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REGULATOR'r INFORMATION DISTRIBUTION SYSTEM                         (RIDS)
REGULATOR'r INFORMATION DISTRIBUTION SYSTEM (RIDS)
'ACCESSION NB/       8009050167,                     DOC ~ DATE e 84/08/23       NOTARIZED!"'O           DOCKET ¹ FACIL:50 315 Donald                     C ~ Cook Nuclear     Power   Pl anti Unf t 1, Indiana-     8 05000315 AUTH ~ NAME   AUTHOR AFFILIATION ALEXICHiM~ P.             Indiana             L Michigan     Electric   Co.
'ACCESSION NB/ 8009050167, DOC ~ DATE e 84/08/23 NOTARIZED!"'O DOCKET ¹ FACIL:50 315 Donald C ~
RECIP, NAME                 RECIPIENT AFFILIATION SUBJECT!     Application for amend to License OPR 58 revising Tech Specs to extend fuel peak pellet burnup L increase FQ value limit in fuels     Fee             paido Qs~ fly&
Cook Nuclear Power Pl anti Unf t 1, Indiana-8 05000315 AUTH~ NAME AUTHOR AFFILIATION ALEXICHiM~ P.
DISTRIBUTION CODE: A001D                         COPIES .RECEIVED:LTR g'         ENCL     SIZE:~ 3 TITLE:   OR   Submittal! General Distribution NayES   .P>< P4f     ~
Indiana L Michigan Electric Co.
get   oc                                                   05000315 OL i 1 0/25/74,',.                                                                                 >>
RECIP, NAME RECIPIENT AFFILIATION 05000315 SUBJECT! Application for amend to License OPR 58 revising Tech Specs to extend fuel peak pellet burnup L increase FQ value limit in fuels Fee paido DISTRIBUTION CODE:
REC I'P-I:.EN,T                   COPIES              RECIPIENT            COPIES ID COOg/NAME                         LTTR ENCL          ID CODE/NAME          LTTR ENCL>>
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NRR ORBi BC                     01       7      7 INTERNAL: ADM/LFMB                                     1      0      ELO/HDS3.                1      0 NRR/DE/MTEB                               1      1      NRR/DL DIR                1    '1 NRR/OL/ORAB                               1    *0      N        -  4ETB        1      1 NRR/OS   I/RAB                           1-     1         EG FI   E       00     1     1 ~
TITLE:
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INDIANA & MICHIGAN ELECTRIC COMPANY P.O. BOX 16631 COLUMBUS, OHIO 43216 August 23, 1984 AEP: NRC: 0745M Donald C. Cook Nuclear Plant Unit No.         1 Docket No. 50-315 License No. DPR-58 TECHNICAL SPECIFICATION CHANGE REQUESTS Mr. Harold R. Denton, Director Office of Nuclear Reactor Regulation U.S. Nuclear Regulatory Commission Washington, D. C. 20555
INDIANA& MICHIGAN ELECTRIC COMPANY P.O. BOX 16631 COLUMBUS, OHIO 43216 August 23, 1984 AEP: NRC: 0745M Donald C.
Cook Nuclear Plant Unit No.
1 Docket No. 50-315 License No. DPR-58 TECHNICAL SPECIFICATION CHANGE REQUESTS Mr. Harold R. Denton, Director Office of Nuclear Reactor Regulation U.S. Nuclear Regulatory Commission Washington, D.
C.
20555


==Dear Mr. Denton:==
==Dear Mr. Denton:==
 
By this letter and its attachments, we request changes to the Technical Specifications for the Donald C.
By this letter   and its   attachments,   we request changes to the Technical Specifications       for the   Donald C. Cook Nuclear Plant Unit No. 1. The proposed revised Technical Specification pages are contained in Attachment A. The reasons for the proposed changes to the Technical Specif'ications, and the Justifications that the changes do not involve significant hazards considerations,   are contained in Attachments B and C to this letter. The changes   described in Attachment B involve extending the peak pellet burnup in fuel supplied by Exxon Nuclear Company from 42,200 MWD/MTU (42.2 %0)/KG) to 48,000 MWD/MTU (48.0 MWD/KG). These changes are supported by a LOCA Analysis and additional information regarding mechanical design, which was sent to you directly by Exxon Nuclear Company with letter JCC:113:84, dated August 21, 1984. The current burnup limit is expected to be reached on November 30, 1984. Without this burnup extension, we would be unable to continue operation of Cycle 8 because   of the requirements of Technical Specification Section 3.2.2. The changes proposed in Attachment C and supported by Attachment D involve an increase in the F limit in fuel supplied by Westinghouse f'rom 1.97 to 2.10. It should be noted that part of this analysis is based on use of the BART code, which has not been previously used for the Donald C. Cook Nuclear Plant, Unit 1 ~
Cook Nuclear Plant Unit No.
1.
The proposed revised Technical Specification pages are contained in Attachment A.
The reasons for the proposed changes to the Technical Specif'ications, and the Justifications that the changes do not involve significant hazards considerations, are contained in Attachments B and C to this letter.
The changes described in Attachment B involve extending the peak pellet burnup in fuel supplied by Exxon Nuclear Company from 42,200 MWD/MTU (42.2 %0)/KG) to 48,000 MWD/MTU (48.0 MWD/KG).
These changes are supported by a LOCA Analysis and additional information regarding mechanical
: design, which was sent to you directly by Exxon Nuclear Company with letter JCC:113:84, dated August 21, 1984.
The current burnup limit is expected to be reached on November 30, 1984.
Without this burnup extension, we would be unable to continue operation of Cycle 8
because of the requirements of Technical Specification Section 3.2.2.
The changes proposed in Attachment C and supported by Attachment D involve an increase in the F limit in fuel supplied by Westinghouse f'rom 1.97 to 2.10. It should be noted that part of this analysis is based on use of the BART code, which has not been previously used for the Donald C.
Cook Nuclear Plant, Unit 1 ~
These proposed changes have been reviewed by the Plant Nuolear Safety Review Committee (PNSRC) and will be reviewed by the Nuclear Safety and Design Review Committee (NSDRC) at their next regularly scheduled meeting.
These proposed changes have been reviewed by the Plant Nuolear Safety Review Committee (PNSRC) and will be reviewed by the Nuclear Safety and Design Review Committee (NSDRC) at their next regularly scheduled meeting.
In compliance with the requirements of 10 CFR 50.91(b)(1), a copy of'his letter and its attachments have been transmitted to Mr. R. C. Callen of the Michigan Public Service Commission.
In compliance with the requirements of 10 CFR 50.91(b)(1),
8409050167 840823 PDR ADOCK F'
a copy of'his letter and its attachments have been transmitted to Mr. R.
050003l5
C. Callen of the Michigan Public Service Commission.
            .        PDR
8409050167 840823 PDR ADOCK 050003l5 F'
PDR


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Mr. Harold R. Denton                               AEP: NRC: 0745M Pursuant to 10 CFR 170.12, we have enclosed a check in the amount of $ 150.00 as payment for the application fee for the proposed amount.
Mr. Harold R. Denton AEP: NRC: 0745M Pursuant to 10 CFR 170.12, we have enclosed a check in the amount of $150.00 as payment for the application fee for the proposed amount.
This document has been prepared following Corporate procedures which incorporate a reasonable set of controls to insure its accuracy and completeness prior to signature by the undersigned.
This document has been prepared following Corporate procedures which incorporate a reasonable set of controls to insure its accuracy and completeness prior to signature by the undersigned.
Very truly yours, M   . Ale ich Vice Preeidect
Very truly yours, M
. Ale ich Vice Preeidect


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Mr. Harold R. Denton                 ~ \3             AEP: NRC:0745M Attachments:   A. Proposed Revised Technical Specifications Pages for D.C. Cook Unit 1.
Mr. Harold R. Denton
B. Reasons   for the extension of the   peak pellet burnup allowed in fuel supplied by Exxon Nuclear Company and Justification that the changes do not involve significant hazards considerations.
~\\3 AEP: NRC:0745M Attachments:
C. Reasons for the increase in     F~ for fuel supplied by Westinghouse.
A.
D.   "D.C. Cook Unit 1 3411 MWt Large Break LOCA Analysis", Westinghouse Electric Corporation, June,   1984.
Proposed Revised Technical Specifications Pages for D.C.
cc: John E. Dolan W. G. Smith, Jr. - Bridgman R. C. Callen G. Charnoff E. R. Swanson, NRC Resident Inspector   - Bridgman
Cook Unit 1.
B.
Reasons for the extension of the peak pellet burnup allowed in fuel supplied by Exxon Nuclear Company and Justification that the changes do not involve significant hazards considerations.
C.
Reasons for the increase in F~ for fuel supplied by Westinghouse.
D.
"D.C. Cook Unit 1 3411 MWt Large Break LOCA Analysis", Westinghouse Electric Corporation,
: June, 1984.
cc: John E. Dolan W. G. Smith, Jr. - Bridgman R.
C. Callen G. Charnoff E.
R. Swanson, NRC Resident Inspector - Bridgman


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Mr. Harold R. Denton                             AEP: NRC: 0745M Attachment D "D.C. Cook Unit 1 3411 MWt Large Break LOCA Analysis",
Mr. Harold R. Denton AEP: NRC: 0745M Attachment D
Westinghouse Electric Corporation, June, 1983.>>
"D.C. Cook Unit 1 3411 MWt Large Break LOCA Analysis",
    'This document has been piepared by Westinghouse Electric Corporation in a format foi eventual inclusion in the Donald C; Cook Nuolear Plant FSAR. Although this is ~o intended for that purpose at this time, the format has been retained for convenience.
Westinghouse Electric Corporation,
: June, 1983.>>
'This document has been piepared by Westinghouse Electric Corporation in a format foi eventual inclusion in the Donald C; Cook Nuolear Plant FSAR.
Although this is ~o intended for that purpose at this time, the format has been retained for convenience.


14.3.1.1   Major LOCA Analyses Applicable to Westinghouse       Fuel Identification of   Causes and Fre uenc   Classification
14.3.1.1 Major LOCA Analyses Applicable to Westinghouse Fuel Identification of Causes and Fre uenc Classification
-A loss-of-coolant accident   (LOCA) is the result of   a pipe rupture of the RCS pressure boundary. For the analyses     reported here, a major pipe break ( large break) is defined as a rupture with a total cross-sectional area equal to or greater than 1.0 ft . This event is considered an 2
-A loss-of-coolant accident (LOCA) is the result of a pipe rupture of the RCS pressure boundary.
ANS Condition IV event, a,limiting fault, in that       it   is not expected to occur during the lifetime of D. C. Cook Unit 1, but is postulated as a conservative design basis.
For the analyses reported
The Acceptance Criteria for the   LOCA are described   in 10 CFR   50.46 (30 CFR 50.46 and Aopendix K of     10 CFR 50   1974)   as   follows:
: here, a major pipe break
: 1. The calculated peak fuel element clad temperature       is below the requirement of 2,200'F.
( large break) is defined as a rupture with a total cross-sectional area equal to or greater than 1.0 ft This event is considered an 2
2,   The amount   of fuel element cladding that reac;s chemically with water or steam does not exceed 1 percent of:he total amount of 2ircaloy in the reac or.
ANS Condition IV event, a,limiting fault, in that it is not expected to occur during the lifetime of D.
: 3. The clad temoerature transient is terminated at a time when the core aeometry is still amenable to cooling. The locali-ed cladding oxidation limit of 17 percent is not exceeded d ring or af er quenching.
C.
: 4. The core remains amenable to cooling during and       after   :he break.
Cook Unit 1, but is postulated as a
: 5. The core temperature is reduced and decay heat is removed for an         'I period of time, as required by he long-lived "radioactivity".     '''..'xtended remaining in the core.
conservative design basis.
The Acceptance Criteria for the LOCA are described in 10 CFR 50.46 (30 CFR 50.46 and Aopendix K of 10 CFR 50 1974) as follows:
1.
The calculated peak fuel element clad temperature is below the requirement of 2,200'F.
2, The amount of fuel element cladding that reac;s chemically with water or steam does not exceed 1 percent of:he total amount of 2ircaloy in the reac or.
3.
The clad temoerature transient is terminated at a time when the core aeometry is still amenable to cooling.
The locali-ed cladding oxidation limit of 17 percent is not exceeded d ring or af er quenching.
4.
The core remains amenable to cooling during and after :he break.
5.
The core temperature is reduced and decay heat is removed for an
'I
'''..'xtended period of time, as required by he long-lived "radioactivity".
remaining in the core.


These   criteria   were established   to provide significant margin in emergency core cooling system (ECCS) performance         following   a LOCA.
These criteria were established to provide significant margin in emergency core cooling system (ECCS) performance following a LOCA.
WASH-1400 (USNRC 1975)           presents a recent study in regards to the probability of occurrence of RCS pipe ruptures.
WASH-1400 (USNRC 1975) presents a recent study in regards to the probability of occurrence of RCS pipe ruptures.
Se uence   of Events and S stems 0   erations Should   a major break occur, depressurizaton of the RCS results in a pressure decrease in the pressurizer.         The reactor trip signal subsequently occurs when the pressurizer low pressure trip setpoint is reached'. A safety injection signal is generated wnen the appropriate setpoint is reached. These countermeasures will limit the consequences of the accident in two ways:
Se uence of Events and S stems 0 erations Should a major break occur, depressurizaton of the RCS results in a pressure decrease in the pressurizer.
: 1. Reactor trip and borated water injection supplement void formation in causing rapid reduction of power to a residual level corresponding to fission product decay heat. However, no credit is taken in the LOCA analysis for the boron content of the injection water. In addition, the insertion of contr".'. rods to shut down the reactor is neglected in the large break analysis.
The reactor trip signal subsequently occurs when the pressurizer low pressure trip setpoint is reached'.
: 2. Injection of borated water provides for heat transfer         rrom the core and   prevents excessive clad temperatures.
A safety injection signal is generated wnen the appropriate setpoint is reached.
Oescr ation of Large Break Loss-of-Coolant Accident Transient The sequence     of events following     a large break LOCA is p".esen ed in Table 14. 3. 1-6.
These countermeasures will limit the consequences of the accident in two ways:
1.
Reactor trip and borated water injection supplement void formation in causing rapid reduction of power to a residual level corresponding to fission product decay heat.
: However, no credit is taken in the LOCA analysis for the boron content of the injection water.
In addition, the insertion of contr".'.
rods to shut down the reactor is neglected in the large break analysis.
2.
Injection of borated water provides for heat transfer rrom the core and prevents excessive clad temperatures.
Oescr ation of Large Break Loss-of-Coolant Accident Transient The sequence of events following a large break LOCA is p".esen ed in Table
: 14. 3. 1-6.


