ML20129C452

Proposed Tech Specs,Revising Pages 89,89a & 90 to Incorporate Changes from Amends 148 & 149

ML20129C452
Person / Time
Site:	Vermont Yankee
Issue date:	10/17/1996
From:	VERMONT YANKEE NUCLEAR POWER CORP.
To:
Shared Package
ML20129C449	List: BVY-96-126, Forwards Revised TS Pages 89,89a & 90 to Incorporate Changes from Amends 148 & 149 to License DPR-28,as Discussed W/Nrc ML20129C452
References
NUDOCS 9610240032
Download: ML20129C452 (9)

Text

1 VYNPS BASES:

3.3 & 4.3 CONTROL ROD SYSTEM A. Reactivity Limitations

1. Reactivity Marcin - Core Loading The specified shutdown margin (SDM) limit accounts for the uncertainty in the demonstration of SDM by testing. Separate SDM limits are provided for testing where the highest worth control rod is determined analytically or by measurement. This is due to the reduced uncertainty in the SDM test when the highest worth control rod is determined by measurement (e.g., SDM may be demonstrated by an in-sequence control rod withdrawal, in which the highest worth control rod is analytically determined, or by local criticals, where the highest worth rod is determined by testing).

1 Following a refueling, adequate SDM must be demonstrated to ensure that the reactor can be made suberitical at any point during the cycle. Since core reactivity will vary during the cycle as a function of fuel depletion and poison burnup, the beginning of cycle (BOC) test must also account for changes in core reactivity during the cycle. Therefore, to obtain the SDM, the initial measured value nust exceed LCO 3.3.A.1 by an adder, l "R", which is the difference between the calculated value of maximum core reactivity during the operating cycle and the calculated BOC core reactivity. If the value of "R" is negative (that is, BOC is the most reactive point in the cycle), no correction to the BOC measured value is required. The value of R shall include the potential shutdown margin loss assuming full B4 C settling in all inverted poison tubes present in the core.

The frequency of 4 hours4.62963e-5 days <br />0.00111 hours <br />6.613757e-6 weeks <br />1.522e-6 months <br /> after reaching criticality is allowed to provide a reasonable amount of time to perform the required calculations and have appropriate verification.

When SDM is demonstrated by calculations not associated with a test (e.g., to confirm SDM during the fuel loading sequence),

additional margin must be included to account for uncertainties in the calculation. During refuelin adequate SDM is required to ensure that the reactor does not'g, reach criticality during control rod withdravals. An evaluation of each in-vessel fuel movement during fuel loading (including shuffling fuel within the core) is required to ensure adequate SDM is maintained during .

refueling. This evaluation ensures that the intermediate loading patterns are bounded by the safety analyses for the final core loading pattern. For example, bounding analyses that demonstrate w adequate SDM for the most reactive configurations during the gj]% refueling may be performed to demonstrate acceptability of the

-oE entire fuel movement sequence. These bounding analyses include 00 additional margins to account for the associated uncertainties in

$@ the calculation.

&O

2. Reactivity Marcin - Inoperable Control Rods gg MO 00 Specification 3.3.A.2 requires that a rod be taken out of service if it cannot be moved with drive pressure. If a rod is disarmed

@@ electrically, its position shall be consistent with the shutdown N

o reactivity limitation stated in Specification 3.3.A.l. This

$$ assures that the core can be shutdown at all times with the m a n- remaining control rods, assuming the highest worth, operable control rod does rod insert. An allowable pattern for control rods valvedThe outnumber of service will be available to the reactor of rods permitted to be inoperable could be operator.

89 Amendment No. 40, :'VY 07 131,148

_.. ~ . .- __... . . _ _ _ . _ . . _ _._ .. _ _ _ _ . - _ _ _ _ _ . . _ _ m._._..._____ .

VYNPS 1y .

R&ggg,- 3.3 & 4.3 (Cont'd) many more than the six allowed by the Specification, particularly late in the operation cycles however, the occurrence of more than six could be indicative of a generic control rod drive problem and the reactor will be shutdown. Also if damage within the control rod drive mechanism and in particular, cracks in drive internal. housing, cannot be ruled out, then a generic problem affecting a number of drives cannot be ruled out.

Circumferential cracks resulting from stress assisted intergranular corrosion have occurred in the collet housing of drives at several BWRs. ' anis type of cracking could occur in a

. number of drives and if the cracks propagated until severance of the collet housing occurred, scram could be prevented in the affected rods. Limiting the period of operation with a potentially severed collet housing and requiring increased surveillance after detecting one stuck rod will assure that the reactor will not be operated with a large number of rods with failed collet' housings.

