 .4156 547.S 413.1 .4961 584.0 404.9 .4155 -. --584.5 404.1 .4154 --* -.

-Sheet 10 of 10 Time Break Flow Energy Flow {sec.} {lblsec.}

{million Btu/sec.)

    • u 4()1..1 .usz oS 404.6 .4151 .o 404.4 .4149 586.5 404.J .uu 517.0 404.z .4146 517.5 4()4.1 .4145 511.0 404.0 .4143 518.S 403.9 .4142 589.0 403.1 .4141 519.5 403.6 .4839 590 .. 0 403.5 .4831 590.5 403.4 .4836 591.0 403.3 .4135 591.5 403.1 .4133 592.0 403.0 .4832 592.5 402.9 .4831 593.0 402.8 .41l9 593.5 402.1 .4828 594.0 402.S .4126 594.5 402.4 .4125 595.0 402.3 .4123 595.5 402.2 .4122 596.0 402.1 .4820 596.5 40Ze0 .4819 597.0 401.I .4811 597.5 401 * ., .4816 599.0 401.6 .4115 599.5 401.S .4113 599.0 401.4 .4112 599.5 401.2 .4110 .o. 401.1 .4809
  • Time (sec.) Sheet 1 of 9 TABLE 15.4-29 O*b p,-L Da AT MASS AND ENERGY RELEASE$ FROM A 8.988 FT 2 SPLIT BREAK ID t.. AT ?8 PERCENT POWER (Worst Temperature Case) Break (lb/sec.)

PROPRIETARY RefeF te (iQ* Jll} "A1313lieatieH rel" Witl'=IAe1EliAg" Ra L. Mittl te Ola" 8. Parr Nu vembe 1 20, 1978 NRG AflflF9\'al letteic, QlaR Q, Paicic to WieseffiaAA danaai) 22, 1979 Energy Flow (million Btu/sec.)

SGS-UFSAR Revision O July 22, 1982 Sheet 2 of 9 Time Break Flow Energy Flow Time Break Flow Energy Flow lb/sec. million Btu/sec. sec. lb/sec. million Btu/sec. .0000 0.0000 0.0000 37050 2215. Z.643 .5000 2048. 2.452 Jl.00 2205. 2.632 , .000 2066. 2.474 Jl.50 219'. 2.621 1.500 2071. 2.418 39.00 2116. 2.610 z.ooo 2089. 2.501 39.50 2177. 2.599 Z.500 2100. 2.514 40.00 2167. 2.5aa 3.000 2111. 2.527 40.50 2158. 2.577 3.500 2122e 2 .. 539 t.1.00 2149. Z.566 4.000 2132. 2.551 41.50 2139. 2.555 4.500 2142. 2.563 42.00 z.w. 5.000 2151. 2.574 5.500 2161. Z.585 6.000 2170. 2.596 42.500 3438. 4.100 60500 2179. Z.606 7.000 2189. Z.617 43.000 2097. 2.505 7.500 2198. Z.628 45.000 1984. 2.371 1.000 2208. Z.640 1.500 2218. 2.651 47.500 1844. 2.204 9.000 2221. 2.663 50.000 1705. 2.039 9.500 2238. 2.674 52.500 1568. , .876 10.00 2248. Z.616 10.50 2258. 2.697 55.000 1432. 1.714 11.00 2268. 2.709 57.500 1298. 1.554 11.50 2278. 2.121 60.000 1165. , .395 12.00 2289. Z.,733 12.50 2m. 2.745 62.500 1033. 1.238 13.00 2310. 2.757 65.000 902.1 , .083 13.50 2320. 2.769 14.00 2330. 2.1ao* 67.500 772.4 0.928 14.50 2340. Z.792 70.000 643.7 0.775 . s.oo 2351. Z.804

  • 50 2357
  • 2.811
  • oo 2365
  • 2.820 6.50 2373. 2.829 70.50 626.6 .7546 17.00 2381. 2.838 71.00 624.7 .7523 71.50 622.7 .7500 Ula. 72.00 620.1 .7477 17.50 2.147 72.50 619.0 .7454 ie.oo 2396. 2.156 73.00 617.1 .7432 11.50 2403. 2.164 73.50 615.3 .7411 19.00 2410. Z.172 74.00 613.6 .7389 19.50 2416. 2.879 74.50 611.1 .7368 zo.oo 2422. 2.116 75.00 610.1 .7341 20.50 2427. Z.191 75.50 60804 .7327 21.00 2431. 2.896 76.00 606.7 .7307 21.50 2526. 3.009 76.50 605.1 .7287 22.00 2661. 3.168 11.00 603.5 .7268 22.50 2865. 3.411 23e00 2825. 3.363 77.50 601.9 .7249 23.50 2751. 3.276 71.00 600.3 .7230 24.00 2677. 3.188 71.50 598.7 .7211 24.50 2597. 3.093 79.00 597.2 .7193 25.00 2521. J.On 79.50 595.7 .7175 25.50 2475. Z.9'9 10.00 594.2 .7157 26.00 2441. 2.908 10.50 592.1 .7139 26.50 2420. Z.813 11.00 591.3 .7122 27.00 Ht:: Z.857 11.50 589.9 .7105 27.50 Z.143 12.00 581.5 .1oaa
  • 28.00 2379. 2.835 12.50 516.9 .7069 . 21.50 2372. 2 .. 827 13.00 585.6 .7053 29.00 2365. 2.111 13.50 514.Z .7037 29.50 2357. 2.809 14.00 582.9 .7021 30.00 . 2349. 2.800 84.50 581.6 .7005 30.50 2341. Z.791 15.00 580.3 .6919 31.00 2333. 2.781 15.50 519.0 .6974 31.50 2324. 2.771 86.00 577.1 .69S9 .
  • oo 2316
  • 2.761 16.SO 576.5 .6944
  • 50 2307
  • 2.751 17.00 575.3 .6929
  • oo 2291
  • Z.740 17.50 574.1 .6915 3.50 2289. 2.730 18.00 572.9 .6900 34.00 22ao. 2.719 18.50 571.7 .6816 34e50 2271. 2.709 89.00 570.5 .6872 35a00 2262. Z.699 89.50 569.4 .68S& 35.50 2252. Z.687 90.00 568.2 .6844 36.00 2243. 2.676 36.50 2233. 2.665 *31.00 2224. 2.654 Sheet 3 of 9 Time Break Flow Energy Flow. Time. .Break.Flow . Energy.Flow lb/sec.} {million Btu/sec.}

{sec.} Pb/sec.} {million 0 567., .6130 127.5 506.1 .61°' 91.00 566.0 .6117 121.0 506.Z 91.50 564.9 *"°' 121.5 505.6 .6099 9Z.OO . 563.1 .6190 1Z9.0 505.0 .6082 56Z.7 .6m 1Z9.5 506.4 .6075 93.00 56,., .6764 130.0 503.1 .6068 93.50 560.6 .6752 130.5 503.Z .6061 94.00 559.5 .6739 131.0 502.6 .6053 94.50 551.5 .6727 131.5 502.0 .6046 9S.OO 557.4 .6714 132.0 501.4 .6039 95.50 556.4 .6702 13Z .. S 500.9 .6032 96 .. 00 555.4 .6690 133.0 500.] .602S 96.50 554.4 .6678 133.5 499.7 .6019 97.00 553.4 .6666 134.0 499.1 .6012 134.,S 498.6 .6005 135.0 498.0 .5998 97.50 552.5 .6654 135.5 497.5 .5991 98.00 551.5 .6643 136.0 496.9 .5994 550.5 -.6631 136.5 496.S .5971 98.50 -137.0 99.00 549.6 .6620 495.1 .5971 99.50 541.7 .6608 100.0 547.7 .6597 137.S 4".Z 100.5 546.1 .6586 .5964 101 .o 545.9 .6575 131.0 494.7 .59SS 101 .5 545.0 .6564 131.5 494.1 .m1 102.0 544.1 .6554 139.0 49J.6 .5945 102.5 543.Z .6543 U9.5 493.1 .5931 103.0 542.3 .6532 140.0 49Z.5 .59JZ 103.5

.652"2 140.5 492.u .59ZS 104.0 540 .. 6 .6512 141.0 491.5 *" . 5. 539.& .6501 141.5 490.9 .S91S 0 538.9 .6491 142.0 490.4 .5906 s 538.1 .6481 142.5 419.9 .S900 .o 537.Z .6471 143.0 .e9.4 .5894 06.S 536.4 .6461 143.5 418.I .5887 107.0 535.6 .6451 144.0 488.] .sae1 107.S 534.1 .6441 144.5 417.1 .5875 108.0 534.0 .6432 145.0 417.J .5869 108.5 533.2 .6422 145.5 416.1 .5863 109.0 53Z .. 4 .6412 146.0 416.J .5856 109.S 531.6 .6403 146.5 415.1 .5850 110.0 530.1 .6394 147.0 415.3 .5144 110.5 530.0 .6314 147.5 414.1 .5831 111.0 5Z9.3 .6375 141.0 414.3 .Sill 111.5 528.5 .6366 141.5 413.1 .sa.Z6 112.0 527.1 .6357 149.0 413.3 .5820 112.5, 527.0 .6341 149.5 412.1 .5114 113.0 526.3 .6339 150.0 412.S .SIOI 113.5 525.5 .6330 150.5 411.8 .5802 114.0 524.1 .6321 151.0 411.3 .5797 114.5 524.1 .6312 151.5 480.1 .51'91 115.0 523.4 .6304 152.0 480.4 .5715 115.5 522.6 .6295 152.5 479.,9 .sm 116.0 521.9 -.6286 153".0 419.4 .5m 116.S 521.2 .6271 153.5 471.9 . .5761 117 .. 0 520.5 .6269 154.0 471.4 .5762 154.5 471.0 .5756 155.0 477.5 .5750 117.5 519.1 .6261 155.5 477.0 .5745 11100 .519.1 .6HJ 156.0 476.6 .5739 111.5 511.4 .6244 ,56.5 476.1 .5733 119.0 517.1 .6236 157.0 475.6 .5728 119.5 517.1 .6221 157.S 475.Z .5722 120.0 516.4 .6220 'il0.5 515.7 .6212 1Slo0 474.1 .5717 1 .o 515. 1 .6204 151.5 474.z* _,,,, .5 514.4 .6196 159.0 473.1 .5706 .o 513.1 .6111 159.5 473.S .5700 .5 513.1 .6180 160.0 47Z.9 .5695 12].0 512.5 .617Z 160.5 472.4 .5689 12].5 511.I .6164 161.0 472.0 .5684 124.0 511.Z .6157 161.5 471.5 .5671 124.5 510.5 .6149 162.0 471 .. 1 .5673 125.0 S09.9 .6141 162.5 470.6 .5667 125.S 509.J .6134 163.0 470.Z .5662 126.0 509.7 .61Z6 163.S 469.7 .5657 126.5 508.0 .6,19 164.0 469.3 .565' 127.0 501.4 _.,,, 164.5 461.1 .5646 165.0 461.4 .5641 Sheet 4 of 9 Break Flow Energy Flow Time Break Flow Energy Flow lb sec. mi 11 ion Btu sec. sec . lb/sec. million Btu/sec.) .s 461.0