Before the break occurs, the unit is in an equilibrium condition; that is, the heat generated in the core is being removed via the secondary system. Ouring blowdown, heat from fission product decay', hot internals and the vessel, continues to be transferred to the reactor coolant.       At the beginning of the blowdown phase, the entire RCS contains subcooled liquid which transfers heat from the core by forced convection with some fully developed nucleate boiling. After the break develops, the time to departure from nucleate boiling is calculated, consistent with (1)
Before the break occurs, the unit is in an equilibrium condition; that is, the heat generated in the core is being removed via the secondary system.
Appendix K of 10 CFR 50.( 'hereafter the core heat transfer is unstable, with both nucleate boiling and film boiling occurring. As the core becomes uncovered, both turbulent and laminar forced convection and radiation are considered as core heat transfer mechanisms.
Ouring blowdown, heat from fission product decay',
The   heat transfer between the RCS and the secondary system may be in either direction, depending on the relative temperatures.       In the case of continued heat addition to the secondary system, the secondary system pressure increases and the main steam safety valves may actuate to limit the pressure.     makeup water to the secondary side is automatically provided by the emergency feedwater .system. The safety injection signal ac uates a feedwater isolation signal which isoiaies normal feedwater flow by closing the main feedwater isolation valves, and also initiates emergency feedwater flow by starting the emergency feedwater pumps.       The secondary   flow aids in the reduction of RCS pressure.
hot internals and the vessel, continues to be transferred to the reactor coolant.
'>)hen the RCS depressurizes to 600 psiz, the accumulators begin to inject borated water into the reactor coolant loops. The conservative assumption is made that accumulator water injec ed bypasses the core and goes out through the break until the termination of bypass.       This conservatism is again consistent with Appendix K of 10CFRSO. Since loss of offsite power (LOOP) is assumed, the RCPs are assumed to trip at the inception of'the accident. 'The e'ffects of'ump coastdown are i'nc'luded
At the beginning of the blowdown phase, the entire RCS contains subcooled liquid which transfers heat from the core by forced convection with some fully developed nucleate boiling.
'n     the blowdown analysis.
After the break develops, the time to departure from nucleate boiling is calculated, consistent with Appendix K of 10 CFR 50.( 'hereafter the core heat transfer is (1)
The blowdown phase     of the transient ends when the RCS pressure (initially assumed at 2280 psia) falls to a value approaching that of the containment atmosphere.     Prior to or at the end of the blowdown, the
: unstable, with both nucleate boiling and film boiling occurring.
As the core becomes uncovered, both turbulent and laminar forced convection and radiation are considered as core heat transfer mechanisms.
The heat transfer between the RCS and the secondary system may be in either direction, depending on the relative temperatures.
In the case of continued heat addition to the secondary
: system, the secondary system pressure increases and the main steam safety valves may actuate to limit the pressure.
makeup water to the secondary side is automatically provided by the emergency feedwater
.system.
The safety injection signal ac uates a feedwater isolation signal which isoiaies normal feedwater flow by closing the main feedwater isolation valves, and also initiates emergency feedwater flow by starting the emergency feedwater pumps.
The secondary flow aids in the reduction of RCS pressure.
'>)hen the RCS depressurizes to 600 psiz, the accumulators begin to inject borated water into the reactor coolant loops.
The conservative assumption is made that accumulator water injec ed bypasses the core and goes out through the break until the termination of bypass.
This conservatism is again consistent with Appendix K of 10CFRSO.
Since loss of offsite power (LOOP) is assumed, the RCPs are assumed to trip at the inception of'the accident.
'The e'ffects of'ump coastdown are i'nc'luded
'n the blowdown analysis.
The blowdown phase of the transient ends when the RCS pressure (initially assumed at 2280 psia) falls to a value approaching that of the containment atmosphere.
Prior to or at the end of the blowdown, the


mechanisms   that are responsible for the emergency core cooling water injected into the RCS bypassing the core are calculated not to be effective. At this time (called end-of-bypass) refill of the reactor vessel lower plenum begins. Refill is completed when emergency core cooling water has filled the lower plenum of the reactor vessel, which is bounded by the bottom of the fuel rods (called bottom of core recovery time).
mechanisms that are responsible for the emergency core cooling water injected into the RCS bypassing the core are calculated not to be effective.
The   reflood phase of the transient is defined as the time period lasting from the end-of-refill until the reactor vessel has been filled with water to the extent that the core temperature rise has been terminated.
At this time (called end-of-bypass) refill of the reactor vessel lower plenum begins.
From the latter stage of blowdown and then the beginning-of-reflood, the safety injection accumulator tanks rapidly discharge borated cooling water into the RCS, contributing to the filling of the reactor vessel downcomer. The downcomer wa'ter elevation head provides the driving force required for the reflooding of the reactor core. The low head and high head safety injec ion pumps aid in the filling of the downcomer and subsequently   supply water to maintain     a full downcomer and complete the reflooding process.
Refill is completed when emergency core cooling water has filled the lower plenum of the reactor vessel, which is bounded by the bottom of the fuel rods (called bottom of core recovery time).
Cont'inued operation of the     ECCS   pumps supplies wa er during longterm cooling. Core temperatures have been reduced to longterm steady state levels associated with dissipation of residual heat generation. After tne water level of the residual water s orage tank (RWST) reaches a minim m allowable value, coolant for long-tern cooling of the core is obtained by switching to the cold recirculation phase of opera ion, in which spilled borated wa er is drawn from the engineered safety ea ures (ESF) containment sumps by the low head safety injection (residual heat removal) pumps and returned to the RCS cold legs. The containment spray system continues to operate to further reduce containment pressure.
The reflood phase of the transient is defined as the time period lasting from the end-of-refill until the reactor vessel has been filled with water to the extent that the core temperature rise has been terminated.
r r.
From the latter stage of blowdown and then the beginning-of-reflood, the safety injection accumulator tanks rapidly discharge borated cooling water into the RCS, contributing to the filling of the reactor vessel downcomer.
The downcomer wa'ter elevation head provides the driving force required for the reflooding of the reactor core.
The low head and high head safety injec ion pumps aid in the filling of the downcomer and subsequently supply water to maintain a full downcomer and complete the reflooding process.
Cont'inued operation of the ECCS pumps supplies wa er during longterm cooling.
Core temperatures have been reduced to longterm steady state levels associated with dissipation of residual heat generation.
After tne water level of the residual water s orage tank (RWST) reaches a
minim m allowable value, coolant for long-tern cooling of the core is obtained by switching to the cold recirculation phase of opera ion, in which spilled borated wa er is drawn from the engineered safety ea ures (ESF) containment sumps by the low head safety injection (residual heat removal) pumps and returned to the RCS cold legs.
The containment spray system continues to operate to further reduce containment pressure.
r r.
Approximately 24 hours 'after initiation of the LOCA, the ECCS is realigned to supply water to the RCS hot legs in order to control the boric acid concentra-ion in the reactor vessel.
Approximately 24 hours 'after initiation of the LOCA, the ECCS is realigned to supply water to the RCS hot legs in order to control the boric acid concentra-ion in the reactor vessel.


Core and   S stem performance Mathematical Model:
Core and S stem performance Mathematical Model:
The requirements of   an acceptable CCS evaluation model are presented     in of 10 CFR 50 (Federal Register 1974).
The requirements of an acceptable CCS evaluation model are presented in Appendix K of 10 CFR 50 (Federal Register 1974). (1)
(1)
Large Break LOCA Evaluation Model The analysis of a large break LOCA transient is divided into three phases:
Appendix  K Large Break   LOCA Evaluation Model The analysis of a large break LOCA transient is divided into three phases:   (1) blowdown, (2) refill, and (3) ref lood. There are three distinct transients analyzed in each phase, including the thermal-hydraulic transient in the RCS, the pressure and temperature transient within the containment, and the fuel and clad temperature transient of the hottest fuel rod in the core. Based on these considerations, a system of interrelated computer codes has been developed for the analysis of the LOCA.
(1) blowdown, (2) refill, and (3) ref lood.
A description of the various aspects of the       LOCA analysis methodology is given by Bordelon, Massie, and     2ordan ( 1974). (6)   Tnis document describes the major pnenomena modeled, the inter-.aces among the computer codes, and the features of the codes which ensure comoliance with the Acceptance Criteria. The SATAN-'ll, WREFLGO0, BART and LOCTA-IV codes, wnich are used in the LOCA analysis, are described in detail by Bordelon et al. (1974)((5) 'elly                    ';
There are three distinct transients analyzed in each
et al. (1974) (9) Young et al.
: phase, including the thermal-hydraulic transient in the
: RCS, the pressure and temperature transient within the containment, and the fuel and clad temperature transient of the hottest fuel rod in the core.
Based on these considerations, a system of interrelated computer codes has been developed for the analysis of the LOCA.
A description of the various aspects of the LOCA analysis methodology is given by Bordelon, Massie, and 2ordan
( 1974).
Tnis document (6) describes the major pnenomena
: modeled, the inter-.aces among the computer
: codes, and the features of the codes which ensure comoliance with the Acceptance Criteria.
The SATAN-'ll, WREFLGO0, BART and LOCTA-IV codes, wnich are used in the LOCA analysis, are described in detail by Bordelon et al. (1974)( 'elly et al.
(1974)
'; Young et al.
(5)
(9)
(4)
(4)
(1980); /~X Bordelon and Murphy (1974)(     '; and Bordelon et al.
(1980);
( 1974).       Code modifications are specified in References 2, 7 and
Bordelon and Murphy (1974)( ';
: 13. These codes assess the core heat transfer geometry and determine if the core remains amenable to cooling throughout.and subsequent to the blowdown, refill, and reflood phases of the LOCA. The SATAN-V1 computer,
and Bordelon et al.
~ , ' co'de'nalyzes the thermal-hydraul'ic;'transi'ent in 'the RCS during blowdow'n and the WREFLOOO computer code calculates thi's transient during the refill and reflood phases to the accident. The LOTiC computer code, described by Hsieh and     Raymund in
/~X
( 1974).
Code modifications are specified in References 2,
7 and 13.
These codes assess the core heat transfer geometry and determine if the core remains amenable to cooling throughout.and subsequent to the blowdown, refill, and reflood phases of the LOCA.
The SATAN-V1 computer,
~,
' co'de'nalyzes the thermal-hydraul'ic;'transi'ent in 'the RCS during blowdow'n and the WREFLOOO computer code calculates thi's transient during the refill and reflood phases to the accident.
The LOTiC computer
: code, described by Hsieh and Raymund in
 
0


0 WCAP-8355 ( 1975) and WCAP-8345 ( 1974)
WCAP-8355 ( 1975) and WCAP-8345 ( 1974)
(3) , calculates the containment pressure transient. The containment pressure transient is input to WREFLOOO for the purpose of calculating the reflood transient.       The LOCTA-IV computer code calculates the thermal transient of the hottest fuel rod during the three phases. The standard Pad Fuel Thermal Safety Model, described in Reference 15, generates the initial fuel rod conditions input to LOCTA-IV.
, calculates the containment (3) pressure transient.
SATAN-VI calculates the RCS pressure, enthalpy, density, and the mass and energy flow rates in the RCS, as well as steam generator energy transfer between the primary and secondary systems as a function of time during the blowdown phase of the LOCA. SATAN-VI also calculates the accumulator water mass and internal pressure and the pipe break mass and energy flow rates that are assumed to be vented to the containment during blowdown. At the end of the blowdown phase, these data are transferred to the WREFLOOD code. Also, at the end-of-blowdown, the mass and energy release rates during blowdown are input to the LOTIC code for use in the determination of the contai.",".ien pressure response during <<his first phase of the LOCA. Additiona', SATAN-VI outout data from the end-of-blowdown, including the core inlet flow rate and enthalpy, the core pressure, and the core power decay transi'ent, are input to the LOCTA-IV code.
The containment pressure transient is input to WREFLOOO for the purpose of calculating the reflood transient.
With input from the SATAN-VI code, WREFLOOO uses a system thermal-hydraulic model to determine the core flooding rate (".hat is, he rate at wnich coolant enters the bottom of'he core),       he cool-ant pressure and"temperature, and the quench front height during the reflood phase of the LOCA. WREFLOOO also calculates the mass and energy flow addition to the containment through the break. WREFLOOO is also linked to the BART and LOCTA-IV codes. The heat transfer calculation for the I         7 II
The LOCTA-IV computer code calculates the thermal transient of the hottest fuel rod during the three phases.
  , average fuel channel in the hot assembly during the ref lood phase of the
The standard Pad Fuel Thermal Safety Model, described in Reference 15, generates the initial fuel rod conditions input to LOCTA-IV.
SATAN-VI calculates the RCS pressure, enthalpy, density, and the mass and energy flow rates in the
: RCS, as well as steam generator energy transfer between the primary and secondary systems as a function of time during the blowdown phase of the LOCA.
SATAN-VI also calculates the accumulator water mass and internal pressure and the pipe break mass and energy flow rates that are assumed to be vented to the containment during blowdown.
At the end of the blowdown phase, these data are transferred to the WREFLOOD code.
Also, at the end-of-blowdown, the mass and energy release rates during blowdown are input to the LOTIC code for use in the determination of the contai.",".ien pressure response during <<his first phase of the LOCA.
Additiona',
SATAN-VI outout data from the end-of-blowdown, including the core inlet flow rate and
: enthalpy, the core pressure, and the core power decay transi'ent, are input to the LOCTA-IV code.
With input from the SATAN-VI code, WREFLOOO uses a system thermal-hydraulic model to determine the core flooding rate (".hat is, he rate at wnich coolant enters the bottom of'he core),
he cool-ant pressure and"temperature, and the quench front height during the reflood phase of the LOCA.
WREFLOOO also calculates the mass and energy flow addition to the containment through the break.
WREFLOOO is also linked to the BART and LOCTA-IV codes.
The heat transfer calculation for the I
7 II
, average fuel channel in the hot assembly during the ref lood phase of the
~
~
(16)
LOCA is performed by the BART'omputer code using a mechanistic (16) core heat transfer model.
LOCA is performed by the BART'omputer code using a mechanistic core heat transfer model. This information is then used by LOCTA-IV throughout the analysis of the LOCA transient to calculate the fuel clad temperature and metal-water reaction of the hottest rod in the core.
This information is then used by LOCTA-IV throughout the analysis of the LOCA transient to calculate the fuel clad temperature and metal-water reaction of the hottest rod in the core.


The large break analysis was performed with the December 1981 version of (16) computer the Evaluation Model modified to incorporate the BART code.
The large break analysis was performed with the December 1981 version of (16) the Evaluation Model modified to incorporate the BART computer code.
Input Parameters   and Initial Conditions:
Input Parameters and Initial Conditions:
The analysis presented in, this section was performed with a reactor vessel upper head temperature equal to the RCS hot leg temperature.
The analysis presented in, this section was performed with a reactor vessel upper head temperature equal to the RCS hot leg temperature.
The bases used   o select the numerical values that are input parameters to the analysis have been conservatively determined from extensive sensitivity studies (Westinghouse 1974 (12) .; Salvatori 1974 (11).
The bases used o select the numerical values that are input parameters to the analysis have been conservatively determined from extensive sensitivity studies (Westinghouse 1974
                                                            ~
; Salvatori 1974 (12).
Johnson, Hassle, and Thompson 1975 (8) ). In addition, the requirements of Appendix K regarding specific model 'features were met by selecting models which provide a significant overall conservatism in the analysis. The assumptions which were made pertain to the conditions of the reactor and associated safety system equipment at the time that the LOCA occurs, and include such items as the core oeaking factors, the containment pressure, and the performance or the =CCS. Gecay heat generated throughout the transient is also conservatively calculated.
~
A meeting was held at :he Mestinghouse     Licensing Office in Bethesda on Oecember 17, 1981 between members of the U. S. Nuclear Regulatory Commission and members of tne Mestinghouse Nuclear 'Safety Oepartment to discuss the impac. of maximum safety injection on the large break ECCS analysis on a generic basis. Further discussion of this issue is provided in a letter from E. P. Rahe, Manager of Westinghouse Nuclear Safety Oepartment, to Robert L. Tedesco of the U. S. Nuclear Regulatory (14) A brief description of this issue is given below.
(11).
Commission.(,
: Johnson, Hassle, and Thompson 1975
analyses currently: assume. minimum s'afeguards for the
).
                                                                                    ~
In addition, the requirements (8) of Appendix K regarding specific model 'features were met by selecting models which provide a significant overall conservatism in the analysis.
.,Mestihghause  ECCS                                                          ~
The assumptions which were made pertain to the conditions of the reactor and associated safety system equipment at the time that the LOCA occurs, and include such items as the core oeaking factors, the containment
                                                                                      ~
: pressure, and the performance or the
safety injection flow, which minimizes the amount of flow to the RCS by       ~
=CCS.
assuming maximum injection line resistances, degraded ECCS pump performance, and the loss of one residual heat removal (QHR) pump as the most limiting single failure. This is the limiting single failure assumption when offsite power is unavailable for most Westinghouse
Gecay heat generated throughout the transient is also conservatively calculated.
A meeting was held at :he Mestinghouse Licensing Office in Bethesda on Oecember 17, 1981 between members of the U.
S. Nuclear Regulatory Commission and members of tne Mestinghouse Nuclear 'Safety Oepartment to discuss the impac. of maximum safety injection on the large break ECCS analysis on a generic basis.
Further discussion of this issue is provided in a letter from E.
P.
: Rahe, Manager of Westinghouse Nuclear Safety Oepartment, to Robert L. Tedesco of the U.
S. Nuclear Regulatory Commission.(,
A brief description of this issue is given below.
(14)
.,Mestihghause ECCS analyses currently: assume. minimum s'afeguards for the
~
safety injection flow, which minimizes the amount of flow to the RCS by
~
assuming maximum injection line resistances, degraded ECCS pump performance, and the loss of one residual heat removal (QHR) pump as the most limiting single failure.
This is the limiting single failure assumption when offsite power is unavailable for most Westinghouse
~
~