B. Control Rods

~

1. Control rod dropout accidents as discussed in the FSAR can lead to significant core damage. If coupling integrity is maintained, the possibility of a rod dropout accident is eliminated. The overtravel position feature provides a positive check as only uncoupled drives may reach this position. Neutron instrumentation response to rod movement provides a verification that the rod is following its drive.

l t

s 4

l Amendment No.148 .

89a

Attachment 2 l

l Amendment 149: Pages 89 and 90 l

l i

)

VYNPS BASES:

3.3 & 4.3 CONTROL ROD SYSTEM A. Reactivity Limitations

1. Reactivity Marcin - Core Loadino l

The core reactivity limitation is a restriction to be applied principally to the design of new fuel which may be loaded in the core or into a particular refueling pattern. Satisfaction of the  ;

limitation can only be demonstrated at the time of loading and I must be such that it will apply to the entire subsequent fuel l cycle. At each refueling the reactivity of the core loading will l be limited so the core can be made suberitical by at least l R + 0.25% Ak with the highest worth control rod fully withdrawn j and all others inserted. The value of R in % Ak is the amount by l which the calculated core reactivity, at any time in the operating cycle, exceeds the reactivity at the time of the l i

demonstration. R must be a positive quantity or zero. The value of R shall include the potential shutdown margin loss assuming full B4 C settling in all inverted poison tubes present in the core. The 0.25% Ak is provided as a finite, demonstrable, sub-criticality margin.

2. Reactivity Marcin - Inoperable Control Rods Specification 3.3. A.2 requires that a rod be taken out of service if it cannot be moved with drive pressure. If a rod is disarmed electrically, its position shall be consistent with the shutdown reactivity limitation stated in Specification 3.3.A.l. This assures that the core can be shutdown at all times with the i remaining control rods, assuming the highest worth, operable I control rod does rod insert. An allowable pattern for control {

rods valved out of service will be available to the reactor operator. The number of rods permitted to be inoperable could be many more than the six allowed by the Specification, particularly late in the operation cycle; however, the occurrence of more than six could be indicative of a generic control rod drive problem and the reactor will be shutdown. Also if damage within the control rod drive mechanism and in par';icular, cracks in drive ]

internal housing, cannot be zuled out, then a generic problem affecting a number of drives cannot be ruled out. )

Circumferential cracks resulting from stress assisted intergranular corrosion have occurred in the collet housing of ,

drives at several BWRs. This type of cracking could occur in a j number of drives and if the cracks propagated until severance of ,

the collet housing occurred, scram could be prevented in the I affected rods. Limiting the period of operation with a I potentially severed collet housing and requiring increased surveillance after detecting one stuck rod will assure that the reactor will not be operated with a large number of rods with failed collet housings. l B. Control Rods

1. Control rod dropout accidents as discussed in the FSAR can lead to significant core damage. If coupling integrity is maintained, the possibility of a rod dropout accident is eliminated. Neutron instrumentation response to rod movement provides a verification that the rod is following its drive. Coupling verification is performed to ensure the control rod is connected to the control rod drive mechanism and will perform its intended freccion when necessary. The surveillance requires verifying a c ontrol rod does not go to the withdrawn over-travel position. The over-travel position featvie provides a positive check on the Amendment No. GO, NVY 07 131,149 89

_ . _ - _ _ _ _ . , _ _ _ . - - . ~ . _ _ _ _ _ _ _ _ _ _ . _ _ _ _ _ _ _ _ . _ _ _ _ _ _

l VYNPS

$_gg,: 3.3 t. 4.3 (Cont'd) coupling integrity since only an uncoupled CRD can reach the over-travel position. The verification is required to be ,

performed when a control rod is fully withdrawn after each refueling outage (since. work on the control rod or CRD System may have affected coupling), and after each uncoupling.

2. The control rod housing support restricts the outward movement of a control rod to less than 3 inches in the extremely remote event of a housing failure. The amount of reactivity which could be added by this small amount of rod withdrawal, which is less than a normal single withdrawal increment, will not contribute to any damage of the primary coolant system. The design basis is given in Subsection 3.5.2 of the FSAR, and the design evaluation is

, given in Subsection 3.5.4. This support is not required if the reactor coolant system is at atmospheric pressure since there t would then be no driving force to rapidly eject a drive housing.

