NL-13-130, Indian Point, Unit 2, Updated Final Safety Analysis Report (Ufsar), Rev. 24, Chapter 3 - Figure 3.2-61C Through Figure 3.2-70

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Indian Point, Unit 2, Updated Final Safety Analysis Report (Ufsar), Rev. 24, Chapter 3 - Figure 3.2-61C Through Figure 3.2-70
ML13291A299
Person / Time
Site: Indian Point Entergy icon.png
Issue date: 09/26/2013
From:
Entergy Nuclear Operations
To:
Office of Nuclear Reactor Regulation
References
NL-13-130
Download: ML13291A299 (58)
v • d • e


Text

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._..... ____ I' e: ti-7151 esc lvF 0 c INDIAN POINT UNIT No. 2 15 X 15 UPGRADED FUEL ASSEMBLY UFSAR FIGURE 3.2-61 C REV. No. 19 2 23 2004 11:50:13 AM vnd 1999MC3583-0-17B.DWG 3.0 -0 BEGINNING-OF-LIFE 0 "'ti 6. MIDDLE-OF-LIFE 0 0 0 END-OF-LIFE 0 m ::0 "'ti m 0 )> 2S 2 G') 6. 2.0 -6 0 0 6 0 ::0 06 0 06 0 0 60 0 0 1.0 I I I I I -15.0 -30.0 -45.0 -60.0 -75.0 AXIAL OFFSET(%)

INDIAN POINT UNIT No. 2 UFSAR FIGURE 3.2-1 TYPICAL POWER PEAKING FACTOR VERSUS AXIAL OFFSET MIC. No. 1999MC3583 I REV. No. 178 90" --@ ,__ iJ (0) Sl S2 SJ S4 Cl C2 Cl C4 PL @ -<*> 'zy @ (Part Length) I@ --,. \!L) A -(Pi.i -[!iJ Q w Cn1 --f@ @ SYMBOL 0 <> D 0 \J t::;, 0 0 0 --li!l I I I £ I I @ I I -I I *} I I § I I I (g) 'W @)' [@ w I' @ @ !'::.. -ij ........ ---210* @3 -. tP_;l 1o/' (PL) -[!jJ @ @ NUMBER OF ROD CLUSTERS 8 8 4 4 8 4 8 9 8 61 INDIAN POINT UNIT No. 2 UFSAR FIGURE 3.2-2 ROD CLUSTER GROUPS CYCLE 1 MIC. No. 1999MC3584 REV. No. 17 A CL CL -* l.l7 -""'"P..--

,.. -.. ---CL l EJEJEJ[JbD I I CL CL -Center -Line FllH = 1.40 (X) INDIAN POINT UNIT No. 2 UFSAR FIGURE 3.2-3 ASSEMBLY AVERAGE POWER & BURNUP, CYCLE 1 CALCULATIONS, BOL, UNRODDED CORE MIC. No. 1999MC3585 REV. No. 17 A

... CL-* 1.03

_ ,_ 16152 -... --. ,_. -... I ______

____

DD DD ---------1.06 [§]*08 0.14 1\9 DD 16302 16120 15741 17011 I . 1.02 14068 I I .79 10620 ___ __, I CL 1.12 1,:1Q1.:11:1 14974 9472 7607 CL -Center -Line F 6 H .. 1.43 (X) INDIAN POINT UNIT No. 2 UFSAR FIGURE 3.2-4 ASSEMBLY AVERAGE POWER & BURNUP, CYCLE 1 CALCULATIONS, EOL, UNRODDED CORE MIC. No. 1999MC3586 I REV. No. 17 A 0 .671 1.090 1.439 1.343 1. 362 1.113 0.882 0.603 "-*-l.09C 1.340 1.447 1.487 1.309 1.088 0. 777 0.579 l.43CJ 1.447 1.544 1.437 1.308 0.944 0.424 0.401 X N X 1. 343 1. 487 1.437 1.407 1.160 1.010 o. 701 0.374 1.362 1.309 1.308 1.160 1.367 0.948 0.812 1.088 0.944 1.010 0.948 1.109 0.535

0. 777 0.424 0. 701 0.812 0.535 0.603 0.579 0.401 0.374 INDIAN POINT UNIT No. 2 UFSAR FIGURE 3.2-5 ASSEMBLY AVERAGE POWER DISTRIBUTION CYCLE 1 CALCULATIONS, BOL, GROUP C4 INSERTED MIC. No. 1999MC3587 I REV. No. 17A x x 1.402 llH 1.349 Y x 1_'>Qn 1.290 1.395 1.286 1.349 1.286 1.227 1.130 1.161 0.962 1.169 o. 989 0.568 1.157 1.110 0.929 1.171 1.149 1.045 0.917 0.867 0.799 1.130 1.169 1.157 1.171 0.917 1.161 0.989 1.110 1.149 0.967 0.962 0.568 0.929 1.045 0.799 0.940 0.830 0.999 1.000 0.633 0.830 1.189 0.954 0.938 0.999 0.954 1.159 0.584 1.000 0.938 0.584 0.633 INDIAN POINT UNIT No. 2 UFSAR FIGURE 3.2-6 ASSEMBLY AVERAGE POWER DISTRIBUTION CYCLE 1 CALCULATIONS, BOL, PART-LENGTH RODS IN MIC. No. 1999MC3588 I REV. No. 17 A 2.4 r---------------------

2.2 a: 2.0 w s: 0 a.. H 1.s d u.. x <( 1.6 1.4 1.2 CYCLE 1 2.32@0' 2.32@6' 2.18@10.8' 1.50@12' NOTE: SEE TECHNICAL SPECIFICATIONS FOR PRESENT REQUIREMENTS ON MEETING Fa LIMITS.