plants. However, for some Westinghouse plants including 0. C. Cook Unit 1, the current nature of the Appendix K ECCS evaluation models is such that it may be more limiting to assume the maximum possible ECCS flow delivery. In that case, maximum safeguards which assume minimum injection line resistances, enhanced ECCS pump performance, and no single failure, result in the highest amount of flow delivered to the RCS.
plants.
Current   LOCA analysis for 'the 0. C. Cook Unit 1 has demonstrated that, maximum   safeguards assumptions result in     he highest peak clad temperatur'e. Therefore, the worst break   for O. C. Cook (CO =   0.6) was re-analyzed, assuming maximum safeguards.
However, for some Westinghouse plants including 0.
C.
Cook Unit 1, the current nature of the Appendix K ECCS evaluation models is such that it may be more limiting to assume the maximum possible ECCS flow delivery.
In that case, maximum safeguards which assume minimum injection line resistances, enhanced ECCS pump performance, and no single failure, result in the highest amount of flow delivered to the RCS.
Current LOCA analysis for 'the 0.
C.
Cook Unit 1 has demonstrated
: that, maximum safeguards assumptions result in he highest peak clad temperatur'e.
Therefore, the worst break for O.
C.
Cook (CO = 0.6) was re-analyzed, assuming maximum safeguards.
Results:
Results:
Based on the   results of the   LOCA sensitivity studies   (Westinghouse 1974     ; Salvatori 1974       ; Johnson, Massie, and Thompson 1975     ) the limiting large break was found to be the double ended cold leg guillotine (OECLG). Therefore, only the OECLG break is considered in the large break ECCS performance analysis. Calculations were performed for a range of Moody break discharge coefficients.           The results of these calculations are summarized in Tables 14.3. 1-5 and 14.3.1-6.
Based on the results of the LOCA sensitivity studies (Westinghouse 1974
The containment data used to generate the LOTIC backpressure transient are shown in Table 14.3. 1-1. The mass and energy release data ror the minimum and maximum safeguards cases are shown in Tables 14.3. 1-2 and 14.3. 1-3 respectively. Nitrogen release rates to the containment are given in Table 14.3.1-4.
; Salvatori 1974
; Johnson,
: Massie, and Thompson 1975
) the limiting large break was found to be the double ended cold leg guillotine (OECLG).
Therefore, only the OECLG break is considered in the large break ECCS performance analysis.
Calculations were performed for a range of Moody break discharge coefficients.
The results of these calculations are summarized in Tables 14.3. 1-5 and 14.3.1-6.
The containment data used to generate the LOTIC backpressure transient are shown in Table 14.3. 1-1.
The mass and energy release data ror the minimum and maximum safeguards cases are shown in Tables 14.3. 1-2 and 14.3. 1-3 respectively.
Nitrogen release rates to the containment are given in Table 14.3.1-4.
Figures 14.3. 1-1 through 14:3. 1-54.present the transients for the
Figures 14.3. 1-1 through 14:3. 1-54.present the transients for the
                                                    'I principal parameters 'for the break size's analyzed. The following items are noted:
'I principal parameters 'for the break size's analyzed.
The following items are noted:


Fi ures 14.3.1-1   The  following quantities are presented at the clad throu h 14.3.1-12 burst location and at the hot spot (location of maximum clad temperature), both on the hottest fuel rod (hot rod):
Fi ures 14.3.1-1 throu h 14.3.1-12 The following quantities are presented at the clad burst location and at the hot spot (location of maximum clad temperature),
: 1. fluid quality;
both on the hottest fuel rod (hot rod):
: 2. mass velocity;
1.
: 3. heat transfer coefficient.
fluid quality; 2.
The heat transfer coefficient shown is calculated by the LOCTA-IV code.
mass velocity; 3.
Fi ures 14.3.1-13   The system  pressure shown is the calculated throu h 14. 3. 1-24 pressure in the core. The flow rate from the break is plotted as the sum of both ends for the guillotine break cases. The core pressure drop shown is from the lower plenum, near the core, to the upper plenum at the core outlet.
heat transfer coefficient.
Figures 14.3.1-25   These  figures show the hot spot clad temperature throu h 14. 3. 1-36 transient and the clad temp rature transient at the burst location. The fluid emperature shown is also for the hot spot and burst location. The core flow (top and bottom) is also snown.
The heat transfer coefficient shown is calculated by the LOCTA-IV code.
Figures 14.3. 1-37 These   figures show he core rerlood transient.
Fi ures 14.3.1-13 throu h 14. 3. 1-24 The system pressure shown is the calculated pressure in the core.
through 14.3. 1-44 Figures 14.3. 1-45 These  figures show the mergency Core Cooling throu h 14. 3. 1-52 System flow for all of the cases analyzed. As described earlier, the accumulator delivery during blowdown is discarded until the.end of bypass is calculated. Accumulator 'flow:, however, is established in the refill and the reflood calculations. The accumulator flow assumed is the sum of that injected in the intact cold legs.
The flow rate from the break is plotted as the sum of both ends for the guillotine break cases.
The core pressure drop shown is from the lower plenum, near the core, to the upper plenum at the core outlet.
Figures 14.3.1-25 throu h 14. 3. 1-36 These figures show the hot spot clad temperature transient and the clad temp rature transient at the burst location.
The fluid emperature shown is also for the hot spot and burst location.
The core flow (top and bottom) is also snown.
Figures 14.3. 1-37 These figures show he core rerlood transient.
through 14.3. 1-44 Figures 14.3. 1-45 throu h 14. 3. 1-52 These figures show the mergency Core Cooling System flow for all of the cases analyzed.
As described earlier, the accumulator delivery during blowdown is discarded until the.end of bypass is calculated.
Accumulator 'flow:, however, is established in the refill and the reflood calculations.
The accumulator flow assumed is the sum of that injected in the intact cold legs.


Fi ures 14.3. 1-53     The  containment pressure transient used in the throu h 14.3.1"54     analysis is also provided for the minimum and maximum SI cases.
Fi ures 14.3. 1-53 throu h 14.3.1"54 The containment pressure transient used in the analysis is also provided for the minimum and maximum SI cases.
Figures 14.3.1-55     These figures show the heat removal rates of the heat and 14.3.1-60          sinks found in the lower compartment and the heat removal by the lower containment drain, andthe heat removal by the sump and LC sprays (minimum and maximum SI cases).
Figures 14.3.1-55 and 14.3.1-60 These figures show the heat removal rates of the heat sinks found in the lower compartment and the heat removal by the lower containment drain, andthe heat removal by the sump and LC sprays (minimum and maximum SI cases).
Fi ures 14.3.1-61     These  figures  show the  temperature transients in throu h 14. 3. 1-64   both the upper and lower compartments of the containment and flow from the upper to lower compartments. Total heat removal in the lower compartment is the sum of all the heat removal rates shown (for minimum and maximum SI cases).
Fi ures 14.3.1-61 throu h 14. 3. 1-64 These figures show the temperature transients in both the upper and lower compartments of the containment and flow from the upper to lower compartments.
The maximum clad temperature calculated for a large break is 2163 F, which is less than the Acceptance Criteria limit of 2200~F. The maximum local metal-water reaction is 9.65,percent, which is well below the embrittlement limit.of 17 percent as required by 10 CFR 50.46. The
Total heat removal in the lower compartment is the sum of all the heat removal rates shown (for minimum and maximum SI cases).
:otal core metal-water reaction is less than 0.3 percent for all breaks, as compared with the 1 percent criterion of 10 CFR 50.46.       The clad temperature transient is terminated at a time when the core geometry is still amenable to cooling. As a result, the core temperature will continue o drop and the ability to remove decay heat generated in the fuel for an extended period of time will be provided.
The maximum clad temperature calculated for a large break is 2163 F,
which is less than the Acceptance Criteria limit of 2200~F.
The maximum local metal-water reaction is 9.65,percent, which is well below the embrittlement limit.of 17 percent as required by 10 CFR 50.46.
The
:otal core metal-water reaction is less than 0.3 percent for all breaks, as compared with the 1 percent criterion of 10 CFR 50.46.
The clad temperature transient is terminated at a time when the core geometry is still amenable to cooling.
As a result, the core temperature will continue o drop and the ability to remove decay heat generated in the fuel for an extended period of time will be provided.
10
10


References for Section 14.3. 1. 1
References for Section 14.3. 1. 1 1.
: 1. "Acceptance Criteria for Emergency Core Cooling System for Light Water Cooled Nuclear Power Reactors," 10 CFR 50.46 and Appendix K of 10 CFR 50, Federal Re ister 1974, Volume 39, Number 3.
"Acceptance Criteria for Emergency Core Cooling System for Light Water Cooled Nuclear Power Reactors,"
: 2. Rahe,   E. P. (Westinghouse),   letter to J. R. Miller (USNRC); Letter No. NS-EPRS-2679,     November 1982.
10 CFR 50.46 and Appendix K of 10 CFR 50, Federal Re ister
: 3. Hsieh, T., and Raymund, M., "Long Term Ice Condenser Containment LOTIC Code Supplement     1," WCAP-8355, Supplement       1, May 1975, WCAP-8345   (Proprietary), July   1974.
: 1974, Volume 39, Number 3.
: 4. Bordelon, F. M. et "al., "LOCTA-IV Program: Loss-of-Coolant Transient Analysis," WCAP-8301 (Proprietary) and WCAP-8305 (Non-proprietary), 1974.
2.
: 5. Bordelon, F. M. et al., "SATAN-VI Program: Comprehensive Space, Time Oependent Analysis of Loss-of-Coolant," WCAP-8302 (Proprietary) and WCAP-8306 (Non-proprietary), 1974.
: Rahe, E.
: 6. Bordelon, F. M.; Massie, H. W.; and 2ordan, T. A., "Westinghouse ECCS Evaluation Model - Summa'ry," WCAP-8339, 1974.
P. (Westinghouse),
: 7. Rahe,   E. P., "Westinghouse   ECCS Evaluation Model, 1981 Version,"
letter to J.
WCAP-9220-P-A (Proprietary Version), WCAP-9221-?-A (Non-proprie~ry version),. Revision 1, 1981.
R. Miller (USNRC); Letter No. NS-EPRS-2679, November 1982.
: 8. Johnson,   W. J.; Massie, H. W.; and Thompson, C. M., "Westinghouse ECCS - Four Loop Plant (17x17) Sensitivity Studies," WCAP-8565-P-A (Propr'ietary)   and WCAP-8566-A   (Non-proprie't'ary), 1975.
3.
PP
Hsieh, T.,
: 9. Kelly,   R. 0. et al., "Calculational   Model   for Core Ref looding After" a Lo'ss-of-Coolant Accident   (WREFLOOO   Code)," WCAP-8170 (Proprietary) and WCAP-8171     (Non-proprietary),   1974.
and
: Raymund, M., "Long Term Ice Condenser Containment LOTIC Code Supplement 1," WCAP-8355, Supplement 1,
May 1975, WCAP-8345 (Proprietary), July 1974.
4.
: Bordelon, F.
M. et "al., "LOCTA-IV Program:
Loss-of-Coolant Transient Analysis," WCAP-8301 (Proprietary) and WCAP-8305 (Non-proprietary),
1974.
5.
: Bordelon, F.
M. et al.,
"SATAN-VI Program:
Comprehensive
: Space, Time Oependent Analysis of Loss-of-Coolant,"
WCAP-8302 (Proprietary) and WCAP-8306 (Non-proprietary),
1974.
6.
: Bordelon, F. M.; Massie, H. W.; and 2ordan, T. A., "Westinghouse ECCS Evaluation Model - Summa'ry,"
WCAP-8339, 1974.
7.
: Rahe, E. P.,
"Westinghouse ECCS Evaluation Model, 1981 Version,"
WCAP-9220-P-A (Proprietary Version),
WCAP-9221-?-A (Non-proprie~ry version),. Revision 1,
1981.
8.
: Johnson, W. J.; Massie, H. W.; and
: Thompson, C. M., "Westinghouse ECCS - Four Loop Plant (17x17) Sensitivity Studies,"
WCAP-8565-P-A (Propr'ietary) and WCAP-8566-A (Non-proprie't'ary),
1975.
PP 9.
Kelly, R. 0. et al., "Calculational Model for Core Ref looding After" a Lo'ss-of-Coolant Accident (WREFLOOO Code),"
WCAP-8170 (Proprietary) and WCAP-8171 (Non-proprietary),
1974.


10 U. S. Nuclear Regulatory Commission 1975 "Reactor Safety Study -       An Assessment of Accident Risks in U. S. Commercial Nuclear Power Plants,"   WASH-1400, NUREG-75/014.
10 U. S. Nuclear Regulatory Commission 1975 "Reactor Safety Study - An Assessment of Accident Risks in U.
: 11. Salvatori, R., "Westinghouse     ECCS   - Plant Sensitivity Studies,"
S.
WCAP-8340 (Proprietary) and   WCAP-8356 (Non-proprietary), 1974.
Commercial Nuclear Power Plants,"
: 12. "Westinghouse   ECCS - Evaluation Model Sensitivity Studies,"
WASH-1400, NUREG-75/014.
WCAP-8341   (Proprietary) and WCAP-8342 (Non-proprietary), 1974.
: 11. Salvatori, R., "Westinghouse ECCS - Plant Sensitivity Studies,"
: 13. Bordelon, F. H.,   et al., "Westinghouse ECCS Evaluation Model-Supplementary Information," WCAP-8471 (Proprietary) and WCAP-8472 (Non-proprietary), 1975;
WCAP-8340 (Proprietary) and WCAP-8356 (Non-proprietary),
: 14. Rahe, E. P. (Westinghouse). Letter to Robert L. Tedesco (USNRC),
1974.
Letter No. NS-EPR-2538,   Oecember   1981.
12.
: 15. Letter from J. F. Stoltz (NRC) to T. M. Anderson (Westinghouse);
"Westinghouse ECCS - Evaluation Model Sensitivity Studies,"
subject: Review of WCAP-8720, Improved Ana'.ytical 4lodels Used in Westinghouse   Fuel Rod Oesign Computations.
WCAP-8341 (Proprietary) and WCAP-8342 (Non-proprietary),
: 16. Young, 4I. Y., et al., "BART-Al: A Computer Code for he Best Estimate Analysis of Reflood Transients, "WCAP-9561-P-A (Proorietary) and WCAP-9695"A (Non-Proprietary) January 1980.
1974.
: 13. Bordelon, F. H., et al.,
"Westinghouse ECCS Evaluation Model-Supplementary Information," WCAP-8471 (Proprietary) and WCAP-8472 (Non-proprietary),
1975; 14.
: Rahe, E.
P. (Westinghouse).
Letter to Robert L. Tedesco (USNRC),
Letter No. NS-EPR-2538, Oecember 1981.
: 15. Letter from J.
F. Stoltz (NRC) to T.
M. Anderson (Westinghouse);
subject:
Review of WCAP-8720, Improved Ana'.ytical 4lodels Used in Westinghouse Fuel Rod Oesign Computations.
16.
: Young, 4I. Y., et al.,
"BART-Al:
A Computer Code for he Best Estimate Analysis of Reflood Transients, "WCAP-9561-P-A (Proorietary) and WCAP-9695"A (Non-Proprietary)
January 1980.
12
12


TABLE 14.3 1-1
TABLE 14.3
                                                  ~
~ 1-1 LARGE BREAK CONTAINMENT DATA
LARGE BREAK CONTAINMENT DATA
( ICE CONDENSER CONTAINMENT)
( ICE CONDENSER CONTAINMENT)
NET FREE VOLUME
NET FREE VOLUME
( Includes Distribution Between Upper, Lower,               UC   746,829'ft.
( Includes Distribution Between
and Dead-Ended Compartments)                                LC  249,446 OE    116,168 IC    122,400 Initial   Conditions Pressure                                               14.7 psia Temperature     for the Upper,     Lower and     UC   100~ F Dead-Ended    Compartments                      LC   120~ F OE   120oF RWST  Temperature                                        70~F Service Mater Temperature                                40oF Temperature Outside Containment                            7oF Initial    Spray Temperature                            70~F Spray System Burnout Flow for       a Spray Pump                   3600 gpm Number   of Spray     Pumps Operating                 2 Post-Accident       Initiation of   Spray System       40 secs Ois ribution of       the Spray Flow to the       LC  2835 gpm Upper and Lower Compartments                     UC   43o5 gpm Deck Fan Post-Accident       Initiation of   Deck Fans         600 secs Flow'at,e Per       Fan                               ~
: Upper, Lower, and Dead-Ended Compartments)
39,000 cfm per'ran
UC LC OE IC 746,829'ft.
                    'I Hydrogen Skimmer System Flow Rate                                 2800 cfm per ran Assumed Spray     Efficiency of Mater from                         100'o Ice Condenser 'Drains 13
249,446 116,168 122,400 Initial Conditions Pressure Temperature for the Upper, Lower and Dead-Ended Compartments RWST Temperature Service Mater Temperature Temperature Outside Containment Initial Spray Temperature 14.7 psia UC 100~ F LC 120~ F OE 120oF 70~F 40oF 7oF 70~F Spray System Burnout Flow for a Spray Pump Number of Spray Pumps Operating Post-Accident Initiation of Spray System Ois ribution of the Spray Flow to the Upper and Lower Compartments 3600 gpm 2
40 secs LC 2835 gpm UC 43o5 gpm Deck Fan Post-Accident Initiation of Deck Fans Flow'at,e Per Fan 600 secs
~ 39,000 cfm per'ran
'I Hydrogen Skimmer System Flow Rate 2800 cfm per ran Assumed Spray Efficiency of Mater from Ice Condenser 'Drains 100'o 13


