ML16280A165

Amendment Update to the Updated Final Safety Analysis Report (Ufsar), Revision 26 - Chapter 3, Reactor, Figures

ML16280A165
Person / Time
Site:	Indian Point
Issue date:	09/19/2016
From:	Entergy Nuclear Operations
To:	Office of Nuclear Reactor Regulation
Shared Package
ML16280A161	List: ML16280A153 ML16280A159 ML16280A160 ML16280A162 ML16280A163 ML16280A164 ML16280A165 ML16280A166 ML16280A167 ML16280A168 ML16280A187 ML16280A188 ML16280A189 ML16280A190 ML16280A191 ML16280A192 ML16280A193 ML16280A194 ML16280A195 ML16280A196 ML16280A197 ML16280A198 ML16280A206 ML16280A207 ML16280A208 ML16280A209 ML16280A210 ML16280A211 ML16280A212 ML16280A213 ML16280A214 ML16280A215 ML16280A216 ML16280A217 ML16280A218 ML16280A220 ML16280A221 ML16280A222 ML16280A223 ML16280A224 ML16280A228 ML16280A229 NL-16-109, HI-2094289, Licensing Report on the Inter-Unit Transfer of Spent Fuel at the Indian Point Energy Center NL-16-109, Indian Point 2 Improved Technical Specifications Bases NL-16-109, Indian Point 2 Technical Requirements Manual NL-16-109, Indian Point Unit No. 2 Amendment Update to the Updated Final Safety Analysis Report (Ufsar), Revision 26, Chapter 10, Steam and Power Conversion System NL-16-109, Indian Point Unit No. 2 Amendment Update to the Updated Final Safety Analysis Report (Ufsar), Revision 26, Chapter 10, Steam and Power Conversion System, Figure 10.1-1, Revision 21 to Figure 10.2-9 NL-16-109, Indian Point Unit No. 2 Amendment Update to the Updated Final Safety Analysis Report (Ufsar), Revision 26, Chapter 10, Steam and Power Conversion System, Figures 10.2-1 to 10.2-7 NL-16-109, Indian Point Unit No. 2 Amendment Update to the Updated Final Safety Analysis Report (Ufsar), Revision 26, Chapter 11, Waste Disposal and Radiation Protection System NL-16-109, Indian Point Unit No. 2 Amendment Update to the Updated Final Safety Analysis Report (Ufsar), Revision 26, Chapter 11, Waste Disposal and Radiation Protection System, Drawing No. 9321-F-2719-136 to Drawing No. 9321-F-2730-75 ... further results
References
NL-16-109
Download: ML16280A165 (58)

Text

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0 6 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* - ~ ~ -- il-(0) ~ Sl S2 SJ S4 Cl C2 Cl C4 PL ~ 'zy (Part Length) fil] \\!L) /\\ - (Pi.i - ~ Q w Cn1 - ~ ~ 1i3 l~l ~ SYMBOL 0 D 0 \\l e:,, 0 0 0 ~ mi ~ I I ~ I ~ £ I ~ I Q I I eJ - I I IQ I l! I ~ § I I I (g) 'W @)' (~9 [@ w ~ I' ~) ~ ij QC.:,) -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 -~io--- -CL I ~L~, EJEJEJEJbD 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 - -cL 1.02 14068 l I I .79 10620 I CL 1.12 r=-1 Q r-:-11:1 14974 ~ ~ ~ ~ 1:11--:11.:l ~~~ CL - Center - Line F 6H.. 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

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0. 777 0.579 l.43CJ 1.447 1.544 1.437 1.308 0.944 0.424 0.401

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1. 487 1.437 1.407 1.160 1.010

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1.088 0.944 1.010 0.948 1.109 0.535 0.88~

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 6H 1.349 Y x l ?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

2.2 a: 2.0 w ~ 0 a. )( x <(

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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. 1. 0 ___ _,___...._____.__-.6-_...L-..--J.---L...--L--L----1.-.....J 0 BOTTOM 2 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. 17A