0 2 BOTTOM 4 6 8 CORE HEIGHT {FT) 10 12 TOP INDIAN POINT UNIT No. 2 UFSAR FIGURE 3.2-7 CYCLE 1 MAXIMUM F Q x POWER VERSUS AXIAL HEIGHT DURING NORMAL OPERATIONS MIC. No. 1999MC3589 REV. No. 17 A 2 23 2004 11 :50:42 AM vnd 1999MC3590-0-17B.DWG 1.2 1. 1 Io. 1.0 I I 6. 1.0 I 1.0 ---.90 12. 0.92 I .80 .70 -.60 .50 .40 .30 .20 .10 0.000 1 2 3 4 5 6 7 Core El1Yation (F*t) 8 9 10 11 12 INDIAN POINT UNIT No. 2 UFSAR FIGURE 3.2-7 A NORMALIZED K (z) -Fq VERSUS AXIAL HEIGHT FOR CYCLE 1 6 MIC. No. 1999MC3590 I REV. No. 178 15 14 13 12 11l10lslsl7 Isl sl4 3 2 1 9 s 9 7 8 12 16 16 12 8 8 20 12 16 12 20 8 20 20 16 16 20 20 12 20 16 16 16 20 12 9 12 16 20 20 16 12 9 p 16 16 20 16 20 16 p 16 7 16 16 16 16 16 16 7 p p 16 16 20 16 20 16 16 9 12 16* 20 20 16 12 9 12 20 16 16 16 20 12 20 20 16 16 20 20 8 20 12 16 12 20 8 8 12 16 16 12 8 9 s 9 7 TOTAL1412 P -PRIMARY /SECONDARY SOURCE COMBINATION S -SECONDARY SOURCE; INDIAN POINT UNIT No. 2 UFSAR FIGURE 3.2-8 BURNABLE POISON & SOURCE ASSEMBLY LOCATIONS

-CYCLE 1 MIC. No. 1999MC3591 REV. No. 17A 181 181 181 l8l l8l 181 181 181 181 181 181 0 181 181 181 181 181 181 181 0 181 0 0 0 181 181 181 181 181 181 ° 181 181 181 181 181 181 181 181 181 181 20 BP's 16 BP'2 t CENTER OF CORE 181 181 0 181 181 181 181 IZI 181 181 0 D 181 181 181 181 181 181 D D D 0 0 0 181 0 D 181 DO OD 181 0 181 181 0 ODD D 12 BP's 9 BP'2 181 181 181 D 181 181 0 181 0 181 D D 181 D 0 0 D 0 OD 0 8 BP's INDIAN POINT UNIT No. UFSAR FIGURE 3.2-9 2 BURNABLE POISON ROD LOCATIONS CYCLE 1 MIC. No. 1999MC3592

!REV. No. 17A

+to -L&... 0 0 -:::E (,,) Q.. -::IC I-;t> --10 I-z I.LI (,,,) L&... L&... -20 LAJ 0 (.,) &.I.I Cl::: :::::>> I-c a:: I.LI -30 Q.. :::E &.I.I ,_ a:: 0 I-c a:: I.LI -1'0 0 0 % -50 0 100 200 300 MODERATOR TEMPERATURE

(°F) 500 +**** ......... -* *

  • t * ** * -* *--............

600 INDIAN POINT UNIT No. 2 UFSAR FIGURE 3.2-10 MODERATOR MODERATOR TEMPERATURE TEMPERATURE MIC. No. 1999MC3593 COEFFICIENT vs EOL, CYCLE 1 REV. No. 17A 1000 ppm 500 ppm -2.5 590 600 0 ppm Moderator Temperature

(*F) INDIAN POINT UNIT No. 2 UFSAR FIGURE 3.2-11 MODERATOR TEMPERATURE COEFFICIENT vs MODERATOR TEMPERATURE

-BOL, CYCLE 1 FULL POWER MIC. No. 1999MC3594 1 REV. No. 17A

-LL 0 ....... E (,) Q. +5 0 . : I , I I , I --..

4 *** 100 200 300 400 500 i ' '--*t * ;--L i . I* , -+ r--I ... I I 500 ppm 0 ppm Moderator Temperature

(°F) INDIAN POINT UNIT No. 2 UFSAR FIGURE 3.2-12 MODERATOR TEMPERATURE COEFFICIENT vs MODERATOR TEMPERATURE

-BOL, CYCLE 1 ZERO POWER MIC. No. 1999MC3595 REV. No. 17A 2.1 2.0 l.9 1.8 1. 7 l.6 1.5 ,,.... Jz. .. ...... 1.4 II"\ CJ) ,...; ....... 1.3 't:I "Q ,...; :.c: 1.2 l.l 1.0 .9 .8 0 DOPPLER COEFFICIENT vs EFFECTIVE FUEL TEMPERATURE 500 1000 1500 2000 2500 EFFECTIVE FUEL TEMPERATURE Teff INDIAN POINT UNIT No. 2 UFSAR FIGURE 3.2-13 DOPPLER COEFFICIENT FUEL TEMPERATURE MIC. No. 1999MC3596 vs EFFECTIVE CYCLE 1 REV. No. 17 A