TABLE 14. 3 1 ~ 1
TABLE 14. 3 1 ~ 1
                                            'continued)
'continued)
STRUCTURAL HEAT SENKS 2
STRUCTURAL HEAT SENKS i
i                      blateri a 1
2 blateri a 1 1.
: 1. LC                 12,105            0.0469/2.0      steel/concrete
LC 2.
: 2. LC                 11,700            2.0            concrete
LC 3.
: 3. LC                 65,980            1.35            concrete
LC 4.
: 4. LC                 5,481            0.0833          steel
LC 5.
: 5. LC                 4,735            0.01147          steel
LC 6.
: 6. LC                     289            0.25            lead
LC 7.
: 7. LC                14,690            0.0079          steel
LC 8.
: 8. LC                  3,439             0.1561          steel
LC 9.
: 9. LC                  5,775             0.009            steel
LC 10.
: 10. LC                  4,966             0.0096          steel
LC 11.
: 11. LC                  7,013             0.037            steel
LC 12.
: 12. LC                  2,457            0.0334           steel
LC 13.
: 13. UC                    378              .1667/.0365   steel/concrete
UC 14.
: 14. UC                29,772              .0092         steel
UC 15.
: 15. UC                  8,033              .0209         steel
UC 16.
: 16. UC                    420              .0052 .
UC 17.
s  eel
UC 18.
: 17. UC                29,330            1.47             concrete
UC 19.
: 18. UC                34 125            0.0469/2.0       steel/concrete
UC 12,105 11,700 65,980 5,481 4,735 289 14,690 3,439 5,775 4,966 7,013 2,457 378 29,772 8,033 420 29,330 34 125 2'10 0.0469/2.0 2.0 1.35 0.0833 0.01147 0.25 0.0079 0.1561 0.009 0.0096 0.037 0.0334
: 19. UC                    2'10            .0052          steel UC:   Upper Compartment
.1667/.0365
~:...... LO: ..Lower. Compartment OE:   Oead-Ended Compartment 1C:   lce Condenser Compartment
.0092
.0209
.0052 1.47 0.0469/2.0
.0052 steel/concrete concrete concrete steel steel lead steel steel steel steel steel steel steel/concrete steel steel s eel concrete steel/concrete steel UC:
Upper Compartment
~:......
LO:..Lower. Compartment OE:
Oead-Ended Compartment 1C:
lce Condenser Compartment


ASS     AiND   9   ?"=Y RE':-~SE ?~iES u!,.<IMUM Si i@SS                                    'tE?GY i !!ME (jb/sac)                              (~is/sec)
ASS AiND 9
(sec)
?"=Y RE':-~SE ?~iES u!,.<IMUM Si i !!ME (sec)
O.                               ~  57888>05                              30jiZc F08
O.
    .2GGGE.Q1                       4783E G5                          .24,78E        ~GS
.2GGGE.Q1
    .cuGQEiyl                     .34228~05                            .179'E i08
.cuGQEiyl
    .6GGGE'v I                   .2563Ei05                            ~  1377E iCjS
.6GGGE'v I
    .8GijGE~Gl                     .2225c+05                            .1223E G8
.8GijGE~Gl
    ~ 10GC;E 02                   .ZQ4cC+05                            .114GE'08
~ 10GC;E 02
    , 1 ZC'C E '02               .18GCE+05                            .1037E+08
, 1 ZC'C E '02
    .124ciE 02                   .16558+05                              .9762E +07
.124ciE 02
    .140QE'02                     . 1561E>05                            .9229E ipr
.140QE'02
                                  .14368 ~G5                                SCQ3Eipr
~ 15GGE+GZ
  '1s15GGE+GZ
'1s OE-02
    ~
.18GQE+02
OE-02                   .1319E +05                            .799GE+07
.190GE+02
    .18GQE+02                     .1134E'05                             .6925Eipr
.200GE'02
    .190GE+02                      .1061E 05                             .6491E 07
.21QQE>02
    .200GE'02                      ~ 991 7E ~04                         .6106E'07
.220GE 02
    .21QQE>02                      .8999E ipc                           .5628E+07
.24,0QE.OZ
    .220GE 02                      .8183E +04                           .5086Eipr
.25CQE+02
    .24,0QE.OZ                    .64G7E+04                            .40cZE>07
.26GPE~QZ
    .25CQE+02                      .5476Eipc                            .34CZE.07
.270QEip2
    .26GPE~QZ                      .445GEipc                            .2730E'07
'28GGE'02
    .270QEip2                      .6099E+04                            .2983E+07
.292GE'02
                      '28GGE'02 68i09EtP4                          .3GGcE+Gr
.3QGQE'02
    .292GE'02                      .7005E nc                            .2753E          .Qr
.31GGE+02
    .3QGQE'02                        .c>31E+0>>                          ~   5 1 38     ~ vr
.32GGEi02
    .31GGE+02                      .5248E Gc                            .ZG'73E'Gr
.33 GGEiQZ
    .32GGEi02                      .6371E.Qc                                19~   '-.07
,35GQE~G2
    .33 GGEiQZ                      .4858E~G4                            ,1391= Or
.37GOE'02
    ,35GQE~G2                      .4315Eipc                            .1019E Gr
.38GQE+02
    .37GOE'02                      .2298Eipc                            .6255c Gb
.3849E~QZ
    .38GQE+02                      .667CE.03                            . 1 7 '> 4E  -C'6
.c5QOE+02
    .3849E~QZ                      .6587E~Q3                            ,fbt9E 05       F
~ 50QGEi02
    .c5QOE+02                      . 173GE.G3                          .6583E 04
.5265E+G2 5325EiQZ
    ~ 50QGEi02                      ,1730E, v3                          ~   6583Eipc
.5355E+02
    .5265E+G2                      , 1 730 E. > 03                      .6583E~04 5325EiQZ                    .1rb8E 03                            .114&E'05
.5375E+02
    .5355E+02                      .1768E i03                          .1145E+G5
. ".5385E+02.
    .5375E+02                      ~ 1767E+03                          .1135E+05
. 5973EQ2
. ".5385E+02.                    .'.1rbrE;03        .-                  .1134E+05'.c>>GE
.7020E 02
    . 5973EQ2                      .205GE+03                                              05
.864OE+02
    .7020E 02                    ~
~ 10698 03
                                    .5402E G3                            .2098E 06
.1302E+03
    .864OE+02                      .5729E+03                            . 2153E+06
. 156OE i03
    ~ 10698      03                .5850E.03                            .2128E Gb
.2152E.03
    .1302E+03                      .5947E+03                            . 2081       E ipb
.2887E+03
    . 156OE    i03                .6022E+03                            .2027E 06
.4107E~Q3
    .2152E.03                      ,616GE.03                            .19G7E             i'c
.4434c+03 i@SS (jb/sac)
    .2887E+03                      .5317E 03                            .17.>= 05
~ 57888>05 4783E G5
    .4107E~Q3                      . 6535c -'-'3                        . 1631E         'Gb
.34228~05
    .4434c+03                      ,659~c 03                            .1635E+05
.2563Ei05
.2225c+05
.ZQ4cC+05
.18GCE+05
.16558+05
. 1561E>05
.14368 ~G5
.1319E +05
.1134E'05
.1061E 05
~ 991 7E ~04
.8999E ipc
.8183E +04
.64G7E+04
.5476Eipc
.445GEipc
.6099E+04 68i09EtP4
.7005E nc
.c>31E+0>>
.5248E Gc
.6371E.Qc
.4858E~G4
.4315Eipc
.2298Eipc
.667CE.03
.6587E~Q3
. 173GE.G3
,1730E, v3
, 1 730 E. >03
.1rb8E 03
.1768E i03
~ 1767E+03
.'.1rbrE;03.-
.205GE+03
~.5402E G3
.5729E+03
.5850E.03
.5947E+03
.6022E+03
,616GE.03
.5317E 03
. 6535c -'-'3
,659~c 03
'tE?GY
(~is/sec) 30jiZc F08
.24,78E ~GS
.179'E i08
~ 1377E iCjS
.1223E G8
.114GE'08
.1037E+08
.9762E +07
.9229E ipr SCQ3Eipr
.799GE+07
.6925Eipr
.6491E 07
.6106E'07
.5628E+07
.5086Eipr
.40cZE>07
.34CZE.07
.2730E'07
.2983E+07
.3GGcE+Gr
.2753E
.Qr
~
5 1 38 ~vr
.ZG'73E'Gr 19~ '-.07
,1391=
Or
.1019E Gr
.6255c Gb 1 7 '> 4 E -C'6
,fbt9E F 05
.6583E 04
~ 6583Eipc
.6583E~04
.114&E'05
.1145E+G5
.1135E+05
.1134E+05'.c>>GE 05
.2098E 06
. 2153E+06
.2128E Gb
. 2081 E ipb
.2027E 06
.19G7E i'c
.17.>= 05
. 1631E 'Gb
.1635E+05


TnQL:- 14.-"'. l-3
TnQL:- 14.-"'. l-3
                                  ~SS neo .qrvI4Y             <e. -45@
~SS neo
l4AX.HUH Si il.i 7VL' "ASS (Sac}                     (ib/SIC) 0
.qrvI4Y <e. -45@
            , 2COOE   0l              . 6776Ei05
l4AX.HUH Si 7VL' il.i (Sac}
              . lCQOE   nl             . 5500Ei05                              <<3607E QS
0
            .5CCCE Ol                 ~  388 lEi05                            ,2874E~QS ROCQEiol               ~  304 l E F05                          ~  ZC69Eioe
, 2COOE 0 l
            . lQCOE F02             ,2738Ei05                                >>  l687EiCS
. lCQOE nl
            . l ZOCE ~02             ~    2382Ei05                                l54ZE~OS
.5CCCE Ol ROCQEiol
          ~ l 24OE ~02             ~    l888Ei05                            . l 379E    ioe
. lQCOE F02
          ~   I 400E ~02           . ISOZEi05                                l l29Eioe
. l ZOCE ~02
          . lSCCE402                 ,    1455E+05                            . lC84E~CS
~ l 24OE ~02
          . l60nE F02               ,    lZSZEi05                            :9098E-07
~ I400E ~02
          . l 7CCE   '02           . l 120E F05                          .SZZSEi07
. lSCCE402
        . lSCCEi02               .9375Ei04                                  .7433Eio7
. l60nE F02
        . lsQOEi02                 ,8597E'04                                .6562E 07
. l 7CCE '02
        .ZCOPEi02                 . 7564Ei04                                5CSSE 07
. lSCCEi02
        . 2 lCCE ~02             .5880Eio4                                  .54 lSE 07
. lsQOEi02
        .220CE'02                 . 4Q47E F04                                444 7E 07 2300Ei02               . 5 l 298~04                                  29 lSE    '07
.ZCOPEi02
      .240CE       '02         .6880Ei04                                  .283ZE i07
. 2 lCCE ~02
      .25QQE'QZ                 .7206Ei04                                  , 2968 E i07
.220CE'02 2300Ei02
      .2600E~OZ                 . 60 lOEi04                                , 2679 E i07
.240CE
      .2700E'02                 . 4829E F04                                . l877E~07
'02
      .Z8CCE 02                 .4337Ei04                                  . l 282E F07
.25QQE'QZ
    .2895E 02                 .3670Ei04                                  , l059E<<07
.2600E~OZ
    . 2900E F02              .2623Ei04                                  ,8232E'06
.2700E'02
    .3CCQE 02                ,24 lSE<<04                                 .44CSEiC6 30 l35-02              ~   2380E       i04                       , 3675E F06
.Z8CCE 02
    . 3 lCOE '02            ,2357E 04                                   .3406E~C6
.2895E 02
    ,38COE 02                ,    'I   54'2E F04                       ,3f95E'06
. 2900E F02
    ,4Q'.43Eio2              , 34'2 5E 03                                   8    l54E F05
.3CCQE 02 30 l35-02
  ,4248EiPZ                  .3425Ei03                                 . l303E iPS
. 3 lCOE '02
  ,4308E~CZ                .3425Ei03                                        l 3CZE PCS
,38COE 02
  .4328Ei<<32                .3470Ei03                                        l 303E    '05 4338E 02              . 3410E~03                                .l892ciPS
,4Q'.43Eio2
  ,4348E 02                ,3470Ei03                                      189 lE "PS
,4248EiPZ
  <<4358Ei02                  .3470E~03                                      l 89OE 05
,4308E~CZ
,4885EiCZ                  ,3469Ei03                                        lSSSE-OS c<4 l E Q2            .3762Ei03                                        <579E CS
.4328Ei<<32 4338E 02
. 7796E 02              .4579E~O4                                      5683E OS lQ IZC b03                l 486E i04                                44 lSE 06
,4348E 02
,    l309E i03            , lSOSE 04                                  2:36c 06
<<4358Ei02
,    l639Ei03              . lS lSEi04                                    '.iCSE'C6
,4885EiCZ c<4 l E Q2
.25l6E 03                  . l 524 E 04                                  "352E ~6
. 7796E 02 lQ IZC b03
                          . f545Ei04                                    23 l 7c <<06 2240'-06
, l309E i03
, l639Ei03
.25l6E 03 "ASS (ib/SIC)
. 6776Ei05
. 5500Ei05
~ 388 lEi05
~ 304 l E F05
,2738Ei05
~ 2382Ei05
~ l888Ei05
. ISOZEi05
, 1455E+05
, lZSZEi05
. l 120E F05
.9375Ei04
,8597E'04
. 7564Ei04
.5880Eio4
. 4Q47E F04
. 5 l 298~04
.6880Ei04
.7206Ei04
. 60 lOEi04
. 4829E F04
.4337Ei04
.3670Ei04
.2623Ei04
,24 lSE<<04
~ 2380E i04
,2357E 04
'I 54'2E F04
, 34'2 5E 03
.3425Ei03
.3425Ei03
.3470Ei03
. 3410E~03
,3470Ei03
.3470E~03
,3469Ei03
.3762Ei03
.4579E~O4 l 486E i04
, lSOSE 04
. lS lSEi04
. l 524 E 04
. f545Ei04
<<3607E QS
,2874E~QS
~ ZC69Eioe
>> l687EiCS l54ZE~OS
. l 379E ioe l l29Eioe
. lC84E~CS
:9098E-07
.SZZSEi07
.7433Eio7
.6562E 07 5CSSE 07
.54 lSE 07 444 7E 07 29 lSE '07
.283ZE i07
, 2968 E i07
, 2679 E i07
. l877E~07
. l 282E F07
, l059E<<07
,8232E'06
.44CSEiC6
, 3675E F06
.3406E~C6
,3f95E'06 8 l54E F05
. l303E iPS l 3CZE PCS l 303E '05
.l892ciPS 189 lE "PS l 89OE 05 lSSSE-OS
<579E CS 5683E OS 44 lSE 06 2:36c 06
'.iCSE'C6 "352E
~6 23 l 7c <<06 2240'-06


