ML20054B505

Primary Reactor Containment Structural Integrity Test, Final Rept

ML20054B505
Person / Time
Site:	Grand Gulf
Issue date:	04/14/1982
From:	BECHTEL GROUP, INC.
To:
Shared Package
ML20054B503	List: AECM-82-140, Forwards Primary Reactor Containment Structural Integrity Test & Primary Reactor Containment Integrated Leakage Rate Test, Final Repts.Fsar Section 3.8 Will Be Revised to Include Results of Containment Structural Integrity Test ML20054B505 ML20054B521
References
TAC-51866, NUDOCS 8204160565
Download: ML20054B505 (52)

Text

C~

ANY MISSISSIPPI POWER & LIGHT CO

' O' GRAND GULF NUCLEAR UNIT 1

/

NT 9

PRIMARY REACTOR CONTAI STRUCTURAL INTEGRITY TE FIN AL REPORT J ANU ARY 1982 9

!!Ple8!PJ8881L PDR

- - - ~

.. - - =

1 i

i i

1 J

l i

t l'

O t

I i

l MISSISSIPPI POWER AND LIGHT COMPANY l

GRAND GULF NUCLEAR STATION UNIT 1 I

I PRIMARY CONTAINMENT j

STRUCTURAL INTEGRITY TEST REPORT O

l f

1 i

i I

1 I

Bechtel Power Corporation

}

San Francisco, California January 1982 l

l l

i

' e j

t t

i I

l

i i

l 4

CONTENTS

[

f i

l E.*E*.

l i

1 i

4 r

1.

INTRODUCTION 1-1 l

2.

SUMMARY

AND CONCLUSIONS 2-1

i i

i i

3.

STRUCTURE AND PRE'SSURIZATION 3-1

)

t i

I I

4.

TEST PLAN AND PROCEDURES 4-1 i

i 1

5.

TEST RESULTS 5-1 1

i t

5.1 Containment Structure Deflections 5-1 5.2 Containment Concrete Cracking 5-3 i

i 5.3 Estimated Accuracy of Measurement 5-3 I

!i 6.

REFERENCES 6-1 i

I i

i 1

i I

e f

l I

b DH-105 11 1

FIGURES Figure No.

3-1 Containment Structure 3-2 SIT Pressure Cycle 4-1 Taut Wire Extensometer Locations - Radials at Elevations 167' and 202', Domes and Verticals 4-2 Taut Wire Extensometer Locations - Radials at Elevations 103'-6",

131', and 230' 4-3 Taut Wire Extensometer Locations - Equipment Hatch 4-4 Schematic Representation of Taut Wire Extensometer 4-5 Concrete Crack Mapping Areas 5-1 Containment Structure Average Deflections at 17.25 psig - Wall and Dome 5-2 Containment Structure Deflections at 17.25 psig - Equipment Hatch Radial 5-3 Typical Deflection / Pressure History - Containment Wall - H8 5-4 Typical Deflection / Pressure History - Containment Wall - H21 5-5 Typical Deflection / Pressure History - Containment Dome - D1 5-6 Typical Deflection / Pressure History - Equipment Hatch - E10 5-7 Concrete Crack Mapping - Area 1 5-8 Concrete Crack Mapping - Area 2 5-9 Concrete Crack Mapping - Area 3 5-10 Concrete Crack Mapping - Area 4 5-11 Concrete Crack Mapping - Area 5 5-12 Concrete Crack Mapping - Area 6 i

i. V DH-105 111

I 4

1.

INTRODUCTION The Unit 1 Containment Structural Integrity Test was conducted during i

the time period December 31, 1981 to January 2, 1982.

The primary purpose of the structural integrity test was to verify the design and structural integrity of the containment structure by imposing one hundred and fif teen percent of the design pressure for a period of not less than one hour.

In order to accomplish the intended test purpose, specialized measuring devices were installed in the containment structure to provide the data needed to evaluate structural response during pressurization and depressurization. The tests were conducted in accordance with written i

procedure QlM61-W-11302WXA (Reference 2), detailing test requirements and instructions for acquiring test data. This procedure is a part of the permanent plant records at the Grand Gulf Nuclear Station.

1 i

4 i

4 l

l I

Dil-105 1-1 i

2.

SUMMARY

AND CONCLUSIONS The containment structural integrity test provided proof of the struc-ture's ability to contain the internal design pressure and provided measurement of structural response to changes in internal pressure.

Test measurements for the containment included gross structural defor-macions and concrete crack growth. Measurement points were located at typical sections of the structure with measurements obtained at speci-fied stages during the pressurization cycle. The structure withstood the internal pressure with no observable indications of structural distress. All measured structural deformations were less than the design allowable values. All dome and vertical measurement points recovered more than 70 percent of their maximum deflection. Radial deflections at the elevation of maximum average deflection recovered more than 70 percent of their maximum deflection, also.

Changes in concrete cracks observed in the various surveillance areas did not change in measured width by more than 0.010 inches. This is considered to be within reasonable expectations based on the results of previous tests and does not adversely af fect the integrity of the structure. Prior to the start of pressurization, no cracks with 1

widths equal to or exceeding 0.010 inches were observed in the inspec-tion areas. Cracks developed in two of the six mapping areas during q

pressurization and closed to below measurable values at zero pressure.

The results of the structural integrity test provide direct experi-

[' T mental evidence that the containment structure can contain the internal

\\~ /

design pressure with a sufficient margin of safety and that the gross response to pressure is predictable.

l O

4 DH-105 2-1

/^}

3.

STRUCTURE AND PRESSURIZATION

' b The containment is a reinforced concrete structure designed to act as a pressure barrier during postulated loss-of-coolant accidents as de-fined in the Final Safety Analysis Report (Reference 1).

The structure consists of a reinforced concrete cylinder and hemispherical dome connected to and supported by a massive reinforced concrete base slab as shown in Figure 3-1.

Reinforced openings in the cylinder are pro-vided for equipment and personnel access as well as for electrical and mechanical feed through.

Principal dimensions for the containment structure are:

o Inside diameter 124 ft.

o Inside height 206 ft. 8-1/2 in.

o Vertical wall thickness 3 ft. 6-in.

o Dome thickness 2 ft. 6 in.

i o Foundation slab thickness 9 ft. 6 in.

The containment structure was pressurized pneumatically to verify the required structural integrity. The internal peak pressure of 17.25 psig was held for a period of two hours to record structural data.

(

For details of the pressure cycle see Figure 3-2.

1 The suppression pool and upper containment pool were both filled with water to their normal level for plant operation to provide the proper load on the containment and basemat.

I 1

1 1

t DH-105 3-1

)

8 0

/

"0

-'1 3

g 1

@0 0

0 7

0 L

9 E

2

3..

~

T f,

A g

NA a'

L P

f E

/

R

~

U T

C U

R TS T

N E"

"0 E

IN9 0

"6 "0

M 1

0 L*-

- 8

• 7 G7 8'

1 3'

N 3

4' N

0 1

r I2 2

1 1

L 8

3 9

AI R

0 L

P L

3 SE L

L E

T E

E E

L N

E O

1l 0

C

(

I j

}

I.

~

0 7

1 2

3

=

=

3 E

=

=

=

R r

y, U

e G

g I

F es 7.

i l

Il I

I I

l

['

.i W

7..

I l..

=

e

=

=

o

=

=

l

=

c

==

i

=

i 0

]

i g

9 uy

O O

18 -

N

[

1246 1900 1146 2000 15 PSIG

/

~

HOLDS 1041 2249 12 -

0930 0153 0730 0600 10 PSIG HOLDS m

Y m

=

0853 cc 8-0444 1137 0343 5 PSIG HOLDS I

4-1802

/

j 2M 2114 0

6 12 18 24 6

12 18 24 4

1 JAN 82 2 JAN 82 FIGURE 3-2 SIT PRESSURE CYCLE i

[]

4.

TEST PLAN AND PROCEDURES LJ Test measurements were made at points on the containment structure which represented typical areas to provide data on structural be-havior during the pressure test. The measured parameters consisted of gross structural deformation and concrete crack growth.

Gross structural deformations were measured using taut wire extenso-meters which spanned between points on the containment wall, dome, and springline and fixed points within and outside the structure.

The extensometers were located to measure radial displacements along typical wall sections and around the lower equipment hatch, vertical displacement of the dome relative to the operating floor, and vertical displacement of the springline relative to the foundation slab. The layout of the extensometer system is shown in Figures 4-1 through 4-3 and exact locations are listed in Table 4-1.

The extensometers, illustrated in Figure 4-4, consist of displacement transducer assemblies and low expansion alloy (invar) taut wires. A movement between opposing points on the containment shell or between a point on the containment shell and a fixed reference structure re-sults in an almost equal movement between the core and body of the linear variable differential transformer (LVDT) which is housed in the transducer assembly. The LVDT output is a voltage which is proportion-al to the position of the core within the body. The spring in the transducer assembly maintains a nominal 20 lb tension on the wire to

[G h

reduce sag and eliminate slack at threaded and swivel connections.

The extensometers are calibrated to establish the displacement - volt-age characteristics and spring constant (nominally 2 lb/in). Spring constant is used to correct for the small changes in wire length which result from transducer displacement. The transducers were calibrated prior to-shipment to the Grand Gulf Nuclear Station and again at the s t atio n.

The two sets of calibration data agreed to within the re-quired limits of accuracy.

The transducer's swivels and opposing taut wire ends were secured to fittings which were welded to the containment liner and other metal structures and epoxy bonded or expansion anchored to concrete. Follow-ing initial attachment, the transducers were aligned with the wires to eliminate LVDT core side loading and the core positions adjusted to provide the desired travel.

The LVDT's were wired to excitation power supplies and a scanning data acquisition system which converted LVDT output voltage to a digital fo rmat for register display, printed record, and direct entry into a microcomputer. The computer was programmed with extensometer calibra-tion constants and a routine which converted raw voltage data into displacement units.

bd DH-105 4-1

~,.

fs During the structural integrity test the deformation data were recorded t

at 2.5 psig pressure increments and decrements, at the beginning and end of all constant pressure holds, and at regular intervals during ex-tended holds. Additional data were recorded following depressurization to monitor post-test structural recovery and during the subsequent in-tegrated leakage rate test.

At each data acquisition point all voltages were recorded three times in rapid succession to provide a 2 out of 3 basis for identifying spurious values caused by electrical transients.

The recording of 3 complete records required about 2 minutes.

Concrete crack patterns were mapped in the areas shown in Figure 4-5.

The lengths and widths (measured by optical comparator) of all visible cracks within these areas were recorded prior to the start of pressuri-zation, at 10 psig during pressurization, at peak test pressure, and following the completion of depressurization.

I w

i 4

J O

DH-105 4-2

~.

(

2700 v4 0 3150 V3 @ 225%

r H

l l

_____A.___

0 195 s 180 '

- -0 0

D1 2700

/

q b

d>

\\

/

S

,g D2

.- ip I

b I

0 H2O @ 150 5

H11 h

8V k

y_Ej H19 @ 300 s-0

)

D3J

(

O V2 @ 135 V1 @ 460 H10 H12 3300

-r 3

9 V

900 750 (NOM)

Y

- Oo ELEVATION 202'-0" e

LIVE END H9 H7 30o O

w

\\

ELEVATION 167'-0" g

H8 o

FIGURE 4-1 go TAUT WIRE EXTENSOMETER LOCATIONS-RADIALS AT ELEVATIONS 167' AND 202', DOMES, AND VEi<TICALS

0 270 H18

(

• b:,.

2700 f

i l p

//

~.';

180*

0 0

0 210 3300 g

./

7

.,f '

H17 H16 150*

' i:

..y' 4

180 0

8 4-0 H15 H13

)

d H14 300

• o 150 2

ELEVATION 131'-0" n

90 H2 ll l

.l l.

i H5 ELEVATION 230*-0"

'EL93-0%. 7

_4

... - l.

BASEMAT ELEVATION 103'--6" (OUTSIDE CONTAINMENT) 0 0

0 0

0 0

6 EXTENSOMETERS AT 30,90,150,210,270, 330 FIGURE 4-2 TAUT WIRE EXTENSOMETER LOCATIONS - RADIALS AT ELEVATIONS 103'-6",131', AND 230'

O O

O DRYWELL WALL

~

CONTAINMErJT WALL i

E1

' I*

l o

e l

4 l

l 2400

-*' O O

23'-6 5/8" 25'- 2 5/8" 16*-10_7/8'*_ _

20'-3 5/8" _

g g

E3 l

10'- 6" 12'-8"

-b Ib

~~

w E L.172'-3" C

y

,' y CTMT WALL I

e.3,.--

a e-4 9-E4

.I co

\\E9 E7 E8 E10 E11 E12 I't -

E5

[

3 r.

3

..;,i,.