2 23 2004 11 :50:42 AM vnd1999MC3590-0-17B.DWG 1.2

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.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 I 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 r&'I l8l 181 181 181 181 181 181 181 0 181 181 121 181 181 r&'I 181 0 181 0 0 0 181 181 181 181 181 r2l 0 181 r2l J81 181 181 181 181 181 181 181 181 20 BP's 16 BP'2 t CENTER OF CORE 181 181 0 181 181 181 181 181 181 181 0 D 181 181 r&'I 181 181 181 D D D 0 0 0 181 0 0 181 DO OD 181 181 ° 181 181 0 o 0 o 0 12 BP's 9 BP'2 181 181 181 0 t2J 181 D 181 0 181 0 0 181 0 0 0 0 0 DO 0 8 BP's INDIAN POINT UNIT No. 2 UFSAR FIGURE 3.2-9 BURNABLE POISON ROD LOCATIONS CYCLE 1 MIC. No. 1999MC3592 !REV. No. 17A

+10 0 0 -

z:

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LLI er: 0,_ -c er: I.LI -110 0 0 :z: -50 0 100 200 300 "00 MODERATOR TEMPERATURE (°F) 500 +****

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• 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 -2.5 600 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 I REV. No. 17A

LL 0 E (,) Q. +5 0 100 , I T.

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--.. ---*~ 4 200 300 400 500 i ' . --*t. ;* - L !. I* -t.. -- ~-... 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 1.9 1.8

1. 7 1.6 1.5 0.....

1.4 &I'\\ CP ~,~ 1.3 "Q "Q ,...; :>e: 1.2 1.1 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

k I p,. 0.... 1.0 ~I~ POWER COEFFICIENT VS PERCENT POWER WITH TMOD - 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

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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 vnd 1999MC3643-0-17B.DWG 0.07 LEGEND: PERCE HT PERCENT ~ THEORETICAL THEORETICAL DENSITY DENSITY 0.06 D GYLLANDER 96.~ 0 HOWARD & GULVIN 96.0 ASAMOTO 95.0

• LUCKS & DEEM 96.5

~ 0 GODFREY 93.~ 0 DANIEL ET AL. 96.5 l'T'I

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~ STORA 92.2 FEITH 97.9 ~ 0.05 r A.O. BUSH 9~.~ 0 VOGT ET AL. 97.0 ("') A SAMO TO 91.0 ~ NISHIJIMA 95.0 0 :z 0 'V KRUGER

93. 7.. WHEELER & AINSCOUGH 97.0 c:

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0 ("') Ll-cr-n-= 0.02 ~'V~v v ' 0.01 0 ~00 800 1200 1600 2000 21WO 2800 3200 TEMPERATURE (T), °C INDIAN POINT UNIT No. 2 UFSAR FIGURE 3.2-38 TYPICAL THERMAL CONDUCTIVITY OF U02 MIC. No. 1999MC3643 IREV. No. 178

27 26 25 24 23 22 21 20 19 t: ~ 18 ~ 17 ~ ~ 16 ~ ~ ~ 15 ~ 14 13 12 11 10 9 8 7

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Defected) -'-* ~~ f (X) No. of Rods V1IlJJID. CVTR. Irradiation Program 11111 Saxton Irradiation Program (LRD Program) flil'.mm Saxton Puo2 + uo2 Progrlllll j.*.*.-:.:*I Yankee Core 5 1-:-1 Current Programs (Date ~ Shown is Completion Date)

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.:.; 425 Rods : : : - - --, ----:--;- ~:-*-

~ . i. ~. 0 10 20 30 4 6 MAXIMUM EXPOSURE - 103 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 vnd 1999MC3645-0-17B.DWG 2-0 N t-u.. I CY.