TABLE 14.3.1-A-3 NITROGEN MASS AND ENERGY RELEASE RATES
TABLE 14.3.1-A-3 NITROGEN MASS AND ENERGY RELEASE RATES
            ~Time sec                         Flow Rate     lbs/sec 37.5                                     71.9'0.7 39.5 45.5                                     37.2 47.5                                     31.6 53.5                                     18.8 55.5                                     15.6 61.5                                        8.5 63.5                                         6'. 9 70.3                                     186.0 72.3                                     158.0 78.5                                     97.3 80.5                                     82.4 86.3                                     48.5 88.3                                     40.0 94.3                                     21.9 96.3                                       18.2 102.2                                       11.7 104.2                                       10.5 110.2                                         7.6 112.2                                         6.8 126.2                                         3.3 128.2                                         2.9 138.2                                         1.8 140.2                                         1.6
~Time sec Flow Rate lbs/sec 37.5 39.5 45.5 47.5 53.5 55.5 61.5 63.5 70.3 72.3 78.5 80.5 86.3 88.3 94.3 96.3 102.2 104.2 110.2 112.2 126.2 128.2 138.2 140.2
          ~
~
146.2                                         1.2'.1 148.2 174.2                                        0.25 176.2                                        0.075 l7 0329L:6/840727
146.2 148.2 174.2 176.2 71.9'0.7 37.2 31.6 18.8 15.6 8.5 6'. 9 186.0 158.0 97.3 82.4 48.5 40.0 21.9 18.2 11.7 10.5 7.6 6.8 3.3 2.9 1.8 1.6 1.2'.1 0.25 0.075 0329L:6/840727 l7


TABLE   14.3.1-A-4 LARGE BREAK OECLG C0=0.4 Results                                         Max SI Peak Clad Temp.               'F                 2162 Peak Clad Location Ft.                         7,. 50 Local Zr/H20 Reaction (Max)i~                   6.58 Local 2r/H20 Location Ft.                       7.50 Total 2r/H20   Reaction,'o'ot
TABLE 14.3.1-A-4 LARGE BREAK OECLG C0=0.4 Results Max SI Peak Clad Temp. 'F Peak Clad Location Ft.
( 0.3 Rod Burst Time sec.                         71.4 Hot Rod Burst Location Ft.                       6.75 Calculation Licensed Core Power (Mwt) 102;o'f                               3250 Peak Linear Power (kw/ft) 102;o'f                               13.225 Peaking Factor (at License Rating)                               1.97 Accumulator Water Volume         (ft3
Local Zr/H20 Reaction (Max)i~
                                      ) per Accumulator         950
Local 2r/H20 Location Ft.
                                              . Cycle Analyzed.,:Cycle 8 18 0329L:6/840727
Total 2r/H20 Reaction,'o'ot Rod Burst Time sec.
Hot Rod Burst Location Ft.
2162 7,. 50 6.58 7.50
( 0.3 71.4 6.75 Calculation Licensed Core Power (Mwt) 102;o'f Peak Linear Power (kw/ft) 102;o'f Peaking Factor (at License Rating)
Accumulator Water Volume (ft ) per Accumulator 3
3250 13.225 1.97 950
. Cycle Analyzed.,:Cycle 8
18 0329L:6/840727


TABLE 14.3. 1-A-5 LARGE BREAK TIME SEQUENCE OF EVENTS Max SI OECLG CO=0.4 (sec)
TABLE 14.3. 1-A-5 LARGE BREAK TIME SEQUENCE OF EVENTS Max SI OECLG CO=0.4 (sec)
START                                 0.00 Reactor Trip Signal                    0.60 Safety Injection Signal                4.05 Accumulator Injection                20'. 50 End  of Blowdown                    38.70 Bottom of Core Recovery              52.78 Accumula'tor Empty                  67.45 Pump  Injection                      29.05
START Reactor Trip Signal Safety Injection Signal Accumulator Injection End of Blowdown Bottom of Core Recovery Accumula'tor Empty Pump Injection 0.00 0.60 4.05 20'. 50 38.70 52.78 67.45 29.05
~ ~
~
19 0329L: 6/840727
~
0329L: 6/840727 19


TABLE 14. 3.1-4 NITROGEN MASS AND ENERGY RELEASE RATES Time   sec                     Flow Rate lbs/sec 37.5                           71.9 39.5                           60.7 45.5                           37.2 47.5                           31.6 53.5                           18.8 55.5                           15.6 57.5                           12.8 60.7                         266.81 66.7                         159.7 68.7                         135.7 74.7                           83.2 76.7                           70.3 78.7                           58.9 80.7                           49.1 86.7                           27.2 88.7                           22.3 98.7                           10.7 100.7                             9.6 110.7                             5.6 112.7                              5.1 122.7                              3.0 124.7                              2.7 130.7                              2.0 132.7                              1.8
TABLE 14. 3.1-4 NITROGEN MASS AND ENERGY RELEASE RATES Time sec Flow Rate lbs/sec 37.5 39.5 45.5 47.5 53.5 55.5 57.5 60.7 66.7 68.7 74.7 76.7 78.7 80.7 86.7 88.7 98.7 100.7 110.7 112.7 122.7 124.7 130.7 132.7
              '146. 6                          ~ 0,8 145.5                            0.7 20 0329L:6/840727
'146. 6 145.5 71.9 60.7 37.2 31.6 18.8 15.6 12.8 266.81 159.7 135.7 83.2 70.3 58.9 49.1 27.2 22.3 10.7 9.6 5.6 5.1 3.0 2.7 2.0 1.8
~ 0,8 0.7 0329L:6/840727 20


TABLE   14.3.1-5 LARGE BREAK OECLG        DECLG    OECLG    OECLG C
TABLE 14.3.1-5 LARGE BREAK Results OECLG C =0.8 D
D
Min SI DECLG CD=0.6 Min SI OECLG
                                          =0.8     CD=0.6 ~
C 0
                                                                =0.4 'O='6 Results                            Min SI       Min SI    Min SI  Max SI Peak Clad Temp.,  F                1942        2014      1956    2163 Peak Clad  Location, ft    .      7.00        5.75      7.00    6.00 Local Zr/H20 Reaction (Max)        2.85        5.65      3.84    9.65 Local Zr/H20 Location,  ft          7.00        5.75      5.75    5.75 Total Zr/H20 Reaction              <0.3        <0.3      <0.3    <0.3 Hot Rod Burst Time, sec            43.8        37.8      47.4    37.8 Hot Rod Burst Location,  ft        6.00        5.75      5.75    5.75 Calculation Licensed Core Power  (MWT) 102;<    of                    3411 Peak  Linear Power (kw/ft)  102;~  of                    14.796 Peaking Factor (at License Rating)                        2.10 Accumulator Water Volume  (ft 3
                                  ) per Accumulator        950 21
~
~
0329L:6/840727
C =0.4 0
Min SI OECLG
'O='6 Max SI Peak Clad Temp.,
F 1942 Peak Clad Location, ft 7.00 Local Zr/H20 Reaction (Max) 2.85 Local Zr/H20 Location, ft 7.00 Total Zr/H20 Reaction
<0.3 Hot Rod Burst Time, sec 43.8 Hot Rod Burst Location, ft 6.00 2014 5.75 5.65 5.75
<0.3 37.8 5.75 1956 7.00 3.84 5.75
<0.3 47.4 5.75 2163 6.00 9.65 5.75
<0.3 37.8 5.75 Calculation Licensed Core Power (MWT) 102;< of 3411 Peak Linear Power (kw/ft) 102;~ of 14.796 Peaking Factor (at License Rating) 2.10 Accumulator Water Volume (ft ) per Accumulator 950 3
21
~ 0329L:6/840727


TABLE 14.3. 1-6 LARGE BREAK TIME SEQUENCE OF EVENTS Min SI      Min SI  Min SI  Max SI OECLG        OECLG    OECLG    OECLG CO=0.8       CO=0.6   CO=0.4   CO=0.6 (sec)        (sec)    (sec)    (sec)
TABLE 14.3. 1-6 LARGE BREAK TIME SEQUENCE OF EVENTS Min SI OECLG CO=0.8 (sec)
START                         0.00        0.00      0.00     0.00 Reactor Trip Signal            0.62       0.63     0.64    0. 63.
Min SI OECLG CO=0.6 (sec)
Safety Injection Signal        3.83.       3.95      4.20    3.95 Accumulator Injection        12.90       15.50     20.80    15.50 End  of Blowdown              29.68     30.43      38.49    30.43 Bottom  of Core Recovery      40.66     43.29     52.64    42.47 Accumulator Empty            56.89     59.29     65.65    60.58 Pump  Injection              28.83     28.95     29.20   28.95 22 0329L: 6/840727
Min SI OECLG CO=0.4 (sec)
Max SI OECLG CO=0.6 (sec)
START Reactor Trip Signal Safety Injection Signal Accumulator Injection End of Blowdown Bottom of Core Recovery Accumulator Empty Pump Injection 0.00 0.00 0.62 0.63 3.83.
3.95 12.90 15.50 29.68 30.43 40.66 43.29 56.89 59.29 28.83 28.95 0.00 0.64 4.20 20.80 38.49 52.64 65.65 29.20 0.00
: 0. 63.
3.95 15.50 30.43 42.47 60.58 28.95 0329L: 6/840727 22


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50.000 COOK LIHIfl (AEPI O.B OECLG HINSI 3i IIHV1 LIPAAIIHC ECCS LBLOCA ullH SARf ANO OLO PAO fOC2. IO HASS VELOCIIY RSI 6.00 f1l l Pf. AK. l.00 fft~ )
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300.00 COOX uvltl IAEP) O.a OECLC )IIRSI ta) I)IMt uPRAIIRC ECCS LBLOCA MIIH BARf ANO OLO PAO f0c2. IO HASS VELOCItV BURSt.
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i  LOO.OO i00.00 Ai 200.00 10.000 30.000 20.000 IMII 6.0000 5.0000 l.0000 3.0000 2.0000
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N'4 600.00 500.00 l00.00 300.00
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t.OOE<05 AEP LBLOCA FOR Rll l HMf UPRAftHC ANALYSIS M[TO BARf lSK l5 OFA 275 PSlC BACKFlLL 5 PC1 SCfP 0.6 OECLC BREAK BREAK FLOV v &.BOERS I
t.OOE<05 AEP LBLOCA FOR Rll l HMf UPRAftHC ANALYSIS M[TO BARf lSK l5 OFA 275 PSlC BACKFlLL 5
6.00E+a 1.00E+01 2.00E+Oi 0.0 Ch CI              C)
PC1 SCfP 0.6 OECLC BREAK BREAK FLOV v
TlHE lSEC)
&.BOERS I
FlCl.lee   it..l-20       BVEAg     rlOg   RATE bECL&(PP= Q       (o) l1hX SI
6.00E+a 1.00E+01 2.00E+Oi 0.0 TlHE lSEC)
CI Ch C)
FlCl.lee it..l-20 BVEAg rlOg RATE bECL&(PP= Q (o) l1hX SI


10.000 AEP LBLOCA FOR   3ill HMT UPRATIMC ARALYSIS MITH BART TSX l5 OFA   275 PSlC BACKFlLL 5 PCT SCTP O.B OECLG BREAK HlgSl CORE PR OROP 50.000 R 25.000 0.0 000
10.000 AEP LBLOCA FOR 3ill HMT UPRATIMC ARALYSIS MITH BART TSX l5 OFA 275 PSlC BACKFlLL 5
-'50.000
PCT SCTP O.B OECLG BREAK HlgSl CORE PR OROP 50.000 R 25.000 0.0 000
-10.000 I." ~
-'50.000
-10.000 I."~
L
L
                                                          ~ e FlC uRE         ld ~ ~-Zl     ~oRE'RE'GsuRi           DROP Dcccc Ccv=o 8)         .bfZN ag
~e FlC uRE ld ~ ~-Zl
~oRE'RE'GsuRi DROP Dcccc Ccv=o 8)
.bfZN ag
 
i


i 10.000 PEP   LSLOC1 fOR 3A I I HUl UPRAIIHG AHALYSIS Mild SARI ISa 15 OfA 215 PSIG OACKfILL 5 PCI SGIP 0.6 OECLG 6REAA rlvSI CORE PR.OROP 50.000 CL Cl 25.000 0.0
10.000 PEP LSLOC1 fOR 3A I I HUl UPRAIIHG AHALYSIS Mild SARI ISa 15 OfA 215 PSIG OACKfILL 5 PCI SGIP 0.6 OECLG 6REAA rlvSI CORE PR.OROP 50.000 CL 25.000 Cl 0.0
  -25.000
-25.000
  <0.000
<0.000
  -10.000 Cl C)
-10.000 o
CI C) o                          Al IIHE iSEC>
Cl C)
CI C)
Al IIHE iSEC>


ID.000 AEP LOLOCA FOR   311l l'V1 UPRAEIHO AHALTSIS MIIH BARE ISX l5 OFA   2)5 PSIC BACHE ILL 5 PC1 SCIP D.l OECLC BREAK HIHSI CORE   PR.OROP CI 25.000 CL'J 0.0
ID.000 AEP LOLOCA FOR 311l l'V1 UPRAEIHO AHALTSIS MIIH BARE ISX l5 OFA 2)5 PSIC BACHEILL 5
    -25.000
PC1 SCIP D.l OECLC BREAK HIHSI CORE PR.OROP 25.000 CI CL'J 0.0
    -50.000
-25.000
    -70.000 CI CI                   CI Cl CI                    CI m
-50.000
IIHE (SEC)
-70.000 CI CI IIHE (SEC)
F~@~(RE'lf.         B. l-28       CORe     F R~uAE         gpOp E>Eeoc(m= D.'/)         NX kl 8Z
CI CI Cl CI m
F~@~(RE'lf. B. l-28 CORe F R~uAE gpOp E>Eeoc(m= D.'/)
NXkl 8Z


10.000 AEP LBLOCA FOR 31 II O'Vl UPRATINC ANALYSIS VITH BART ISX I5 OFA 215 PSIG BACKFILL 5 PCT SGTP 0.6 OECLG BREAK CORE PR.OROP 50.000 IL 25 000 R.
10.000 AEP LBLOCA FOR 31 II O'Vl UPRATINC ANALYSIS VITH BART ISX I5 OFA 215 PSIG BACKFILL 5
PCT SGTP 0.6 OECLG BREAK CORE PR.OROP 50.000 IL 25 000 R.
0.0
0.0
  -25.000
-25.000
  -50.000 10i000 ED n
-50.000 10i000 ED C>n C>
C>
C>
TIVE (SEC)
TIVE (SEC)
F 1 I'4RE'0-B. I- 2't       C.ORE     f'R<5SQRE'R~I
F 1 I'4RE'0-B. I-2't C.ORE f'R<5SQRE'R~I
                                        ><C   I C-PC.D=0.4)     YlAX
><C I C-PC.D=0.4)
YlAX


2500.0 coo< URIII iAfP) O.a Offf6 HIKSI 3llIHQt UWRAIINC fccs <e<ocA ultu OARt ANO OLO PAO F0=2.IO flAD AVG.tfHP.HOt ROO   OURSt. 6.00 Ftr > PfAA. ).00 Ftt ~ i Vl 2000.0 l500.0 T
2500.0 coo< URIII iAfP) O.a Offf6 HIKSI 3llIHQt UWRAIINC fccs
a   l000.0 EJ 0.0 CI CI CI                                       CI             CI CI CI                         CI CI CI                                                   III CI tlHI tSff)
<e<ocA ultu OARt ANO OLO PAO F0=2.IO flAD AVG.tfHP.HOt ROO OURSt.
              >>~ficE     l ),3,l-~~       P~~< C~nD- TEnll~~~Tu~~
6.00 Ftr PfAA. ).00 Ftt ~i Vl 2000.0 l500.0 T
a l000.0 EJ 0.0 CI CI CI CI CI CI CI III CI CI CI CI tlHI tSff)
>>~ficE l ),3,l-~~
P~~<
C~nD-TEnll~~~Tu~~


2SOO.O COOK UNlll tAEP) 0.6 DECLC HINSI SlllHV1 UPRAllNC ECCS lRCOCA   VllN BART AND 0<D PAD fO 2.IO CLAD AVG.TEHP.HOf ROD     SURSf   5.1S foal I PEAK S.)S fAol I/I 2000.0 l500.0 X
2SOO.O COOK UNlll tAEP) 0.6 DECLC HINSI SlllHV1 UPRAllNC ECCS lRCOCA VllN BART AND 0<D PAD fO 2.IO CLAD AVG.TEHP.HOf ROD SURSf 5.1S foal I
a   l000.0 4J 500.00 0.0 CL C3                                             Cl CI Cl                                                 IA             O Vl CI                                                              AI I4 flHE lSECI
PEAK S.)S fAol I/I 2000.0 l500.0 X
a l000.0 4J 500.00 0.0 Cl C3 CI flHE lSECI Cl IA O
AI CL CI Vl I4