-"' I p.. " ...... "" 0 .... 1.0 -l"'ffW POWER COEFFICIENT VS PERCENT POWER WITH TMOD a 572. °F E '"' 2. 7 W/O BOL ,,. 2100 ppm PERCENT OF FULL POWER, 2758 MWT INDIAN POINT UNIT No. 2 POWER UFSAR FIGURE 3.2-14 COEFFICIENT vs CYCLE PERCENT 1 POWER MIC. No. 1999MC3597 REV. No. 17A

., j!' . !'. : : ' ... I . I .. L i ! .: .L ' 0 . J_.1 j_ I . I . . l.' .. _J . ___ _.__ g i i. i I ' . i .I **i* -__ .,-1-__ --7-::-* *-r---*--; **-j-

-. : I . I .* 1' . . I : I 't .. rH :Jrt , .. J_ --__ J -_I **rl-'-. --L_ -_: __ . ' ' I . ' I 0 \D 0 "' 0 (\J 4 Power Coefficient, -dp/oP (x 10 "" Ill :. 0 0.. ..... 3 rs. _.., c: Ill CJ "" it INDIAN POINT UNIT No. 2 UFSAR FIGURE 3.2-15 POWER COEFFICIENT CLOSED GAP MODEL MIC. No. 1999MC3598 REV. No. 17 A 2 23 2004 11:51:30 AM vnd1999MC3643-0-17B.DWG 0.07 LEGEND: PERCENT PERCENT THEORETICAL THEORETICAL DENS ITV DENSITY 0.06 D GYLLANDER 0 HOWARD & GULVIN 96.0

  • ASAMOTO 95.0
  • LUCKS & DEEM 96.5 :i! 0 GODFREY 93 0 DANIEL ET AL. 96.5 l'T'I * :::0 STORA 92.2 FEITH 97.9 0.05 r
  • A.O. BUSH 0 VOGT ET AL. 97 .o C'>
  • A SAMO TO 91 .0 NISHIJIMA 95.0 0 :z 0 'V KRUGER 93. 7 .. WHEELER & AINSCOUGH 97 .o c: C'> -i <

SEE REFERENCES FOR THERMAL-HYDRAULIC SECTION ::;! ::><:: -..3 ::E 0.03 * -C'> ::;c I 0 C'> 0.02 v 0.01 0 800 1200 1600 2000 2ll00 2800 3200 TEMPERATURE (T), °C INDIAN POINT UNIT No. 2 UFSAR FIGURE 3.2-38 TYPICAL THERMAL CONDUCTIVITY OF U02 MIC. No. 1999MC3643 I REV. No. 178 27 26 25 24 23 22 21 20 19 t: 18 p:; 17 16 15 14 13 12 11 10 8 E ::.:...,.--'

Csf-<4) . *. i . * ::: :* _._ . , : : . -(2, 1 Intentionally
  • -** *. (3) ' ::-: Defected)

-'-* f ;* ., ** (X) No. of Rods V1IlJJID.

CVTR. Irradiation Program 11111 Saxton Irradiation Program (LRD Program) flil'.mm Saxton Puo 2 + uo 2 Progrlllll j.*.*.-:.:*I Yankee Core 5 1-:-1 Current Programs (Date Shown is Completion Date) :::::*:::::::::;

_:_; 425 Rods : : : ----, ----:--;-
  • ...... * . . . . . . . -i . . ' ! *** **** . . . . . . 0 10 20 30 4 6 MAXIMUM EXPOSURE -10 3 HWD/MTH INDIAN POINT UNIT No. UFSAR FIGURE 3.2-39 HIGH POWER FUEL ROD EXPERIMENTAL PROGRAM MIC. No. 1999MC3644 I REV. 2 No. 17A 2 23 2004 11:51:40 AM vnd1999MC3645-0-17B.DWG 2-0 N t-JC u.. I CY. :c -:::> t-1*5 0 a:l "° S2 .. a:l z 0 = er 0 l*O u.i a:: :::> V') < u.i :E 0*5 0 UNIFORM FLUX OATA >C EOUIVALEHT .UM I FORM DATA CONVERTED FROM HON-UNIFORM DATA 0*5 l*O 1*5 2*0 2*5 PREDICTED q"ONB I0 6 BTU/HR-FT 2 INDIAN POINT UNIT No. 2 UFSAR FIGURE 3.2-40 TYPICAL COMPARISON OF W-3 PREDICTION AND UNIFORM FLUX DATA MIC. No. 1999MC3645 I REV. No. 178 2 23 2004 11:51:50 AM vnd1999MC3678-0-17B.DWG -a r---, -.a = c z m 3: ,,, > V1 c: ::0 ,,, c -..ct : c z m -a ::0 ,.,, 0 -("") -4 ,,, 0 v --3: z 0 z m J) 40 50 60 70 80 90 95 98 99 99.8 99.9 I e 99.99 ..,... / / / / / , / / ... v 10. OF DATA POINTS = 809 MEAN VALUE = 0.996 STANDARD DEVIATION

= 0. 132 0. 6 0. 7 0. 8 0. 9 1.0 (I/ MIN DNBR) W-3 CORRELATION PROBABILITY DISTRIBUTION CURVE INDIAN POINT UNIT No. 2 UFSAR FIGURE 3.2-41 TYPICAL W-3 CORRELATION PROBABILITY DISTRIBUTION CURVE MIC. No. 1999MC3678 I REV. No. 17B 1.0 c LI.I 0.6 a:: :::i Cl'll <( LI.I al z 0 0.4 'er ().2 LEGEND: L GRID DATA ba 8' HEATED LENGTH COSµ 26" 0 14' HEATED LENGTHµ SINEµ 26" 0 14' HEATED LENGTH µ SINE µ 26" COLDWALL INLET MASS VELOCITY:

INLET TEMPERATURE:

INLET PRESSURE:

DNB QUALITY: -23% q" DNB (PREDICTED)

= 1" DNB (PREDICTED BY W-3) X F'sL 1.96 TO .3.68 X 106 LB/HR-FT2 403.7 TO 626.JOF 1460 TO 2430 PSIA -15.12 TO 13.34/

o 0.2 0.4 0.6 0.8 1.0 1.2 1.4 q" DNB (PREDICTED).