  • 5635 z02.s 431.6 .5l80 166.0 461.5 .5630 Z03.0 431.Z .5276 166.5 . 467.1 .5625 203 .. S 437.8 .5271 167.0 466.7 .5619 204.0 437.5 .5267 167.S 466.Z .5614 204.5 437.1 .5263 168.0 465.8 .5609 205.0 436.1 .52sa 161.5 465.4 .5604 205.5 436.4 .5254 169.0 464.9 .5599 206.0 436.0 .5250 169.5 464.5 .5593 206.5 435.7 .5245 170.0 464.1 .ssaa 207.0 435.3 .5241 170.5 463.7 .5583 207.5 435.0 .5237 171 .. 0 463.Z .5578 2oe.o 434.6 .5232 171.5 w.1 .5573 209.5 434.3 .5zza 17Z.O W.4 .5561 209.0 433.9 .5224 17Z.5 w.o .5563 209.5 433.5 .5219 173 .. 0 461.5 .55sa 210.0 433.2 .5215 173.5 461.1 .5553 210.s 432.1 .5211 174.0 460 .. 7 .. 5548 211.0 432.5 .5207 174.5 460.J .5543 211.5 432.1 .5202 11s.o 459.9 .5531 212.0 431.I .5198 175.5 459.5 .5533 212.5 431.4 .5194 176.0 459.1 .ss2a 213.0 431.1 .5190 176.S 458.6 .55l3 213.5 430.7 .5185 177.0 458.2 .5511 214.0 430.4 .5181 214.5 430.0 .517-1 215.0 429.7 .5173 11705 457.1 .5513 215.5 429.4 .5169 216.0 429.1 .5165 111.0 457.4 .55oe* 216.5 421.a .5162 171 .. 5 457.0 .5503 211 .. 0 428.S .5158 O* 456.6 .5491 456.2 .5493 455.8 .5481 .5 455.4 .5413 217.S 428.1 .5154 1.0 455.0 .5471 21a.o 427.8 .5150 1151 .5 454.6 .5474 211.5 427.5 .5146 112.0 454.Z .5469 219.0 427.2 .5143 112.5 453.1 .5464 219.5 426.9 .5139 113.0 453.4 .S459 220.0 426.6 .5135 11305 453.0 .5454 220.5 426 .. 3 .5132 114.0 452.6 .5450 221.0 426.0 .5121 114.5 452.Z .5445 221.5 425.7 .5124 115.0 451.I .5440 222.0 425.4 .5120 115.5 451.4 .5435 222.5 425.0 .5117 116 .. 0 451.0 .5431 223.0 424.7 .5113 116 .. 5 450.6 .5426 223.5 424.4 .5109 111.0 450.Z .5421 224 .. 0 424.1 .5105 187 .. S 449.9 .S416 224.5 423.1 .5102 181.0 449.5 .541Z 225.0 423.5 .5cm 181.5 449.1 .5407 225.5 423.2 .5094 189.0 441.7 .540Z 226.0 422.9 .5091 189.5 441.J .5398 226.5 422.6 .5057 190.0 447.9 -*.5393 221.0 422.3 .sou 190.S 447.5 .5389 227.S 422.0 .5079 191.0 447.Z .5384 221.0 421.7 .5076 191.S 446.I .5379 221.s 421.4 .5072 192.0 446.4 -.5375 229.0 421.0 .5068 192.S 446.0 .5370 229.5 420.7 .5065 193.0 445.6 .5365 230.0 420.4 .5061 193.S 445.J .5361 230.5 420.1 .5057 194.0 444.9 .5356 231.0 419.I .5053 194.5 444.5 .5352 231.5 419.5 .5050 195.0 444.1 .5347 232.0 419.Z .5046 195.5 443.7 .5343 232.5 411.9 .5042 196.0 443.4 .5331 233.0 411.6 .5039 196.5 443.0 .5334 233.5 411.3 .5035 0 442.6 .5329 234.0 411.0 .5031 234.5 417.7 .* 5026 .5 442.3 .5325 235.0 417.4 .5024 18.0 441.9 .S320 235.5 417.1 .S020. 198.5 441.5 .5316 236.0 416.I .5016 199.0 441.1 .5311 236.5 416.5 .son 199.5 440.1 .5307 237.0 416.2 .5009 200.0 440.4 .5302 200.5 440.0 .5298 201 .o 439.7 .5293 201.5 439.J .5289 202.0 438.9 .5215 Sheet 5 of 9 Break Flow Energy Flow Time Break Flow Fl ow lb/sec.) {million

{sec.} {1 b/sec. {million Btu/sec.)

Z37.5 415.t .5005 z15.o 393.J .4733 ne.o 415.5 .5002 Z75.5 393.0 .4729 Z38.5 415.Z .4998 276.0 392.7 .4725 Z39.0 414.9 .4"4 Z76.5 392.4 .4722 Z39.5 414.6 .4"1 211.0 392.1 .4711 Z40.0 414.J .4917 Z40.5 614.0 .4913 Z41.0 413.7 .4990 Z41.5 41J.4 .4976 Z77.5 J91.I .4715 Z42o0 41J., .497Z Z71.0 J91.5 .4711 242.5 412.1 .'969 Z71.5 . J91.2 .4708 243.0 412.5 .4965 279.0 390.9 .4704 Z4J.,5 412.2 .4961 279.5 390.6 .4701 244.0 411.9 .4951 zao.o J90.4 .4697 z,4.5 4,1.6 .4954 210.s J90.1 .4694 245.0 4n.J .4950 za1.o 389.8 .4690 245.S 4n.o .4947 211.5 389.5 .4687 Z46.0 .. ,0.7 .4943 212.0 389.2 .4683 Z46.5

.4939 212.s JU.9 .4680 247.0 410.1

  • 4936 2n.o 318.6 .4676 . 247.5 40'1.I .4932 zn.s JU.4 .4673 Z41.0 409.5 .4921 Zl4.0 __ , .4669 241.5 409.2 .4925 284.5 317.8 .4666 Z49.0 408.9 .49Z1 2es.o 317.5 .4662 Z49.S 408.6 .4918 zes.s 317.Z 250.0 408.3 .4914 286.0 316.9 .4656 250.5 408.9 .4910 Z86.5 . 316.6 .4652 zs1.o 401 .. .4907 . 217.0 316.4 .4649 251.5 401.4 .490J Zl7.5 386.1 .4645 407.1 .4899 288.0 385.1 .4642 406.I .4896 zsa.s 315.S .4631 406.5 .4892 219.0 315.Z .4635 406.2 .4189 289.5 315.0 .4632 r..o 405.9 .4185 290.0 384.7 .4628 .,4.5 405.6 .4181 290.5 384.4 .4625 255.0 405.S .4178 291.0 314.1 .4622 255.5 405.0 .4174 291.5 313.9 .4618 256.0 404.7 .4170 292.0 383.6 .4615 256.5 404.4 .4867 292.S *313.3 .4612 257.0 404.1 .4863 293.0 313.0 .46()8 293.5 382.7 .4605 294.0 382.5 .t.602 294.S 312.Z .4598 257.5 403.1 .4860 295.0 311.9 .459S 2sa.o 403.5 .4156 295.S 311.7 .4592 2sa.5 403.2 .4153 296.0 311.4 .4588 259.0 402.9 .4149 296.5 381 .1 .4585 259.5 402.6 .4145 297.0 380.8 .4582 260.0 402.3 .4142 260.5 402.0 .4138 261.0 401.7 .4135 297.5 3'0.6 .4579 261.5 401.4 -.4131 Z98.0 380.J .4S1S 262.0 401.1 .4127 298.5 380.0 .4572 262.5 400.1 .4124 299.0 379.1 .4S69 263.0 400.6 .4120 . 299.5 379.5 .4565 263.5 400.3 .4117 300.0 379.2 .4562 264.0 400.0 .4113 300 .. 5 J78.9 .4559 264.5 m.1 .4110 301.0

.4556 265.0 399.4 .4806 301.5 371.4 .4552 265.5 399.1 .4802 302.0 371., .4549 266.0 398 .. 1 .4199 302.5 377.9 .4546 266.S 399.4 .4795 303.0 377.6 .4543 267.0 391.1 .4791 303.5 377.J .4539 267.5 397.1 .4788 304.0 377.1 .4536 ?.d.O 397.5 .4714 304.5 376.1 .4533 5 397.2 .4780 305.0 376.5 .4530 0 396.9 .4777 305.5 376.J .4527 396.6 .4773 306.0 376.0 .4523 70.0 396.3 .4769 306.5 375.1 .4520 ,70.5 396.0 .4766 307.0 375.5 .4517 271.0 395.7 .4762 307.5 375.Z .45'4 271.5 395.4 .4758 :sos.a 375.0 .4511 272.0 395.1 .4754 308.5 374.7 .4508 Z72.5 394.1 .4751 309.0 374.4 .45°' 273.0 394 .. 5 .4747 309.5 374.Z .4501 273.5 394.2 .4743 310.0 373.9 .4491 274.0 393.9 .4740 310.5 373.7 .4495 .L ...


Sheet 6 of 9 Time Break Flow Energy Flow Time . Break Flow Energy Flow ., (lb/sec.) (million Btu/sec.) (sec.) (lb/sec.) (million Btu/sec.)