2500.0 COOr uKttt LAEP> O.a OECLC HtKSf SaltHVt UPRAttNC ECCS LBLOCA VltN BAR1 ANO OLO PAD F0*2.10 CLAD AVG.IEHP.VOt ROO   BuRSt. 5.15 Flt > PfAr. 7.00 Ftt ~ I 2000.0 1500.0 X
2500.0 COOr uKttt LAEP> O.a OECLC HtKSf SaltHVt UPRAttNC ECCS LBLOCA VltN BAR1 ANO OLO PAD F0*2.10 CLAD AVG.IEHP.VOt ROO BuRSt.
IL X
5.15 Flt PfAr. 7.00 Ftt ~ I 2000.0 1500.0 X
tw a   1000.0 LJ 500.00 0.0 cS                                          Cb C>                                             CI 43                                         sA Cl llHE'SEC)
ILX tw a
1000.0 LJ 500.00 0.0 C>
Cl cS 43 llHE'SEC)
Cb CI sA


~ ~
~
~


2000.0 COO< uRltt <AEPt 0.& DECLC HtRSt 3otlHMt uPRAtlRC ECCS LBI.OCA MttH SARt ARD OLD PAD to=2. lo tI.Uto tEHPERA1UAE         BuRSt. 6.00 ft< 1 PEA<. l,00 ft< ~ >
2000.0
          't50.0 l 500.0 l250.0 I
't50.0 COO< uRltt
I l000.0 t50.00 500.00 250.00 0.0 CI                                                 CI               Cl CI CI             CI             Cl CI                                          CI
<AEPt 0.& DECLC HtRSt 3otlHMt uPRAtlRC ECCS LBI.OCA MttH SARt ARD OLD PAD to=2. lo tI.Uto tEHPERA1UAE BuRSt.
                                            ~ A                                         ~ II CI ttHE <SEC)
6.00 ft<
1 PEA<. l,00 ft<~ >
l500.0 l250.0 I
I l000.0 t50.00 500.00 250.00 0.0 CI CI CI CI CI CI
~A Cl ttHE
<SEC)
CI Cl CI
~II


2000.0 COOK UNITI IAEPI O.C OECLG HINSI )LIIHVT UPRATING ECCS LBLOCA VITH QART ARO OLO PAO F0=2.IO FLUIO TEHPERATURE         BURST. S.1S ft>> I PEAK. S.PS fthm ~ )
2000.0 a
a   I)50.0 a    ISOO.O I250.0 CL I000.0 X,
I)50.0 COOK UNITI IAEPI O.C OECLG HINSI )LIIHVT UPRATING ECCS LBLOCA VITH QART ARO OLO PAO F0=2.IO FLUIO TEHPERATURE BURST.
I 3   ISO.OO S00.00 2$ 0.00 0.0 E3 C3 C) vs IIHE ISECI
S.1S ft>> I PEAK.
S.PS fthm ~)
a ISOO.O I250.0 I000.0
: CLX, I
3 ISO.OO S00.00 2$0.00 0.0 C)
E3 C3 vs IIHE ISECI


2000.0 COOK UNIlI lAEPI O.l OECLG HINSI 3i I IHU1 UPRAlING ECCS LBLOCA MIIN SARI ANO OLO PAO F0*2 10 fLUIO IEHPERAlURE         SURSF   5.)5 fll ) PEAK ).00 fll )
2000.0 I)50.0 COOK UNIlI lAEPI O.l OECLG HINSI 3i I IHU1 UPRAlING ECCS LBLOCA MIIN SARI ANO OLO PAO F0*2 10 fLUIO IEHPERAlURE SURSF 5.)5 fll )
                                                                          ~
PEAK
I)50.0 lal 1500.0 1250.0 1000.0 I
).00 fll~ )
3   )50.00 5'.OO 250.00 0.0 CI                    CI D
lal 1500.0 1250.0 1000.0 I
ofl
3
            ~
)50.00 5'.OO 250.00 0.0 Do
lIHE ISEC)
~fl CI lIHE ISEC)
CI


2000.0       COOK Ut)lTl lAEP) 0.6 OECLG HAXSl 31 l)H'LIT UPRATlNQ ECCS LBLOCA MlTH BART ANO OLO PAO F0=2. IO FLUlD TEHPERATURE         BURST ~ 5.15 FT( )   PEAK   6,00 FT)0)
2000.0 P
P l)50.0 1500.0
l)50.0 COOK Ut)lTl lAEP) 0.6 OECLG HAXSl 31 l)H'LIT UPRATlNQ ECCS LBLOCA MlTH BART ANO OLO PAO F0=2. IO FLUlD TEHPERATURE BURST ~
  )250.0 I l000.0 X
5.15 FT(
)
PEAK 6,00 FT)0) 1500.0
)250.0 I
l000.0 X
750.00 500.00 250 00 0.0 CI sn TlHE lSEC)
750.00 500.00 250 00 0.0 CI sn TlHE lSEC)
F [G QP  f  ) L.3. I -32     FLL()P TF-.YIPERATLlRE DiC LCr CCb= o.lo')
F [G QPf
) L.3. I -32 FLL()P TF-.YIPERATLlRE DiC LCr CCb= o.lo')


1000.0 ACP LBLOCA FOR jA I I HUT UPRATIIIG AIIALYSIS VITH BART ISx IS OFA 215 PSlC BACKFILL 5 PCT SGTP 0.8 OCCLC BRf AX HIRSI 2-FLOUR>lf CORf BOlTOH     I I TOP ~   I~ I 5000.0 2500.0 CI 0.0
1000.0 ACP LBLOCA FOR jA I I HUT UPRATIIIG AIIALYSIS VITH BART ISx IS OFA 215 PSlC BACKFILL 5
  -2500.C
PCT SGTP 0.8 OCCLC BRf AX HIRSI 2-FLOUR>lf CORf BOlTOH I I TOP
  -5000.0
~
  -1000.0 Cl                                       Cl Cl                                               Cl Cl                       Cl Cl                                                 Cl Cl                       m CI                        Al TIHf <SfCI Fy@~Rg         ]q g )-33         pygmy       FI II~(TN &MD 3$ TTDYI)
I~ I 5000.0 2500.0 CI 0.0
DecLc       (cI =08) N' 8T
-2500.C
-5000.0
-1000.0 Cl CI Cl Cl Cl Cl Al TIHf <SfCI Cl Cl Cl m
Cl Fy@~Rg
]q g )-33 pygmy FI II~(TN &MD 3$ TTDYI)
DecLc (cI =08)
N'8T


1000.0 AEP LBLOCA FOR 3l I!. HV'I UPRAEIIIC AIIALYSIS VIIN BARf 15115 OFA 2)5 PSIG BACKFILL 5 PCI SG'IP 0.6 OECLC BREAK HIHSI 2-FLOVRAIE (OR~ 80110H       I I   10P I   1 ~ 1 5000.0 2500.0 I
1000.0 AEP LBLOCA FOR 3l I!. HV'I UPRAEIIIC AIIALYSIS VIIN BARf 15115 OFA 2)5 PSIG BACKFILL 5 PCI SG'IP 0.6 OECLC BREAK HIHSI 2-FLOVRAIE (OR~
80110H I
I 10P I
1 ~ 1 5000.0 2500.0 I
0.0
0.0
  -2500.I3
-2500.I3
  -5000.0
-5000.0
  -)000.0 CI                      CI                          CI C)                     CI                         4D CI                     CI                         CI
-)000.0 CI C)
                                  ~ II                       m I!HE ISE C I FZG IIRE     Ig 3. (-g.'I       QORE           V'LOW CT boccie- (c.p= o     t )
CI CI CI CI
~II I!HE ISE C I CI 4D CI m
FZG IIRE Ig 3. (-g.'I QORE V'LOW CT boccie- (c.p= o t )
 
1000.0 ACP LBLOCA fOR 34 II HVT UPRATIHG AHALYSIS UITH BART ISl l5 OfA 215 PSIG BAC<fILL 5.PCT SGTP O.l OCCLG BREAK ~IHSI 2 fLOVRATK CORC BOTTOH I
)
: TOP, l~ I Ll Vl CQ 5000.0 2500.0
~aI 0.0
-2SOO.O
-5000.0
-1000. 0 CI IV TIllC (SIC)


1000.0 ACP LBLOCA fOR 34 II HVT UPRATIHG AHALYSIS UITH BART ISl l5 OfA 215 PSIG BAC<fILL 5.PCT SGTP O.l OCCLG BREAK ~IHSI 2 fLOVRATK CORC    BOTTOH  I ) TOP,      l~ I 5000.0 Ll Vl CQ 2500.0
0
~a I
0.0
  -2SOO.O
  -5000.0
  -1000. 0 CI IV TIllC (SIC)


0 7000.0 AEP LBLOCA FOR 3ell HMT UPRATINC ANALYSIS MITH BART ISX l5 OFA 275 PSIG BACKFILL 5 PCT SCTP           0.6 OECLC BREAK 7-FLOMRATE CORE   BOTTOH I ) TOP ~ (+)
7000.0 AEP LBLOCA FOR 3ell HMT UPRATINC ANALYSIS MITH BART ISX l5 OFA 275 PSIG BACKFILL 5
5000.0 EJ 4%
PCT SCTP 0.6 OECLC BREAK 7-FLOMRATE CORE BOTTOH I
2500.0 I
)
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5000.0 2500.0 I
o I
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0.0
0.0
    -2500.0
-2500.0
    -5000.0
-5000.0
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-7000.0 CS C)
P)QQ+E     [Q 3 }   Q(z   Q,QQg PLDW             ESTOP AND   BOTTOPl)
ID C)
Pggl ~ggb =O. a)                 M AX  Bg
CU T I >) 6 (5:. C )
C1 Cl CI m
Cl P)QQ+E
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Pggl ~ggb =O. a)
MAX Bg


20.000 AEP UPRAIIHG CD D.R OECLG RK HlkSl QART-REFL000 27S RXPlLL PRESSURE lS17$ ofA UATER LEVELIfll l7.500 90MHCoWER l$ .000 l2.S00 l0.000 g
20.000 l7.500 AEP UPRAIIHG CD D.R OECLG RK HlkSl QART-REFL000 27S RXPlLL PRESSURE lS17$ ofA UATER LEVELIfll l$.000 90MHCoWER l2.S00 l0.000 g
LJ 7.5000 J
LJ 7.5000 J
~ s.oooo 2.5000 0.0 CI CI                                 CI TIVE <SEC)
~
FT~upp       iq.3.(-2 I     'REFLooD Y'RAASZ<PL ba+NCONER WA EaL     L EVILS
s.oooo 2.5000 0.0 CI CI CI TIVE <SEC)
                                            ~eC.~~<   C,E =O.G) ~X~ aZ
FT~upp iq.3.(-2 I
'REFLooD Y'RAASZ<PL ba+NCONER WA EaL L EVILS
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20.000 AEP UPRATIHC Coco.g OECLG Ba HIHSI PART-REELOOO 2TS &<FILL PRESSVRE TSx TS OFA MATER LEVELLETT IT.500
20.000 IT.500 AEP UPRATIHC Coco.g OECLG Ba HIHSI PART-REELOOO 2TS
                                                          ~WHCOPlEA.
&<FILL PRESSVRE TSx TS OFA MATER LEVELLETT IS.OOO
IS.OOO I2.500 IO.OCO D T.SOOO 5.0000 2.5000 9.0 CI CI CI                     CI CI CD CI                     CI CI                      ~ II C7 TIME iSEC'el Fggqgg       l'l,3. I-SS   RE'T=LOOP W A TER, LEVELS aeCLa CCO-     O.r.)
~WHCOPlEA.
I2.500 IO.OCO D
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tO.COO Af~ u<<<<lhC     CO:0.~ Of fC 84 >I'aSI 8>>f.~(<F003
tO.COO Ig SOO IS.OCO Af~ u<<<<lhC CO:0.~
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DowNComCR IS.OCO It. S03 I0.000
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DoWllCornER LnJATE. R LEVEm De.C.I I I f g=O.1) frlXN SX


20.000 AEP uPRALIHC (0=0.6 OEElC Ba HAISI SART-REFL000 215 SAIILL PRESSuRE   ISIls ofA MALER LEVEL{F1)
20.000 11.500 AEP uPRALIHC (0=0.6 OEElC Ba HAISI SART-REFL000 215 SAIILL PRESSuRE ISIls ofA MALER LEVEL{F1)
Oowgc,omEP.
Oowgc,omEP.
11.500 L5.000 12.500 Io.ooo
L5.000 12.500 Io.ooo
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CORE PgQ   QgP     )q. 3. l - QO   RFFLOotO TRAHSZEH>
CI CI
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2.0000 AEP UtRAIINC CD 0.$ OECLC BK HINSI BARI-REFLOOD 27$ REFILL tRESSORE ISX IS OFA FLOOD RAIELIIIISEC) 1.7500 1.5000 1.2500 u   I.OOM
2.0000 1.7500 AEP UtRAIINC CD 0.$
~ 0.75M CC CI CI 0.5000 0.2500 0.0 8
OECLC BK HINSI BARI-REFLOOD 27$
CI Cl ~ n fIHE (SEC)
REFILL tRESSORE ISX IS OFA FLOOD RAIELIIIISEC) 1.5000 1.2500 u
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gPPLQQD TR IH I e.O~~
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2.0000 AEP   uPRitIRC CO=0.6 OECLC Ba HIHSI SiRt-PEFL000 275 SwtlLL PRESSURE l51 IS OFA I'L000 RAIE{IR/SEC)
, 2.0000 I.)500 AEP uPRitIRC CO=0.6 OECLC Ba HIHSI SiRt-PEFL000 275 SwtlLL PRESSURE l51 IS OFA I'L000 RAIE{IR/SEC)
I.)500 I. 5000 l.2500 u     I.0000 0.7500 IC CI CI 0.5000 0.2500 0.0 ID                  CI CI                                             CI                   CI CI                   CI Al                    m tIVE LSECl F~gggE           Iq,3. /- 'l2. RE I. LOO+     TRhg SX
I.5000 l.2500 u
                                                        ~pl PT'E
I.0000 0.7500 IC CI CI 0.5000 0.2500 0.0 CI CI Al tIVE LSECl ID CI CI m
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CI CI F~gggE Iq,3. /- 'l2.
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ATTACHMENT 8 LOCA Rci   A-"0 -."CH SPECS Plant Name:       Oonald C. Cook Unit   1 (AFP)
ATTACHMENT 8 LOCA Rci A-"0 -."CH SPECS Plant Name:
O.lp Tyoe/Date o                   0C
Oonald C.
                                  = ~-4   (max SI case)   Large Break LOCA Analysis Analysis 'OCA Df'Qg Total Peaking Factor F~.             ~     g ,'IQ Cold Leg Accumula or.         980   ft /accumulator     (nominal) unchanged -,rom Water Yolume:                  cur rent tech specs Cold Leg Accumulator           600   psia (minimum) unchanged from current Gas  Pressure:                tech specs K(z) Cu. ve:                 See   next page
Cook Unit 1
(AFP)
Tyoe/Date o
'OCA Analysis O.lp 0C
= ~-4 (max SI case)
Large Break LOCA Analysis Df'Qg Total Peaking Factor F~. ~ g,'IQ Cold Leg Accumula or.
Water Yolume:
980 ft /accumulator (nominal) unchanged
-,rom cur rent tech specs Cold Leg Accumulator Gas Pressure:
600 psia (minimum) unchanged from current tech specs K(z) Cu. ve:
See next page


1.5000 AEP   4         LOOP CALC. NOTE     SEC-RFFA-1481-CO f
1.5000 AEP 4
CURR NT LIH ITS  RUN           05/15/84 K(Z) l/S. CORE KE ICHT (FICURE 1.2500 1.0000 0.7500
LOOP CALC.
~V 0.5000 TOTAL FO
NOTE SEC-RFFA-1481-CO CURRfNT LIHITS RUN 05/15/84 K(Z) l/S.
: 2. 100 CORE       REICHT 0   'g<
CORE KE ICHT (FICURE 1.2500 1.0000 0.7500
              .al'ii
~V 0.5000 0.2500 TOTAL FO
                      ~
: 2. 100 CORE REICHT 0
                        ~ s
'g< ~ ~ s c.al'ii I I. I83 12.000
: l. Oon 0.2500 c                            1.000 I  I. I83                    0.935 12.000                        0.714 0.0 nCJ            C1 nn Q ~
: l. Oon 1.000 0.935 0.714 0.0 Q ~nn EU n
CD CJ             ca C3 EU                                    lO             OO CORE   HEICHT (FT)
CJ CJ lO CORE HEICHT (FT)
C1 CD ca C3 OO


    ~
~
c,~}}
c,~}}

Latest revision as of 13:38, 7 January 2025

Application for Amend to License DPR-58,revising Tech Specs to Extend Fuel Peak Pellet Burnup & Increase Fq Value Limit in Fuel.Fee Paid
ML17334A814
Person / Time
Site: Cook American Electric Power icon.png
Issue date: 08/23/1984
From: Alexich M
INDIANA MICHIGAN POWER CO. (FORMERLY INDIANA & MICHIG
To:
Shared Package
ML17334A815 List:
References
AEP:NRC:0745M, AEP:NRC:745M, NUDOCS 8409050167
Download: ML17334A814 (130)


Text

1 ~

REGULATOR'r INFORMATION DISTRIBUTION SYSTEM (RIDS)

'ACCESSION NB/ 8009050167, DOC ~ DATE e 84/08/23 NOTARIZED!"'O DOCKET ¹ FACIL:50 315 Donald C ~

Cook Nuclear Power Pl anti Unf t 1, Indiana-8 05000315 AUTH~ NAME AUTHOR AFFILIATION ALEXICHiM~ P.