3. In the course of performing normal startup and shutdown procedures, a pre-specified sequence for the withdrawal or insertion of control rods is followed. Control rod dropout accidents which might lead to significant core damage, cannot occur if this sequence of rod withdrawals or insertions is followed. The Rod Worth Minimizer restricts withdrawals and insertions to those listed in the pre-specified sequence and provides an additional check that the reactor operator is following prescribed sequence. Although beginning a reactor startup without having thw RWM operable would entail unnecessary risk, continuing to withdraw rods if the RWM fails subsequently is acceptable if a second licensed operator verifies the withdrawal sequence. Continuing the startup increases core power, reduces the rod worth and reduces the consequences of dropping any rod. Withdrawal of rods for testing is permitted with the RWM inoperable, if the reactor is subcritical and all-other rods are fully inserted. Above 20% power, the RWM is not "

needed since even with a single error an operator cannot withdraw a-rod with sufficient worth, which if dropped, would result in anything but minor consequences.

4. Refer to the Vermont Yankee Core Performance Analysis report.

5. The Source Range Monitor (SRM) system has no scram functions. It does provide the operator with a visual indication of neutron level. The consequences of reactivity accidents are a function of the initial neutron flux. The requirement of at least three counts per second assures that any transient should it occur, begins at or above the initial value of 10-e ,of rated power used '

in the analyses of transients from cold conditions. One operable SRM channel is adequate to monitor the approach to criticality, therefore, two' operable SRM's are specified for added conservatism.

6. The Rod Block Monitor (RBM) is designed to automatically prevent fuel damage in the event of erroneous rod withdrawal from loca-tions of high power density during high power level operation.

During reactor operation with certain limiting control rod patterns, the withdrawal of a designated single control rod could result in one or more fuel rods with MCPR less than the fuel cladding integrity safety limit. During use of such patterns, it is judged that testing of the RBM system prior to withdrawal of such rods will provide added assurance that improper withdrawal does not occur. It is the responsibility of the Nuclear Engineer to identify these limiting patterns and the designated rods either when the patterns are initially established or as they develop due to the occurrence of inoperable control rods.

Amendment No. M, M, 44, M,149 90

Attachment 3 Current Vermont Yankee Technical Specification pages 89,89a,90

1

. VYNPS BASES:

3.3 & 4.3 CONTROL ROD SYSTEM A. Reactivity Limitations

1. Reactivity Marqin - Core Loading The specified shutdown margin (SDM) limit accounts for the uncertainty in the demonstration of SDM by testing. Separate SDM limits are provided for testing where the highest worth control rod is determined analytically or by measurement. This is due to the reduced uncertainty in the SDM test when the highest worth control rod is determined by measurement (e.g., SDM may be demonstrated by an in-sequence control rod withdrawal, in which the highest worth control rod is analytically determined, or by local criticals, where the highest worth rod is determined by testing).

Following a refueling, adequate SDM must be demonstrated to ensure that the reactor can be made suberitical at any point during the cycle. Since core reactivity will vary during the cycle as a function of fuel depletion and poison burnup, the beginning of cycle (BOC) test must also account for changes in core reactivity during the cycle. Therefore, to obtain the SDM, the initial measured value must exceed LCO 3.3.A.1 by an adder, "R", which is the difference between the calculated value of maximum core reactivity during the operating cycle and the calculated BOC core reactivity. If the value of "R" is negative (that is, BOC is the most reactive point in the cycle), no correction to the BOC measured value is required. The value of R shall include the potential shutdown margin loss assuming full B4 C settling in all inverted poison tubes present in the core.

The frequency of 4 hours4.62963e-5 days <br />0.00111 hours <br />6.613757e-6 weeks <br />1.522e-6 months <br /> after reaching criticality is allowed to provide a reasonable amount of time to perform the required calculations and have appropriate verification.

When SDM is demonstrated by calculations not associated with a test (e.g., to confirm SDM during the fuel loading sequence),

additional margin must be included to account for uncertainties in the calculation. During refuelin adequate SDM is required to ensure that the reactor does not'g, reach criticality during control rod withdrawals. An evaluation of each in-vessel fuel movement during fuel loading (including shuffling fuel within the core) is required to ensure adequate SDM is maintained during ,

refueling. This evaluation ensures that the intermediate loading patterns are bounded by the safety analyses for the final core loading pattern. For example, bounding analyses that demonstrate adequate SDM for the most reactive configurations during the refueling may be performed to demonstrate acceptability of the entire fuel movement sequence. These bounding analyses include additional margins to account for the associated uncertainties in the calculation.

2. Reactivity Marcin - Inoperable Control Rods Specification 3.3.A.2 requires that a rod be taken out of service if it cannot be_ moved with drive pressure. If a rod is disarmed electrically, its position shall be consistent with the shutdown reactivity limitation stated in Specification 3.3.A.l. This assures that the core can be shutdown at all times with the remaining control rods, assuming the highest worth, operable control rod does rod insert. An allowable pattern for control rods valvedThe outnumber of service willpermitted of rods be available to betoinoperable the reactor could be operator.