10 6 BTU/HR-FT 2 INDIAN POINT UNIT No. 2 UFSAR FIGURE 3.2-42 COMPARISON OF "L" GRID TYPICAL AND THIMBLE COLD WALL CELL ROD BUNDLE DNB DATA FOR NON-UNIFORM AXIAL HEAT FLUX WITH PREDICTIONS OF W-3 x F'sL MIC. No. 1999MC3679 I REV. No. 17 A 2 23 2004 11 :52:01 AM vnd 1999MC3680-0-17B.DWG 1*2 -0

  • 15 JCDN 8 + 0
  • I 5 i*I N ,_ l*O I c:: :c 9 :::> I-al '°o 0*8 .. x 0*7 :::> I-< 0-6 I.I.I :c ca z 0*5 c -20% c I.I.I 0-4 c:: :::> vi < 0*3 I.I.I NO. OF RODS PRESSURE SOURCE 20 2000 WAPD-0*2 PSIA LPR-256 19-21 1500 WCAP-O*I PSIA 2956 0 0 O*I 0*2 0*3 0-4 0*5 0-6 0*7 O.S 0*9 l*O PREDICTED DNB HEAT FLUX, 10 6 BTU I HR-FT 2 INDIAN POINT UNIT No. 2 UFSAR FIGURE 3.2-43 TYPICAL COMPARISON OF W-3 CORRELATION WITH ROD BUNDLE DNB DATA (SIMPLE GRID WITHOUT MIXING VANE) MIC. No. 1999MC3680 I REV. No. 178 2 23 2004 11:52:07 AM vnd1999MC3681-0-17B.DWG

'° N t:;: I c:::: :I: -::::> I-al Vl < Li.J : er .8 .7 .6 .5 .4 .3 .2 .I o P = 1614 PSIA 6 P = 1814 PSIA c P = 20l4 PSIA 0 P = 2314 PSIA -25'¥o

__ _._ __ _.._ ____ .,__ __ _._ ____

0 .I .2 .3 .4 .5 .6 .7 .8 q II (BTU /HR-FT 2) 10-6 PRED INDIAN POINT UNIT No. 2 UFSAR FIGURE 3.2-44 TYPICAL COMPARISON OF W-3 CORRELATION WITH ROD BUNDLE DNB DATA (SIMPLE GRID WITH MIXING VANE) MIC. No. 1999MC3681 I REV. No. 178 2 23 2004 11:52:14 AM vnd 1999MC3682-0-17B.DWG 1.2 ... I-II. 1.1 3 I-1.0 )I( :::i 0.9 ... II. I-0.8 c( IA.I = ... 0.7 c( :: = 0.6 = u Q 0.5 II.I = :::i 111 c( 0.4 "" 2 "' O.l * ... _:s.

  • 0.2 = --=j 0.1 0 0 0.1 0.2 + + *95% OF DATA WILL FALL ABOVE THIS LINE WITH 95'4 CONFIDENCE O.l 0.4 0.5 0.6 0.7 0.8 0.9 1.0 1.1 PREDICTED CRITICAL HEAT FLUX IBTU/HA*FT2) 1.2 INDIAN POINT UNIT No. 2 UFSAR FIGURE 3.2-44A TYPICAL MEASURED VERSUS PREDICTED CRITICAL HEAT FLUX-WRB-1 CORRELATION MIC. No. 1999MC3682 I REV. No. 178 2 23 2004 11 :52:20 AM vnd 1999MC3683-0-17B.DWG

/

HEAT FUJI llTUIHR*n 2 Q11*0.ll 1io' /

  • MASS FUJW RATE L.a/HR*n 2 Q119*2.5al0*

/ / :.ss:; .,

////// ' TUIE LD., IN. Q.IO*Q.32 COOLANT Ta., *F 483* 105 9LL TE* * ., U8*ll09 2 z z 4

  • INDIAN POINT UNIT No. 2 UFSAR FIGURE 3.2-45 TYPICAL STABLE FILM BOILING HEAT TRANSFER DAT A AND C 0 RR ELA TI 0 N MIC. No. 1999MC3683 I REV. No. 17B CORE BAFFLE THERMAL SHIELD REACTOR VESSEL CORE BARREL FUEL ASSEMBLY 193 FUEL ASSEMBLIES INDIAN POINT UNIT No. 2 UFSAR FIGURE 3.2-46 CORE CROSS SECTION MIC. No. 1999MC3684 REV. No. 17 A LIFTING LUG UPPER SUPPORT PLATE INTERNALS SUPPORT LEDGE CORE BARREL SUPPORT COLUMN THERMAL SHIELD REACTOR VESSEL ACCESS PORT RADIAL SUPPORT BOTTOM SUPPORT __ _ CASTING MIC. INSTRUMENTATION PORTS CLOSURE HEAD ASSEMBLY THERMAL SLEEVE SHROUD TUBE HOLD-DOWN SPRING ALIGNMENT PIN CONTROL ROD GUIDE TUBE flttt-+;--l...--l_L CONTROL ROD DRIVE SHAFT BAFFLE BAFFLE RADIAL SUPPORT ---LOWER CORE PLATE FLOW MIXER PLATE -CORE SUPPORT COLUMNS INSTRUMENTATION THIMBLE GUIDES INDIAN POINT UNIT No. 2 UFSAR FIGURE 3.2-47 REACTOR VESSEL INTERNALS No. 1999MC3685 l REV. No. 17A ENRICHMENTS 2.2 W/0 2.8 W/0 3.3 W/0 INDIAN POINT UNIT No. 2 UFSAR FIGURE 3.2-48 CORE LOADING ARRANGEMENT