Indiana L Michigan Electric Co.

RECIP, NAME RECIPIENT AFFILIATION 05000315 SUBJECT! Application for amend to License OPR 58 revising Tech Specs to extend fuel peak pellet burnup L increase FQ value limit in fuels Fee paido DISTRIBUTION CODE:

A001D COPIES.RECEIVED:LTR g' ENCL SIZE:~ 3 Qs~ fly&

TITLE:

OR Submittal!

General Distribution NayES.P><

~ P4f get oc OL i 1 0/25/74,',.

'XTERNALS ACRS NRC POR NTIS 09 02 REC I'P-I:.EN,T ID COOg/NAME NRR ORBi BC 01 INTERNAL: ADM/LFMB NRR/DE/MTEB NRR/OL/ORAB NRR/OS I/RAB RGN3 COPIES LTTR ENCL 7

7 1

0 1

1 1

  • 0 1-1 1

1 6

6 1

1 1

ELO/HDS3.

NRR/DL DIR N

4ETB EG FI E

00 1

0 1

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INDIANA& MICHIGAN ELECTRIC COMPANY P.O. BOX 16631 COLUMBUS, OHIO 43216 August 23, 1984 AEP: NRC: 0745M Donald C.

Cook Nuclear Plant Unit No.

1 Docket No. 50-315 License No. DPR-58 TECHNICAL SPECIFICATION CHANGE REQUESTS Mr. Harold R. Denton, Director Office of Nuclear Reactor Regulation U.S. Nuclear Regulatory Commission Washington, D.

C.

20555

Dear Mr. Denton:

By this letter and its attachments, we request changes to the Technical Specifications for the Donald C.

Cook Nuclear Plant Unit No.

1.

The proposed revised Technical Specification pages are contained in Attachment A.

The reasons for the proposed changes to the Technical Specif'ications, and the Justifications that the changes do not involve significant hazards considerations, are contained in Attachments B and C to this letter.

The changes described in Attachment B involve extending the peak pellet burnup in fuel supplied by Exxon Nuclear Company from 42,200 MWD/MTU (42.2 %0)/KG) to 48,000 MWD/MTU (48.0 MWD/KG).

These changes are supported by a LOCA Analysis and additional information regarding mechanical

design, which was sent to you directly by Exxon Nuclear Company with letter JCC:113:84, dated August 21, 1984.

The current burnup limit is expected to be reached on November 30, 1984.

Without this burnup extension, we would be unable to continue operation of Cycle 8

because of the requirements of Technical Specification Section 3.2.2.

The changes proposed in Attachment C and supported by Attachment D involve an increase in the F limit in fuel supplied by Westinghouse f'rom 1.97 to 2.10. It should be noted that part of this analysis is based on use of the BART code, which has not been previously used for the Donald C.

Cook Nuclear Plant, Unit 1 ~

These proposed changes have been reviewed by the Plant Nuolear Safety Review Committee (PNSRC) and will be reviewed by the Nuclear Safety and Design Review Committee (NSDRC) at their next regularly scheduled meeting.

In compliance with the requirements of 10 CFR 50.91(b)(1),

a copy of'his letter and its attachments have been transmitted to Mr. R.

C. Callen of the Michigan Public Service Commission.

8409050167 840823 PDR ADOCK 050003l5 F'

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Mr. Harold R. Denton AEP: NRC: 0745M Pursuant to 10 CFR 170.12, we have enclosed a check in the amount of $150.00 as payment for the application fee for the proposed amount.

This document has been prepared following Corporate procedures which incorporate a reasonable set of controls to insure its accuracy and completeness prior to signature by the undersigned.

Very truly yours, M

. Ale ich Vice Preeidect

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Mr. Harold R. Denton

~\\3 AEP: NRC:0745M Attachments:

A.

Proposed Revised Technical Specifications Pages for D.C.

Cook Unit 1.

B.

Reasons for the extension of the peak pellet burnup allowed in fuel supplied by Exxon Nuclear Company and Justification that the changes do not involve significant hazards considerations.

C.

Reasons for the increase in F~ for fuel supplied by Westinghouse.

D.

"D.C. Cook Unit 1 3411 MWt Large Break LOCA Analysis", Westinghouse Electric Corporation,

June, 1984.

cc: John E. Dolan W. G. Smith, Jr. - Bridgman R.

C. Callen G. Charnoff E.

R. Swanson, NRC Resident Inspector - Bridgman

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Mr. Harold R. Denton AEP: NRC: 0745M Attachment D

"D.C. Cook Unit 1 3411 MWt Large Break LOCA Analysis",

Westinghouse Electric Corporation,

June, 1983.>>

'This document has been piepared by Westinghouse Electric Corporation in a format foi eventual inclusion in the Donald C; Cook Nuolear Plant FSAR.

Although this is ~o intended for that purpose at this time, the format has been retained for convenience.

14.3.1.1 Major LOCA Analyses Applicable to Westinghouse Fuel Identification of Causes and Fre uenc Classification

-A loss-of-coolant accident (LOCA) is the result of a pipe rupture of the RCS pressure boundary.

For the analyses reported

here, a major pipe break

( large break) is defined as a rupture with a total cross-sectional area equal to or greater than 1.0 ft This event is considered an 2

ANS Condition IV event, a,limiting fault, in that it is not expected to occur during the lifetime of D.

C.

Cook Unit 1, but is postulated as a

conservative design basis.

The Acceptance Criteria for the LOCA are described in 10 CFR 50.46 (30 CFR 50.46 and Aopendix K of 10 CFR 50 1974) as follows:

1.

The calculated peak fuel element clad temperature is below the requirement of 2,200'F.

2, The amount of fuel element cladding that reac;s chemically with water or steam does not exceed 1 percent of:he total amount of 2ircaloy in the reac or.

3.

The clad temoerature transient is terminated at a time when the core aeometry is still amenable to cooling.

The locali-ed cladding oxidation limit of 17 percent is not exceeded d ring or af er quenching.

4.

The core remains amenable to cooling during and after :he break.

5.

The core temperature is reduced and decay heat is removed for an

'I

..'xtended period of time, as required by he long-lived "radioactivity".

remaining in the core.

These criteria were established to provide significant margin in emergency core cooling system (ECCS) performance following a LOCA.

WASH-1400 (USNRC 1975) presents a recent study in regards to the probability of occurrence of RCS pipe ruptures.

Se uence of Events and S stems 0 erations Should a major break occur, depressurizaton of the RCS results in a pressure decrease in the pressurizer.

The reactor trip signal subsequently occurs when the pressurizer low pressure trip setpoint is reached'.

A safety injection signal is generated wnen the appropriate setpoint is reached.

These countermeasures will limit the consequences of the accident in two ways:

1.

Reactor trip and borated water injection supplement void formation in causing rapid reduction of power to a residual level corresponding to fission product decay heat.

However, no credit is taken in the LOCA analysis for the boron content of the injection water.

In addition, the insertion of contr".'.

rods to shut down the reactor is neglected in the large break analysis.

2.

Injection of borated water provides for heat transfer rrom the core and prevents excessive clad temperatures.

Oescr ation of Large Break Loss-of-Coolant Accident Transient The sequence of events following a large break LOCA is p".esen ed in Table

14. 3. 1-6.

Before the break occurs, the unit is in an equilibrium condition; that is, the heat generated in the core is being removed via the secondary system.

Ouring blowdown, heat from fission product decay',

hot internals and the vessel, continues to be transferred to the reactor coolant.

At the beginning of the blowdown phase, the entire RCS contains subcooled liquid which transfers heat from the core by forced convection with some fully developed nucleate boiling.

After the break develops, the time to departure from nucleate boiling is calculated, consistent with Appendix K of 10 CFR 50.( 'hereafter the core heat transfer is (1)

unstable, with both nucleate boiling and film boiling occurring.

As the core becomes uncovered, both turbulent and laminar forced convection and radiation are considered as core heat transfer mechanisms.

The heat transfer between the RCS and the secondary system may be in either direction, depending on the relative temperatures.

In the case of continued heat addition to the secondary

system, the secondary system pressure increases and the main steam safety valves may actuate to limit the pressure.

makeup water to the secondary side is automatically provided by the emergency feedwater

.system.

The safety injection signal ac uates a feedwater isolation signal which isoiaies normal feedwater flow by closing the main feedwater isolation valves, and also initiates emergency feedwater flow by starting the emergency feedwater pumps.

The secondary flow aids in the reduction of RCS pressure.

'>)hen the RCS depressurizes to 600 psiz, the accumulators begin to inject borated water into the reactor coolant loops.

The conservative assumption is made that accumulator water injec ed bypasses the core and goes out through the break until the termination of bypass.

This conservatism is again consistent with Appendix K of 10CFRSO.

Since loss of offsite power (LOOP) is assumed, the RCPs are assumed to trip at the inception of'the accident.

'The e'ffects of'ump coastdown are i'nc'luded

'n the blowdown analysis.

The blowdown phase of the transient ends when the RCS pressure (initially assumed at 2280 psia) falls to a value approaching that of the containment atmosphere.

Prior to or at the end of the blowdown, the

mechanisms that are responsible for the emergency core cooling water injected into the RCS bypassing the core are calculated not to be effective.

At this time (called end-of-bypass) refill of the reactor vessel lower plenum begins.

Refill is completed when emergency core cooling water has filled the lower plenum of the reactor vessel, which is bounded by the bottom of the fuel rods (called bottom of core recovery time).

The reflood phase of the transient is defined as the time period lasting from the end-of-refill until the reactor vessel has been filled with water to the extent that the core temperature rise has been terminated.

From the latter stage of blowdown and then the beginning-of-reflood, the safety injection accumulator tanks rapidly discharge borated cooling water into the RCS, contributing to the filling of the reactor vessel downcomer.

The downcomer wa'ter elevation head provides the driving force required for the reflooding of the reactor core.

The low head and high head safety injec ion pumps aid in the filling of the downcomer and subsequently supply water to maintain a full downcomer and complete the reflooding process.

Cont'inued operation of the ECCS pumps supplies wa er during longterm cooling.

Core temperatures have been reduced to longterm steady state levels associated with dissipation of residual heat generation.

After tne water level of the residual water s orage tank (RWST) reaches a

minim m allowable value, coolant for long-tern cooling of the core is obtained by switching to the cold recirculation phase of opera ion, in which spilled borated wa er is drawn from the engineered safety ea ures (ESF) containment sumps by the low head safety injection (residual heat removal) pumps and returned to the RCS cold legs.

The containment spray system continues to operate to further reduce containment pressure.

r r.

Approximately 24 hours2.777778e-4 days <br />0.00667 hours <br />3.968254e-5 weeks <br />9.132e-6 months <br /> 'after initiation of the LOCA, the ECCS is realigned to supply water to the RCS hot legs in order to control the boric acid concentra-ion in the reactor vessel.

Core and S stem performance Mathematical Model:

The requirements of an acceptable CCS evaluation model are presented in Appendix K of 10 CFR 50 (Federal Register 1974). (1)

Large Break LOCA Evaluation Model The analysis of a large break LOCA transient is divided into three phases:

(1) blowdown, (2) refill, and (3) ref lood.

There are three distinct transients analyzed in each

phase, including the thermal-hydraulic transient in the
RCS, the pressure and temperature transient within the containment, and the fuel and clad temperature transient of the hottest fuel rod in the core.

Based on these considerations, a system of interrelated computer codes has been developed for the analysis of the LOCA.

A description of the various aspects of the LOCA analysis methodology is given by Bordelon, Massie, and 2ordan

( 1974).

Tnis document (6) describes the major pnenomena

modeled, the inter-.aces among the computer
codes, and the features of the codes which ensure comoliance with the Acceptance Criteria.

The SATAN-'ll, WREFLGO0, BART and LOCTA-IV codes, wnich are used in the LOCA analysis, are described in detail by Bordelon et al. (1974)( 'elly et al.

(1974)

'; Young et al.

(5)

(9)

(4)

(1980);

Bordelon and Murphy (1974)( ';

and Bordelon et al.

/~X

( 1974).

Code modifications are specified in References 2,

7 and 13.

These codes assess the core heat transfer geometry and determine if the core remains amenable to cooling throughout.and subsequent to the blowdown, refill, and reflood phases of the LOCA.

The SATAN-V1 computer,

~,

' co'de'nalyzes the thermal-hydraul'ic;'transi'ent in 'the RCS during blowdow'n and the WREFLOOO computer code calculates thi's transient during the refill and reflood phases to the accident.

The LOTiC computer

code, described by Hsieh and Raymund in

0

WCAP-8355 ( 1975) and WCAP-8345 ( 1974)

, calculates the containment (3) pressure transient.

The containment pressure transient is input to WREFLOOO for the purpose of calculating the reflood transient.

The LOCTA-IV computer code calculates the thermal transient of the hottest fuel rod during the three phases.

The standard Pad Fuel Thermal Safety Model, described in Reference 15, generates the initial fuel rod conditions input to LOCTA-IV.

SATAN-VI calculates the RCS pressure, enthalpy, density, and the mass and energy flow rates in the

RCS, as well as steam generator energy transfer between the primary and secondary systems as a function of time during the blowdown phase of the LOCA.

SATAN-VI also calculates the accumulator water mass and internal pressure and the pipe break mass and energy flow rates that are assumed to be vented to the containment during blowdown.

At the end of the blowdown phase, these data are transferred to the WREFLOOD code.

Also, at the end-of-blowdown, the mass and energy release rates during blowdown are input to the LOTIC code for use in the determination of the contai.",".ien pressure response during <<his first phase of the LOCA.

Additiona',

SATAN-VI outout data from the end-of-blowdown, including the core inlet flow rate and

enthalpy, the core pressure, and the core power decay transi'ent, are input to the LOCTA-IV code.

With input from the SATAN-VI code, WREFLOOO uses a system thermal-hydraulic model to determine the core flooding rate (".hat is, he rate at wnich coolant enters the bottom of'he core),

he cool-ant pressure and"temperature, and the quench front height during the reflood phase of the LOCA.

WREFLOOO also calculates the mass and energy flow addition to the containment through the break.

WREFLOOO is also linked to the BART and LOCTA-IV codes.

The heat transfer calculation for the I

7 II

, average fuel channel in the hot assembly during the ref lood phase of the

~

LOCA is performed by the BART'omputer code using a mechanistic (16) core heat transfer model.

This information is then used by LOCTA-IV throughout the analysis of the LOCA transient to calculate the fuel clad temperature and metal-water reaction of the hottest rod in the core.

The large break analysis was performed with the December 1981 version of (16) the Evaluation Model modified to incorporate the BART computer code.

Input Parameters and Initial Conditions:

The analysis presented in, this section was performed with a reactor vessel upper head temperature equal to the RCS hot leg temperature.

The bases used o select the numerical values that are input parameters to the analysis have been conservatively determined from extensive sensitivity studies (Westinghouse 1974

Salvatori 1974 (12).