c

-D~ t-1*5 0 m '° 0 -.. m z Q = er Q l*O a:: vi LW

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UNIFORM FLUX OATA x EOUIVALEHT.UM I FORM DATA CONVERTED FROM HON-UNIFORM DATA 0*5 l*O 1*5 2*0 2*5 PREDICTED q"oNB I06 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 IREV. No. 178

2 23 2004 11 :51 :50 AM vnd 1999MC3678-0-17B.DWG -a r---, .a = c z m 3:,,, V1 c: ~ c - ..Ct -- c z m ~ ~ 0 ("") -t c v -- 3: -z 0 z m l) 40 50 60 70 80 90 95 98 99 99.8 99.9 l ~' 99.99 v ./' Ii"" 0.6 ~ / / / ~ / / / /

10. OF DATA POINTS = 809 MEAN VALUE

= 0.996 STANDARD DEVIATION = 0. 132 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 IREV. No. 17B

1.0 ~ I&. rl: J: 0.8 a:i (Q 0.... Ci w 0.6 a:

i Cl)

<( w ~ al z 0 0.4 'er ().2 LEGEND: L GRID DATA ~ 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/ 0--~~-----~~---'---~~~...._~~~.1.-~~~.r..-~~~...._~~--' 0 0.2 0.4 0.6 0.8 1.0 1.2 1.4 q" DNB (PREDICTED). 106 BTU/HR-FT2 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

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0*5 c -20% c I.I.I 0-4 ~ vi < 0*3 I.I.I ~ 110. 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, 106 BTU I HR-FT2 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 IREV. No. 178

2 23 2004 11:52:07 AM vnd1999MC3681-0-17B.DWG .8 .7 '° .6 'o ~ c: I .5 c::::

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I-al .4 Vl LA.J ~ = .3 er .2 .I o P = 1614 PSIA 6 P = 1814 PSIA c P '" 20l4 PSIA 0 P

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-25'fo QK----'-----'.__ __ _._ __ --' ____ _,_ __ --1. ____..J.-__......J 0 .I .2 .3 .4 .5 .6 .7 .8 q II (BTU /HR-FT2) 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 IREV. No. 178

2 23 2004 11:52:14 AM vnd 1999MC3682-0-17B.DWG 1.2 .. I- ~ 1.1 a: -- ~ I-1.0 ~ )I(

i Q.9 w..

I-0.8 c( II.I - 0.7 c( :: I-- Q.6 a: u c o.s II.I =

i 111 c(

0.4 ~ "' Q.l _2 0.2 = --.... =j 0.1 o 0 0.1 0.2 + + +

• 9S% 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 (Q~H,:10G1 PREOICTEO CRITICAL HEAT FLUX IBTU/HR*FT21 INDIAN POINT UNIT No.

UFSAR FIGURE 3.2-44A TYPICAL 1.2 2 MEASURED VERSUS PREDICTED CRITICAL HEAT FLUX-WRB-1 CORRELATION MIC. No. 1999MC3682 IREV. No. 178

2 23 2004 11 :52:20 AM vnd 1999MC3683-0-17B.DWG 4 / HEAT FUJI llTUIHR*n2 011*0.111 '°' /* MASS FUJW RATE L.a/HR*n2 QM*Z.5al0* / // PRESSUM, PSIA 51()* 3190 / F1UI TEMP. DROP, *F

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/ / TUIE LO., IN. Q.IO*Q.32 / COOLANT TEMP., *F 483* 105 / z 9LL TE....., 158*ll09 z z 4 INDIAN POINT UNIT No. 2 UFSAR FIGURE 3.2-45 TYPICAL STABLE FILM BOILING HEAT TRANSFER DATA AND CORRELATION 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 i-{==~tt"""~..;_~_L THERMAL SLEEVE )12~~f.i:.l~r-J.~CONTROLROO SHROUD TUBE ffi~~~~z'(j_~HOLD-DOWN SPRING ALIGNMENT PIN ~1Df-.i..4-- CONTROL ROD GUIDE TUBE lritt--1:4--+......LL 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 J 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