-CYCLE 1 MIC. No. 1999MC3686 I REV. No. 17 A

ROD ASSEMBLY ROD ----ABSORBER ---TOP NOZZLE ---FUEL ROD "'GRID ASSEMBLY ROD GUIDE SHEATHS "'GRID ASSEMBLY DASH POT ----REGION

---BOTTOM NOZZLE INDIAN POINT UNIT No. UFSAR FIGURE 3.2-49 TYPICAL ROD CLUSTER CONTROL ASSEMBLY 2 MIC. No. 1999MC3687 I REV. No. 17A TOP VIEW Note: Dimensions are expressed in inches. COUPLING SPIDER BODY MIC. INDIAN POINT UNIT No. 2 UFSAR FIGURE 3.2-50 ROD CONTROL CLUSTER ASSEMBLY OUTLINE No. 1999MC3688 I REV. No. 17A ffi ;!l ' I ! I ':!,,I : _J __ ; I I / :; I /i I

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1 _JN INDIAN POINT UNIT No. 2 UFSAR FIGURE 3.2-51 CORE BARREL ASSEMBLY MIC. No. 1999MC3705 I REV. No. 17A

(/) _... c <.O -0 <.O -oc <.O 0-o :::0 -0 () -I f'Tl (/) :::0 0 -I() 01 :::0 0 c :::0 () f'Tl -I :::0 c f'Tl :::0 < f'Tl . z ?I _... '-.I )> c ""T') (/) )> :::0 ""T') C) c :::0 f'Tl VI . N :z 0 " (I) -'*O ::I-'* 3 .... ro ::s ::s (j Vl ::::I"-'*

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  • 204 Hote: (l) All d1m. corrected to 2° (2) Dimensions are expressed in inches INDIAN POINT UNIT No. UFSAR FIGURE 3.2-54 2 FUEL ASSEMBLY AND CONTROL CLUSTER CROSS SECTION -HIPAR, LOPAR, OFA AND VANTAGE+ MIC. No. 1999MC3708 jREV. No. 17A 1.280 I REF. I I 2.250 PIA. IREFl I 6.945REf.

6220REF. 153.680 REF. 161.3811 REF. OVERALL LENGTH ---f __ .

1 149.n6 FUEL TUBE LENGTH. 144.00 FUEL COLLI-LENGTH--------. 142.00 REF_

  • GUll>E THIMBLE fl)= 0.516 GUll>E THIMBLE 00 = 0.54S " ,, " ,, ... " ,, ,, ,, ,. ,, -., 1r* " J! ,, II -_u " j[ II *11 " " " " ABSORBER LENGTH 59.66 REF. l 41.16 REF. 112.91 c REF. 93.41 REF. L. 76.54 REF. 162.16REF.

Note: 169.300 169.280 Dimensions are expressed in inches. INDIAN POINT UNIT No. UFSAR FIGURE 3.2-55 HIPAR FUEL ASSEMBLY MIC. No. 1999MC3709 REV. i-.. Y--MARK 2 No. 17A Note: Dimensions are expressed 1n inches. INDIAN POINT UNIT No. 2 UFSAR FIGURE 3.2-56 LOPAR FUEL ASSEMBLY MIC. No. 1999MC3710 REV. No. 17A OPTIMIZED (QFAJ FUEL ASSEMBLY l I 159.975 134.07 113.26 93.70 76.77 59.84 41 .28 23.47 6.383 OFA LMOOOO RECONSTITUTABLE TOP NOZZLE INCONEL GRID OFA ZIRC GRIDS (7) FUEL ROD LENGTH= 152.17 MID GRID HEIGHT = 2.25 INCONEL GRID DEBRIS FILTER BOTTOM NOZZLE INDIAN POINT UNIT No. UFSAR FIGURE 3.2-56A OFA FUEL ASSEMBLY MIC. No. 1999MC3711 I REV. 2 No. 17 A INGONEL t 133. 7 c I 122.78 f 112. BS 1 0 2 50 t 3 3 ."3 3 i B .JS t 7 6 .... 0 5 9. 4 7 I 1 0. 9 1 t 2 3. 1 0 INCONEL GRID 6. 3 8 3 DEBRIS FILTER BOTTOM NOZZLE

  • VANTAGE+ FUEL WITH PERFORMANCE

+ FEATURES WILL HAVE ZIRLOTM MIDGRIDS.