.. .o J7J.4 .449Z 349.0 J54.I .4267 311.5 J7J.1 .4419 349.5 354.6 .4264 312 .. 0 Jn.9 .4415 350.0 354.4 .4261 312 .. 5 J7Z.6 .4482 . 350.5 354.1 .4251 313.0 72 .. 4 .4419 351.0 353.9 .4256 313.5 J7Z.1 .4476 351.5 J53.7 .4253 314.0 371.I .4473 352.0 353.4 .4250 314 .. 5 371.6 .4470 352.5 353.Z .4247 315.0 371.3 .4467 353.0 353.0 .4245 315.,5 371.1 .4464 353.5 352.8 .4242 316.0 370.I .4461 354.0 352.5 .4239 316 .. 5 370.6 *.4451 354.5 352.3 .42.37 317.0 370.3 .4454 355.0 352 .. 1 .42.34 355.5 351.9 .4231 317.5 370.1 .4451 356.0 351.6 .4Z28 311.0 369.1 *"" *"356.5 351.4 .4226 311.5 369.5 .4445 357.0 351.2 .422.3 319.0 369.3 .4442 319.5 369.0 .4439 357.5 J51.0 .4220 320.0 368.1 .4436 351.0 350.1 .4211 320.S 368.5 .4433 351 .. 5 350.5 .4215 321.0 368.3 .4430 359.0 350.3 .4212 321.5 368.0 .4427 359.5 350.1 .4210 322.0 367.8 .4424 360.0 349.9 .4207 322.5 367.5 .4421 360.5 349.7 .4204 323.0 367.3 .4411 361.0 349.4 .4202 323.5 367.0 .4415 361.,S

.4199 324.0 366.8 .4412 362.0 9.0 .4196 324.5 366.S .,44()9 362.S 348.i .4194 325.0 366.3 .4406 363.0 341.6 .4191 ti 366.0 .4403 363.5 341.4 .4189 365.1 .4400 364.0 341.1 .4186 365.6 .4397 364.5 347.9 .4113 365.3 .4394 365.0 347.7 .4181 *.5 365.1 .4391 365.5 347.5 .4171 364.8 .4388 366.0 347.J .4176 321.5 364.6 .4315 366.5 347.1 .4173 329.0 364.3 .4312 367.0 346.9 .4170 329.5 364.1 .4379 367.5 346.6 .4161 330.0 363.I .4376 368.0 346.4 .4165 330.5 363.6 .4373 368.5 346.Z .4163 331.0 363.3 .4370 369.0 346.0 .4160 331.5 363.1 .4367 369.5 345.1 .4151 332.0 362.1 .4364 370.0 345.6 .4156 332.5 362.6 .4361 370.5 345.4 .4153 333.0 362.4 .4351 371.0 345.Z .4151 333.5 362.1 .4355 371.5 345.0 .4149 334.0 361.9 .4352 372.0 344.9 .4146 334 .. 5 361.6 .4.349 372.5 344.7 .4144 335.0 361.4 .4347 373.0 344.5 .4141 335.5 361.2 .4344 373.5 344.3 .4139 336.0 360.9 .4341 374.,Q 344 .. 1 .4137 336.5 360.'I .4331 374.5 343.9 .4134 337.0 360.4 .4335 375.0 343.7 .4132 375.5 343.5 .4130 . 337.5 360.2 .433Z 376.0 343.J .4127 338.0 360.0 .4329 376.5 343 .. 1 .4125 338.5 359.7 .4326 377.0 342.9 .4123 339.0 359.5 .4323 339.5 359.2 .4320 377.5 34Z.7 .4120 340.0* 359.0 .4318 371.0 342.5 .4111 340.5 351.1 .4315 371.S 342.J .4116 341.0 351.5 .4312 319.0 342.2 .4113 341.5 358.3 .4309 379.5-:S4Z.O .4111 342.0 351.1 .4306 380.o 341.I .4109 -357.1 .4303 380.5 341.6 .4107 357.6 .4300 381.0 341.4 .4104 . 357.4 .4298 381.S 341.Z .4102 357.1 .4295 382.0 341.0 .4100 ** s 356.9 .4292 382.S 340.1 .4097 ... 5.0 356.7 .4l89 383.0 340.6 .409S 345.5 356.4 .4216 383.5 340.4 .4093 346.0 356.Z .4284 384.0 340.3 .4090 346.5 356.0 .4211 384.5 340.1 .40!8 347.0 355.7 .4278 385.0 339.9 .4086 347.5 355.5 .4275 315.5 339.7 .4084 341.0 355.3 .4272 316.0 S39.5 .4082 348.5 355.0 .4270_

Sheet 7 of 9 Time Break Flow Energy F*r ow Time Break Flow Energy Flow lb/sec. million Btu/sec. sec. lb/sec. million Btu/sec. Q J'9.J .4019 424.0 321.1 .3943 387.0 J39.Z .4!J71 . 424.5 JZl.O .3942 387.5 "9.0 .4075 425.0 327.9 .3941 318.0 S31*.* ,.emJ 425.5 327.1 .3940 318.5 J31.,6 .4n70 426.0 327.7 .3931 389.0 331.4 .4069 426.5 327.6 .3937 389.5 331.Z .4066 427.,0

.3936 390.0 S31.1 .4064 427 .. 5

.3935 390.5 11 1.9 .4062 421.0 327.J .3934 391.,0 7.7 .4059 421.5 321.z .3933 391.5 331.5* .4057 429.0 327.1 .l931 392.0 337.3 .4055 429.5 327.0 .3930 392.5 337.1 .4053 430.0 326.9 .3929 393.0 337.0 .4051 430.5 J26.9 .3921 393.5 S36.I .4048 431.0 326.8 .3927 394.0 J]6.6 .4()1.6 431.5 526.7 .3926 394.5 S36.4 .4044 432.0 326.6 .392S 395.0 S36.3 .4042 432.5 326.5 .3924 395.5 S36.1 .4040 433.,0 326.4 .3923 396.0 335 .. 9 .4038 433.5 326.J .*3922 396.5 335.I .40.36 434.0 326.J .3921 397.0 335.6 .40l4 434.5 326.Z .3920 435.0 326.1 .3919 397.5 J35.4 .4032 435.5 326.0 .3911 391.0 335.Z .4030 436.0 325.9 .39:17 391.5 335.1 .4021 436.S 325.9 .3916 399.0 334.9 .4026 437.0 325.8 .3915 399.5 3l4.7 .4024 400.0 334.6 .. 4022 437.5 325.7 400.5 3l4.4 .4020 .3914 -334 .. 3 .4011 4Ja.O 325.6 .3913 3l4.1 .4016 438.5 325.6 .3912 333.9 .4014 439.0 325.5 .3911 333.1 .4012 439.5 325.4 .3911 .* 5 440.0 J.O J33.6 .4010 325.J .3910 -IJ3.5 333.5 .4008 440.5 325.3 .3909 404.0 333.3 .4006 441.0 325.2 .3908 404.5 333.Z .4005 441.5 325.1 .3907 405.0 333.0 .4003 442.0 325.1 .)906 405.5 332.9 .4001 442.5 325.0 .3905 406.0 332.7 .3999 443.0 324.9 .3905 406.5 332.6 .3997 443.5 324.I .3904 407.0 332.4 .3996 444.0 324.I .3903 407.5 332.J .3994 444.5 324.7 .3902 408.0 m*1 .399Z 445.0 324.6" .3901 408.5 .o .l990 445.5 . 324.6 .3901 409.0 331.I .3988 446.0 324.5 .3900 409.5 331.7 .'987 446.5 324.5 .3899 410.0 331.6 .3985 447.0 324.4 .3898 410.5 331.4 .'983 447.5 324.3 .3898 411.0 331.J .3982 443.0 324.J .3897 411.5 331.1 .3980 443.5 324.Z .3896 -412.0 331.0 .'971 449.0 324.1 .3895 412.5 330.9 .m1 449.5 324.1 .3895 413 .. 0 330.7 .l975 450.0 324.0 .3894 413.5 330.6 .3974 450.5 324.0 .3893 451.0 414.0 330.5 .397Z 451.5 323.9 .3892 414.5 330.J .3970 452.0 323.1 .3892 415.0 330.Z .3969 452.5 323.1 .3891 415.5 330.1 .3967 453.0 323.7 .3890 416.0 . 330.0 .3966 453.5 323.7 .3889 416.5 329.1 .3964 454.0 323.6 .3889 417.0 329.7 .3963 454.5 323.5 .3881 455.0 323.5 .3887 417.5 329.6 .3961 455.5 323.4 .3887 II 329.5 .3960 456.0 323.4 .3886 329.4 .J9SI 456.5 323.3 .3885 329.Z .3957 457.0 323.3 .3885 329.1 .39S6 323.2 .3884 J.0 329.0 .3954 .. ,o.5 328.9 .3953 421.0 321.1 .3951 421.S 321.7 .3950 422.0 328.6 .3949 422.S 321.4 .3947 328.3 .3946 423.5 328.Z .39'11 .

---Sheet 8 of g Time Break Energy Flow Time Break Flow Energy Flow Pb/S£d:.}

Btulsec.}

Btu/sec.)

-szs.1 .SNS 496.0 S11.4 .3126 szs.1 .wz 496.S 111.s .3125 Rs.g .3182* 497.0 11.3 .3124 459.0 RS. .3181 459.5 JZZ.9 .J880 s11.2 460.0 '2Z.t .3880 497.5 .3123 460.5 J:Z.I .3179 491.0 )11.1 .3122 461.0 322.7 .3171 491.S s11.1 .3822 461.5 S22.7 .3171 4"oO s11.o .3121 462.0 JZZ.6 .,)117 499.5 J17.9 e3120 462.S S22.6 .3176 500.0 J17.I .3119 463.0 szz.s .3176 500.5 ,,, .. .3811 463.5 szz.s .3175 501.0 111.1 .3117 464e0 322.4 .3174 501.5 17.6 .. 3116 464.5 S22 .. 4 .3174 502.0 J17.5 .Jl1S 465.0 m*s .3173 502.5 J17.5 .3114 465.5 .z .3172 503.0 J17.4 .311J 466.0 su.z .3172 503.5 . S17.J .311J 46605 SZZ.1 .3171 504.0 J17.Z .3112 467.0 tiz.1 .3170 504.5 111.z .3111 467.5 2.0 .3170 505.0 11.1 .3110 461.0 su.o .3169 505.5 J.17.0 .Jam 46105 321.9 .3161 506.0 316.9 .JIOS 469e0 JZ1.I .3167 S06o5 316.9 .3807 469.5 321.I .S867 507.0 J16.e .3806 470.0 321.7 .S866 507.S J16.7 .3805 470.5 321.7 .S865 5oe.o J16.6 .3804 . 471.0 321.6 .S865 508.5 J16.5 .3803 .471.5 321.6 .3164 509.0 J16.5 .3802 472.0 321.5 .3863. 509.5 J16.4 .3801 321.4 .S863 510.0 316.J .3800 . 473.0 321.4 .3162 510.5 316.Z .J799 5 ' 321.3 .3161 511.0 I"*' .3191 0 S21.3 .3860 511.S 16.1 .3797 5 321.Z .3860 512.0 16.0 .3196 .o 321.1 .3159 S12.5 315.9 .3195 ,75.5 321.1 .3151 513.0 . 315.1 .3194 476.0 S21.0 .3851 513.5 315.7 .3793 476.5 321.0 .3857 514.0 315.7 .3793 477 .o 320.9 .3156 514.S 315.6 .3792 515.0 315.5 .3791 477.5 JZ0.9 03155 515.S 315.4 .3790 471.0 JZO.I 516.0 315.3 .3789 478.5 HS*' .3155 516.S 315.3 .3788 .3154 315.Z 479.0 .7 .. 3153 517.0 .371i' 479.5 JZ0.6 .31Sl 480.0 320.5 .3152 5Ha5 315.1 .3716 480.5 320.5 .3151 511.0 315.0 .3715 481.0 :SZ0.4 .3150 511.5 314.9 .3714 481.5 JZ0.4 .3149 519.0 314.I .3713 482.0 320.S .3149 519.5 J14.I .3711 482.5 JZ0.2 .3141 520.0 314.7 .37&0 413.0 320.Z .3147 *520.5 J14.6 .3779 413.5 szo.1 5Z1e0 314 .. 5 .3779 484.0 szo.o .3146 s21.5 314.4 .3777 484.5 320.0 .3145 522.0 314.J .3776 415.0 I"*' .3144 522.S J14.2 .3775 485.S 19.I .Jl4J 523.0 314.Z .3774 416.0 J19.I .3142 523.5 314.1 .3773 486.S r**7 .3142 524.0 314.s .3772 487.0 19.7 .3141 524.S 313. .3771 487.5 "*' .ll40 525.0 31J*J .J770 488.0 J19.5 418.S 319.5