~CONTROL ROD ~ ASSEMBLY ROD --- ABSORBER ---TOP NOZZLE ---FUEL ROD ~GRID ASSEMBLY ~ABSORBER 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. SPIDER BODY MIC. INDIAN POINT UNIT No. 2 UFSAR FIGURE 3.2-50 ROD CONTROL CLUSTER ASSEMBLY OUTLINE No. 1999MC3688 I REV. No. 17A

I i 1 I I I I : I i I < i -'i _J ___ ; I I / I /i I ~ INDIAN POINT UNIT No. 2 UFSAR FIGURE 3.2-51 CORE BARREL ASSEMBLY MIC. No. 1999MC3705 I REV. No. 17A

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Hote: (1) All d1m. corrected to 68~F ~ 2° (2) 01mens;ons 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

153.680 REF. *

• 161.380 REF. OVERALL LENGTH *- --*

1611.JOO 1611.280 Note: Dimensions are expressed in inches. INDIAN POINT UNIT No. UFSAR FIGURE 3.2-55 HIPAR FUEL ASSEMBLY MIC. No. 1999MC3709 1 REV. - -- -- *-*-*1 2 No. 17A

Note: Dimensions are expressed 1n 1nches. INDIAN POINT UNIT No. 2 UFSAR FIGURE 3.2-56 LOPAR FUEL ASSEMBLY MIC. No. 1999MC3710 REV. No. 17A

OPTIMIZED (QFAJ FUEL ASSEMBLY I 159.975 153.60 134.07 113.26 93.70 76.77 59.84 41.28 23.47 6.383 OFA 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 0 I 122.78 f 112. B 9 1 0 2 50 t 3 3."3 3 i B ~.JS t 7 6. -+ 0 t 5 9. 1 7 I 1 0. 9 1 t 2 3. 1 0 INCONEL GRID DEBRIS FILTER BOTTO~ NOZZLE

• VANTAGE+ FUEL WITH PERFORMANCE +

FEATURES WILL HAVE ZIRLO' MIDGRIDS. LPD ZIRC* GRIDS (i) FUEL ROD LENGTH 1~2.55 ~ID GRID HEIGHT 1.50 ZIRLO'" CL.~DDING 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 MIC. ____. z1RCALOY THIMBLE ~ lZIRLOrn forVANTAGE+l SPOT WELD ~SS INSERT ZIRCALOY THIMBLE END PLUG INDIAN POINT UNIT No. UFSAR FIGURE 3.2-57 GUIDE THIMBLE TO BOTTOM NOZZLE JOINT 2 No. 1999MC3713 f REV. No. 17A

BUTT WE LO 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 I REV. No. 17A

~---- A.."""'/\\->--~ ...., Lt :-1,... I ::. ~ =r AT=- ~~-\\. I ADAPTER P1 A-- I t:. THRU HOLE SST NOZZLE INSERT

4. LOBE BULGE JOINTS

~THIMBLE / TUBE TOP ----t-..... / GRID "- '~..--.. UNASSEMBLED INDIAN POINT UNIT No. 2 UFSAR FIGURE 3.2-58A OFA and VANTAGE+ TOP GRID TO NOZZLE ATTACHMENT MIC. No. 1999MC3715 REV. 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 REV. No. 17 A

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~ID G~IO EXPANSION LOBE ~~~--~...._-ZIRC 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

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b c 0 0 0 0 ID I ID$Q* I&.;;;; ft o BURNABLE POISON ROD (7 BP'S ASYMMETRICAL) UNIRRADIATED Sb-ROD PERMANENT SOURCE SPIDER ASSEMBLY x 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 l SPACER TUBE .4005DIA.~ ~~--- 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 i~i~~l~G r mE*" ~M" :~*:;*cm I .445MAX. WELD DIA. J ID $;',t;:::.~~=t'J

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142.68 REF. B:RNABLE POISON LENGTH_/ 3.410 REF.---..... ~~------ 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. 147.286 REF. CLADDING TUBE TYPE 304SST 142.95 REF. SPACER TUBE LENGTH .243 DIA. REF. .396DIA. REF. l .446MAX. WELD DIA. I :::::::?: 1* b ~5 55"" J..j-L-,.Jb"!d!jo::::::J=.=62

R:E-F~.::::~11=411:;;,'='-:::::;:.1;1-!i!!!!IREF. TUBE LENGTH 0.875 REF.