LPD ZIRGl(I GRIDS (i) FUEL ROD LENGTH 152.55 MID GRID HEIGHT 1.50 ZIRLO'"

INDIAN POINT UNIT No. 2 UFSAR FIGURE 3.2-568 VANTAGE+ FUEL ASSEMBLY MIC. No. 1999MC3712 REV. No. 17 A THIMBLE/END PLUG INERT-GAS FUSION WELD INSERT/END PLUG WELD ____. z1RCALOY THIMBLE lZIRLOrn forVANTAGE+l I BOTTOM GRID _ _..:.._ SPOT WELD INSERT ZIRCALOY THIMBLE END PLUG INDIAN POINT UNIT No. 2 UFSAR FIGURE 3.2-57 GUIDE THIMBLE TO BOTTOM NOZZLE JOINT MIC. No. 1999MC3713 REV. No. 17 A BUTT WELD All AROUND TOP NOZZLE ADAPTER PLATE STAINLESS STEEL SLEEVE EXPANSION LOBE TOP GRID INDIAN POINT UNIT No. 2 UFSAR FIGURE 3.2-58 LOPAR TOP GRID TO NOZZLE ATTACHMENT MIC. No. 1999MC3714 REV. No. 17A

.*.u.-...-

I

=r AT=-.

I -ADAPTER P 1 A--.... I c:. THRU HOLE UNASSEMBLED SST NOZZLE INSERT ; / INDIAN POINT UNIT No. UFSAR FIGURE 3.2-58A OFA and VANTAGE+ 2 TOP GRID TO NOZZLE ATTACHMENT MIC. No. 1999MC3715 lREV. No. 17A INDIAN POINT UNIT No. 2 UFSAR FIGURE 3.2-59 SPRING CLIP GRID ASSEMBLY MIC. No. 1999MC3716 I REV. No. 17 A THI!-181.E:

l='UEL 1<00 EXPANSION LOSE INDIAN POINT UNIT No. 2 UFSAR FIGURE 3.2-60 MID-GRID EXPANSION JOINT DESIGN PLAN VIEW MIC. No. 1999MC3717 lREV. No. 17A w ..J m :E ::c I-CJ a: N I I I I I I I I I I I a I I I I ' I I r I w I m I 0 ..J I 2 r 0 I c;; 2 I <( I a.. I x w I I ) I f I I \ ) I I INDIAN POINT UNIT No. 2 UFSAR FIGURE 3.2-61 ELEVATION VIEW -LOPAR GRID TO THIMBLE ATTACHMENT MIC. No. 1999MC3718 REV. No. 17 A

EXPANSION LOBE SLEEVE ZIRLO THIMBLE INDIAN POINT UNIT No. 2 UFSAR FIGURE 3.2-61 A ELEVATION VIEW -VANTAGE+ GRID TO THIMBLE ATTACHMENT MIC. No. 1999MC3719 I REV. No. 17A 3 2 2004 6:50:50 AM vnd1999MC3720-0-17B.DWG I V1 "' "' e r r:;:J = " r:;:J q ee*

  • ----* !-M . o ....... . H k!:J:

I ,-lmDJffimnld_

i:;:J 0 INDIAN POINT UNIT No. 2 UFSAR FIGURE 3.2-61 B VANTAGE+ FUEL ASSEMBLY WITH PERFORMANCE+

ENHANCEMENTS MIC. No. 1999MC3720 REV. No. 178 0 0 0 0-(11 IO !1 "d 1o0$0 I<> ' In ft "0 x Ill Q 0 0 lo

  • BURNABLE POISON ROD (16 BP"S) UN IRRADIATED Sb-Se Rod PRIMARY Po-Be ROD (100 CURIES) 0 c eo ... I © I ;o©: I<> c ..... ". 0 0 0 0 lo '

la n no IX BURNABLE POISON ROD (7 BP'S ASYMMETRICAL)

UNIRRADIATED Sb-ROD PERMANENT SOURCE SPIDER ASSEMBLY INDIAN POINT UNIT No. UFSAR FIGURE 3.2-62 CYCLE 1 -0 N 2 NEUTRON SOURCE LOCATIONS MIC. No. 1999MC3721 IREV. No. 17A TYPE 304SST 1 SPACER TUBE REF. . 4395DIA. REF. I .2235 DIA . REF. . 2365 DIA. REF. SECTIONA*A SCALE 10:1 150.395 REF. 147.285 REF. CLADDING TUBE TYPE 304SST .243 DIA. REF . .3911 DIA. REF. J r

..

1 .44SMAX. WELD DIA. J IQ i

I ( F _J 1----3.lB REF.

  • I. 142.68 REF. B:RNABLE POISON LENGTH_/ 3.410 REF. ----+-i--------

146.11 REF. TUBE LENGTH 0.875 eonOM END PLUG Note: Dimensions are expressed in inches. INDIAN POINT REF. UNIT No. UFSAR FIGURE 3.2-63 HIPAR BURNABLE POISON ROD MIC. No. 1999MC3722 I REV. TYPE 304SST 2 No. 17A

. 4395DIA. REF. j .223501A.