~

(11).

Johnson, Hassle, and Thompson 1975

).

In addition, the requirements (8) of Appendix K regarding specific model 'features were met by selecting models which provide a significant overall conservatism in the analysis.

The assumptions which were made pertain to the conditions of the reactor and associated safety system equipment at the time that the LOCA occurs, and include such items as the core oeaking factors, the containment

pressure, and the performance or the

=CCS.

Gecay heat generated throughout the transient is also conservatively calculated.

A meeting was held at :he Mestinghouse Licensing Office in Bethesda on Oecember 17, 1981 between members of the U.

S. Nuclear Regulatory Commission and members of tne Mestinghouse Nuclear 'Safety Oepartment to discuss the impac. of maximum safety injection on the large break ECCS analysis on a generic basis.

Further discussion of this issue is provided in a letter from E.

P.

Rahe, Manager of Westinghouse Nuclear Safety Oepartment, to Robert L. Tedesco of the U.

S. Nuclear Regulatory Commission.(,

A brief description of this issue is given below.

(14)

.,Mestihghause ECCS analyses currently: assume. minimum s'afeguards for the

~

safety injection flow, which minimizes the amount of flow to the RCS by

~

assuming maximum injection line resistances, degraded ECCS pump performance, and the loss of one residual heat removal (QHR) pump as the most limiting single failure.

This is the limiting single failure assumption when offsite power is unavailable for most Westinghouse

~

~

plants.

However, for some Westinghouse plants including 0.

C.

Cook Unit 1, the current nature of the Appendix K ECCS evaluation models is such that it may be more limiting to assume the maximum possible ECCS flow delivery.

In that case, maximum safeguards which assume minimum injection line resistances, enhanced ECCS pump performance, and no single failure, result in the highest amount of flow delivered to the RCS.

Current LOCA analysis for 'the 0.

C.

Cook Unit 1 has demonstrated

that, maximum safeguards assumptions result in he highest peak clad temperatur'e.

Therefore, the worst break for O.

C.

Cook (CO = 0.6) was re-analyzed, assuming maximum safeguards.

Results:

Based on the results of the LOCA sensitivity studies (Westinghouse 1974

Salvatori 1974
Johnson,
Massie, and Thompson 1975

) the limiting large break was found to be the double ended cold leg guillotine (OECLG).

Therefore, only the OECLG break is considered in the large break ECCS performance analysis.

Calculations were performed for a range of Moody break discharge coefficients.

The results of these calculations are summarized in Tables 14.3. 1-5 and 14.3.1-6.

The containment data used to generate the LOTIC backpressure transient are shown in Table 14.3. 1-1.

The mass and energy release data ror the minimum and maximum safeguards cases are shown in Tables 14.3. 1-2 and 14.3. 1-3 respectively.

Nitrogen release rates to the containment are given in Table 14.3.1-4.

Figures 14.3. 1-1 through 14:3. 1-54.present the transients for the

'I principal parameters 'for the break size's analyzed.

The following items are noted:

Fi ures 14.3.1-1 throu h 14.3.1-12 The following quantities are presented at the clad burst location and at the hot spot (location of maximum clad temperature),

both on the hottest fuel rod (hot rod):

1.

fluid quality; 2.

mass velocity; 3.

heat transfer coefficient.

The heat transfer coefficient shown is calculated by the LOCTA-IV code.

Fi ures 14.3.1-13 throu h 14. 3. 1-24 The system pressure shown is the calculated pressure in the core.

The flow rate from the break is plotted as the sum of both ends for the guillotine break cases.

The core pressure drop shown is from the lower plenum, near the core, to the upper plenum at the core outlet.

Figures 14.3.1-25 throu h 14. 3. 1-36 These figures show the hot spot clad temperature transient and the clad temp rature transient at the burst location.

The fluid emperature shown is also for the hot spot and burst location.

The core flow (top and bottom) is also snown.

Figures 14.3. 1-37 These figures show he core rerlood transient.

through 14.3. 1-44 Figures 14.3. 1-45 throu h 14. 3. 1-52 These figures show the mergency Core Cooling System flow for all of the cases analyzed.

As described earlier, the accumulator delivery during blowdown is discarded until the.end of bypass is calculated.

Accumulator 'flow:, however, is established in the refill and the reflood calculations.

The accumulator flow assumed is the sum of that injected in the intact cold legs.

Fi ures 14.3. 1-53 throu h 14.3.1"54 The containment pressure transient used in the analysis is also provided for the minimum and maximum SI cases.

Figures 14.3.1-55 and 14.3.1-60 These figures show the heat removal rates of the heat sinks found in the lower compartment and the heat removal by the lower containment drain, andthe heat removal by the sump and LC sprays (minimum and maximum SI cases).

Fi ures 14.3.1-61 throu h 14. 3. 1-64 These figures show the temperature transients in both the upper and lower compartments of the containment and flow from the upper to lower compartments.

Total heat removal in the lower compartment is the sum of all the heat removal rates shown (for minimum and maximum SI cases).

The maximum clad temperature calculated for a large break is 2163 F,

which is less than the Acceptance Criteria limit of 2200~F.

The maximum local metal-water reaction is 9.65,percent, which is well below the embrittlement limit.of 17 percent as required by 10 CFR 50.46.

The

otal core metal-water reaction is less than 0.3 percent for all breaks, as compared with the 1 percent criterion of 10 CFR 50.46.

The clad temperature transient is terminated at a time when the core geometry is still amenable to cooling.

As a result, the core temperature will continue o drop and the ability to remove decay heat generated in the fuel for an extended period of time will be provided.

10

References for Section 14.3. 1. 1 1.

"Acceptance Criteria for Emergency Core Cooling System for Light Water Cooled Nuclear Power Reactors,"

10 CFR 50.46 and Appendix K of 10 CFR 50, Federal Re ister

1974, Volume 39, Number 3.

2.

Rahe, E.

P. (Westinghouse),

letter to J.

R. Miller (USNRC); Letter No. NS-EPRS-2679, November 1982.

3.

Hsieh, T.,

and

Raymund, M., "Long Term Ice Condenser Containment LOTIC Code Supplement 1," WCAP-8355, Supplement 1,

May 1975, WCAP-8345 (Proprietary), July 1974.

4.

Bordelon, F.

M. et "al., "LOCTA-IV Program:

Loss-of-Coolant Transient Analysis," WCAP-8301 (Proprietary) and WCAP-8305 (Non-proprietary),

1974.

5.

Bordelon, F.

M. et al.,

"SATAN-VI Program:

Comprehensive

Space, Time Oependent Analysis of Loss-of-Coolant,"

WCAP-8302 (Proprietary) and WCAP-8306 (Non-proprietary),

1974.

6.

Bordelon, F. M.; Massie, H. W.; and 2ordan, T. A., "Westinghouse ECCS Evaluation Model - Summa'ry,"

WCAP-8339, 1974.

7.

Rahe, E. P.,

"Westinghouse ECCS Evaluation Model, 1981 Version,"

WCAP-9220-P-A (Proprietary Version),

WCAP-9221-?-A (Non-proprie~ry version),. Revision 1,

1981.

8.

Johnson, W. J.; Massie, H. W.; and
Thompson, C. M., "Westinghouse ECCS - Four Loop Plant (17x17) Sensitivity Studies,"

WCAP-8565-P-A (Propr'ietary) and WCAP-8566-A (Non-proprie't'ary),

1975.

PP 9.

Kelly, R. 0. et al., "Calculational Model for Core Ref looding After" a Lo'ss-of-Coolant Accident (WREFLOOO Code),"

WCAP-8170 (Proprietary) and WCAP-8171 (Non-proprietary),

1974.

10 U. S. Nuclear Regulatory Commission 1975 "Reactor Safety Study - An Assessment of Accident Risks in U.

S.

Commercial Nuclear Power Plants,"

WASH-1400, NUREG-75/014.

11. Salvatori, R., "Westinghouse ECCS - Plant Sensitivity Studies,"

WCAP-8340 (Proprietary) and WCAP-8356 (Non-proprietary),

1974.

12.

"Westinghouse ECCS - Evaluation Model Sensitivity Studies,"

WCAP-8341 (Proprietary) and WCAP-8342 (Non-proprietary),

1974.

13. Bordelon, F. H., et al.,

"Westinghouse ECCS Evaluation Model-Supplementary Information," WCAP-8471 (Proprietary) and WCAP-8472 (Non-proprietary),

1975; 14.

Rahe, E.

P. (Westinghouse).

Letter to Robert L. Tedesco (USNRC),

Letter No. NS-EPR-2538, Oecember 1981.

15. Letter from J.

F. Stoltz (NRC) to T.

M. Anderson (Westinghouse);

subject:

Review of WCAP-8720, Improved Ana'.ytical 4lodels Used in Westinghouse Fuel Rod Oesign Computations.

16.

Young, 4I. Y., et al.,

"BART-Al:

A Computer Code for he Best Estimate Analysis of Reflood Transients, "WCAP-9561-P-A (Proorietary) and WCAP-9695"A (Non-Proprietary)

January 1980.

12

TABLE 14.3

~ 1-1 LARGE BREAK CONTAINMENT DATA

( ICE CONDENSER CONTAINMENT)

NET FREE VOLUME

( Includes Distribution Between

Upper, Lower, and Dead-Ended Compartments)

UC LC OE IC 746,829'ft.

249,446 116,168 122,400 Initial Conditions Pressure Temperature for the Upper, Lower and Dead-Ended Compartments RWST Temperature Service Mater Temperature Temperature Outside Containment Initial Spray Temperature 14.7 psia UC 100~ F LC 120~ F OE 120oF 70~F 40oF 7oF 70~F Spray System Burnout Flow for a Spray Pump Number of Spray Pumps Operating Post-Accident Initiation of Spray System Ois ribution of the Spray Flow to the Upper and Lower Compartments 3600 gpm 2

40 secs LC 2835 gpm UC 43o5 gpm Deck Fan Post-Accident Initiation of Deck Fans Flow'at,e Per Fan 600 secs

~ 39,000 cfm per'ran

'I Hydrogen Skimmer System Flow Rate 2800 cfm per ran Assumed Spray Efficiency of Mater from Ice Condenser 'Drains 100'o 13

TABLE 14. 3 1 ~ 1

'continued)

STRUCTURAL HEAT SENKS i

2 blateri a 1 1.

LC 2.

LC 3.

LC 4.

LC 5.

LC 6.

LC 7.

LC 8.

LC 9.

LC 10.

LC 11.

LC 12.

LC 13.

UC 14.

UC 15.

UC 16.

UC 17.

UC 18.

UC 19.

UC 12,105 11,700 65,980 5,481 4,735 289 14,690 3,439 5,775 4,966 7,013 2,457 378 29,772 8,033 420 29,330 34 125 2'10 0.0469/2.0 2.0 1.35 0.0833 0.01147 0.25 0.0079 0.1561 0.009 0.0096 0.037 0.0334

.1667/.0365

.0092

.0209

.0052 1.47 0.0469/2.0

.0052 steel/concrete concrete concrete steel steel lead steel steel steel steel steel steel steel/concrete steel steel s eel concrete steel/concrete steel UC:

Upper Compartment

~:......

LO:..Lower. Compartment OE:

Oead-Ended Compartment 1C:

lce Condenser Compartment

ASS AiND 9

?"=Y RE':-~SE ?~iES u!,.<IMUM Si i !!ME (sec)

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TABLE 14.3.1-A-3 NITROGEN MASS AND ENERGY RELEASE RATES

~Time sec Flow Rate lbs/sec 37.5 39.5 45.5 47.5 53.5 55.5 61.5 63.5 70.3 72.3 78.5 80.5 86.3 88.3 94.3 96.3 102.2 104.2 110.2 112.2 126.2 128.2 138.2 140.2

~

146.2 148.2 174.2 176.2 71.9'0.7 37.2 31.6 18.8 15.6 8.5 6'. 9 186.0 158.0 97.3 82.4 48.5 40.0 21.9 18.2 11.7 10.5 7.6 6.8 3.3 2.9 1.8 1.6 1.2'.1 0.25 0.075 0329L:6/840727 l7

TABLE 14.3.1-A-4 LARGE BREAK OECLG C0=0.4 Results Max SI Peak Clad Temp. 'F Peak Clad Location Ft.

Local Zr/H20 Reaction (Max)i~

Local 2r/H20 Location Ft.

Total 2r/H20 Reaction,'o'ot Rod Burst Time sec.

Hot Rod Burst Location Ft.

2162 7,. 50 6.58 7.50

( 0.3 71.4 6.75 Calculation Licensed Core Power (Mwt) 102;o'f Peak Linear Power (kw/ft) 102;o'f Peaking Factor (at License Rating)

Accumulator Water Volume (ft ) per Accumulator 3

3250 13.225 1.97 950

. Cycle Analyzed.,:Cycle 8

18 0329L:6/840727

TABLE 14.3. 1-A-5 LARGE BREAK TIME SEQUENCE OF EVENTS Max SI OECLG CO=0.4 (sec)

START Reactor Trip Signal Safety Injection Signal Accumulator Injection End of Blowdown Bottom of Core Recovery Accumula'tor Empty Pump Injection 0.00 0.60 4.05 20'. 50 38.70 52.78 67.45 29.05

~

~

0329L: 6/840727 19

TABLE 14. 3.1-4 NITROGEN MASS AND ENERGY RELEASE RATES Time sec Flow Rate lbs/sec 37.5 39.5 45.5 47.5 53.5 55.5 57.5 60.7 66.7 68.7 74.7 76.7 78.7 80.7 86.7 88.7 98.7 100.7 110.7 112.7 122.7 124.7 130.7 132.7

'146. 6 145.5 71.9 60.7 37.2 31.6 18.8 15.6 12.8 266.81 159.7 135.7 83.2 70.3 58.9 49.1 27.2 22.3 10.7 9.6 5.6 5.1 3.0 2.7 2.0 1.8

~ 0,8 0.7 0329L:6/840727 20

TABLE 14.3.1-5 LARGE BREAK Results OECLG C =0.8 D

Min SI DECLG CD=0.6 Min SI OECLG

~

C =0.4 0

Min SI OECLG

'O='6 Max SI Peak Clad Temp.,

F 1942 Peak Clad Location, ft 7.00 Local Zr/H20 Reaction (Max) 2.85 Local Zr/H20 Location, ft 7.00 Total Zr/H20 Reaction

<0.3 Hot Rod Burst Time, sec 43.8 Hot Rod Burst Location, ft 6.00 2014 5.75 5.65 5.75

<0.3 37.8 5.75 1956 7.00 3.84 5.75

<0.3 47.4 5.75 2163 6.00 9.65 5.75

<0.3 37.8 5.75 Calculation Licensed Core Power (MWT) 102;< of 3411 Peak Linear Power (kw/ft) 102;~ of 14.796 Peaking Factor (at License Rating) 2.10 Accumulator Water Volume (ft ) per Accumulator 950 3

21

~ 0329L:6/840727

TABLE 14.3. 1-6 LARGE BREAK TIME SEQUENCE OF EVENTS Min SI OECLG CO=0.8 (sec)

Min SI OECLG CO=0.6 (sec)

Min SI OECLG CO=0.4 (sec)

Max SI OECLG CO=0.6 (sec)

START Reactor Trip Signal Safety Injection Signal Accumulator Injection End of Blowdown Bottom of Core Recovery Accumulator Empty Pump Injection 0.00 0.00 0.62 0.63 3.83.

3.95 12.90 15.50 29.68 30.43 40.66 43.29 56.89 59.29 28.83 28.95 0.00 0.64 4.20 20.80 38.49 52.64 65.65 29.20 0.00

0. 63.

3.95 15.50 30.43 42.47 60.58 28.95 0329L: 6/840727 22

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ATTACHMENT 8 LOCA Rci A-"0 -."CH SPECS Plant Name:

Oonald C.

Cook Unit 1

(AFP)

Tyoe/Date o

'OCA Analysis O.lp 0C

= ~-4 (max SI case)

Large Break LOCA Analysis Df'Qg Total Peaking Factor F~. ~ g,'IQ Cold Leg Accumula or.

Water Yolume:

980 ft /accumulator (nominal) unchanged

-,rom cur rent tech specs Cold Leg Accumulator Gas Pressure:

600 psia (minimum) unchanged from current tech specs K(z) Cu. ve:

See next page

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