BOTTOM END PLUG TYPE 304 SST Note: Dimensions are expressed in inches. !NDIAN 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. 3.75" INDIAN POINT UNIT No. 2 UFSAR FIGURE 3.2-65 CONTROL ROD DRIVE MECHANISM ASSEMBLY No. 1999MC3724 lREV. No. 17A

-- DISCONNECT ROD --- LIFT POLE 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 ~-t~+---*- 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 ~ ~ ~ § Note: Part-length rods have been removed since the orginal design. [ii! ~!..' A \\":,\\ ~ t7 ~ 1,.-;:\\ \\: "' x ~ §] ~ [)( ~ 1,;, 'fl ~ I I

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§] INDIAN POINT UNIT No. UFSAR FIGURE 3.2-67 THIMBLE LOCATIONS - FIXED INCORE DETECTORS 2 MIC. No. 1999MC3726 f REV. No. 17A

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80I 80I 80I 80I 80I 80I 80I 80I RCCA RCCA RCCA RCCA RCCA RCCA RCCA RCCA RCCA RCCA RCCA RCCA RCCA RCCA RCCA RCCA RCCA RCCA RCCA RCCA RCCA RCCA RCCA RCCA RCCA RCCA RCCA RCCA RCCA RCCA RCCA RCCA RCCA RCCA RCCA 148I RCCA 148I RCCA 148I 148I RCCA 148I RCCA 148I RCCA 148I RCCA 148I RCCA 148I RCCA 148I RCCA 148I RCCA 148I RCCA 148I 148I 148I 148I 16W 116I 16W 116I 20W 116I 20W 116I 16W 148I 16W 148I 16W 148I 16W 148I 16W 116I 16W 148I 16W 148I 16W 148I 16W 116I 16W 148I 20W 116I 16W 116I 16W 116I 16W 148I 16W 148I 20W 116I 16W 148I 16W 148I 16W 116I 16W 116I 20W 116I 20W 116I 20W 116I 16W 148I 16W 148I 20W 116I 20W 116I 20W 116I 20W 116I 20W 116I 148I 148I 148I 148I 16W 116I 16W 116I 16W 148I 16W 148I 16W 116I 16W 148I 16W 148I 16W 116I 16W 148I 16W 148I 16W 116I 16W 116I 16W 148I 16W 148I 16W 116I 16W 116I 16W 148I RCCA 15 14 13 12 11 10 8 8 7 5 4 3 2 1 6 R P M L K J H G F E D C B A N FIGURE 2 INDIAN POINT UNIT 2, CYCLE 23 CORE COMPONENTS AND FRESH INTEGRAL BA LOCATIONS 0 270 RCCA RCCA 148I 16W 116I RCCA 148I RCCA 148I RCCA 148I RCCA 148I