REF . . 2365DIA. REF. SECTION A-A SCALE 10:1 152.535 REF. 147.285 REF. CLADDING TUBE TYPE 304SST 142.95 REF. SPACER TUBE LENGTH .243 DIA. REF . .396DIA. REF. l .446MAX. WELD DIA. I :::::::?:

1* b 55""

TUBE LENGTH REF. BOTTOM END PLUG TYPE 304 SST Note: Dimensions are expressed in inches. INDIAN POINT UNIT No. 2 UFSAR FIGURE 3.2-64 LOPAR BURNABLE POISON ROD MIC. No. 1999MC3723 REV. No. 17 A CABLE CONN'ECTION 10.718" x 10.718" OPERATING COIL STACK ASSEMBLY PRESSURE HOUSING THERMAL SLEEVE __ _ HEAD AOAPTE R DRIVE SHAFT ASSEMBLY DISCONNECT ROD --MIC. INDIAN POINT UNIT No. 2 UFSAR FIGURE 3.2-65 CONTROL ROD DRIVE MECHANISM ASSEMBLY No. 1999MC3724 IREV. No. 17A

--DISCONNECT ROD ---LIFT POLE COIL GUIDE TUBE MOVABLE GRIPPER POLE MOVABLE GRIPPER COIL MOVABLE LATCH SUPPORT TUBE MOVABLE LATCH LOCK PLUNGER MOVABLE GRIPPER LATCHES LINKS STATIONARY GRIPPER POLE PLUNGER HALF SHIM STATIONARY LATCH LOCK PLUNGER STATIONARY LATCH SUPPORT TUBE STATIONARY GRIPPER LATCHES LINKS INDIAN POINT UNIT No. 2 UFSAR FIGURE 3.2-66 CONTROL ROD DRIVE MECHANISM SCHEMATIC MIC. No. 1999MC3725 REV. No. 17A

§ w @ 90"----G x @ § Note: Part-length rods have been removed since the orginal design. [ii! ,-l A ,-\":,\ @ t7 1,.-;:\ \: "' [)( §] --@ --1,;, .... @ I I Ji< A I l ' G I I *@* I I @ I I I 11 I I I I 00 @ 1;;_, , __ Ii!] --G* , ... \P_;J @ ROO CLUSTER CONTROL BANKS BANK SYMBOL Sl 0 S2 0 S3 0 S4 D Cl \7 C2 6 CJ 0 C4 0 Pl ,-, \. .... 'V x --r>< '7 (PART-LENGTH ROD)* FIXED INCORE x @ "fY

...... @ -A. x -----2700 r .....

@ w §] @ INDIAN POINT UNIT No. UFSAR FIGURE 3.2-67 THIMBLE LOCATIONS

-FIXED INCORE DETECTORS 2 MIC. No. 1999MC3726 I REV. No. 17A 15 J. , 10 9 8 7 6 5 L J 2 1 ' I

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L£ LOCAT I ON **** _ * *

  • 65 YOYA3l£ D::T::CTOR LOCATION .*.* 50 lc=>I FLOT l.llXING DEVICE LOCATION .. 132 0 FIXED DE:TE:CTOR LOCATION **.... 8 INDIAN POINT UNIT No. 2 INCORE DETECTOR, THERMOCOUPLE AND FLOW MIXING DEVICE LOCATIONS UFSAR FIGURE 3.2-68 I REV. No. 19 lllUTI NGHOUSlll PROPRI lll'l.'Al\Y CLASS 2 ll'IGU:U:

2 INDIAN POINT UNIT 2, CYCLE 21 CORE COMPONENTS ANO ll':U:SH INTEGRAL BA LOCATIONS 15 14 13 12 11 10 llCCA 2011 lOOI 148I l48I 2011 RCCA 148I RCCA RCCA ll6I l6w 20W 148I RCCA l48I 148! l 6W 20W lOOI RCCA l4 8I l48I RCCA 20W 20W 20W RCCA 148I ll6I 148I 148I 20W 20W 20W RCCA RCCA 148I 14 8I 148I RCCA 20W 20W 20W RCCA RCCA 14SI 14SI HSI 148I 20W 2 ow 20W RCCA 148I 14 8I USI RCCA 20W 20W 20W RCCA l48I ll6I l48I HSI l 6W 20W lOOI RCCA RCCA 14 SI l48I 6SSA 16W 20W RCCA 148I 148I 14SI 20W RCCA 14 SI RCCA RCCA ll6I RCCA 20W lOOI l48I 148I LEGEND COMPO!fEN'l" TYP& NUMBER OF FR&SB IFBA RODS RCCA -CON'l'ROL oa SHUTDOWN RCCA #IW NUMBD 01' RODLETS ON WABA ASSEMBLY #SSA -NUMBD OJ' RODL&TS ON SECONDARY' SOURCE ASSEMBLY 8 RCCA U8I 2 011 14 SI RCCA 2 ow l48I RCCA 20W 14 8I RCCA 2 ow 14 SI RCCA 2 ow l48I RCCA 2 ow 14 SI RCCA 14 SI 270° 7 2011 l48I RCCA 20W l48I RCCA 20W 148I 20W l48I 20W 148I 20W 148I RCCA 20W 148I 6 RCCA 148I 20W ll6I 20W 148I RCCA 20W l48I RCCA 20W l48I RCCA 20W l48I 20W ll6I RCCA l48I 5 4 3 2 1 lOOI p RCCA 1481 RCCA l6W USA llCCA M l48I l48I l6W RCCA lOOI -L l48I 20W 20W RCCA -K 148I ll6I l48I 20W 20W RCCA -J 14 SI l48I 20W 20W RCCA RCCA -H l48I 148I l48I 20W 20W RCCA RCCA -G l48I l4SI 20W 20W RCCA -I' l48I ll6I 14SI l6W RCCA lOOI -E 14 SI 16W RCCA l48I -o l48I RCCA 14 SI RCCA -c lOOI -B A Fuel Assembly Ori en tat ion