DRYWELL WAL' a-

-e, E6 3

O A

I

~

l SECTION FIGURE 4-3 TAUT WIRE EXTENSOMETER LOCATIONS - EQUIPMENT HATCH

C O

(';

v V

v ORE 1 IN. RANGE LVDT B

ING

. BODY LOCKABLE

/

SWlVEL LINER Q

LINER EYE l,

n, ~wnw,

,(WELD

\\

h

(

N INVAR WIRE

~

WELD 0.05 IN. DIA I

g ELECTRICAL CONNECTION SPRING B

BACKPLATE

[

FRAME FIGURE 4-4 SCHEMATIC REPRESENTATION OF TAUT WIRE EXTENSOMETER

O O

O CRACK MAPPING AREA 6 LOCATED AT APEX OF DOME (EL. 302'-3") 7' x 7'

\\

E L.237'-9" (SPRINGLINE)

AZ 260o CRACK MAPPING AREA #3 (7' x 7')

UPPER e

4 PERSONNEL LOCK CR ACK M APPI 4G r AREA #4 (4' x 10')

0 AZ 80 EQUIPMENT-CRACK MAPPING HATCH AREA #2 2

( AT EL.169'-6"-

( 7 x 7')

( OF AREAS 4 & 5 AT EL 172'-3'*-

X

/-

I CCR ACK MAPPING AREA #5 (4' x 10')

LOWER

- PERSONNEL AZ 260 CRACK MAPPING AREA #1 (7'x7')

E L.93'-1/4

0 (BASEMAT) 180 90 3600 2700 1800 i

0 0

FIGURE 4-5 CONCRETE CRACK MAPPING AREAS

TABLE 4-1 O-EXTENSOMETER LOCATIONS Elevation Radials (H) and Hatch (E) or Radius Table Extensometer Verticals (V) and Dome (D)

Azimuth A-2 H-1

.EL. 103'-0" 30*

A-3 H-2 EL. 103'-0" 90*

4 A-4 H-3 EL. 103'-0" 150*

A-5 H-4 EL. 103'-0" 210' A-6 H-5 EL. 103'-0" 270*

A-7 H-6 EL. 103'-0" 330*

i A-8 H-7 EL. 167'-0" 30' A-9 H-8 EL. 167'-0" 90*

A-10 H-9 EL. 167'-0" 150*

A-ll H-10 EL. 167'-0" 211*-08' A-12 H-il EL. 167'-0" 270*

A-13 H-12 EL. 167'-0" 330*

A-14 H-13 EL. 230'-0" 210*

A-15 H-14 EL. 230'-0" 270*

A-16 H-15 EL. 230'-0" 150*

i A-17 H-16 EL. 131'-0" 30*

A-18 H-17 EL. 131'-0" 150*

A-19 H-18 EL. 131'-0" 270*

g A-20 H-19 EL. 202'-0" 30*

d A-21 H-20 EL. 202'-0" 150*

A-22 H-21 EL. 202'-0" 270*

A-23 D-1 R

3'-1" 165*-30' A-24 D-2 R

31'-0" 75*

A-25 D-3 R

45'-0" 75*

i A-26 V-1 2

61'-8" 46*

A-27 V-3 K

61'-8" 225" i

A-28 V-4 R

61'-8" 315' l

A-29 E-1 EL. 198'-6" 240*

A-30 E-2 EL. 191'-2-1/2" 240' A-31 E-3 EL. 182'-9" 240' A-32 E-4 EL. 161'-9" 240*

A-33 E-5 EL. 153'-10-1/2" 240*

A-34 E-6 EL. 146'-6" 240*

A-35 E-7 EL. 172'-6" 217*-47' A-36 E-8 EL. 172'-3" 223*-14' A-37 E-9 EL. 172'-6" 230*-14' A-38 E-10 EL. 168'-2" 247*-07' A-39 E-Il EL. 172'-7-1/4" 259' A-40 E-12 EL. 172'-0" 264*

l DH-105 4-8

O 5.

TEST RESULTS k-)

The results of the structural integrity test provide direct experi-mental evidence that the containment structure can contain the design internal pressure with an ample margin of safety. Further, the test data confirm the validity of the analytical methods employed to deter-mine the structural effects of loading combinations and to predict the resulting deflections.

5.1 CONTAINMENT STRUCIURE DEFLECTIONS The response of the containment to the maximum test pressure of 17.3 psig is illustrated in Figures 5-1 and 5-2.

Figure 5-1 shows the measured radial and vertical growth of the cylinder wall and the measured vertical growth of the dome as well as the predicted growth based on both clastic and cracked section analyses. The measured vertical growth of the dome and wall is less than the elastic case prediction. This demonstrates that the stress in the dome and the vertical stress in the wall were not sufficient to cause extensive tensile cracking. It further demonstrates that the actual elastic modulus of the concrete is higher than that used in the computations.

The radial growth of the wall is between the elastic and cracked wall section case predictions. This demonstrates that hoop stress caused tensile cracking but did not develop the complete cracked section used as a model in the cracked section analysis.

O\\--

The wall radial deflections listed and plotted in Figure 5-1 are averages of the measurements made on several azimuths at each eleva-t io n.

The individual measurements made at each elevation show a variation from azimuth to azimuth which is attributed to round out of minor irregularities in the cylinder wall. This behavior is typical for concrete containments and is expected for any singly curved struc-tural element which does not have a perfectly true radius. In contrast the measured dome deflections show a smooth trend which is typical for a doubly curved surface. The measured wall vertical deflection listed in the figure is the average of the measurements at extensometers V1, V3, and V4 (V2 malfunctioned). Here the individual measurements are tightly grouped as is expected for the uncurved direction on the wall.

Figure 5-2 shows the measured radial growth of the wall in the vicinity of the equipment opening. The deflections measured along the horizon-tal center plane of the hatch are approximately symmetrical about the vertical center line. Measurements along the vertical center plane of the hatch show that the outward movement in the vicinity of the hatch increased with elevation. This behavior is typical for a large opening located close to the containment base mat.

Deflection / pressure histories at various points on the containment are illustrated in Figures 5-3 through 5-6 and all measured deflections are listed in Tables 5-1 through 5-39.

The plotted deflection / pres-

[)

sure histories all show essentially linear response during the initial e

DH-105 5-1

(}

stages of pressurization and throughout depressurization. Deviations

(_,/

from linearity are the deflection lags at the start of pressurization /

depressurization, creep response at constant pressure hold periods, and the increase in slope at higher pressures during pressurization.

The lag results from friction between moving parts of the extensometer and is normally not evident at the start of the test since the extenso-meter is initially set for motion in the proper direction. Where lag does occur at the start of the test, it is generally due to the extensometer being disturbed af ter being set.

Lag at the start of depressurization is always evident, except for extensometers with very short wires. This lag results from a reversal of friction forces in the extensometer and a consequent shortening of the wire.

Lag ef fects are corrected for where required by extrapolating the linear part of the plot through 0 psig (initial lag) or 17.3 psig (depressuri-zation lag) and calculating the deflection on the extrapolated line at this pressure. The difference between the deflection on the extra-polated line and the measured deflection at the same pressure is added to (initial lag) or subtracted from (depressurization lag) subsequent measurements to provide corrected values. The correction procedure is illustrated in Figures 5-3 and 5-5.

Creep response of the concrete is generally evident at the constant pressure hold periods, particularly at higher pressures. This is ex-pected and typical for reinforced concrete structures.

f~)/

All extensometers show on essentially linear deflection / pressure s-characteristic at low pressures which demonstrates initial elastic behavior of the containment. The characteristics for the dome and wall vertical extensometers remain linear through peak test pressure thus verifying the previously stated conclusion that the stresses in the dome and in the vertical direction in the wall are not sufficient to cause extensive tensile cracking and consequent departure from elastic response. The wall radial and equipment opening extensometers show significant changes in the deflection / pressure slope at varying levels of higher pressure. The point where the slope breaks represents initial tensile cracking.

If the initial slopes of the wall radial extensometers are extrapolated to 17.3 psig and corrected for initial lag as required (see Figure 5-3), the displacements on the extrapolated lines at peak test pressure are quite close to the displacement pre-dicted using the elastic case. This further verifies the validity of the constants and techniques used in containment analysis.

The recovery of containment deflections following the completion of depressurization was at least the required 70 percent at the points of maximum deflection. All dome and the three functioning vertical extensometers recovered over 70 percent of their maximum displacements.

Radial extensometers at elevation 167'-0", the maximum expected deflec-tion location, recovered 74 percent (af ter correcting for lag) of the average deflection of 0.178 inches. The two extensometers which measured the largest deflections at that elevation recovered over 80 percent of the deflected value. The largest average measured deflection f3 occurred at elevation 202'-0", where three extensometers were located.

G 5-2 DH-105 l

(}

The average maximum deflection at that elevation was 0.226 inches.

(_,/

The extensometers recovered 72.1 percent of the maximum value. The radial extensometer recovery data are based on readings taken af ter the ILRT, with readings ending at noon, January 5, 1982. Final de-flection values for all extensometers are listed in Tables 5-1 through 5-39.

Final values are adjusted for exteosometer lag where noted on the tables.

5.2 CONTAINMENT CONCRETE CRACKING The patterns of surface concrete cracks on the containment wall at specified internal pressures are shown in Figures 5-7 through 5-12.

A variety of surface cracks were mapped immediately prior to pressuri-zation, and a minimum number showed increases in length or width during the pressurization cycle. This is consistent with the low deflections recorded. The observed crack patterns are typical of those found on reinforced concrete containment structures.

During the subsequent ILRT pressure cycle to 12.5 psig, cracks which appeared in Crack Mapping Area 2 were monitored. Those cracks enlarged slightly from the zero pressure recovery value, and returned to hair-line width which was not accurately measurable with the optical comparators. Growth during the ILRT pressure cycle was estimated at 0.002 inches at the locations observed.

5.3 ESTIMATED ACCURACY OF MEASUREMENT The accuracy of measurement is based on the following items:

o Calibration of instrumentation a

o Laboratory testing as in the case of invar wire o Human factor, i.e., judgement of the reader Displacements in the containment structure were measured using taut wire extensometers. Accuracy of the extensometer is + 0.002 inches so long as wire tension remains constant. When the direction of pressurization changes, extensometer response lags due to friction in the mechanism. Typical lag is 0.02 inches for a 100-foot long wire.

The crack patterns were measured using optical comparators calibrated to measure crack width of 0.001 inches and wider. However, since most cracks observed on the containment were irregular traces on coarse textured concrete surfaces, it was not generally possible to estimate true crack width to better than approximately 0.003 inches. For this reason, reported crack widths are considered to be accurate to within

+ 0.003 inches.

O DH-105 5-3

DEFLECTIONS (INCHES)

WALL EL MIN MAX AVG PRED 1 PRED 2 103'-6**

.024 944

.034

.08

.01 131'- 0"

.056

.082

.071

.38

.05 167'- 0"

.084

.283

.178 42

.05

'g....,,

N 202'-0"

.201

.271

.226 42

.05

\\

230'-0" 184

.249

.214

.39

.04

' * * *.6 **

s DOME S.,

RADIUS DEFL PRED 1 PRED2 3'- 1"

.114

.54

.15 31'

.112

.51

.15 45'

.107

.46

.14 SP G

.027

.034

.031

.20

.08

(

i e

i i

i i

i I

Z i

i REFERENCE l

O l*J

[

0

.20

.40

.60 l

j g

SCALE - INCH ES i

I j#

l CRACKED ANALYSIS

=---

DISPLACEMENT l

l ELASTIC ANALYSIS j

f DISPLACEMENT I

i f

8 MEASURED VALUE I

NOTES:

/

1. PREDICTED DISPLACEMENT FROM CRACKED j

ANALYSIS

2. PREDICTED DISPLACEMENT FROM ELASTIC I/

ANALYSIS 6/

/

Z FIGURE 5-1 CONTAINMENT STRUCTURE AVERAGE DEFLECTIONS AT 17.25 PSIG -WALL AND DOME 5-4

i i

O O

O I

CONTAINMENT WALL if a

2400 E1 1

.233 G

23'-6 5/8" 25'- 2 5/8" F4 16*-10 7/8" 20'-3 5/8" E2 I

.258 G

.-4 10'-6" 12*-8" l

h bs CONTAINMENT

. 3'.e

,I 7

s Q 's WALL

.244

p

_g y

N

/

. 77..

g 1

lt.

. l- -

~

[.

.s. l *.y..

o O'

r w

i M

ja

=*f1.

8

';; y o

I E L.172'-3" E7 E8 E9 E10 E11 E12 la i6

,$c

.210 235

.205

.173

.200

.170

]

.213 G

y

. t, -

g an I

N E5 I

.187

=

. f

^

o, 0

.20 40

.60 I

SCALE - INCH ES I

I O

.167,

g b

[p[*

-f" FIGURE 5-2

~

CONTAINMENT STRUCTURE DEFLECTIONS AT 17.25 PSIG-EQUIPMENT HATCH RADIAL 1

1

O O

O e

g

.32

.283 a

1

.267-

\\

2

.241

\\

p

/

U

.24 Y

w d

u

.267

.162 I

\\

h

.16 N.

.136

.174 a-142 lN

.111

.108

.08

.038

%.052

.048 4

.004

\\

\\

\\

.008

• gig

.0 5 g

2.5 g-7.5 10-12.5 5'

17 5 PRESSURE (PSIG)

FIGURE 5-3 TYPICAL DEFLECTION / PRESSURE HISTORY-CONTAINMENT WALL-H8

O O

O

.206

.206

.197 N

.200 g

.183

/

\\

.160

\\

.185 -

z I

.131 O

i I

131 4

0

.120

.109

.113 4

5

.080

.040

.036

.008

.026

\\

\\

.020 y

.014 0

2.5 5.

7.5 10.

12.5 15.