  • 31'9 525.5 J1 * .J769 489.0 319.4 .3131 526.0 11s.* .3761 489.5 J19.S .3131 526.S 1J.6 .3767 .3137 527.0 S1S.5 .3766 490.0 I"*' .3136 527.5 S1S.4 .3765 19.Z .3135 521.0 S1S.J .3764 J19.1 .3134 521.S 313.Z .3763 J19.0 .3134 5Z9.0 313.1 .3762 .o 319.0 .3133 5Z9.5 313.0 .3761 .t2.5 318.9 .3132 530.0 313.0 .3760 493.0 111.1 .3131 530.5 312.9 .3759 493.5 11.1 .3830 531.0 312.1 .3751 494.0 311.7 .3129 531.5 312.7 .3756 494.5 311.6 .3821 532.0 312.6 .3755 495.0 311.6 .llll 532.5 312.5 .3754 495.5 311.S .38Z7 1..4
  • **
  • TABLE 15.2-1 (Sheet 2 of 10) TIME SEQUENCE Of £VENTS FOR CONDITION I I EVENTS Accident Uncontro11cd RCCA Withdrawal at Power 1. Case A 2. Case B SGS-UFSAR Event Initiation of uncontrolled RCCA withdrawal at maximum reactivity insertion rate (7.5 x 10-4 aK/sec.) Power range high neutron flux high trip point reached Rods begin to fall into core Minimum DNBR occurs Initiation of uncontrolled RCCA withdrawal at a small reactivity insertion rate (3.0 x 10-5 aK/sec. for 3 0 -5 . loop, 3. x 10 aK/sec. for 4 1 oop) Overtemperature aT reactor trip signal initiated Rods begin to fall into core Minimum DNBK occurs Time (sec.) 0 1.5 2.0 2.7 o 32.6 34.6 34. 7 Revision 0 July 22, 1982
  • TABLE 15.2-1 (Sheet J of 10) TIME SEQUENCE OF EVENTS FOR CONDITION II EVENTS* Accident Uncontrolled Suren un uti on 1.-Dilution during refueling and startup. 2. Dilution During Full Power Operation -a. Automatic Reactor Control b. Manual Reactor Control SGS-UFSAR I:: vent Dilution begins
  • Operator isolates source of dilution; minimum margin to criticality occurs One percent shutdown margin 1 ost Dilution begins Reactor trip setpoint reached for overtemperature Rods begin to fall into core One percent shutdown is lost (if dilution continues) after trip) Time (sec.)
  • 0 -2400 or more -1300 0 52 54 -goo Revision O July 22, 1982
  • ------------------------

TAdLE 15.2-1 (Sheet 4 of 10) TIME SEQUENCE OF EVENTS FOR CONDITION II EVENTS Accident PartiCJ1 Loss of Forced ReJctor Coolant Flow 1. All loops operating, two pumps coasting down 2. All uut one loop operatiny, two pumps coasting down. SGS-UFSAR Event beyins Low flow reactor trip Rods begin to drop Minimum DNBR occurs Coastdown begins Low fl ow reactor trip Rods begin to drop Minimum DNBR occurs Time (sec.) 0 1.26 2.76 3.7 0 2.30 3.80 4.70 Re vision 0 July 22, 1982

  • TABLE 15.2-1 (Sheet 5 of 10) TIME SEQUENCE OF EVENTS FOR CONDITION II EVENTS Accident Loss of L.oad 1.

pressuri_zer control (BOL) 2. Wi th pressurizer control ( EOL) SGS-UFSAR Events Loss of electrical load Initiation of steam release from steam generator safety va lve*s Overtemperature Rods begin to drop Minimum DNBR occurs Peak pressurizer pressure occurs Loss of electrical load Initiation of steam release from steam generator safety valves Overtemperature Reactor Trip Point Reached rt.ads begin to drop Time (sec.) 0 9.0 9.1 11.1 11. 5 12.5 0 9.0 9.5 11. 5 Revision O July 22, 1982

  • *
  • TABLE 15.2-1 (Sheet 6 of 10) TIME SEQUENCE OF EVENTS FOR CONUITION II EVENTS Accident 3. Without surizer control (BOL) Event Minimum DNBR occurs Peak pressurizer pressure occurs Loss of electrical load Initiation of steam release from steam generator safety valves High pressuriz.er pressure reactor trip point reached Rods begin to drop Minimum DNBR occurs Peak pressurizer pressure occurs (1) does not decrease below its initial value
  • SGS-UFSAR Time (sec.) ( 1\ '., 10. 5 0 9.0 6.1 8.1 ( 1) 9.5 Revision 0 July 22, 1982
  • TABLE 15.2-1 (Sheet 7 of 10) TIME SEQJENCE OF EVENTS FOR CONDITION II EVENTS Accident 4. Without pres-surizer control (EOL) Event Loss of electrical load Initiation of steam release from steam generator safety valves Hi pressuriier pressure reactor trip point reached Rods begin to drop Minimum DNBR Peak pressurizer pressure occurs (1) DNBR does not decrease below its initial value
  • SGS-UFSAR Time (sec.) 0 9.0 6.0 a.a (1) 9.0 Revision 0 July 22, 1982
  • TABLE lS.2-1 {Sheet 8 of lu) TIME SEQUENCE OF tVENTS FOR CONDITION II EVENTS Accident Loss of Nonnal and Loss of Off-site Power to the Station Auxiliaries (Station Blackout)

Excessive feedwater at full loacL SGS-UFSAR Event Low-low steam generator water level reactor trip; reactor cool ant pumps begin to coast down Rods begin to drop Two steam generators begin to receive auxiliary feed from one motor-d riven aux i l i a ry feedwa ter pump Peak water level in pressurizer occurs One main feedwater control valve fails fully open Minimum ONBR occurs Feedwater flow isolated due to high-high steam generator level Time {sec.) 0 2 60 3250 0 15.2 14.0 Revision 0 July 22, 1982

  • TABLE 15.2-1 (Sheet 9 of 10) TIME SEQUENCE OF EVENTS FOR CONDITION II EVENTS Accident Excessive Load Increase 1. Mdnual Reactor Control (BOL) 2. Manual Reactor Control (EOL) 3. Automatic Keactor Control (BOL) 4. Automatic Control ( EOL) SGS-UFSAR Event Time {sec.) 10 percent step load increase 0 Equilibrium conditions
  • reached (approximate times only) 200* 10 percent step 1 oad increase 0 Equilibrium conditions reached (approximate times only) 75 10 percent step load increase Equilibrium conditions reached 10 percent step load increase Equilibrium conditions reached (approximate time only) 0 100 0 50 Revision 0 July 22, 1982
  • TABLE 15.2-1 (Sheet 10 of 10) TIME SEQUENCE OF EVENTS FOR CONDITION II EVENTS Accident Accidental zation of the Reactor Coolant system Accidental zation of the Main Steam System Inadvertent Operation.

of SI during Power Operation B928f).l9/979BBS Events Inadvertent Opening of one RCS Safety Valve Reactor Trip Minimum DNBR occurs Inadvertent Opening of one main steam safety or relief valve -Pressurizer Empties 2,000 ppm boron reaches RCS loops

  • Charging pumps begin borated water Low pressure trip point T1me (sec.) 0 22.1 24.0 0 172 214 0 . reached 64 Rods begin to drop 66 14202., I .04 1.03 . a: 1.02 0 r-u < la.. z 1.0 I 0 .... I-< u .... ...I 1.00 CL .... I-...I ::) :E 0.99 0.98 0.97 .........

-

200 250 300 350 400 450 500 550 CORE AVERAGE TEMPERATURE

(*F) PUBLIC SERVICE ELECTRIC AND GAS COMPANY Vari*tion of KEFF with Core Temperature SALEM NUCLEAR GENERATING STATION Updated FSAR Figure 15.2*41 *

  • 2t+OO 2200 2000 1800 1600 -411: I ijQO Cl) ""' ex 1200 ;:) Cl) Cl) ""' ex Cl) 1000 (,,.) ex 800 600 200 0 -0 100 200 300 t+OO 500 600 700 SAFETY INJECTION FLOW
  • PUBLIC SERVICE ELECTRIC AND GAS COMPANY Safety Injection Curve SALEM NUCLEAR GENERATING STATION Updated FSAR Figure 15.2-42 14202.2
  • 600 SSC = 500 -UJ -I--LL.. 450 -UJ > (!) 400 -UJ-a: 350 -0 u 300 -250 0.250 UJ 0.200 m-=t 0.150 o. 100 tn 0.500 0 2500 2000 >-1000 I-... _ > :E 0 -1000 -2000 -2500 0 100 200 300 400 500 600 TIME (SEC) Transient Response for a Steam Line Break PUBLIC SERVICE ELECTRIC AND GAS COMPANY Equivalent to 228 Lb/Sec at 1015 PSIA with SALEM NUCLEAR GENERATING STATION Outside Power Available Updated FSAR Figure 15.2-43 *
  • 0: L.i I-""' L.i a: 0 (,,) L.i a: I--""' 0: u.. L.i 0 Q,. -x L.i I-> I-=--3000 700 600 500 300 2.5 .;;,t. . t; <J ""' L.i Cl!:: -5.0 0 100 LE.TE... PUBLIC SERVICE ELECTRIC AND GAS COMPANY SALEM NUCLEAR GENERATING STATION 20 ..goo p PM BO RON REACH ES LOOPS AT 201 SEC 200 300 1+00 TIME (SECONDS)

Transient Response for a Steam Line Break Equivalent to 228 Lb/Sec at 1015 PSIA with Outside Power Available (Unit 2) Updated FSAR Figt1re 44... .

r-0 I \tJ oO IJ} N </. v . ::> _J <t \-. Q,.. './) ::> QI. ( IJ} () -... a,.. 1-rJ r!J I: V'l IJJ \-cJ '--1 "r <t( 111 v1 t-lJ.. "2. t..IJ ! I: < uJ 0 u J '2 .t£ 4'. VJ ,_ , ... 111 <( Cl UJ L1 -0 "'> ...., uJ .<( l: * *

  • 15.4.2 MAJOR SECONDARY SYSTEM PIPE RUPTURE 15.4.2.1 IDENTIFICATION OF CAUSES AND ACCIDENT DESCRIPTION The steam release arising from a rupture of a main steam pipe would result in an initial increase in steam flow which decreases during the .accident as the steam pressure falls. The removal from the Reactor Coolant System causes a reduction of coolant temperature and pressure.