  • JRaference Hole OCore Pin Hole \ Holdown Bar NOTE: Figures are Top View C<MPONENT ORIENTATION SHOwN IN TABLE 2 INDIAN POINT UNIT No. 2 CYCLE 21 REGION AND FUEL ASSEMBLY LOCATIONS UFSAR FIGURE 3.2-68A I REV. No. 23 LEGEND 15 14 13 2llil lf31 218 22lil lf32 X48 228 238 X40 2A83 22B 23lil 228 :X:56 2Al3 X34 228 23lil 23lil :X:45 2A38 2A21 22B 23lil 22lil :X:49 2A62 X07 21A 23A 23A W16 2A05 2A06 228 238 228 :X:71 2A30 XlO 22l!I 238 23l!I :X:O!I 2A55 2A23 22l!I 23lil 228 :X:62 2Al5 Xl3 22l!I 23lil X29 2A68 21l!I 228 lf28 X26 2ll!I lf38 Reqion Identifier WESTINGHOUSE PROPRIETARY CLASS 2 FIGURE 1 INDIAN POINT UNIT 2, CYCLE 21 REGION AND FUEL ASSEMBLY LOCATIONS 12 11 10 9 s 7 5 22lil 22lil 22lil 21A 22lil 22lil 22lil :X:73 :X:18 :X:75 lf 11 X64 X14 :X:67 228 238 238 23lil 23A 238 23lil 23lil X31 2A10 2A29 2A51 2A02 2A54 2A70 2Al2 2 3lil 22lil 238 22lil 2 3A 22lil 23lil 228 2A72 :X:23 2Al8 XJO 2A04 :X:28 2A20 :X:35 228 23lil 22B 23B 2 2lil 238 228 238 :X:79 2A36 :X:82 2A63 X68 2A65 X50 2A59 2 38 22B 238 22B 2 38 22B 238 228 2A50 X76 2AS3 :X:87 2A25 xeo 2A69 :X:84 228 23B 22B 23lil 2 2B 238 22lil 238 :X:93 2A77 XU 2A75 ll:96 2A67 :X:37 2A88 2 38 228 238 22B 23B 22B 238 228 2A74 X81 2A37 X20 2A79 xos 2A35 :X:63 22B 23l!I 228 23lil 22A 238 228 23B :X:89 2A57 :X:Sl 2A76 X03 2A78 :X:60 2A87 238 22l!I 23l!I 22l!I 2 3l!I 22l!I 23l!I 22l!I 2A86 :X:88 2A31 X38 2A43 Xl5 2A34 :X:90 22l!I 23l!I 22l!I 238 2 2l!I 238 228 23lil X54 2A39 ll:l7 2A71 X91 2A60 X41 2A80 238 228 23B 22l!I 2 38 22l!I 23l!I 228 2A40 :X:83 2A49 X55 2A33 X66 2A32 :X:86 22B 23lil 22l!I 23lil 2 2lil 238 22l!I 23B X72 2A81 X59 2A42 X92 2A28 X74 2A26 238 22l!I 23lil 22lil 23A 22lil 23lil 228 2A85 :X:25 2A24 X43 2A08 X46 2Al9 :X:24 22l!I 238 23l!I 23B 23A 23l!I 23l!I 23l!I X47 2A16 2A84 2A46 2A03 2A45 2A64 2All 22l!I 22l!I 22lil 2 lA 22lil 22l!I 228 X52 :X:44 X94 lfl9 X53 Xll X6l 270° 4 3 2 1 22lil 218 X27 lf40 238 228 218 2A27 X22 lf33 22lil 238 228 X65 2A61 X33 23B 228 23B 228 2A48 X42 2Al4 :X:77 22B 23B 23B 22B :X:7 8 2A22 2A66 :X:l2 238 228 23lil 22B 2A52 X06 2A73 X58 228 23A 23A 21A X85 2A07 2A01 lfl8 23l!I 22lil 23lil 22l!I 2A44 X36 2A56 us 22l!I 23lil 23l!I 22l!I X69 2Al7 2A58 ll:l6 23l!I 22l!I 23l!I 22lil 2A41 X21 2A09 X70 22l!I 23l!I 22l!I X57 2A47 xn 23l!I 22lil 2ll!I 2A82 X32 lf30 22l!I 2ll!I :x:oe lf45 Fuel Assembly Orientation -R -J? N -L -K -J -H -G -I' -E D -c -B -A Fuel Assembly Identifier
  • Reference Hole OCore Pin Hole Holdown Bar NOTE: Figures are Top View INDIAN POINT UNIT No. 2 CYCLE 21 CORE COMPONENTS AND FRESH IFBA LOCATIONS UFSAR FIGURE 3.2-688 I REV. No. 23 BA Rod Cladding Zone Number Pnmous Oesiqn BA WA.BA Desiqn 0 *1 AJt' Wamr 1 -2 St41iniess steef Zin:aloy 2-J Air Helium I* ....... I 3-4 Borosilicate glass Al203
  • a 4 c 4-5 Air HeJium 5*6 Stain less stetd Zin:aJoy INDIAN POINT UNIT No. 2 UFSAR FIGURE 3.2-69 COMPARISON OF BOROSILICATE GLASS ABSORBER ROD WITH WABA ROD MIC. No. 1999MC3730 IREV. No. 17A rn I I ANNULAR PLENUM 150.0 TYPICAL r A 134.0 TYPICAL ABSORBER LENGTH J_ MIC. FLOW PATH t UPPER END PLUG ZIRCALOY TUBES -,.

ANNULAff PELLETS Fl.OW PATH INDIAN POINT UNIT No. UFSAR FIGURE 3.2-70 WET ANNULAR BURNABLE ABSORBER ROD 2 No. 1999MC3732 f REV. No. 17A

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