17.5 PRESSURE (PSIG)

FIGURE 5-4 TYPICAL DEFLECTION / PRESSURE HISTORY-CONTAINMENT WALL-H21

O O

O 5

Z EXTRAPOLATED DEFLECTIOrl =.133 IN.

}

CORRECTION =.133.114 =.0 19 IN.

h EXTRAPOLATION OF L NEAR PART p

C F DEPRESSURIZATION PLOT y

.120

.105 Y

IIi

[

i "N /

.1oe -

/

s sy N

xg

.0e,

.054 CORRECTED RE SIDUAL

.050

\\

x'= O 71N x:

.035

\\

.008 0

2.5 5.

7.5 10.

12.5 15.

17.5 PRESSURE (PSIG)

FIGURE 5-5 TYPICAL DEFLECTION / PRESSURE HISTORY-CONTAINMENT DOME-D1

O O

O

.205

.192

.200

\\

.174

.152

\\

I

.160

.186 -

l 2

.113 b.129 x

.120 4

g g

l

.117 O

.090

_a N

5

.080 a:

\\

.068

.040 x

g,

.021

\\

.011 0

2.5 5.

7.5 10.

12.5 15.

17.5 i

PRESSUR E (PSIG) i i

FIGURE 5-6 TYPICAL DEFLECTION / PRESSURE HISTORY-EQUIPMENT HATCH-E10

O Y

E L. 96'- 6" 1' SQUARE 260 TEMPOF DATE TIME STAGE PSIG REMAR KS IN OUT 12/31 1203 69.80 64 1

0 1/1 0800 76.7 66 2

10 NO CRACKS > 3 THOUS.

1/1 1407 78.2 66 3

17.30 NO CRACKS > 5 THOUS.

1/2 2124 67.4 64 4

0 NO CRACKS > 5 THOUS.

FIGURE 5-7 CONCRETE CRACK MAPPING O

AREA 1 5-10

.01

).0 2"

.01 16**

V l

010" o)

N L

DN N

n 8"

.012"

-t-

- E L.169'- 6" r

l' SQUARE l

800 5"

5" 4

2

.012"

.013" O

@W L

LOCATION OF CRACK WIDTH MEASUREMENT N = STAGE NUMBER L = CRACK LENGHT IN INCHES W = CRACK WIDTH IN INCHES TEMP 0F DATE TIME STAGE PSIG REMARKS IN OUT 12/31 1210 75.37 72 1

0 ONLY TWO CR ACKS OVER.01" WERE 1/1/82 830 76.7 61 2

10 OBSERVED. NO OTHER CRACKS OB-SERVED GREATER TH AN.008'.'

NO OTHER CRACKS GREATER 1/1/82 14:19 78.2 61 3

17.25 THAN.00B" OBSE RVED.

!/2/82 21:30 69 69 4

0 NO OTHER CR ACKS OBSERVED.

O FIGURE 5-8 CONCRETE CRACK MAPPING AREA 2 5-11

t i

O Y

E L. 2 37'- 9" l

m 1' SQUARE 0

260 TEMP OF DATE TIME STAGE PSIG REMARKS 12/31 1230 76.98 6B 1

0 1/1/82 8:06 AM 76.7 61 2

10 NOTHING OBSERVED OVER 0.005" NOTHING OBSERVED OVER 0.005",

1/1/82 2:20 PM 78.2 62 3

17.25 THESE CRACKS EXTENDED IN LENGTH ONLY.NO NEW CRACKS.

NOTHING OBSERVED OVER.003 1/2/82 9:28 PM 74.3 68 4

0 CRACKS DECREASED IN WIDTH l

FIGURE 5-9 CONCRETE CRACK MAPPING lqb AREA 3 5-12

O E L.172'-T' I

1' SQUARE I

TEMP F DATE TIME STAGE PSIG REMARKS IN OUT 12/31 12:17 75.38 66 1

0

^

^

"^

1/1/82 07:45 76.7 55 2

10 ERVED NO CRACKS LARGER THAN 0.007" 1/1/82 14:00 78.2 58 3

17.3 OBSERVED 1/2/81 21:40 72 69 4

0 NO OTHER CR ACKS OBSERVED FIGURE 5-10 CONCRETE CRACK MAPPING AREA 4

\\'

5-13

l 1

I O

20 30 40 10 9

8 7

6

- E L.17 2'- 3" 5

/

21" A

/

0.010P' 4

LOCATION OF CRACK WIDTH MEASUREMENT

\\

o 8'

1' SQUARE I

N = STAGE NUMBER 1

L = CRACK LENGTH 1/ \\

IN INCHES 11 21 31 \\

A 15" W = CRACK WlDTH 2

U 0.010" IN INCHES 1.5" 3

0.011" TEMP F DATE TIME STAGE PSIG REMARKS IN OUT 12/31 12:20 15.33 66 1

0 BLOCKS 6 & 7 HAD NEW CRACKS 1/1 8:30 76.7 63 2

10 NO GREATER THAN 0.003 NEW CRACK 13" BLOCK 33.

1/1 14:10 74.2 55 3

17.30 NEW CRACK BLOCK 37 1/2 21:34 72 64 4

0 NO CRACKS >.004" O

rieune e-,, concnere cnAcx uAre,se AREA 5 5-14

/

-t-900 o

1' SQUARE l

180 7-DENOTES APEX OF DOME TEMP 'F DATE TIME STAGE PSIG R Ef.1AR KS 12/31 12/25 77.31 67 1

0 1/1/82 8:27 AM 76.7 65 2

10 NOTHING OBSERVED OVER. 008 NOTHING OBSERVED OVER.008 1/1/82 2:53 PM 78.2 68 3

17:25 SLIGHT EXTENSION IN LENGTH OF EXISTING CRACXS ONLY 1/2/82 9:36 PM 74.7 67 4

0 NOTHING OBSERVED OVER.008 CRACKS DECREASED IN WIDTH FIGURE 5-12 CONCRETE CRACK MAPPING AREA 6 5-15

~

. - =

1 4

4]O TABLE 5-1 t'

SUMMARY

OF DATA FOR TRANSDUCER H-1 i

j' (Psig)

Displacement Date Time Pressure (inches) i 1/1 0000 0

0.000 1/1 0205 2.5 0.000 1/1 0343 5.0 0.002 1/1 0622 7.5 0.004 1/1 0930 10.0 0.006 1/1 1041 12.6 0.C09 l

1/1 1246 15.0 0.024 1/1 1349

'17.3 0.027 1/1 1630 17.3 0.029 1/1 2000 15.1 0.029 1/1 2249 12.5 0.028 1/2 0153 9.8 0.026 1/2 1458 5.1 0.021 1/2 1802 2.5 0.019 l

1/2 2114 0

0.015 TABLE 5-2

SUMMARY

OF DATA FOR TRANSDUCER H-2 O

(Psig)

Displacement Date Time Pressure (inches) l 1/1 0000 0

0.000 1/1 0205 2.5 0.000 i

1/1 0343 5.0 0.002 i

1/1 0622 7.5 0.004 1/1 0930 10.0 0.007 1/1 1041 12.6 0.010 1/1 1246 15.0 0.025 1/1 1349 17.3 0.028 1/1 1630 17.3 0.031 1/1 2000 15.1 0.031 1/1 2249 12.5 0.029

+

1/2 0153 9.8 0.026 1/2 1458 5.1 0.022 1/2 1802 2.5 0.020 1/2 2114 0

0.017

+

I i

1 O

DH-105 5-16 i-

=..

.~

. ~ _

i f

I TABLE 5-3 y/

SUMMARY

OF DATA FOR TRANSDUCER H-3 (Psig)

Displacement Date Time Pressure (inches)

-1/1 0000 0

0.000 1/1 0205 2.5 0.000 1/1 0343 5.0 0.000 1/1 0622 7.5 0.000 1/1 0930 10.0 0.000 1/1 1041 12.6 0.012 1/1 1246 15.0 0.020 1/1 1349 17.3 0.023 1/1 1630 17.3 0.024 1/1 2000 15.1 0.024 s

1/1 2249 12.5 0.024 1/2 0153 9.8 0.024 1/2 1458 5.1 0.021 1/2 1802 2.5 0.019 1/2 2114 0

0.017 I

TABLE 5-4

SUMMARY

OF DATA FOR TRANSDUCER H-4 (Psig)

Displacement Date Time Pressure (inches) 1 1/1 0000 0

0.000 1/1 0205 2.5 0.000 1/1 0343 5.0 0.001 1/1 0622 7.5 0.003 1/1 0930 10.0 0.006 i

1/1 1041 12.6 0.009 1/1 1246 15.0 0.030 1/1 1349 17.3 0.036

}

1/1 1630 17.3 0.039 1/1 2000 15.1 0.039 1/1 2249 12.5 0.038 1/2 0153 9.8 0.035 1

1/2 1458 5.1 0.029 l

1/2 1802 2.5 0.026 1/2 2114 0

0.023 i

i O

DH-105 5-17 1

1

O TABLE 5-5

SUMMARY

OF DATA FOR TRANSDUCER H-5 (Psig)

Displacement Date Time Pressure (inches) 1/1 0000 0

0.000 1/1 0205 2.5 0.002 1/1 0343 5.0 0.004 1/1 0622 7.5 0.006 1/1 0930 10.0-0.009 1/1 1041 12.6 0.011 1/1 1246 15.0 0.029 1/1 1349 17.3 0.034 1/1 1630 17.3 0.036 1/1 2000 15.1 0.035 1/1 2249 12.5 0.033 1/2 0153 9.8 0.030 1/2 1458 5.1 0.026 1/2 1802 2.5 0.024 1/2 2114 0

0.022

' TABLE 5-6

SUMMARY

OF DATA FOR TRANSDUCER H-6 (Psig)

Displacement-Date Time Pressure (inches) 1/1 0000 0

0.000 1/1 0205 2.5 0.001 1/1 0343 5.0 0.004 1/1 0622 7.5 0.007 1/1 0930 10.0 0.011 1/1 1041 12.6 0.015 1/1 1246 15.0 0.036 1/1 1349 17.3 0.041 1/1 1630 17.3 0.044 1/1 2000 15.1 0.044 1/1 2249 12.5 0.042 1/2 0153 9.8 0.038 1/2 1458 5.1 0.032 1/2 1802 2.5 0.029 1/2 2114 0

0.025 O

DH-105 5-18

1 O

TABLE 5-7

SUMMARY

OF DATA FOR TRANSDUCER H-7 i

(Psig)

Displacement Date Time Pressure (inches) 1/1 0000 0

0.000 1/1 0205 2.5 0.003 1/1 0343 5.0 0.007 1/1 0622 7.5 0.011 1/1 0930 10.0 0.019 1/1 1041 12.6 0.025 1/1 1246 15.0 0.057 1

1/1 1349 17.3 0.089 1/1 1630 17.3 0.101 1/1 2000 15.1 0.099 1/1 2249 12.5 0.093 1/2 0153 9.8 0.086 1/2 1458 5.1 0.068 1/2 1802 2.5 0.056 1/2 2114 0

0.043

?

Final Adjusted Recovery Value: 0.043 TABLE 5-8 i

SUMMARY

OF DATA FOR TRANSDUCER H-8 (Psig)

Displacement Date Time Pressure (inches) 1/1 0000 0

0.000 1/1 0205 2.5 0.004 1/1 0343 5.0 0.008 1/1 0622 7.5 0.019 1/1 0930 10.0 0.038 1/1 1041 12.6 0.052 1/1 1246 15.0 0.174 1/1 1349 17.3 0.267 1/1 1630 17.3 0.283 1/1 2000 15.1 0.267 1/1 2249 12.5 0.241 1/2 0153 9.8 1/2 1458 5.1 0.161 1/2 1802 2.5 0.136 1/2 2114 0

0.111 i.-

Final Adjusted Recovery Value: 0.054 I

• Invalid Reading - Out of Scale O

DH-105 5-19

= _.

1 l

O TABLE 5-9 j

SUMMARY

OF DATA FOR TRANSDUCER H-9 f

(Psig)

Displacement Date Time Pressure (inches) 1/1 0000 0

0.000 1/1 0205 2.5 0.002 1/1 0343 5.0 0.008 1/1 0622 7.5 0.016 1/1 0930 10.0 0.028 i

1/1 1041 12.6 0.056 l

1/1 1246 15.0 0.185 i

1/1 1349 17.3 0.246 1/1 1630 17.3 0.263 1/1 2000 15.1 0.257 1/1 2249 12.5 0.233 i

1/2 0153 9.8 0.204 1/2 1458 5.1 0.153 l'/

!"i

1' I

Final Adjusted Recovery Value: 0.037 O

TABLE 5-10

SUMMARY

OF DATA FOR TRANSDUCER H-10 (Psig)

Displacement

^

Date Time Pressure (inches) 1/1 0000 0

0.000 1/1 0205 2.5 0.005 1/1 0343 5.0 0.010 s

1/1 0622 7.5 0.018 1/1 0930 10.0 0.030 1/1 1041 12.6 0.049 1/1 1246 15.0 0.107 1/1 1349 17.3 0.145 1/1 1630 17.3 0.166 1/1 2000 15.1 0.163 1/1 2249 12.5 0.150 1/2 0153 9.8 0.134 1/2 1458 5.1 0.108 1/2 1802 2.5 0.094 1/2 2114 0

0.079 Final Adjusted Recovery Value: 0.077 1

DH-105 5-20

~ _ _, - _ _ _

j TABLE 3-11

SUMMARY

OF DATA FOR TRANSDUCER H-11 (Psig)

Displacement Date Time Pressure (inches) i 1/1 0000 0

0.000 1/1 0205 2.5 0.005 1/1 0343 5.0 0.010 1

1/1 0622 7.5 0.015 1/1 0930 10.0 0.025 1

1/1 1041 12.6 0.041 1/1 1246 15.0 0.109 1/1 1349 17.3 0.152 1/1 1630 17.3 0.168 1/1 2000 15.1 0.164 1/1 2249 12.5 0.156 1/2 0153 9.8 0.144 l

1/2 1458 5.1 0.122 1/2 1802 2.5 0.108 1/2 2114 0

0.093 i

i Final Adjusted Recovery value: 0.090 TABLE 5-12

SUMMARY

OF DATA FOR TRANSDUCER H-12 (Psig)

Displacement Date Time Pressure (inches) q f

1/1 0000 0

0.000

?