In the presence of a negative moderator temperature coefficient, the cooldown results in a reduction of core shutdown margin. If the most reactive rod cluster control assembly is assumed stuck in its fully withdrawn position after reactor trip, there is an increased possibility that the core will become critical and return to power. A return to power following a steam pipe rupture is a potential problem mainly because of the high power peaking factors which exist assuming the most reactive rod cluster control assembly to be stuck in its fully withdrawn position.

The core is ultimately shutdown by the boric acid injection delivered by the Safety Injection System. The analysis of a main steam pipe rupture is performed to demonstrate that the following criteria are satisfied:

1. Assuming a stuck rod cluster control assembly, with or without offsite power, and assuming a single failure in the engineered safeguards there is no consequential damage to the primary system and the core remains in place and intact. 2. Energy release to containment from the worst steam pipe break does not cause failure of the containment structure.

Although DNB and possible clad perforation following*

a steam pipe rupture are not necessarily unacceptable, the following analysis, in fact, shows that no DNB occurs for any rupture assuming the. most reactive assembly stuck in its *fully withdrawn position . SGS-UF.SA.'2..

8920QilD'070SSS IS* 4-.r' The fo11ow1ng functions provide the protection against a steam pipe

  • rupture: 1. Safety 1njection system actuation from any of the following:
  • a. Two-out-of-three channels of low pressurizer pressure b. High differential pressure signals between steam lines c. High steam 11ne flow in two main steam lines (one-out-of-two per line) 1n coincidence with either low-low Reactor Coolant System average temperature or low steam line pressure in any two lines. d.

high containment pressure 2. The overpower reactor trips (neutron flux and 6T) and the reactor trip occurring in conjunction with receipt of the safety injection signal. 3. Redundant isolation of the main feedwater lines: Sustained high feedwater flow would cause additional cooldown.

Therefore.

in add1t1on to the normal control action which will close the main feedwater valves, a safety injection signal will rapidly close all feedwater control valves, trip the main feedwater pumps, and close the feedwater pump discharge valves. 4. Trip of the fast acting steam line stop valves (designed to close in less than 5 seconds) on: a. High steam flow in two main steam lines in coincidence with low-low Reactor-Coolant System average temperature or low steam line pressure in any two iines. b. High-high containment pressure SGS-8920Q:lQ/Q1Q88§ IS.4-l7

  • Fast-act1ng valves are prov1ded 1n each steam line that will fully w1thin 7 seconds of a signal to close (including instrumentation delays). For breaks downstream of the isolation valves, closure of all valves would completely terminate the blowdown.

For any break, in any location, no more than one steam generator would blowdown even if one of 'the 1solat1on valves fails to close. A description of steam line isolation is included in Chapter 10. Steam flow 1s measured by monitoring dynam1c head in nozzles inside the steam pipes. The nozzles which are of considerably smaller diameter than the main steam pipe are located inside the containment near the steam generators and also serve to limit the maximum steam flow for any break further downstream.

15.4.2.2 METHOD OF ANALYSIS The analysis of the steam pipe rupture has been performed to determine:

l. The core heat flux and Reactor Coolant System temperature and pressure resulting from the cooldown following the steam line break. The LOFTRAN[2?] code has been used. 2. The thermal and hydraulic behavior of the core following a steam line break. A detailed thermal and hydraulic digital-computer code, THINC, has J been used to determine if DNB occurs for the core conditions computed in (l) above. The following conditions were assumed to exist at the time of a main steam line break. ace i de_nt. l. End of life shutdown margin at no load, equilibrium xenon conditions, and the most reactive assembly stuck in its fully withdrawn position:

Operation of the control rod banks during core burnup is restricted in such a way that addition of posit1ve reactivity in a steam line break accident will not lead to a more adverse condition than the case analyzed.

SGS-99266.lB/071185

\5'*4-18

  • 2
  • The negat1ve moderator coeff1c1ent correspond1ng to the end of life rodded core with the most reactive rod in the fully withdrawn position:

The variation of the coefficient with temperature and pressure has been included.

The keff versus temperature at 1000 psi corresponding to the negative moderator temperature coefficient used is shown in Figure 15.4-48. The effect of power generat1on in the core on over-all reactivity is shown in Figure 15.4-49. The core properties associated with the sector nearest the affected steam generator and those associated with the remaining sector were conservatively combined to obtain average core properties for reactivity feedback calculations.

Further, it was conservatively assumed that the core power distribution was uniform. These two conditions cause underprediction of the reactivity feedback in the high power region near the stuck rod. To verify the conservatism of this method, the reactivity as well as the power distribution was checked. These core analyses considered the Doppler reactivity from the high fuel temperature near the stuck RCCA, moderator feedback from the high water enthalpy near the stuck RCCA, power redistribut1on and nonuniform core inlet temperature effects. For cases in which steam generation occurs in the high flux regions of the core, the effect of void formation was also included.

It was determined that the reactivity employed in the kinetics analysis was always larger than the reactivity calculated for all cases. These results verified conservatism; i.e., underprediction of negative reactivity feedback from power generation.

3. Minimum capability for injection of boric acid (2,000 ppm) solution corresponding to the most restrictive single failure in the safety injection 9'YStem. This corresponds to the flow delivered by one charging pump delivering its full flow to the cold leg header. Low concentration boric acid (<2,000 ppm) must be purged from the safety injection lines downstream of the Refueling Water Storage Tank prior to the delivery of boric acid to the reactor coolant loops. This effect has been allowed for in the analysis by assuming the lines to contain unborated water. The modeling of the Safety Injection System in LOFTRAN is described in Reference
27. S.GS-U\:.SAfl....

15"*4-15

  • For the cases where offsite power is assumed. the sequence of events in the Safety Injection System is the following.

After the generation of the safety injection signal (appropriate delays for instrumentation.

logic and signal transport included), the appropriate valves begin to operate and the high head injection pump starts. In an additional 12 sec, the valves are assumed to be in their final position and the pump is assumed to be at full speed. The volume containing the unborated water is purged before the 2,000 ppm boron reaches the core. This delay, described above, is inherently 1ricluded in the modeling.

  • In cases where offsite power is not available, a 12-sec delay is assumed to start the diesels and to load the necessary safety injection equipment onto them. 4. Four combinations of break sizes and initial plant conditions have been considered in determining the core power and Reactor Coolant System transients:
5. a. Complete severance of a pipe outside the containment, downstream of the steam flow measuring nozzle, with the plant initially at no load conditions, full reactor coolant flow with offsite power available.
b. Complete severance of a pipe inside the containment at the outlet of the steam generator with the plant initially at no load conditions with offsite power available.
c. Case (a) above with loss of offsite power simultaneous with the initiation of the safety injection signal. Loss of offsite power results-in coolant pump coastdown.
d. Case tb) above with the loss of offstte power simultaneous with the initiation of the safety injection signal. Power peaking factors corresponding to one stuck RCCA and non uniform core inlet coolant temperatures are determined at end of core life. The coldest core inlet temperatures are assumed to occur in the sector with the stuck rod. The power peaking factors account for the effect of the UFSA'-.. -e92ee .1 e/01eees . \5*4-'2.0
  • ** local void in the region of the stuck control assembly during return to power phase following the steam line break. This void in conjunction with the large negative moderator coefficient partially offsets the effect of the stuck assembly.

The power peaking factors depend upon the core power, temperature, pressure, and flow, and thus, are different for each. case studied. All the cases above assume 1n1t1al hot shutdown conditions at time zero since th1s represents the most pessim1st1c initial condition.

Should the reactor be just cr1tical or operating at power at the time of a steam line break, the reactor will be tripped by the normal overpower protection system when power level reaches a trip point. Following a trip at power the Reactor Coolant System contains more stored energy than at no load, the average coolant temperature 1s higher than at no load and there is appreciable energy stored 1n the fuel. Thus, the additional stored energy is removed via the cooldown caused by the steam line break before the no load conditions of Coolant System temperature and shutdown margin assumed 1n the analyses are reached. After the add1t1onal stored energy has been removed, the and reactivity insertions proceed in the same manner as in the analysis which assumes no load condition at time zero. However, since the in1tial steam generator water inventory is greatest at no load, the magnitude and duration of the Reactor Coolant System cooldown are less for steam line breaks occurring at power. 6. In computing the steam flow during a steam line break 0 the Moody Curve[2 S] for fl/D = 0 is used. 7. Perfect moisfure separation in the steam generator is assumed. The assumption leads to conservative results since, in fact, considerable water would be discharged.

Water carryover would reduce the magnitude of the temperature decrease in the core and the pressure increase in the containment . SC.S-UFSAk 8920Q.l9197ll85

\5"*4-2.\

15.4.2.3 RESULTS

  • The results presented are a conservative indication of the events which would occur assuming a steam line rupture since it is postulated that all of the conditions described above occur simultaneously.
  • 15.4.2.4 CORE POWER AND REACTOR COOLANT SYSTEM TRANSIENT o.. ..... ct rS* 4-so 3 the Reactor Coolant System transient and core heat flux following a main steam pipe rupture (complete severance of a pipe) outside the containment, downstream of the flow measuring nozzle, at initial no load condition (case a). The break assumed is the largest break which can occur anywhere outside the containment either upstream or downstream of the isolation valves. Offsite power is assumed available such that full reactor coolant flow exists. The transient shown assumes an uncontrolled steam release from only one steam generator.

Should the core be critical at near zero power when the rupture occurs the initiation of safety injection by high differential pressure between any steam line and the remaining steam lines, or by high steam flow signals in coincidence with either low-low Reactor coolant System temperature or low steam line pressure will trip the reactor. Steam release from more than one steam generator will be prevented by automatic trip of the fast action isolation valves in the steam lines by the high steam flow signals in coincidence with either low Reactor Coolant System temperature or low steam line pressure.

The steam line isolation valves are designed to be fully closed in less than 5 seconds after receipt of closure signal with no flow through them. With the high flow existing during a steam line rupture the valves will close considerably faster. S OB 15* 4-5 2..b LL"'-<{ 51B 7 The steam flow--en Figure as well as Figures U1rcn1gl:I 15.4-53B "-represent steam flow from the faulted steam generator only. In addition, all steam generators were assumed to discharge through the break until steam line isolation has occurred .

-8929Q. l 9/979885 lS*4-22.

  • 52t> 53D As shown 1n F1gures 15.4-?2" the core atta1ns cr1t1cal1ty w1th the rod cluster control assembl1es inserted (with the design shutdown assuming one stuck assembly}

before boron solution at 2,000 ppm enters the Reactor Coolant system from the Safety Injection System. The delay time consists of the time to receive and actuate the safety inje.ction signal and the time to completely open valve tra1ns 1n the safety 1njection lines. The safety injection pumps are then ready to deliver At th1s stage a further delay time 1s 1ncurred before 2,000 ppm boron solution can be 1njected to the Reactor Coolant System due to low concentration solution being purged from the safety 1nject1on 11nes. A peak core power well below the nominal full power value is atta1ned.