AND FRESH IFBA LOCATIONS CYCLE 23 CORE COMPONENTS UFSAR FIGURE 3.2-68B REV. No. 26 INDIAN POINT UNIT No. 2 25A 2D17 25A 2D19 25A 2D11 25B 2D57 25B 2D33 25B 2D97 25B 2D91 24A 2C04 25B 2D64 25B 2D49 25B 2D90 25B 2D42 25B 2D31 25B 2D32 24B 2C80 25B 2D65 25B 2D76 25A 2D05 25A 2D01 25B 2D94 25B 2D79 25A 2D02 25A 2D04 24B 2C53 25B 2D81 25B 2D67 15 14 13 12 11 10 9 8 7 5 4 3 2 1 6 R P M L K J H G F E D C B A N LEGEND ID 24A 2C18 24B 2C64 24A 2C07 23B 2A55 24A 2C09 24B 2C30 24A 2C14 23B 2A60 23B 2A23 24B 2C67 25B 2D23 25B 2D46 25B 2D25 24B 2C59 25A 2D14 25B 2D69 25A 2D16 23B 2A19 25B 2D50 25B 2D52 24B 2C79 24B 2C22 24B 2C24 24B 2C84 23B 2A31 25B 2D59 25B 2D83 24B 2C96 25B 2D78 24B 2C43 24B 2C73 25B 2D66 24B 2C57 24B 2C36 25B 2D37 25B 2D84 24B 2C45 24B 2C48 24B 2C90 24B 2C89 25B 2D26 24B 2C86 25B 2D27 24B 2C78 24A 2C17 24A 2C16 24B 2C55 24B 2C93 24B 2C92 24B 2C29 24B 2C76 24B 2C44 24B 2C38 24B 2C56 24B 2C69 24B 2C25 24B 2C26 24B 2C60 24B 2C61 24A 2C08 24A 2C03 25B 2D58 24B 2C34 24B 2C40 25A 2D20 24B 2C31 25B 2D80 24B 2C58 25A 2D08 25A 2D10 24B 2C47 24B 2C32 24A 2C01 24A 2C12 23B 2A64 23B 2A84 24B 2C21 24B 2C65 24B 2C35 25B 2D82 25B 2D36 25B 2D92 25B 2D89 24B 2C66 24B 2C27 25B 2D86 24B 2C70 24A 2C06 24A 2C11 25B 2D38 25B 2D22 25B 2D30 25B 2D70 25A 2D03 25B 2D55 25A 2D13 25B 2D41 24B 2C87 24B 2C88 25A 2D12 24B 2C81 24B 2C72 24B 2C52 24B 2C51 24A 2C13 25A 2D21 24B 2C82 24B 2C75 24B 2C33 24B 2C71 25B 2D28 24B 2C91 25B 2D54 25B 2D95 24B 2C77 25A 2D09 25B 2D88 25B 2D56 24A 2C20 24B 2C74 24A 2C10 24B 2C49 24B 2C42 24B 2C85 24B 2C68 24B 2C83 24B 2C54 25B 2D47 25B 2D48 25B 2D73 25B 2D63 25B 2D71 24B 2C50 25B 2D85 23B 2A21 25B 2D61 25A 2D07 24B 2C41 25A 2D06 25B 2D72 24B 2C94 24B 2C95 25B 2D96 24B 2C28 24B 2C23 23B 2A35 25B 2D75 24B 2C46 25A 2D18 25B 2D93 25A 2D15 24B 2C37 25B 2D24 25B 2D29 23B 2A37 25B 2D44 25B 2D34 23B 2A20 24B 2C63 23B 2A38 24B 2C39 24A 2C15 24A 2C05 24A 2C02 24A 2C19 24B 2C62 25B 2D39

BA Rod Cladding Zone Number Previous Design BA WABA Desiqn 0 *1 AJr Wamr W-.dJ 1. 2 Stainless stem Zin:aloy 2-J Air Helium I*....... I 3.4 Borosilicate glass Al203

• a4c 4.5 Air HaJium

~a 5*6 Stain less steej 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

ANNULAR PLENUM 150.0 TYPICAL r A 134.0 TYPICAL ABSORBER LENGTH _L rn I I FLOW PATH t 1Y1~- UPPER END PLUG ZIRCALOY TUBES Al~:r!4C ANNULAff l'ELLETS Fl.OW PATH INDIAN POINT UNIT No. 2 UFSAR FIGURE 3.2-70 WET ANNULAR BURNABLE ABSORBER ROD MIC. No. 1999MC3732 REV. No. 17 A}}