1/1 0205 2.5 0.004 1/1 0343 5.0 0.009 1/1 0622 7.5 0.015 1/1 0930 10.0 0.023 1/1 1041 12.6 0.029 1/1 1246 15.0 0.060 1/1 1349 17.3 0.078

't 1/1 1630 17.3 0.084 1/1 2000 15.1 0.084 4

1/1 2249 12.5 0.080 1/2 0153 9.8 0.074 1/2 1458 5.1 0.063 1/2 1802 2.5 0.057 1/2 2114 0

0.049 Final Adjusted Recovery Value: 0.050 d

. O DH-105 5-21

l.

l TABLE 5-13 4

SUMMARY

OF DATA FOR TRANSDUCER H-13 (Psig)

Displacement Date Time Pressure (inches) 1/1 0000 0

0.000 1/1 0205 2.5 0.000 1

1/1 0343 5.0 0.000 1/1 0622 7.5 0.011 j

1/1 0930 10.0 0.026 1/1 1041 12.6 0.043 i

1/1 1246 15.0 0.125 j

1/1 1349 17.3 0.185 1/1 1630 17.3 0.210 1/1 2000 15.1 0.210 1/1 2249 12.5 0.198 1

1/2 0153 9.S 0.173 1/2 1458 5.1 0.130 1/2 1802 2.5 0.110 1/2 2114 0

0.088 1

4 TABLE 5-14

SUMMARY

OF DATA FOR TRANSDUCER H-14 (Psig)

Displacement Date Time Pressure (inches) l l

1/1 0000 0

0.000 1/1 0205 2.5 0.006 1/1 0343 5.0 0.013 1/1 0622 7.5 0.023 1/1 0930 10.0 0.039 1/1 1041 12.6 0.057 1/1 1246 15.0 0.154 1/1 1349 17.3 4

1/1 1630 17.3 0.249 1/1 2000 15.1 0.244 1/1 2249 12.5 1/2 0153 9.8 0.197 1/2 1458 5.1 0.147 1

4 1/2 1802 2.5 0.124 4

1/2 2114 0

0.102

• Invalid Reading - Out of Scale O

}

DH-105 5-22

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

....~

I O

TABLE 5-15

SUMMARY

OF DATA FOR TRANSDUCER H-15 (Psig)

Displacement i

Date Time Pressure (inches) 1 1/1 0000 0

0.000 l

1/1 0205 2.5 0.005 r

1/1 0343 5.0 0.009 l

1/1 0622 7.5 0.017 1/1 0930 10.0 0.029 1/1 1041 12.6 0.040 1/1 1246 15.0 0.108 l

1/1 1349 17.3 0.165 1/1 1630 17.3 0.184 1/1 2000 15.1 0.184 1

1/1 2249 12.5 0.171 1/2 0153 9.8 0.150 j

1/2 1458 5.1 0.112 1

1/2 1802 2.5 0.097 I

1/2 2114 0

0.080 1

]

TABLE 5-16 1

SUMMARY

OF DATA FOR TRANSDUCER H-16 (Psig)

Displacement

{

Date Time Pressure (inches) 1/1 0000 0

0.000 1/1 0205 2.5 0.004 1/1 0343 5.0 0.009 1/1 0622 7.5 0.014 a

1/1 0930 10.0 0.019 4

1/1 1041 12.6 0.024 1/1 1246 15.0 0.044 i

1/1 1349 17.3 0.051 1/1 1630 17.3 0.056 1/1 2000 15.1 0.055 1/1 2249 12.5 0.051 1/2 0153 9.8 0.046 1/2 1458 5.1 0.037 1/2 1802 2.5 0.032 1/2 2114 0

0.026

.!O DH-105 5-23

)

i

_ _ _. _. _ _ ~ _ _

__. ___ _ _ = _ _ _ _ _ _ _._.- _

I i

}

I 1

O TABLE 5-17

SUMMARY

OF DATA FOR TRANSDUCER H-17 (Psig)

Displacement Date Time Pressure (inches) 1/1 0000 0

0.000 1/1 0205 2.5 0.005 1/1 0343 5.0 0.010 1

1/1 0622 7.5 0.015 j

1/1 0930 10.0 0.021 1/1 1041 12.6 0.027 3

1/1 1246 15.0 0.060 i

1/1 1349 17.3 0.075 l

1/1 1630 17.3 0.082

]

1/1 2000 15.1 0.081 1/1 2249 12.5 0.075 i

1/2 0153 9.8 0.067 1/2 1458 5.1 0.054 1/2 1802 2.5 0.047 1/2 2114 0

0.039 l

TABLE 5-18 l

SUMMARY

OF DATA FOR TRANSDUCER H-18 1

(Psig)

Displacement Date Time Pressure (inches) 1/1 0000 0

0.000 l

1/1 0205 2.5 0.003 1/1 0343 5.0 0.006 1/1 0622 7.5 0.009 1/1 0930 10.0 0.013 1/1 1041 12.6 0.016 1/1 1246 15.0 0.038 1/1 1349 17.3 0.058 t

1/1 1630 17.3 0.074 1/1 2000 15.1 0.072 1/1 2249 12.5 0.068 1

1/2 0153 9.8 0.064 1/2 1458 5.1 0.056 l

1/2 1802 2.5 0.051 1/2 2114 0

0.046 f

O 4

DH-105 5-24

~

=

i 1

TABLE 5-19 i

SUMMARY

OF DATA FOR TRANSDUCER H-19 i

l i

(Psig)

Displacement Date Time Pressure (inches) 1/1 0000 0

0.000 1/1 0205 2.5 0.004 1/1 0343 5.0 0.008 4

1/1 0622 7.5 0.013 l

1/1 0930 10.0 0.025 i

1/1 1041 12.6 0.041 1/1 1246 15.0 0.123 1/1 1349 17.3 0.182 1/1 1630 17.3 0.201 1/1 2000 15.1 0.193 1/1 2249 12.5 0.177 1/2 0153 9.8 0.157 1/2 1458 5.1 0.118 1/2 1802 2.5 0.096 1/2 2114 0

0.074 i

Final Adjusted Recovery Value: 0.068 TABLE 5-20

\\

SUMMARY

OF DATA FOR TRANSDUCER H-20 (Psig)

Displacement i

Date Time Pressure (inches) l 1/1 0000 0

0.000 1/1 0205 2.5 0.003 1/1 0343 5.0 0.008 1/1 0622 7.5 0.013 1/1 0930 10.0 0.021 1/1 1041 12.6 0.042 1/1 1246 15.0 0.176 1/1 1349 17.3 0.255 j

1/1 1630 17.3 0.271 1/1 2000 15.1 0.258

)

1/1 2249 12.5 0.231 1/2 0153 9.8 1/2 1458 5.1 0.144 1/2 1802 2.5 0.117 1/2 2114 0

0.091 Final Adjusted Recovery Value: 0.100

• Invalid Reading - Out of Scale

O DH-105 5-25 1

c.

..r.

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

\\

i O

TABLE 5-21

SUMMARY

OF DATA FOR TRANSDUCER H-21 t

(Psig)

Displacement Date Time Pressure (inches) j l

1/1 0000 0

0.000 1/1 0205 2.5 0.003 4

I 1/1 0343 5.0 0.008 1/1 0622 7.5 0.014 1/1 0930 10.0 0.026 i

1/1 1041 12.6 0.036 1

4 1/1 1246 15.0 0.131 1/1 1349 17.3 0.185 l

1/1 1630 17.3 0.206 1

1/1 2000 15.1 0.206 1/1 2249 12.5 0.197 1/2 0153 9.8 0.183 1/2 1458 5.1 0.150 1/2 1802 2.5 0.131 1/2 2114 0

0.109 Final Adjusted Recovery Value: 0.020 TABLE 5-22

SUMMARY

OF' DATA FOR TRANSDUCER D-1 (Psig)

Displacement Date Time Pressure (inches) 1/1 0000 0

0.000 1/1 0205 2.5 0.008 1/1 0343 5.0 0.020 1/1 0622 7.5 0.035 1/1 0930 10.0 0.054 l

.1/1 1041 12.6 0.069 i

1/1 1246 15.0 0.089 1/1 1349 17.3 0.106 t

1/1 1630 17.3 0.114 1/1 2000 15.1 0.114 1/1 2249 12.5 0.105 1/2 0153 9.8 0.090 1/2 1458 5.1 0.064

{

1/2 1802

2. 5,

0.051 1/2 2114 0

0.036 j

Final Adjusted Recovery Value: 0.017 lO 4

DH-105 5-26 f

,.r_,

_-__-,..rc.

,-.,m-

_.p--,--.x.-

g,_,

.v-y.-.---.

O' TABLE 5-23

SUMMARY

OF DATA FOR TRANSDUCER D-2 l

(Psig)

Displacement Date Time Pressure (inches) i 1/1 0000 0

0.000 i

1/1 0205 2.5 0.015 1

1/1 0343 5.0 0.026 1/1 0622 7.5 0.040 1/1 0930 10.0 0.056 4

1 1/1 1041 12.6 0.069 1/1 1246 15.0 0.091 1/1 1349 17.3 0.106 1/1 1630 17.3 0.112 1/1 2000 15.1 0.112 1/1 2249 12.5 0.106 1/2 0153 9.8 0.092 1/2 1458 5.1 0.067 1/2 1802 2.5 0.055 1/2 2114 0

0.043 Final Adjusted Recovery Value: 0.025 l

O' TABLE 5-24

SUMMARY

OF DATA FOR TRANSDUCER D-3 (Psig)

Displacement Date Time Pressure (inches) 1/1 0000 0

0.000 1/1 0205 2.5 0.000 1/1 0343 5.0 0.000 1/1 0622 7.5 0.012 1/1 0930 10.0 0.030 1/1 1041 12.6 0.039 1/1 1246 15.0 0.060 1/1 1349 17.3 0.073 1/1 1630 17.3 0.081 1/1 2000 15.1 0.080 1/1 2249 12.5 0.080 1/2 0153 9.8 0.073 1/2 1458 5.1 0.051 1/2 1802 2.5 0.051 1/2 2114 0

0.032 Final Adjusted Recovery Value: 0.014 O

V DH-105 5-27

- - _ _. _. _ ~

y,_,.--y

,,,w r

wwv

--v r----v

_-_._m m

{

O TABLE 5-25

SUMMARY

OF DATA FOR TRANSDUCER V-3 (Psig)

Displacement Date Time Pressure (inches)

+

t 1/1 0000 0

0.000 I

1/1 0205 2.5 0.000 1/1 0343 5.0 0.009 1/1 0622 7.5 0.009 j

1/1 0930 10.0 0.009 l

1/1 1041 12.6 0.015 l

1/1 1246 15.0 0.023 1/1 1349 17.3 0.029 1/1 1630 17.3 0.031 t

1/1 2000 15.1 0.031 i

1/1 2249 12.5 0.031 l

1/2 0153 9.8 0.031 1/2 1458 5.1 0.027 1/2 1802 2.5 0.022 1/2 2114 0

0.017

)

Final Adjusted Recovery Value: 0.007 4

O TABLE 5-26

SUMMARY

OF DATA FOR TRANSDUCER V-1 (Psig)

D'splacement Date Time Pressure (inches) 1/1 0000 0

0.000 1/1 0205 2.5 0.000 1/1 0343 5.0 0.001 1/1 0622 7.5 0.005 1/1 0930 10.0 0.011 1/1 1041 12.6 0.013 1/1 1246 15.0 0.019 1/1 1349 17.3 0.024 1/1 1630 17.3 0.027 1/1 2000 15.1 0.027 1/1 2249 12.5 0.027 1/2 0153 9.8 0.024 1/2 1458 5.1 0.014 1/2 1802 2.5 0.011 1/2 2114 0

0.007 Final Adjusted Recovery Value: 0.003 6

1 DH-105 5-28

,, - -.,, - - - y m-

.y-

--x-t - n v 3

,ww,n-r,

m.-.,

y r-,c,.

r

,,e---

-- --e

. _ - - - - = _ - -. -..