The calculation assumes the boric acid is mixed with. and diluted by the water flowing in the Reactor Coolant System prior to entering the reactor core. The concentration after mixing depends upon the relative flow rates in the Reactor Coolant System and in the Safety Injection System. The variation of mass flow rate in the Reactor Coolant system due to water density changes is included in the calculation as in the variation of flow rate from the Safety Injection System and accumulator due to changes 1n the Reactor Coolant System pressure.

The Safety Inject1on System flow calculation includes the line losses in the system as well as the pump head curve. The accumulators provide the addit1onal source of borated water if the RCS pressure decreases to below 580 psia. The integrated flow rate of borated water from both the accumulators and the Safety Injection System for each of the four cases analyzed are shown in Figure 15.4-54. 5 I A o.. ..... el I 5

  • 4 -5 I D Figuresl5.4-}'f case b. a steam line rupture at the exit of a steam generator at load. The sequence of events is similar to that described above for the outs1de the conta1nment except that cr1ticality 1s atta1ned earlier due to more rapid cooldown and a higher peak core average power is attained .

15*4 -23 I

  • 51-A,52 l?:> 5"3 A, 5 .3 B F1gure5 15.4-}l'.

and show the responses of the sal1ent parameters for cases c and d which correspond to the cases discussed above with additional loss of offsite power at the time the safety injection signal is generated.

The Safety Injection System delay time 1ncludes 12 seconds to start the diesel (including instrumentation delay time) and 12 seconds to get the safety injection pump to full. speed. In each case criticality is achieved later and the core power increase is slower than in the similar case w1th offsite power available.

The ability of the emptying steam generator to extract heat from the Reactor Coolant System is reduced by the decreased flow 1n the Reactor Coolant System. For both these cases the peak core power remains well below the nominal full power value. It should be noted that follow1ng a steam 11ne break only one steam generator blows down completely.

Thus, the remaining steam generators are still available for dissipat1on of decay heat after the initial transient is over. In the case of loss of offsite power this heat is removed to the atmosphere via the steam line safety* valves which have been sized to cover this condition.

The sequence of events is shown on Table 15.4-1. 15.4.2.5 MARGIN TO CRITICAL HEAT FLUX A DNB analysis was performed for the three cases most critical to DNB. It was found that all cases had a minimum DNBR greater than 1.30. 15.4.2.6 OFFSITE DOSES The off-site doses resulting from the steam line break accident, assuming a primary to secondary steam generator tube leak in the intact steam generators, were calculated.

The assumptions and parameters including the mass. transferred through the steam generator tube leak used in the analysis are listed below: l. Prior to the accident, activity of fission products in the primary system 1s as given in Table 15.4-8. The 1odine concentration in the secondary side is 0.28 uCi/cc of equivalent Sc-.s ..

8929Q:19/97988S IS-* 4-2.4

  • 2. Off-s1te power 1s lost, main steam condensers are not ava11able for steam dump. 3. Eight hours after the accident the Residual Heat Removal System starts operation to cool down the plant. 4. The primary to secondary leakage is evenly d1str1buted in the three non-defective steam generators.

no tube leakage in the defective steam generator.

5. Defective fuel is l percent. 6. After eight hours following the accident.

no steam and activity are released to the environment.

7. No air ejector release and no steam generator blowdown during the accident.
8. No noble gas is dissolved in the steam generator water. amount of iodine/unit mass steam = 0 1 9. The iodine partition factor amount of 1odine/unit mass liquid . in steam generators
10. The atmosphere dispersion factors (x/Q) at site boundary and low population zone are as listed in Table 15.4-9. The breathing rate is 3.47 x 10-4 m 3/sec for 0-8 hours. 11. In the affected steam generator, all the water boils off and releases through the break inmediately after the accident.

One tenth of the iodines in the is released to the environment.

12. The primary pressure remains constant at 2235 psig for 0-2 hour and decreases linearly to atmosphere from 2235 psig during the period 2-B hour . sc...s.

8929Q.lBIB78BB'

\S'*4-25"

  • STEAM LINE BREAK STEAM RELEASE Mass release from defect1ve S.G. lbs Steam release from non-defect1ve S.G.'s lbs Feedwater Flow to 3 non-defect1ve S.G.'s lbs Mass of reactor coolant transferred 1nto 3 non-defective S.G.'s lbs for a primary to secondary leak rate of l gpm, lbm 0-2 Hours 95.000 424,000 433,000 719 2-8 Hours 0 1,188,000 1,300,000
2. 510 Us1ng the above assumpt1ons, the thyro1d 1nhalat1on exposure was calculated to be 2.1 rem at the m1n1mum exclus1on d1stance (1270 meters) and 0.37 rem at the 5 m1le low populat1on zone rad1us. Us1ng the conservat1ve calculational models presented 1n Safety Gu1de 4, the whole body doses were calculated to be 0.0067 rem at the m1nimum exclus1on d1stance and 0.0014 .rem at the low population zone radius . Sc:-...s-8929Q:19/Q7988S

\5"-4-2.(,

TABLE 15.4-1 (Sheet 1 of 3) TIME SEQUENCE OF EVENTS FOR CONDIT ION IV EVENTS Accident Major Reactor Coo 1 ant System Pipe Ruptures Double-Ended Cold Leg Guillotine

1. { C 0 = 1.0) 2. (.c 0 = o.8) 3. ( C 0 = O. 6) SGS-UFSAR Event Start Reactor trip signal Safety injection signal AccLmulator injection End of B Bottom of core recovery Accllllulators empty Pllllp i nj ecti on End of bypass Start Reactor trip signal* Safety injection signal Accllllulator injection End of 8 . Bottom of core recovery Ace llllU l ators empty Pllllp injection End of bypass Start Reactor trip si gna 1 Safety injection signal Ace IJ11U l ator injection Time{ Seconds) 0.0 1.65 0.86 14.1 28.1 . 40.34 51.15 25.86 25.4 o.o 1.66 0.92 14.6 28.8 40.95 51.6 25.92 26.0 0.0 1.66 1.03 16.8 Revision 0 July 22, 1982 . -
  • TABLE 15.4-1 (Sheet 2 of 3) TIME SEQUENCE OF EVENTS FOR CONDITION rv* t:VErHS Accident Rupture of main feedwater pipe SGS-UFSAR Event End of B lo\l<<iown Bottom of core recovery Accurn ... lators empty P1J11p injection

£nd of bypass Feedline rupture occurs

  • High pressure reactor trip setpoint reached (This trip was not considered in the analysis).

Affected steam generate'.

liquid discharge; low level coincident with feed/steam flow mismatch in other steam generators; Time( Seconds) J0.46 42.5 53.64 26.03 27.51 o.oo 11.0 reactor trip setpoi nts reached. 18. 5 Reactor trip occurs 20. 5 Peak steam relief from pressurizer safety valves Pressurizer fills Bulk boiliny oegins in reactor cool ant fluid 22.5 527 876 Re vision 0 July 22, 1982 TABLE 15.4-1 (Sheet 3 of 3) TIME SEQUENCE OF EVENTS FOR CONDITION IV EVENTS Accident Event Time (Seconds)

Core decay heat decreases to auxiliary feedwater heat removal capacity 2100 Major Secondary System Pipe Rupture

1. Case a Steam line ruptures 0 Criticality attained 40 Pressurizer empty 13 2,000 ppm boron reaches loops 27
  • 2 . Case b Steam line ruptures 0 Criticality attained 24 Pressurizer empty 13 2,000 ppm boron reaches loops 27 3. Case C Steam line ruptures 0 Criticality attained 49 Pressurizer empty 14 2,000 ppm boron reaches loops 33 4. Case d Steam line ruptures 0 Criticality attained 28 Pressurizer empty 15 2,000 ppm boron reaches loops 34 8920Q:l0/070885 CORC: PARAf'ETERS USED IN ST£AM BREAK DNB ANALYSIS Case a Time Point Parameter 2 3 5 Unit 1 Unit 2 Unit 1 Unit 2 Unit 1 Unit 2 Reactor Vessel inlet temperature to sector connected to affected steam generator

°F 454.8 443.2 220.1 421.9 405.2 406.9 392.8 396.8 Reactor Vessel inlet temperature to re-mai ni ng sector 497.4 495.3 494.3 49

  • 493.0 483.2 485.5 468.0 473.8 RCS pressure, psi a 869.5 868.6 649.1 796.7 693.1 702.4 578.0 597.4 RCS fl ow, 100 100 100 100 100 100 100 100 100 Heat flu . 6.18 6.76 6.63 8.28 6.99 8.14 6.83 7.39 6.43 6.32 25 30 32.5 34.5 47.5 45.5 70 67.5 97.5 92.5 SGS-UFSAR i ..... Revision O Jul v 22, 1982
  • TABL£ 15. (Sheet 2 of 3) 15* 4.7 CORE PARAftE T£ RS USED IN ST£AM BR£AK DNB ANALYSIS Case b Time Point Parameter 2 . 3 Unit2 Unit 1 Unit 2 Unit 1 Reactor Vessel inlet temperature to sector connected to affected steam generator

°F 391.4 386.7 348.7 372.5 340.l Reactor Vessel inlet temperature to re-maining sector °F 526.8 518.8 516.4 512.0 451.0 RCS pressure, psi a 1098.8 898.9 879.9 573.9 523.8 RCS flow, 100 100 100 100 100 100 1 8.22 9.57 B.37 12.45 9.65 11.65 8.46 25 27.5 35 37 80 41.5 100 SGS-UFSAR I ..... 4 367.7 505.3 795.5 100 1 58 49.5 5 Unit 1 Unit 2 328.6 358.4 427.8 488.7 487.9 644.4 100 100 7.75 12.02 2.5 70 Revision 0 .Julv 22. 1982

  • '°DE:..LEIE.. -r P--\3 L \ S°
  • L\* -7 TABLE 15. -(Sheet 3 of J) CORi USl:D IN ST£AM BR£AK DNB ANALYSIS Case d, Time Point Parameter 2 3 4 5 Unit 1 Unit 2 Unit 1 Unit 1 Unit 2 Unit 1 Unit 2. Reactor Vessel inlet temperature to sector connected to affected steam generator

°F 390.5 375.5 356.6 345.5 322.1 312.1 303.2 281.5 284.3 Reactor Vessel inlet temperature to re-maining sector °F 530.2 528.9 529.2 528.0 527.5