89 Amendment No. 40,:""I 07 131,148

d VYNPS BASES: 3.3 & 4.3 (Cont'd) many more than the six allowed by the Specification, particularly late in the operation cycle; however, the occurrence of more than six could be indicative of a generic control rod drive problem and the reactor will be shutdown. Also if damage within the J

control rod drive mechanism and in particular, cracks in drive internal housing, cannot be ruled out, then a generic problem i affecting a number of drives cannot be ruled out. I Circumferential cracks resulting from stress assisted l intergranular corrosion have occurred in the collet housing of  !

drives at several BWRs. This type of cracking could occur in a i number of drives and if the cracks propagated until severance of l the collet housing occurred, scram could be prevented in the affected rods. Limiting the period of operation with a .

potentially severed collet housing and requiring increased surveillance after detecting one stuck rod will assure that the reactor will not be operated with a large number of rods with l failed collet housings.

l 1

B. Control Rods  !

1. Control rod dropout accidents as discussed in the FSAR can lead to significant core damage. If coupling integrity is maintained, the possibility of a rod dropout accident is eliminated. Neutron '

instrumentation response to rod movement provides a verification that the rod is following its drive. Coupling verification is performed to ensure the control rod is connected to the control rod drive mechanism and will perform its intended function when necessary. The surveillance requires verifying a control rod does not go to the withdrawn over-travel position. The over-travel position feature provides a positive check on the coupling integrity since only an uncoupled CRD can reach the over-travel position. The verification is required to be performed when a control, rod is fully withdrawn after each refueling outage (since work on the control rod or CRD System may have affected coupling), and after each uncoupling.

. l l

l J

l Amendment No. 148, 149 89a

.. .- VYNPS BASES: 3.3 & 4.3 (Cont'd)

2. The control rod housing support restricts the outward move.nent of l a control rod to less than 3 inches in the extremely remote event of a housing failure. The amount of reactivity which could be added by this small amount of rod withdrawal, which is less than a normal single withdrawal increment, will not contribute to any l damage of the primary coolant system. The design basis is given l

in Subsection 3.5.2 of the FSAR, and the design evaluation is '

given in Subsection 3.5.4. This support is not required if the reactor coolant system is at atmospheric pressure since there would then be no driving force to rapidly eject a drive housing.

3. In the course of performing normal startup and shutdown procedures, a pre-specified sequence for the withdrawal or l insertion of control tods is followed. Control rod dropout i accidents which might lead to significant core damage, cannot l occur if this sequence of rod withdrawals or insertions is followed. The Rod Worth Minimizer restricts withdrawals and insertions to those listed in the pre-specified sequence and provides an additional check that the reactor operator is following prescribed sequence. Although beginning a reactor startup without having the RWM operable would entail unnecessary risk, continuing to withdraw rods if the 6MM fails subsequently is acceptable if a second licensed operator serifies the withdrawal sequence. Continuing the startup increases core power, reduces the rod worth and reduces the consequences of dropping any rod. Withdrawal of rods for testing is permitted with the RWM inoperable, if the reactor is suberitical and all other rods are fully inserted. Above 20% power, the RWM is not needed since even with a single error an operator cannot withdraw l a rod with sufficient worth, which if dropped, would result in anything but minor consequences.

l 4. Refer to the Vermont Yankee Core Performance Analysis report.

5. The Source Range Monitor (SRM) system has no scram functions. It does provide the operator with a visual indication of neutron  ;

level. The consequences of reactivity accidents are a function i of the initial neutron flux. The requirement of at least three should it occur, countspersecondassuresthatanytransieng,ofratedpowerused begins at or above the initial value of 10-in the analyses of transients from cold conditions. One operable SRM channel is adequate to monitor the approach to criticality, therefore, two operable SRM's are specified for added conservatism.

6. The Rod Block Monitor (RBM) is designed to automatically prevent fuel damage in the event of erroneous rod withdrawal from locations of high power density during high power level operation. During reactor operation with certain limiting control rod patterns, the withdrawal of a designated single control rod could result in one or more fuel rods with MCPR less than the fuel cladding integrity safety limit. During use of such patterns, it is judged that testing of the RBM system prior to withdrawal of such rods will provide added assurance that improper withdrawal does not occur. It is the responsibility of the Nuclear Engineer to identify these limiting patterns and the designated rods either when the patterns are initially established or as they develop due to the occurrence of inoperable control rods.

Amendment No. 26, 49, 6t, 70 90