I l

TABLE 5-27 i

SUMMARY

OF DATA FOR TRANSDUCER V-4 i

j (Psig)

Displacement Date Time Pressure (inches) l 1/1 0000 0

0.000 1/1 0205 2.5 0.000 i

1/1 0343 5.0 0.004 1/1 0622 7.5 0.010 2

1/1 0930 10.0 0.016 1/1 1041 12.6 0.021 1/1 1246 15.0 0.027 1/1 1349 17.3 0.031 1/1 1630 17.3 0.034 1/1 2000 15.1 0.033 1/1 2249 12.5 0.033 1/2 0153 9.8 0.028 1/2 1458 5.1 0.018 1/2 1802 2.5 0.013 1/2 2114 0

0.008 Final Adjusted Recovery Value: 0.001 I

i TABLE 5-28

SUMMARY

OF DATA FOR TRANSDUCER E-1 (Psig)

Displacement Date Time Pressure (inches) 1/1 0000 0

0.000 1/1 0205 2.5 0.000 1/1 0343 5.0 0.009 1/1 0622 7.5 0.017 1/1 0930 10.0 0.031 1/1 1041 12.6 0.045 j

1/1 1246 15.0 0.145 1/1 1349 17.3 1/1 1630 17.3 0.233 1/1 2000 15.1 0.225 1/1 2249 12.5 I

1/2 0153 9.8 0.181 1/2 1458 5.1 0.137 1/2 1802 2.5 0.115 1/2 2114 0

0.093

• Invalid Reading - Out of Scale o

DR-105 5-29 4

w.3,-

,--.------,c,-. -.,

--r.r,.-.,

,-+--->.w...-

r

i i

TABLE 5-29

SUMMARY

OF DATA FOR TRANSDUCER E-2 (Psig)

Displacement Date Time Pressure (inches) i 1/1 0000 0

0.000 1/1 0205 2.5 0.005 1/1 0343 5.0 0.013 1/1 0622 7.5 0.022 1/1 0930 10.0 0.037 1/1 1041 12.6 0.052 1

1/1 1246 15.0 0.116 1/1 1349 17.3 0.213 1/1 1630 17.3 0.258 1/1 2000 15.1 0.228 i

1/1 2249 12.5 0.207 1/2 0153 9.8

'0.183 1/2 1458 5.1 0.138 1/2 1802 2.5 0.110 1/2 2114 0

0.091 TABLE 5-30

SUMMARY

OF DATA FOR TRANSDUCER E-3 (Psig)

Displacement Date Time Pressure (inches) 1/1 0000 0

0.000 1/1 0205 2.5 0.011 4

1 1/1 0343 5.0 0.022 1/1 0622 7.5 0.034 1/1 0930 10.0 0.051 1/1 1041 12.6 0.068 j

1/1 1246 15.0 0.156 1/1 1349 17.3 0.220 1/1 1630 17.3 0.224 1/1 2000 15.1 0.232 1/1 2249 12.5 0.209 1/2 0153 9.8 0.182 1/2 1458 5.1 0.134 1/2 1802 2.5 0.110 1/2 2114 0

0.085 i

O DH-105 5-30 i

e-,

,,n,

~.., - -, -

.-,.-n n.-

n

A TABLE 5-31 h

SUMMARY

OF DATA FOR TRANSDUCER E-4 (Psig)

Displacement Date Time Pressure (inches) i 1/1 0000 0

0.000 1/1 0205 2.5 0.009 1/1 0343 5.0 0.019

~

1/1 0622 7.5 0.031 1/1 0930 10.0 0.053 1/1 1041 12.6 0.072 1

1/1 1246 15.0 0.134 1/1 1349 17.3 1/1 1630 17.3 0.213 1/1 2000 15.1 0.207 1/1 2249 12.5' 1/2 0153 9.8 0.163 1/2 1458 5.1 0.118 1/2 1802 2.5 0.096 1/2 2114 0

0.073

• Invalid Reading - Out of Scale 4

TABLE 5-32

SUMMARY

OF DATA FOR TRANSDUCER E-5 (Psig)

Displacement Date Time Pressure (inches) 1/1 0000 0

0.000 1/1 0205 2.5 0.000 1/1 0343 5.0 0.014 1/1 0622 7.5 0.026 1/1 0930 10.0 0.040 1/1 1041 12.6 0.059 i

1/1 1246 15.0 0.116 1/1 1349 17.3 0.166 1/1 1630 17.3 0.187 1/1 2000 15.1 0.187 1/1 2249 12.5 0.183 l

1/2 0153 9.8 0.164 1/2 1458 5.1 0.128 1/2 1802 2.5 0.108 1/2 2114 0

0.088

O j

DH-105 5-31 i

O TABLE 5-33

SUMMARY

OF DATA FOR TRANSDUCER E-6 i

(Psig)

Displacernent Date Time Pressure (inches) 1/1 0000 0

0.000 1/1 0205 2.5 0.008 1/1 0343 5.0 0.014 1/1 0622 7.5 0.022 1

1/1 0930 10.0 0.036 1/1 1041 12.6 0.049 1/1 1246 15.0 0.104 1/1 1349 17.3 0.145 1/1 1630 17.3 0.167 1/1 2000 15.1 0.166 1/1 2249 12.5 0.153 1/2 0153 9.8 0.137 1/2 1458 5.1 0.106 1/2 1802 2.5 0.089 1/2 2114 0

0.072 TABLE 5-34

SUMMARY

OF DATA FOR TRANSDUCER E-7 (Psig)

Displacement Date Time Pressure (inches) j 1/1 0000 0

0.000 1/1 0205 2.5 0.007 1/1 0343 5.0 0.014 1/1 0622 7.5 0.023 1/1 0930 10.0 0.037 1/1 1041 12.6 0.055 1/1 1246 15.0 0.117 1/1 1349 17.3 0.172 i

1/1 1630 17.3 0.200 1/1 2000 15.1 0.196 1/1 2249 12.5 0.177 1/2 0153 9.8 0.155 1/2 1458 5.1 0.116 1/2 1802 2.5 0.096 1/2 2114 0

0.076 l

1 O

DH-105 5-32

i d

TABLE 5-35

SUMMARY

OF DATA FOR TRANSDUCER E-8 (Psig)

Displacement 4

Date Time Pressure (inches) 1/1 0000 0

0.000 1/1 0205 2.5 0.009 1/1 0343 5.0 0.017 6

1/1 0622 7.5 0.027 i

1/1 0930 10.0 0.044 1/1 1041 12.6 0.062 i

i 1/1 1246 15.0 0.125

}

1/1 1349 17.3 0.184 1/1 1630 17.3 0.210 1/1 2000 15.1 0.200 l

1/1 2249 12.5 0.180 1/2 0153 9.8 0.155 a

1/2 1458 5.1 0.112 j

1/2 1802 2.5 0.090 1/2 2114 0

0.068 TABLE 5-36 l

SUMMARY

OF DATA FOR TRANSDUCER E-9 1

(Psig)

Displacement Date Time Pressure (inches) i 1/1 0000 0

0.000 I

1/1 0205 2.5 0.010 i

1/1 0343 5.0 0.022 i

1/1 0622 7.5 0.035 1/1 0930 10.0 0.055 1/1 1041 12.6 0.075 1/1 1246 15.0 0.144

}

1/1 1349 17.3 0.209 1/1 1630

~17.3 0.235 1/1 2000 15.1 0.224 l

1/1 2249 12.5 0.200 1/2 0153 9.8 0.172 l

1/2 1458 5.1 0.121 l

1/2 1802 2.5 0.094 j

1/2 2114 0

0.068 O

DH-105 5-33 1

1

,,--,r----s,--w

-w--

-,w w-m, -

---w--r-

,----,-w

--- - + - - - - - - ~ - - - - -,

re

. n n---

m-s-m

?

(

TABLE 5-37

SUMMARY

OF DATA FOR TRANSDUCER E-10 (Psig)

Displacement j

Date Time Pressure (inches) i 1/1 0000 0

0.000 1/1 0205 2.5 0.011 1/1 0343 3.0 0.021 l

1/1 0622 7.5 0.033 1

1/1 0930 10.0 0.050 1/1 1041 12.6 0.070 1/1 1246 15.0 0.129 1/1 1349 17.3 0.186 1/1 1630 17.3 0.205 1/1 2000 15.1 0.192 1/1 2249 12.5 0.174 1/2 0153 9.8 0.152 1/2 1458 5.1 0.112 1/2 1802 2.5 0.090 1/2 2114 0

0.068 TABLE 5-38

SUMMARY

OF DATA FOR TRANSDUCER E-11 (Psig)

Displacement Date Time Pressure (inches) 1/1 0000 0

0.000 1/1 0205 2.5 0.007 1/1 0343 5.0 0.015 1/1 0622 7.5 0.023 1/1 0930 10.0 0.033 l

1/1 1041 12.6 0.055 4

1/1 1246 15.0 0.117 l

1/1 1349 17.3 0.155 1/1 1630 17.3 0.173

'l 1/1 2000 15.1 0.171 1/1 2249 12.5 0.159 1/2 0153 9.8 0.144 1/2 1458 5.1 0.116 1/2 1802 2.5 0.100 1/2 2114 0

0.082 O

DH-105 5-34

TABLE 5-39 SUWiARY OF DATA FOR TRANSDUCER E-12 (Psig)

Displacement Date Time Pressure (inches) 1/1 0000 0

0.000 1/1 0205 2.5 0.006 1,* 1 0343 5.0 0.012 1/1 0622 7.5 0.020 1/1 0930 10.0 0.030 1/1 1041 12.6 0.046 1/1 1246 15.0 0.117 1/1 1349 17.3 0.152 1/1 1630 17.3 0.170 1/1 2000 15.1 0.168 1/1 2249 12.5 0.158 1/2 0153 9.8 0.145 1/2 1458 5.1 0.120 1/2 1802 2.5 0.104 1/2 2114 0

0.087 O

DH-105 5-35

__-.~

_..m_.._.._._

t i

I i

4 6.

REFERENCES 1.

Final Safety Analysis Report, Grand Gulf Nuclear Station, j

Unit No. 1, Mississippi Power and Light Company.

4 2.

Procedure Q1M61-W-11302WXA, Containment Structural Integrity i

Test, Grand Gulf Nuclear Station Unit 1, Mississippi Power j

and Light Company.

l i

l i

l 4

l i

4 l

1 4

i 1

t

.1 0

i i

i 1

i l

l I

t l

l l

l t

6 DH-105 6-1 i

[

O MISSISSIPPI POWER & LIGHT COMPANY GRAND GULF NUCLEAR STATION UNIT 1 O

PRIMARY REACTOR CONTAINMENT STRUCTURAL INTEGRITY TEST FIN AL REPORT JANUARY 1982 O

y mb :

... ~ -. -

i 1

i i

l I

i 9

\\

l r

I l

i l

MISSISSIPPI POWER AND LIGHT COMPANY f

GRAND GULF NUCLEAR STATION l

UNIT 1 l

i I

4 i

l l

l PRIMARY CONTAINMENT STRUCTURAL INTEGRITY TEST REPORT k

lO i

i I

Bechtel Power Corporation San Francisco, California January 1982 0

1

N i

4 I

i CONTENTS r

i i

M

~

1.

INTRODUCTION 1-1 I

i e

i 2.

SUMMARY

AND CONCLUSIONS 2-1 i

i 3.

STRUCTURE AND PRESSURIZATION 3-1 i

t i

I 4.

TEST PLAN AND PROCEDURES 4-1 f

1 i

l 5.

TEST RESULTS 5-1 5.1 Containment Structure Deflections 5-1 5.2 Containment Concrete Cracking 5-3 5.3 Estimated Accuracy of Measurement 5-3 1

1 6.

REFERENCES 6-1 l0 4

l l

i i

i E

F O

DH-105 11

.=

=_

i FIGURES Figure No.

3-1 Containment Structure 3-2 SIT Pressure Cycle 4-1 Taut Wire Extensometer Locations - Radials at Elevations 167' and 202', Domes and Verticals 4-2 Taut Wire Extensometer Locations - Radials at Elevations 103'-6",

131', and 230' 4-3 Taut Wire Extensometer Locations - Equipment lch 4-4 Schematic Representation of Taut Wire Extensometer 4-5 Concrete Crack Mapping Areas 5-1 Containment Structure Average Deflections at 17.25 psig - Wall and Dome 5-2 Containment Structure Deflections at 17.25 psig - Equipment Hatch Radial

' O 5-3 Typical Deflection / Pressure History - Containment Wall - H8 5-4 Typical Deflection / Pressure History - Containment Wall - H21 5-5 Typical Deflection / Pressure History - Containment Dome - D1 5-6 Typical Deflection / Pressure History - Equipment Hatch - E10 5-7 Concrete Crack Mapping - Area 1 5-8 Concrete Crack Mapping - Area 2 5-9 Concrete Crack Mapping - Area 3 5-10 Concrete Crack Mapping - Area 4 5-11 Concrete Crack Mapping - Area 5 5-12 Concrete Crack Mapping - Area 6 O

v DH-105 111

i

)

1 1.

INTRODUCTION I

The Unit 1 Containment Structural Integrity Test was conducted during l

the time period December 31, 1981 to January 2, 1982.