  • 524.5 526.8 RCS pressure, psi a 1469.3 1359.l 1264.8 1270.4 998.3 >377. 5 891 RCS flow, 47 40.6 33.9 32.3 30.7 24 .* 9 22. 20.9 17.0 Heat fl ' 5.27 5.8 6.10 6.74 6.2 7.87 4.52 3.59 3.58 ime (sec) 20 25 32.5 35 37.5 50.5 57.5 65 8
  • 85 SGS-IJFSAR
  • 1* ... Revision 0 .1111 v n. 1982

-* TABLE 15.4-8 REACTOR COOLANT EQUILIBRIUM FISSION AND CORROSION PRODUCT ACTIVITIES (BASED ON PARAMETERS GIVEN IN TABLE Activity Isotope µ.C/CC Isotope Br-84 3.34 x 10-2 CS-136 Rb-88 2.66 Cs-137 Rb-89 6.74 x Cs-138 3.18x 10-Ba-140 Sr-90 7 .88 x 10-5 La-140 Sr-91 1.42 x 10-3 Ce-144 . Sr-92 5.97 x 10-4 Pr-144 Y-90 1.05 .x 10-4 Kr-85 Y-91 5.83*x 10-3 Kr-85m Y-92 7.68 x 10-4 Kr-87 Zr-95 6.66 x 10-4 Kr-88 Nb-95 6.57 x 10-4 Xe-133 Mo-99 2.36 Xe-133m I-131 1.87 Xe-135 I-132 .657 Xe-135m I-133 2.89 Xe-138 I-134 .376 Mn-54 I-135 1.46 Mn-56 Te-132 .208 Co-58 Te-134 2.04 x 10-2 Co-60 Cx-134 .142 Fe-59 SGS-UFSAR 11.1-7) Activity µ.C/CC 2.93 x 10-2 .859 .670 3.24 x 10-3 1.27 x 10-3 3.88 x 10-4 3.88 x 10-4 3.93 1. 70 .942 2.66 194.7 2.09 5.45 .132 .*468 5.87 x 10-4 2.20 x 10-2 1.89 x 10-2 5. 67 x 10-4 7 .87 x 10-4 Revision O July 22, 1982 .

  • *
  • TABLE 15.4-9 ATMOSPHERIC DISPERSION FACTORS AND BREATHING RATES Distance, m Atmospheric Df spersfon Factors, X/Q (sec/m 3) 1270 8052 Time Perf od, hr a -a 8 -24 24 -720 SGS-UFSAR 1785Q:l a -2 hrs 2 -24 hrs 1 .. 5 days 5.0 x 10-4 2.5 x 10-4 4.25 x 10-6 4.0 x 10-5 2.0 x 10-5 Breathing Rates, m /sec 3.47 x io-4 1.75 x 10 -4 2.32 x 10-4 5 -30 days 2.53 x 10-6 9.6 x 10-8 Revis ion l 22, 1983 14202.3 1.04 1.03 :.: . a: I .02 0 .... u < IL z I .0 I 0 ..... .... < u ..... _J 1.00 a. * ..... t-_J :::> ::i 0.99 0.98

.......

200 250 300 350 400 450 500 550 CORE AVERAGE TEMPERATURE

(*F) PUBLIC SERVICE ELECTRIC AND GAS COMPANY Variation of KEFF with Core Temperature SALEM NUCLEAR GENERATING STATION

  • Updated FSAR Figure 15.4-48
  • -:E u Q.. -I-z UJ -u -LL. LL. UJ 0 u a: D..
  • LL 0 _J < a: (!) LL.I I-z --2000 ------------------------------------------------------------, -1000 .* I I I I 0 lt-------...J....--------1...._

____ -'-____ _. _____________ 14202.4 0 0. 10 0.20 0.30 0.40 0.50 0.60 POWER (FRACTION OF 3423 MWt) PUBLIC SERVICE ELECTRIC AND GAS COMPANY SALEM NUCLEAR GENERATING STATION Variation of Reactivity with Power at Constant Core Average Temperature Updated FSAR Figure 15.4-49 14202.5 600 550 !! 500 UJ 450 < UJ 400 c UJ-13 350 u 300 250 2500 2250 Pressurizer Empties at 13 Sec 2000 ffi -Ul 1750 UJ -1500 a: Ul

  • a.. a.. 1250 en 1000 750 500 0 100 200 300 400 500 600 TIME (SEC} Transient Response to Steam Line Break Downstream PUBLIC SERVICE ELECTRIC AND GAS COMPANY of Flow Measuring Nozzle with Safety SALEM NUCLEAR GENERATING STATION Injection nnd Offsite Power (Ccise al
  • Updated FSAR Figure 15.4-50A 14202.6 3.500 3.000 -2.500 ..J 2.000 IL Faulted Steam Generator Only :::E 1.500 < u UJ < 1.000 I-er. U) IL 0.500 0 0.250 0.200 ..J :::E IL 0 z I-IL 0.150 <o 0.100 UJ < er. er. 0 IL 0.050 u-0 0 100 200 300 400 500 600 2500 2000 2,000 PPM Boron Reaches Loops at 27 Sec. > 1000 .... .... _ > :::E j:: 0 UJ -1000 er. -2000 -2500 0 100 200 300 400 500 600 700 TIME (SEC) PUBLIC SERVICE ELECTRIC AND GAS COMPANY SALEM NUCLEAR GENERATING STATION Transient Response to Steam Line Break Downstream of Flow Measuring Nozzle with Safety Injection and Offsite Power (Case a) Updated FSAR Figure 15.4-508 14202.7 600 550 c.. ::::E 500 Ll..I ..,._ LL. 450 Ll..I > (!) < Ll..I 400 0 1.1..1-a: 350 0 u 300 250 2500 2250
  • Ll..I 2000 Pressurizer Empties at 13 Sec. a: :::> (/) -1750 (/) < 1.1..1-a: (/) 1500 a.. a.. (/) 1250 u 1000 a: 750 500 0 100 200 300 400 500 600 TIME (SEC) Transient Response to Steam Line Break at Exit PUBLIC SERVICE ELECTRIC AND GAS COMPANY of Steam Generator with SafetY Injection and SALEM NUCLEAR GENERATING STATION Offsite Power (Case bl
  • Updated FSAR figure 15.4.51A 14202.8
  • 3.500 3.000 2.500 -' z LLLL 2.000 :I 0 1.500 <u UJ < I-a: I .000 Ul LL 0.500 0 0.250 X ,_ 0.200 ::> :::E o. 150 I-LL <o 0. 100 UJ < !5 IE 0.500 u-0
  • 2500 2000 -2,000 PPM Boron Reaches Loops at 27 Sec. >-1000 I-..... .... --> :::E -u 0 -I-a. f -1000 -2000 --2500 I I 0 100 200 PUBLIC SERVICE ELECTRIC AND GAS COMPANY SALEM NUCLEAR GENERATING STATION I I r 300 400 500 600 TIME (SEC} Transient Response to Steam Line Break at Exit of Steam Generator with Safetv Injection and Ofhite Power (Case b) Updated FSAR Figure 15.4.518 14202.9
  • 600 550 -500 UJ ......... 450 C!) 400 ---350 ---0 u 300 -250 2500 2250 UJ 2000 s Ul ..... 1750 (/) < Pressurizer Empties at 14 Sec. UJ ... 1500 IE If (/) 1250 1000 750 500 0 100 200 300 400 500 600 TIME (SEC} Transient Response to Steam Line Break Downstream PUBLIC SERVICE ELECTRIC AND GAS COMPANY of Flow Measuring Nozzle with Safety Injection, SALEM NUCLEAR GENERATING STATION Without Offsite Power (Case c) Updated FSAR Figure 15.4-52A 14202.10 3.500 3.000 2.500 _J z 2.000 IL :::E 1.500 <u UJ < I-a: 1.000 Ul IL 0.500 0 0.250 0.200 0.150 !i! u 0.100 UJ < 25 fE 0.500 u-* 0 2500 2000 2,000 PPM Boron Reaches Loops at 33 Sec. >-1000 I-. ........ 0 I-a.. UJ -1000 a: -2000 -2500 0 100 200 300 400 500 600 TIME (SEC) Transient Response to Steam Line Break Downstream PUBLIC SERVICE ELECTRIC AND GAS COMPANY of Flow Measuring Nozzle with Safety Injection, SALEM NUCLEAR GENERATING STATION Without Offsite Power (Cue c)
  • Updated FSAR Figure 15.4-528 14202. 11
  • 600 550 500 UJ 450 LIJ (!) > UJ 400 "'c 350 u 300 250 2500 2250 Pressurizer Empties at 15 Sec. UJ 2000 s Ul _.. 1750
  • Ul < UJ -1500 a:: Ul !l.. D.. 1250 Ul u 1000 a:: 750 500 0 100 200 PUBLIC SERVICE ELECTRIC AND GAS COMPANY SALEM NUCLEAR GENERATING STATION 300 400 500 600 TIME (SEC) Transient Response to Steam Line Break at Exit of Steam Generator With Safety Injection and Without Offsite Power (Case di Updated FSAR Figure 15.4-53A h202.12
  • 3.500 3.000 E5 2.500 _J z i.. i.. 2.000 :::Eo 1.500 <u UJ < t-a:: 1.000 Ill i.. 0.500 0 0.250 x ..... 0.200 :::::> :::E _J 0 i.. z o. 150 I-i.. :I: u 0. 100 UJ < a:: a:: 0 i.. 0.500 u-a 2500 2000 2,000 PPM Boron Reaches Loops at 34 Sec. >-1000 I--> ...... -:::E I-u 0 u a.. <--1000 -2000 -2500 0 100 200 PUBLIC SERVICE ELECTRIC AND GAS COMPANY SALEM NUCLEAR GENERATING STATION 300 400 500 600 TIME (SEC) Transient Response to Steam Line Break at Exit of Steam Generator With Safety Injection and Without Offsite Power (Case d) Updated FSAR Figure 15.4-53B )

14202.13 ,

  • 500 400 -Case A 300 ..... 200 ..... 100 ..__ 0 500 400 -Case 8 300 .._ ! 200 .._ I ::E r Cl. Cl. 100 ..... z 0 0 a: 0 soo aJ IJJ 400 Case C a: -0 u 300 * -200 .._ 100 -0 500 400 -Case D 300 -*200 -100 -I I I I 0 0 100 200 300 400 500 600 TIME (SEC) PUBLIC SERVICE ELECTRIC AND GAS COMPANY Integrated Flow Rate of Borated Water versus Time SALEM NUCLEAR GENERATING STATION Updated FSAR Figure 15.4*54
  • 1-:z: u.. 0 Q. 2i I-600 500 3000 ...J en g 2000 <.) 0 2.5 0 u.I <.) ex !:. -2. 5 E ] PRESSURIZER EM FTI ES AT 1 SEC INITIAL STEAM FLOW IS 11261 L SEC FROM FAULTED STEAM GENERATOR 2983 LBS/SEC FROM INTACT STEAM !ENERArO S) STEAM GEHERATOR ONLY 20.000 PPM BOROll REACHES 0 25 50 75 I 00 I 25 I 50 TIME (SECONDS) E:.. L \:: . .'TE. PUBLIC SERVICE ELECTRIC AND GAS COMPANY SALEM NUCLEAR GENERATING STATION Transient Response to Steam Line Break at Exit of Steam Generator with Safety Injection and Offsite Power (Case b)
  • Unit 2 / 0 ' 1982 Updated FSAR Fi9WF8 1 li.4 56