The primary purpose of the structural integrity test was to verify the design and I

structural integrity of the containment structure by imposing one hundred and fif teen percent of the design pressure for a period of not less than one hour.

i l

In order to accomplish the intended test purpose, specialized measuring devices were installed in the containment structure to provide the data needed to evaluate structural response during pressurization and i

depressurization. The tests were conducted in accordance with written procedure Q1M61-W-11302WXA (Reference 2), detailing test requirements i

and instructions for acquiring test data. This procedure is a part of the permanent plant records at the Grand Gulf Nuclear Station.

I r

+

O 1

i l

i l

i l

l i

Dil-105 1-1 i

[d 2.

SUMMARY

AND CONCLUSIONS The containment structural integrity test provided proof of the strue-ture's ability to contain the internal design pressure and provided measurement of structural response to changes in internal pressure.

Test measurements for the containment included gross structural defor-mations and concrete crack growth. Measurement points were located at typical sections of the structure with measurements obtained at speci-fled stages during the pressurization cycle. The structure withstood the internal pressure with no observable indications of structural d is tr es s.

All measured structural deformations were less than the design allowable values.

All dome and vertical measurement points recovered more than 70 percent of their maximum deflection. Radial deflections at the elevation of maximum average deflection recovered more than 70 percent of their maximuu deflection, also.

Changes in concrete cracks observed in the various surveillance areas did not change in measured width by more than 0.010 inches. This is considered to be within reasonable expectations based on the results of previous tests and does not adversely affect the integrity of the structure.

Prior to the start of pressurization, no cracks with widths equal to or exceeding 0.010 inches were observed in the inspec-tion areas.

Cracks developed in two of the six mapping areas during pressurization and closed to below measurable values at zero pressure.

The results of the structural integrity test provide direct experi-I T mental evidence that the containment structure can contain the internal

\\- /

design pressure with a sufficient margin of safety and that the gross response to pressure is predictable.

~

(m /

DH-105 2-1

3.

STRUCTURE AND PRESSURIZATION i

The containment is a reinforced concrete structure designed to act as a pressure barrier during postulated loss-of-coolant accidents as de-fined in the Final Safety Analysis Report (Reference 1).

The structure consists of a reinforced concrete cylinder and hemisph'erical dome connected to and supported by a massive reinforced concrete base slab as shown in Figure 3-1.

Reinforced openings in the cylinder are pro-vided for equipment and personnel access as well as for electrical and mechanical feed through.

Principal dimensions for the containment structure are:

o Inside diameter 124 ft.

o Inside height 206 ft. 8-1/2 in.

i o Vertical wall thickness 3 ft. 6 in.

o Dome thickness 2 ft. 6 in.

o Foundation slab thickness 9 ft. 6 in.

.The containment structure was pressurized pneumatically to verify the required structural integrity. The internal peak pressure of 17.25 psig was held for a period of two hours to record structural data.

For details of the pressure cycle see Figure 3-2.

The suppression pool and upper containment pool were both filled with water to their normal level for plant operation to provide the proper load on the containment and basemat.

O DH-105 3-1

3 0

)/

\\

"0

/

1 3

1 0

1 0

0 7

1, l

0 L

2 9

E ug A

T N

A 2

L P

E R

U

! - e T

C U

R TS T

N E"

0" E

N9 0

M I

1 L*-

- 8 0

6 0

G7 1

N 3'

N 3

8 I2 0

4 1

I 8

3 9

A R.

2 1

1 L

L P

L L

L E

T E

S E

E E

L N

E O

0 C

k n

?

0 7

1 2

3 E

=

=

R 7,'

U G

I F

7.

[

~

l I

I l

g 7I

=

s

=

!(

f7 I

=

/.

=

cc

=

00

]

t l

9 vA

O O

O 1349 1630 y

17.25 PSIG 1246 1900 1146 2000 I

15 PSIG

/

HOLDS

~

1041 2249 12 -

l 0930 0153 s\\

/

10 PSIG HOLDS g

E Y

a v

m 0853 cc 8-0444 1137 0343

/

)

S PSIG HOLDS f

4-1802 205 l

2114 i

i i

i i

i i

0 6

12 18 24 6

12 18 24 1 JAN 82 2 JAN 82 FIGURE 3-2 SIT PRESSURE CYCLE

l O

4.

TEST PLAN AND PROCEDURES U

Test measurements were made at points on the containment structure which represented typical areas to provide data on structural be-havior during the pressure test. The measured parameters consisted of gross structural deformation and concrete crack growth.

Gross structural deformations were measured using taut wire extenso-meters which spanned between points on the containment wall, dome, and springline and fixed points within and outside the structure.

The extensometers were located to measure radial displacements along typical wall sections and around the lower equipment hatch, vertical displacement of the dome relative to the operating floor, and vertical displacement of the springline relative to the foundation slab. The layout of the extensometer system is shown in Figures 4-1 through 4-3 and exact locations are listed in Table 4-1.

The extensometers, illustrated in Figure 4-4, consist of displacement transducer assemblies and low expansion alloy (invar) taut wires. A movement between opposing points on the containment shell or between a point on the containment shell and a fixed reference structure re-sults in an almost equal movement between the core and body of the linear variable differential transformer (LVDT) which is housed in the transducer assembly. The LVDT output is a voltage which is proportion-al to the position of the core within the body. The spring in the transducer assembly maintains a nominal 20 lb tension on the wire to f) reduce sag and eliminate slack at threaded and swivel connections.

G The extensometers are calibrated to establish the displacement - volt-age characteristics and spring constant (nominally 2 lb/in). Spring constant is used to correct for the small changes in wire length which result from transducer displacement. The transducers were calibrated prior to shipment to the Grand Gulf Nuclear Station and again at the station. The two sets of calibration data agreed to within the re-quired limits of accuracy.

The transducer's swivels and opposing taut wire ends were secured to fittings which were welded to the containment liner and other metal structures and epoxy bonded or expansion anchored to concrete. Follow-ing initial attachment, the transducers were aligned with the wires to eliminate LVDT core side loading and the core positions adjusted to provide the desired travel.

i The LVDT's were wired to excitation power supplies and a scanning data acquisition system which converted LVDT output voltage to a digital fo rmat for register display, printed record, and direct entry into a microcomputer. The computer was programmed with extensometer calibra-tion ccnstants and a routine which converted raw voltage data into displacement units.

OG DH-105 4-1

I

()g During the structural integrity test the deformation data were recorded at 2.5 psig pressure increments and decrements, at the beginning and g

s, end of all constant pressure holds, and at regular intervals during ex-tended holds. Additional data were recorded following depressurization to monitor. post-test structural recovery and during,the subsequent in-tegrated leakage rate test.

At each data acquisition point all voltages were recorded three times in rapid succession to provide a 2 out of 3 basis for identifying spurious values caused by electrical transients.

The recording of 3 corplete records required about 2 minutes.

Concrete crack patterns were mapped in the areas shown in Figure 4-5.

The lengths and widths (measured by optical comparator) of all visible cracks within these areas were recorded prior to the start of pressuri-zation, at 10 psig during pressurization, at peak test pressure, and following the completion of depressurization.

a i

I O

DH-105 4-2 4

2700 i

V4 @ 3150 V3 @ 225" r

3 H2 l

l

____A. _. _ _

195 s

/

\\

0

[fx l

6

)

0 180 --

_-00 b

4>

\\

/

N D2

--a p I

g 0

H2O @ 150 H1 w-y i

3' 7j H190 300 0

)

D3J W

V2 @ 135

(

H10 H12 3300

+-

4g.3 900 750 (NOM) 4 Do ELEVATION 202'-0" e

LIVE END H9 H7 30o O

w

\\

ELEVATION 167'-0" g

HB n

9 0 TAUT WIRE EXTENSOMETER LOCATIONS-RADIALS AT ELEVATIONS 167' AND 202', DOMES, AND VERTICALS

270' o

H12

('

'**L':,,.,,

2700 p.

f o

4 $

4 180*

0 0

210*

3300 4

./

f

• ?

H17 H16 30*

150*

4 180

/

0 h

H15 H13 90o 150 6

H14 300 7

ELEVATION 131'-0" n

90 H2

.'l.

l'

~}l,.)

HS 5

E E

5 Ai 0*-0" EL93-0%"7 BASEMAT

=

ELEVATION 103'-6" (OUTSIDE CONTAINMENT) 0 0

0 0

0 6 EXTENSOMETERS AT 30,90,150,210,270, 330 FIGURE 4-2 TAUT WIRE EXTENSOMETER LOCATIONS - RADIALS AT ELEVATIONS 103'-6",131', AND 230' i

O O

O DRYWELL WALL CONTAINMEtJT

[

WALL E1 O

O M

?

E2

- 3 g

__23'-6 5/8" 25'- 2 5/8" M

t to 16*-10 7/8" 20*-3 5/8 _

O E3 n

T

.I 10'-6" _ ; 12'-8" _

co 20 i

N E L.172'-3" E

/'

~

e fa 7-CTMT WALL y

' ?,

i.

g e

w

-S -

E4 3

=

E7 E8 E9 E10 E11 E12 e'n

.I

.a.

N E5 O

e

1. .4. '

'*I e-DRYWELL WAL'

/

i E6 O

e A

• * ~

g

_g-SECTION FIGURE 4-3 TAUT WIRE EXTENSOMETER LOCATIONS - EQUIPMENT HATCH I

ps p}

d G

n-ORE 1 IN. RANGE LVDT B

ING

. BODY LOCKABLE

=

/

i SWlVEL Q

LINER LINER EYE

}

j p

\\

/

1 f.

t ln h"J A

. aaar a.

r 3

s m.a n..

h WELD

(

INVAR WIRE 0.05 IN. DIA WELD I

g ELECTRICAL CONNECTION SPRING B

BACKPLATE FRAME FIGURE 4-4 SCHEMATIC REPRESENTATION OF TAUT WIRE EXTENSOMETER

O O

O CRACK MAPPING AREA 6 3

LOCATED AT APEX OF DOME (EL. 302'-3") 7' x 7' i

E L.237*-9" (SPRINGLINE)

AZ 2600 CR ACK M APPING AREA #3 (7* x 7')

UPPER 4

-PERSONNEL LOCK CR ACK M APPI VG r AREA #4 (4' x 10')

AZ 800 EQUIPMENT CRACK MAPPING HATCH AREA #2 b_;

Q AT EL.169*-6-

( 7 x 7')

( OF AREAS 4 & 5 AT EL 172*-3

CCRACK MAPPING AREA #5 (4' x 10')

I LOWER

- PERSONNEL LOCK AZ 260 CRACK MAPPING AREA #1 E L.93'-1/4" (BASEMAT) 1800 900 3600 2700 1800 0

0 FIGURE 4-5 CONCRETE CRACK MAPPING AREAS

("

TABLE 4-1

(

EXTENSOMETER LOCATIONS Elevation Radials (H) and Hatch (E) or Radius Table Extensometer Verticals (V) and Dome (D)

Azimuth A-2 H-1 EL. 103'-0" 30*

A-3 H-2 EL. 103'-0" 90*

A-4 H-3 EL. 103'-0" 150' A-5 H-4 EL. 103'-0" 210*

A-6 H-5 EL. 103'-0" 270*

A-7 H-6 EL. 103'-0" 330*

A-8 H-7 EL. 167'-0" 30*

A-9 H-8 EL. 167'-0" 90*

A-10 H-9 EL. 167'-0" 150*

A-ll H-10 EL. 167'-0" 211*-08' A-12 H-ll EL. 167'-0" 270*

A-13 H-12 EL. 167'-0" 330' A-14 H-13 EL. 230'-0" 210' A-15 H-14 EL. 230'-0" 270*

A-16 H-15 EL. 230'-0" 150*

A-17 H-16 EL. 131'-0" 30*

A-18 H-17 EL. 131'-0" 150*

A-19 H-18 EL. 131'-0" 270*

O' A-20 H-19 EL. 202'-0" 30' A-21 H-20 EL. 202'-0" 150*

A-22 H-21 EL. 202'-0" 270*

A-23 D-1 R

3'-1" 165'-30' A-24 D-2 R

31'-0" 75*

A-25 D-3 R

45'-0" 75*

A-26 V-1 R

61'-8" 46*

A-27 V-3 R

61'-8" 225*

A-28 V-4 R

61'-8" 315*

A-29 E-1 EL. 198'-6" 240' A-30 E-2 EL. 191'-2-1/2" 240*

A-31 E-3 EL. 182'-9" 240*

A-32 E-4 EL. 161'-9" 240*

A-33 E-5 EL. 153'-10-1/2" 240*

A-34 E-6 EL. 146'-6" 240*

A-35 E-7 EL. 172'-6" 217*-47' A-36 E-8 EL. 172'-3" 223*-14' a

A-37 E-9 EL. 172'-6" 230*-14' A-38 E-10 EL. 168'-2" 247*-07' A-39 E-ll EL. 172'-7-1/4" 259' A-40 E-12 EL. 172'-0" 264*

O DH-105 4-8 i

m-

i 5.

TEST RESULTS

%d The results of the structural integrity test provide direct experi-mental evidence that the containment structure can contain the design internal pressure with an ample margin of safety. Further, the test data confirm the validity of the analytical methods employed to deter-mine the structural effects of loading combinations and to predict the resulting deflections.

5.1 CONTAINMENT STRUCTURE DEFLECTIONS The response of the containment to the maximum test pressure of 17.3 psig is illustrated in Figures 5-1 and 5-2.

Figure 5-1 shows the measured radial and vertical growth of the cylinder wall and the measured vertical growth of the dome as well as the predicted growth based on both elastic and cracked section analyses. The measured vertical growth of the dome and wall is less than the elastic case prediction. This demonstrates that the stress in the dome and the vertical stress in the wall were not sufficient to cause extensive tensile cracking. It further demonstrates that the actual elastic modulus of the concrete is higher than that used in the computations.

The radial growth of the wall is between the elastic and cracked wall section case predictions. This demonstrates that hoop stress caused tensile cracking but did not develop the complete cracked section used as a model in the cracked section analysis.

4

\\m/

The wall radial deflections listed and plotted in Figure 5-1 are averages of the measurements made on several azimuths at each eleva-t io n.

The individual measurements made at each elevation show a variation from azimuth to azimuth which is attributed to round out of minor irregularities in the cylinder wall. This behavior is typical for concrete containments and is expected for any singly curved struc-tural element which does not have a perfectly true radius. In contrast the measured dome deflections show a smooth trend which is typical for a doubly curved surface. The measured wall vertical deflection listed in the figure is the average of the measurements at extensometers VI, V3, and V4 (V2 malfunctioned). Here the individual measurements are tightly grouped as is expected for the uncurved direction on the wall.

Figure 5-2 shows the measured radial growth of the wall in the vicinity of the equipment opening. The deflections measured along the horizon-tal center plane of the hatch are approximately symmetrical about the vertical center line. Measurements along the vertical center plane of the hatch show that the outward movement in the vicinity of the hatch increased with elevation. This behavior is typical for a large opening located close to the containment base mat.

Deflection / pressure histories at various points on the containment are illustrated in Figures 5-3 through 5-6 and all measured deflections are listed in Tables 5-1 through 5-39.

The plotted deflection / pres-sure histories all show essentially linear response during the initial s-l DH-105 5-1

[' '/

g stages of pressurization and throughout depressurization. Deviations

(_,

from linearity are the deflection lags at the start of pressurization /

depressurization, creep response at constant pressure hold periods, and the increase in slope at higher pressures during pressurization.

The lag results from friction between moving parts of the extensometer and is normally not evident at the start of the test since the extenso-meter is initially set for motion in the proper direction. Where lag does occur at the start of the test, it is generally due to the extensometer being disturbed af ter being set.

Lag at the start of depressurization is always evident, except for extensometers with very short wires. This lag results from a reversal of friction forces in the extensometer and a consequent shortening of the wire. Lag a

ef fects are corrected for where required by extrapolating the linear part of the plot through 0 psig (initial lag) or 17.3 psig (depressuri-zation lag) and calculating the deflection on the extrapolated line at this pressure. The difference between the deflection on the extra-polated line and the measured deflection at the same pressure is added to (initial lag) or subtracted from (depressurization lag) subsequent measurements to provide corrected values. The correction procedure is illustrated in Figures 5-3 and 5-5.

Creep response of the concrete is generally evident at the constant pressure hold periods, particularly at higher pressures. This is ex-pected and typical for reinforced concrete structures.

fN All extensometers show on essentially linear deflection / pressure N--

characteristic at low pressures which demonstrates initial elastic behavior of the containment. The characteristics for the dome and wall vertical extensometers remain linear through peak test pressure thus verifying the previously stated conclusion that the stresses in the dome and in the vertical direction in the wall are not suf ficient to cause extensive tensile cracking and consequent departure from elastic response. The wall radial and equipment opening extensometers show significant changes in the deflection / pressure slope at varying levels of higher pressure. The point where the slope breaks represents initial tensile cracking.

If the initial slopes of the wall radial extensometers are extrapolated to 17.3 psig and corrected for initial lag as required (see Figure 5-3), the displacements on the extrapolated lines at peak test pressure are quite close to the displacement pre-dicted using the elastic case. This further verifies the validity of the constants and techniques used in containment analysis.

The recovery of containment deflections following the completion of depressurization was at least the required 70 percent at the points of maximum deflection. All dome and the three functioning vertical extensometers recovered over 70 percent of their maximum displacements.

Radial extensometers at elevation 167'-0", the maximum expected deflec-tion location, recovered 74 percent (af ter correcting for lag) of the average deflection of 0.178 inches. The two extensometers which measured the largest deflections at that elevation recovered over 80 percent of the deflected value. The largest average measured deflection occurred at elevation 202'-0", where three extensometers were located.

,(

5-2 DH-105

()/

The average maximum deflection at that elevation was 0.226 inches.

\\_,

The extensometers recovered 72.1 percent of the maximum value. The radial extensometer recovery data are based on readings taken after the ILRT, with readings ending at noon, January 5, 1982.

Final de-flection values for all extensometers are listed in Tables 5-1 through 5-39.

Final values are adjusted for extensometer lag where noted on the tables.

5.2 CONTAINMENT CONCRETE CRACKING The patterns of surface concrete cracks on the containment wall at specified internal pressures are shown in Figures 5-7 through 5-12.

A variety of surface cracks were mapped immediately prior to pressuri-zation, and a minimum number showed increases in length or width during the pressurization cycle. This is consistent with the low deflections recorded. The observed crack patterns are typical of those found on I

reinforced concrete containment structures.

During the subsequent ILRT pressure cycle to 12.5 psig, cracks which appeared in Crack Mapping Area 2 were monitored. Those cracks enlarged slightly from the zero pressure recovery value, and returned to hair-line width which was not accurately measurable with the optical comparators. Growth during the ILRT pressure cycle was estimated at 0.002 inches at the locations observed.

5.3 ESTIMATED ACCURACY OF MEASUREMENT The accuracy of measurement is based on the following items:

i o Calibration of instrumentation o Laboratory testing as in the case of invar wire o Human factor, i.e., judgement of the reader Displacements in the containment structure were measured using taut wire extensometers. Accuracy of the extensometer is + 0.002 inches so long as wire tension remains constant. When the direction of pressurization changes, extensometer response lags due to friction in the mechanism. Typical lag is 0.02 inches for a 100-foot long wire.

l The crack patterns were measured using optical comparators calibrated to measure crack width of 0.001 inches and wider. However, since most cracks observed on the containment were irregular traces on coarse textured concrete surfaces, it was not generally possible to estimate true crack width to better than approximately 0.003 inches. For this re as on, reported crack widths are considered to be accurate to within

+ 0.003 inches.

O DH-105 5-3

DEFLECTIONS (INCHES)

WALL EL MIN MAX AVG PRED1 PRED 2 103*- 6"

.024 044

.034

.08

.01 131*- 0"

.056

.082

.071

.38

.05

\\

167'- 0"

.084

.283

.178 42

.05

\\

kg....,,,,

g 202*- 0"

.201

.271

.226 42

.05

' * ***6

\\

230'- 0"

.184

.249

.214

.39

.04 s

DOME U.

RADIUS DEFL PRED 1 PRED2 3'- 1"

.114

.54

.15 31'

.112

.51

.15 45'

.107

.46

.14 SP G

.027

.034

.031

.20

.08 I

i G

I i

l i

I Z

i i

REFERENCE l

l LINE j

G l

g l

l 0

.20

.40

.60 I

g SCALE - lNCH ES l

l9 l

CRACKED ANALYSIS DISPLACEMENT I

f ELASTIC ANALYSIS l

l DISPLACEMENT I

i

/

8 MEASURED VALUE

/

NOTES:

l

/

!j

1. PREDICTED DISPLACEMENT FRCM CRACKED ANALYSIS

2. PREDICTED DISPLACEMENT FROM ELASTIC ANALYSIS 6/

/

Z l!O FIGURE 5-1 CONTAINMENT STRUCTURE AVERAGE DEFLECTIONS f

V AT 17.25 PSIG -WALL AND DOME 5-4

O O

O CONTAINMENT WALL

• /

2400 El

-T

.i 25'- 2 5/8" 23'-6 5/8" i

I j

k l

16*-10 7/8" 20'-3 5/8" E2 3

r

.258 -

G

-4 10'-6" 12'-8" 4

s 8

'h I

'~

CONTAINMENT

's E3 O'

g

_,i

& 's WALL

.244 g.c O',

.~.

r-

,1

.'g-l 4... *". l.

j A.. l. q..g., ;,' g

.g g

e!!

-I,-

.l..

n b

.y.

y E L.172'-3" E7 E8 E9 E10 E11 E12 l

b I

h

.210 235

.205

.173 w

E4 1

.200

.170 I

.213 9

. r.

5 1

I N

I a

I E5 i

.187 c

y

• 't 0

.20 40

,so SCALE - INCHES I

6

.167,

h*

t FIGURE 5-2 CONTAINMENT STRUCTURE DEFLECTIONS AT 17.25 PSIG'-EQUIPMENT HATCH RADIAL

O O

O

=6~

.283 2

3 N#:

~"

~24, 8

\\ /

vj g

.24 g

/

.2.,

.is2

<C

.136 174

\\

C i

.142 A

.m

.08

.108

.038

.004 053 _ _ _,

.048

\\

T

.oog

.019

.035 0

2.5 5.

7.5 10.

12.5 15.

17.5 PRESSUR E (PSIG)

FIGURE 5-3 TYPICAL DEFLECTION / PRESSURE HISTORY-CONTAINMENT WALL-H8 l

O O

O l

.206

.206

.197 "200

.183

.160 I

.131 2

' s b

.120

.131 i

U

^

b N

\\

.iO2

.us O

Y 5

.080 I

i

.040

.036

.008

.026

~

\\

\\

.020 s

.014 0

2.5 5.

7.5 10.

12.5 15.

17.5 PRESSURE (PSIG)

FIGURE 5-4 TYPICAL DEFLECTION / PRESSURE HISTORY-CONTAINMENT WALL-H21

i O

O O

5 2

EXTRAPOg ATED DEFLECTIOl}l =.1331N.

}

CORRECTION =.133.114 =.019 IN.

h EXTRAPOLATION OF L NEAR PART

.i p

C'F DEPRESSURIZATION PLOT p#

y

.120

.105

-f b

i O

.090

.114

\\

J

.106 -

(

.089

.064

\\

.087

.069

• 040 f CORRECTED RE SIDUAL

.050 i

\\

.008 0

2.5 5.

7.5 10.

12.5 15.

17.5 PRESSURE (PSIG)

FIGURE 5-5 TYPICAL DEFLECTION / PRESSURE HISTORY-CONTAINMENT DOME-D1

O O

O 4

.205

.192

.200 x

.174

.152 I

160

\\

.186 -

l z

.113 b.129 x

.120 g

1 117 uJ O

.090 a

N

'080 f

j

\\

.068

.040

~

x

/

x

.021

\\

.011 0

2.5 5.

7.5 10.

12.5 15.

17.5 PRESSURE (PSIG)

FIGURE 5-6 TYPICAL DEFLECTION / PRESSURE HISTORY-EQUIPMENT HATCH-E10

O Y

E L. 96'- 6" o

1' SQUARE o

0 260 TEMP OF DATE TIME STAGE PSIG REMARKS IN OUT 12/31 1203 69.80 64 1

0 1/1 0800 76.7 66 2

10 NO CRACKS > 3 THOUS.

1/1 1407 78.2 65 3

17.30 NO CRACKS > 5 THOUS.

1/2 2124 67.4 64 4

0 NO CRACKS > 5 THOUS.

t i

FIGURE 5-7 CONCRETE CRACK MAPPING

\\

AREA 1 5-10

.01

.0 2"

[

.01 is a

N V

l

.010" L

&m N

A 8"

.012" Y

- EL.16 9'- 6" r

l'SOUARE I

800

.0 2"

.0 O

@W L

LOCATION OF CRACK WIDTH MEASUREMENT N = STAGE NUMBER L = CRACK LENGHT IN INCHES W = CRACK WIDTH IN INCHES TEMP 0F DATE TIME STAGE PSIG REMARKS IN OUT 12/31 1210 75.37 72

'1 0

ONLY TWO CRACKS OVER.01" WERE 1/1/82 830 76.7 61 2

10 OBSERVED. NO OTHER CRACKS OB-SERVED GREATER TH AN.008'.'

NO OTHER CRACKS GREATER 1/1/82 14:19 78.2 61 3

17.25 TH AN.00B" OBSERVED.

1/2/82 21:30 69 69 4

0 NO OTHER CRACKS OBSERVED.

O FIGURE 5-8 CONCRETE CRACK MAPPING AREA 2 5-11

O Y

E L. 2 37'- 9" m

1' SQUARE o

O 260 k./

TEMP OF DATE TIME STAGE PSIG REMARKS IN OUT 12/31 1230 76.98 68 1

0 1/1/82 8:06 AM 76.7 61 2

10 NOTHING OBSERVED OVER 0.005" NOTHING OBSERVED OVER 0.005",

1/1/82 2:20 PM 78.2 62 3

17.25 THESE CR ACKS EXTENDED IN LENGTH ONLY NO NEW CRACKS.

NOTHING OBSERVED OVER.003 1/2/82 9:28 PM 74.3 68 4

0 CRACKS DECREASED IN WIDTH FIGURE 5-9 CONCRETE CRACK MAPPING O

AREA 3 5-12 l

O

\\

E L.172'-3" i

l' SQUARE I

TEMP *F DATE TIME STAGE PSIG REMARKS 12/31 12:17 75.38 66 1

0

^

^"