.\ w 3000 a:: :::i en a:: en I PRESSURIZER EMPTIES AT 19 SEC

  • 2000 u Q,, -c -en w I-Q,,

1000 ....I 0 0 u 1-....I % ><O II ....I :::i % w ....I en ao Q. WO I-.....1-w w % a: u.. ::w 0 u %

a:w 0 Q,, I-w u-cnu a: w Q,, 0 600 500 2.5 2.0 I. 5 1.0 -2.5 0 INITIAL STEAM FLOW IS I I 53 LBS/SEC FROM FAULTED STEAM GENERATO (ANO 29BL4 LBS/ SEC FROM INTACT STEAM G ERATORS) 20.000 PPM BORON REACHES LOOPS AT 35 S 25 50 75 I 00 125 I SO 175 TIME (SECOHOS)

DE.. LE:.IE. u fL.E PUBLIC SERVICE ELECTRIC AND GAS COMPANY SALEM NUCLEAR GENERATING STATION Transient Response to Steam Line Break at Exit of Steam Generator With Safety Injection and Without Offsite Power (Case d) -Unit 1 Updated FSAR Jiii9wre 15 4 5S
  • I-z: Cit ...J -0 w 0 QC <..:> :::::> Cit en en en w Q.. ex Q.. w ex 0 I-<..:> ""' I-I.I.I z: ar::: ""' ...J 0 0 <..:> <..:> ...J w """ en z: -en % CZ) ><0 ...J :::::> :z: I.I.I ...J ""' (') 0 WO I-...J -
w 0 <..:> % war:: Cit I-QCW wz OQ.. 1-W <..:>-en<..:>

C¥ I.I.I Q.. """ -""" > <J I-I-z: <..:> u.i ""' <..:> I.I.I QC ex w Q.. 3000 2000 I 000 3.0 2.5 2.0 I. 5 0.5 0 2.5 0 -2.5 PRESSURIZER EMPTIES AT 19 SEC FL i S 11 261 LBS/ SEC FROM HERATOR (AN02983 LB/SEC EAM GENERA TORS) __ ..._ ___ _ 20.000 PPM BORON REACHES LOOPS AT 0 25 50 75 I 00 I 2 5 I 50 I 7 5 TIME (SECONDS)

PUBLIC SERVICE ELECTRIC AND GAS COMPANY SALEM NUCLEAR GENERATING STATION Transient Response to Steam Line Break at Exit of Steam Generator With Safety Injection and Without Offsite Power (Case. d) . Unit 2 Updated FSAR T-i91.1r11

'5 a.'iL

  • 30.000 20,000 CASE A 10.000 0 en ao ...J -IX w I-""" Q 30. 000 w I-""" 20.000 IX 0 ao u.. 0 10,000 w I-* 0 IX 0 ...J u.. Q 10.000 w I-5,000 ai:: C!3 w I-:z: 0 CASE D
  • PUBLIC SERVICE ELECTRIC AND GAS COMPANY SALEM NUCLEAR GENERATING STATION --------------100 TIME (SECONDS) 200 Revi si o July 22, Integrated Flow Rate of Borated Water versus Time
  • Unit 1 I 0 982 Updated FSAR l5 4-5.8._. . I I -I I
  • 140.000 "' ca -50.000 a: UJ ..... -c 311: 0 w 30.000 ..... '4 a: 0 ca 20. 000 I.&.. 0 UJ ..... 10.000 -c a: 311: 0 0 ""-0 w 10.000 I--c a: C::J 5.000 I-:z: CASE D 0 0 so "°3) E.. L E I E.. 1 PUBLIC SERVICE ELECTRIC AND GAS C9MPANY SALEM NUCLEAR GENERATING STATION 100 150 TIME (SECOHOS)

Integrated Flow Rate of Borated Water versus T,ime -Unit 2 Updated FSAR figa1e HU-58 .

  • * * (';) 1'. C> ,. "fl "P 0 r {ii 0 > I -\ c -\ l. -0 )' (l (ii >-fl l -l (/'I (i1 -> l. ()t I i., (Ta -l > -l > 'T1 z.. VI r. .l> 'fl tJ r {It -\ "" > () -ii3 ,, (i\ L r r* ""\) 00 ,. (j' V\ t I (..) 0 :t I -l 11'* w -\ IT1 r (/t
  • *** TABLE 6. 3-3 BORON INJECTION DESIGN PARAMETERS Number Total volume, gal (also useable volume) BereA eaAEeRtratigR NomiAal, ppm MaximYm, ppm Mi Ai mi:.m, ppm Design pressure, psig -Design temperature, °F Material Code Ty19e SGS-UFSAR llEATERS l 900 21,000 22,§00 20,000 2735 150-180 SS Clad Carbon Steel ASME III Class C Revision 0 July 22,

.S. At.E.M -r L..E \S*\-2. SU 1"\M C \: \ N \I 1 A. L.. C:.. c iJ .0 N ..S c t'\

c:.. 0 .n E. .s lJ .s. *. 0

  • FAULTS CONDIT ION I I Uncontrolled RCC assembly Bank Withdrawal from a Subcritical Condition*

Uncontrolled RCC Assembly.Bank Withdrawal at Power RCC Assembly Misalignment Uncontrolled Boron Dilution Partial Loss of Forced Reactor Coolant Flow Start-up of an Inactive Reactor Coolant Loop Loss of External Electrical Load and/or Turbine Trip Loss of Nonnal Feedwater Loss of Off-Site Power to the Plant Auxiliaries (Plant Blackout)

  • TABLE 15.1-2 (Sheet l of 4)

SUMMARY

Of INITIAL CONDITIONS AND COMPUTER_

CODES USED COMPUTER CODES UTILIZED WIT-6 .* FACTRAN LOFTRAN THINC, TURTLE, LOFTRAN NA PHOENIX, LOFTRAN THINC, FACTRAN MARVEL, THINC LOFT RAN BLKOUT BLKOUT REACTIVITY COEFFICIENTS ASSUMED MODERATOR(l)

MODERATOR(l)

TEMPERATURE (tik/"Fl NA DENSITY (tiK/gm/cc) 0 and 0.43 0 NA 0 0.43 0 and D.43 NA NA DOPPLER(Z)

Lower lower and upper upper NA upper lower upper NA NA INITIAL NSSS THERMAL POWER OUTPUT ASSUMED (MWT) 0 3423 3423 O and 3423 2396 and 3423 2369 3423 3577 3423 Revision 0 lulu ?? lQA?

  • CONDITION.

11 (cont\nued)

Excessive Heat Removal Due to Feedwater System Malfunctions Excesslve Load Increase Accident Depressur\zatton of the Reactor Coolant System Accident Depressurizat\on of the Main Steam System / Inadvertent Operat\on of ECCS Durtng Power Operatton CONDITION 111 Loss of Reactor Coolant from Small Ruptured Pipes or from Cracks tn Large Ptpe which Actuate Emergency Core Coo 11 ng nn'lnn. 1 n 1n-,noos::

TABLE 15.1-2 !Shoot 2

SUMMARY

OF INITIAL CONDITIONS AND COMPUTER CODES USED COMPUTER CODES UTILIZED MARVEL LOFT RAN LOFTRAN LOFTRAN LOFTRAN REACTIVITY COEFFICIENTS ASSUMED MODERATOR(l)

MODERATOR(l)

TEMPERATURE (6K/*f) DENSITY (AK/gm/cc) 0.43 0 and 0.43 0 Functton of Mod-era tor Dens tty See Sec. 15.2.13 (Fig. 15.2.41) 0 WFLASH, LOCTA-R2 . DOPPLER(2) lower lower upper Fig. 15.4-49 lower INITIAL NSSS THERMAL POWER OUTPUT ASSUMED (Mwt) O and 3423 3423 3423 0 (Subcr1ttca1) 3423 3511

  • TABLE 15.1-2 (Sheet 3 OF INITIAL CONDITIONS AND COMPUTER CODES USED CONDITION Ill (continued)

Inadvertent Loading of a Fuel Assembly into an Improper Position Complete Loss of Forced Reactor Coolant Flow Waste Gas Decay Tank Rupture Single RCC Assembly Withdrawal at Full Power CONDITION IV COMPUTER CODES UTILIZED LEOPARD, TURTLE PHOENIX, LOFTRAN THINC, FACTRAN NA TURTLE, THINC LEOPARD Major rupture of pipes containing reactor SATAN coolant up to an including double-ended LOCTA-R2 rupture of the largest pipe in the Reactor Coolant System (loss of Coolant Accident)

Major secondary syste111 pipe rupture up to and including double ended rupture (Rupture of a Steam Pipe) 8920Q:lD/071185 LOFTRAN, THINC REACTIVITY COEFFICIENTS ASSUMED MODERATOR(l)

MODERATOR(l)

TEMPERATURE (1Ut/9F) Function of Moderator

  • density See Section 15.4.1 Function of Moderator Density See Sect ion 1 5. 2. 13 (Fig. 15 . 2-41 ) DENSITY (AK/gm/cc)

NA 0 NA NA* DOPPLER(2) NA upper NA NA Function of Fuel Temp. See Section 15 .4 .1 INITIAL N*sss THERMAL POWER OUTPUT ASSUMED (Mwt) . 3423 2391> and 3423 3571 3423 3579 Fig. 15.4-49 0 (Subcritical)

  • TABLE 15.1-2 (Sheet 4 of 4)

SUMMARY

OF INITIAL CONDITIONS AND COMPUTER CODES USED REACTIVITY COEFFICIENTS ASSUl"lD MODERATOR(!)

MODERATOR( l l COMPUTER TEMPERATURE DENSITY FAULTS CODES UTILIZED (11k/°Fl (11K/gm/cc)

CONDITION IV (cont'd) Steam Generator Tube Rupture NA NA NA Single Reactor Coolant Pump Locked PHOENIX, LOFTRAN 0 Rotor THINC, FACTRAN Fuel Handling Accident NA NA NA Rupture of a Control Rod Mechanism TWINKLE, FACTRAN -1 pcm/°E BOL Housing (RCCA Ejection)

LEOPARD -26 pcmrF EOL NOTES: (ll Only one is used fn an analysis i.e. either moderator temperature or moderator density coefffcfent (2) Reference Figure 15.1-5 SGS-UFSAR DOPPLER(2) NA upper Consistent wf th lower lfmft shown Ffg. 15.1-5 INITIAL NSSS THERMAL POWER OUTPUT ASSUMED (MWTI 3577 2396 and 3423 3577 0 and 3423 Revision 0 h1lu ?? 10Q?