^

1/1/82 07:46 76,7 55 2

10 RVED 1/1/82 14:00 78.2 58 3

17.3 O ERVED 1/2/81 21:40 72 69 4

0 NO OTHER CRACKS OBSERVED FIGURE 5-10 CONCRETE CRACK MAPPING AREA 4

\\

5-13

O 20 30 40 10 9

8 7

6

- E L.17 2*- 3" 21" f

0.010" 4

LOCATION OF CRACK WIDTH MEASUREMENT O

\\ ei 1* SQUARE t

N = STAGE NUMBER 1

L = CRACK LENGTH 1/ \\

IN INCHES 11 21 31 \\

A 15" W = CRACK WIDTH 2

U 0 017' IN INCHES 15.5" 3

0.011" TEMP F DATE TIME STAGE PSIG REMARKS 12/31 12:20 15.38 66 1

0 BLOCKS 6 & 7 HAD NEW CRACKS 1/1 8:30 76.7 63 2

10 NO GREATER THAN 0.003 NEW CR ACK 13" BLOCK 33.

1/1 14:10 74.2 55 3

17.30 NEW CRACK BLOCK 37 l

1/2 21:34 72 64 4

0 NO CRACKS >.004" FIGURE 5-11 CONCRETE CRACK MAPPING AREA 5 5-14

/

O 4

900 1' SQUARE l 0 180 4 DENOTES APEX OF DOME TEMP 'F DATE TIME STAGE PSIG REr.1 ARKS IN OUT 12/31 12/25 77.31 67 1

0 1/1/82 8:27 AM 76.7 65 2

10 NOTHING OBSERVED OVER. 008 NOTHING OBSERVED OVER.008 1/1/82 2:53 PM 78.2 68 3

17:25 SLIGHT EXTENSION IN LENGTH OF EXISTING CRACKS ONLY NOTHING OBSERVED OVER.008 1/2/82 9:36 PM 74.7 67 4

0 CRACKS DECREASED IN WIDTH FIGURE 5-12 CONCRETE CRACK MAPPING O'

AREA 6 5-15

4 l

TABLE 5-1 d

SUMMARY

OF DATA FOR TRANSDUCER H-1 (Psig)

Displacement Date Time Pressure (inches).

1/1 0000 0

0.000 l

1/1 0205 2.5 0.000 1/1 0343 5.0 0.002 1/1 0622 7.5 0.004 1/1 0930 10.0 0.006 1/1 1041 12.6 0.009 1/1 1246 15.0 0.024 1/1 1349 17.3 0.027 1/1 1630 17.3 0.029 1/1 2000 15.1 0.029 1/1 2249 12.5 0.028 1/2 0153 9.8 0.026 1/2 1458 5.1 0.021 1/2 1802 2.5 0.019 1/2

'2114 0

0.015 i

TABLE 5-2 j

SUMMARY

OF DATA FOR TRANSDUCER H-2

\\

(Psig)

Displacement Date Time Pressure (inches) i 1/1 0000 0

0.000 1/1 0205 2.5 0.000 1/1 0343 5.0 0.002 1/1 0622 7.5 0.004 1/1 0930 10.0 0.007 1/1 1041 12.6 0.010 1/1 1246 15.0 0.025 1/1 1349 17.3 0.028 1/1 1630 17.3 0.031 4

1/1 2000 15.1 0.031 1/1 2249 12.5 0.029 j

1/2 0153 9.8 0.026 1/2 1458 5.1 0.022 1/2 1802 2.5 0.020 1/2 2114 0

0.017 1*

1 h

) o DH-105 5-16

)

I

i g

TABLE 5-3

SUMMARY

OF DATA FOR TRANSDUCER H-3 4

(Psig)

Displacement Date Time Pressure (inches) 1/1 0000 0

0.000 1/1 0205 2.5 0.000 1/1 0343 5.0 0.000 1.

1/1 0622 7.5 0.000 1/1 0930 10.0 0.000 1/1 1041 12.6 0.012 1/1

~1246 15.0 0.020 1/1 1349 17.3 0.023 1/1 1630 17.3 0.024 1/1 2000 15.1 0.024 1/1 2249 12.5 0.024 1/2 0153 9.8 0.024 1/2 1458 5.1 0.021 1/2 1802 2.5 0.019 1/2 2114 0

0.017 TABLE 5-4 i

SUMMARY

OF DATA FOR TRANSDUCER H {

(Psig)

Displacement Date Time Pressure (inches) 1/1 0000 0

0.000 1/1 0205 2.5 0.000 1/1 0343 5.0 0.001

{.

1/1 0622 7.5 0.003 1

1/1 0930 10.0 0.006 3

1/1 1041 12.6 0.009 i

1/1 1246 15.0 0.030 l

1/1 1349 17.3 0.036 j

1/1 1630 17.3 0.039 1/1 2000 15.1 0.039 l

1/1 2249 12.5 0.038 1/2 0153 9.8 0.035 1/2 1458 5.1 0.029 l

1/2 1802 2.5 0.026 1/2 2114 0

0.023 4

)

O l

DH-105 5-17 i

4

,s-n,..

--,,.,m-ry,--

-..-op-w-

,m-w.

e-

~~

• -~m-

• ~-w mm

-'ev~--=----

w*

-' ' * = ' ' ~ ~ ' " *

' " " ^ ^ ^ ^ ^ ^ ^

O TABLE 5-5

SUMMARY

OF DATA FOR TRANSDUCER H-5 (Psig)

Displacement Date Time Pressure (inches) 1/1 0000 0-0.000 1/1 0205 2.5 0.002 1/1 0343 5.0 0.004 1/1 0622 7.5 0.006 1/1 0930 10.0 0.009 1/1 1041 12.6 0.011 1/1 1246 15.0 0.029 1/1 1349 17.3 0.034 1/1 1630 17.3 0.036 1/1 2000 15.1 0.035 1/1 2249 12.5 0.033 1/2 0153 9.8 0.030 1/2 1458 5.1 0.026 1/2 1802 2.5 0.024 1/2 2114 0

0.022 i

TABLE 5-6

SUMMARY

OF DATA FOR TRANSDUCER H-6 O

\\w l (Psig)

Displacement

{

Date Time Pressure (inches) 1/1 0000 0

0.000 1/1 0205 2.5 0.001 1/1 0343 5.0 0.004 1/1 0622 7.5 0.007 1/1 0930 10.0 0.011

]

1/1 1041 12.6 0.015 1/1 1246 15.0 0.036 i

}

1/1 1349 17.3 0.041 1/1 1630 17.3 0.044 1/1 2000 15.1 0.044 1/1 2249 12.5 0.042 1/2 0153 9.8 0.038 1/2 1458 5.1 0.032 1/2 1802 2.5 0.029 1/2 2114 0

0.025 1

4 1

l

\\_-)

j DH-105 5-18 i

i

~.

O TABLE 5-7 V

SUMMARY

OF DATA FOR TRANSDUCER H-7 (Psig)

Displacement Date Time Pressure (inches) 1/1 0000 0

0.000 1/1 0205 2.5 0.003 1/1 0343 5.0 0.007 1/1 0622 7.5 0.011 i

1/1 0930 10.0 0.019 1/1 1041 12.6 0.025 i

1/1 1246 15.0 0.057 1/1 1349 17.3 0.089 i

1/1 1630 17.3 0.101 1/1 2000 15.1 0.099 1/1 2249 12.5 0.093 1/2 0153 9.8 0.086 1/2 1458 5.1 0.068 1/2 1802 2.5 0.056 1/2 2114 0

0.043 Final Adjusted Recovery Value: 0.043 O

TABLE 5-8

SUMMARY

OF DATA FOR TRANSDUCER H-8 (Psig)

Displacement Date Time Pressure (inches) j 1/1 0000 0

0.000 1/1 0205 2.5 0.004 1/1 0343 5.0 0.008 1/1 0622 7.5 0.019 1/1 0930 10.0 0.038 1/1 1041 12.6 0.052 1/1 1246 15.0 0.174 1/1 1349 17.3 0.267 1/1 1630 17.3 0.283 1/1 2000 15.1 0.267 4

1/1 2249 12.5 0.241 1/2 0153 9.8 1/2 1458 5.1 0.161 1/2 1802 2.5 0.136 1/2 2114 0

0.111 Final Adjusted Recovery Value: 0.054

• Invalid Reading - Out of Scale DR-105 5-19

---

~m,w

'w-ann----

we.1-nm.v

-r----,m-ww-

-m

---w-

---

,----,.r--r,-r,w

TABLE 5-9

SUMMARY

OF DATA FOR TRANSDUCER H-9 (Psig)

Displacement Date Time Pressure (inches) 1/1

'0000 0

0.000 1/1 0205 2.5 0.002 1/1 0343 5.0 0.008 1/1 0622 7.5 0.016

]

1/1 0930 10.0 0.028 1/1 1041 12.6 0.056 1/1 1246 15.0 0.185 1/1 1349 17.3 0.246 1/1 1630 17.3 0.263 1/1 2000 15.1 0.257 1/1 2249 12.5 0.233 1/2 0153 9.8 0.204 1/2 1458 5.1 0.153 1/2 1802 2.5 0.127 1/2 2114 0

0.102 Final Adjusted Recovery Value: 0.037 TABLE 5-10

SUMMARY

OF DATA FOR TRANSDUCER H-10 (Psig)

Displacement Date Time Pressure (inches) 1/1 0000 0

0.000 1/1 0205 2.5 0.005 i

1/1 0343 5.0 0.010 1/1 0622 7.5 0.018 1/1 0930 10.0 0.030 1/1 1041 12.6 0.049 1/1 1246 15.0 0.107 1/1 1349 17.3 0.145 1/1 1630 17.3 0.166 I

1/1 2000 15.1 0.163 1/1 2249 12.5 0.150 1/2 0153 9.8 0.134 1/2 1458 5.1 0.108 1/2 1802 2.5 0.094 1/2 2114 0

0.079 Final Adjusted Recovery Value: 0.077 l

O DH-105 5-20 4

i

=.

f TABLE 5-11 s

SUMMARY

OF DATA FOR TRANSDUCER H-11 (Psig)

Displacement Date Time Pressure (inches) a 1/1 0000 0

0.000 1/1 0205 2.5 0.005 1/1 0343 5.0 0.010 1/1 0622 7.5 0.015 1/1 0930 10.0 0.025 1/1 1041 12.6 0.041 1/1 1246 15.0 0.109 1/1 1349 17.3 0.152 1/1 1630 17.3 0.168 1/1 2000 15.1 0.164 1/1 2249 12.5 0.156 1/2 0153 9.8 0.144 1/2 1458 5.1 0.122 1/2 1802 2.5 0.108 1/2 2114 0

0.093 Final Adjusted Recovery Value: 0.090 0-TABLE 5-12

SUMMARY

OF DATA FOR TRANSDUCER H-12 (Psig)

Displacement Date Time Pressure (inches) 1/1 0000 0

0.000 1/1 0205 2.5 0.004 1/1 0343 5.0 0.009 1/1 0622 7.5-0.015 1/1 0930 10.0 0.023 1/1 1041 12.6 0.029 1/1 1246 15.0 0.060 1/1 1349 17.3 0.078 1/1 1630 17.3 0.084 1/1 2000 15.1 0.084 1/1 2249 12.5 0.080 1/2 0153 9.8 0.074 1/2 1458 5.1 0.063 1/2 1802 2.5 0.057 i

1/2 2114 0

0.049 Final Adjusted Recovery Value: 0.050 O

V DH-105 5-21 4

---

n-vm-

,w

--tw nc

-r-w-.,

-+-

--o-+,--,+,m--

-,-m

~ -,------ --- -, - -

r-~-----

TABLE 5-13 s

SUMMARY

OF DATA FOR TRANSDUCER H-13 (Psig)

Displacement Date Time Pressure (inches) 1/1 0000 0

0.000 1/1 0205 2.5 0.000 1/1 0343 5.0 0.000 i

1/1 0622 7.5 0.011 l

1/1 0930 10.0 0.026 1

1/1 1041 12.6 0.043 1/1 1246 15.0 0.125 1/1 1349 17.3 0.185 1/1 1630 17.3 0.210 1/1 2000 15.1 0.210 1/1 2249 12.5 0.198 1/2 0153 9.8 0.173 1/2 1458 5.1 0.130 1/2 1802 2.5 0.110 4

1/2 2114 0

0.088 i

TABLE 5-14

SUMMARY

OF DATA FOR TRANSDUCER H-14 (Psig)

Displacement Date Time Pressure (inches) 1/1 0000 0

0.000 1/1 0205 2.5 0.006 1/1 0343 5.0 0.013 1/1 0622 7.5 0.023 1/1 0930 10.0 0.039 1/1 1041 12.6 0.057 1/1 1246 15.0 0.154 1/1 1349 17.3 1/1 1630 17.3 0.249 1/1 2000 15.1 0.244 1/1 2249 12.5 1/2 0153 9.8 0.197 1/2 1458 5.1 0.147 1/2 1802 2.5 0.124 1/2 2114 0

0.102

• Invalid Reading - Out of Scale l

' O 1

e i

DH-105 5-22

m

()

TABLE 5-15

SUMMARY

OF DATA FOR TRANSDUCER H-15 i

(Psig)

Displacement Date Time Pressure (inches)__

1/1 0000 0

0.000 1/1 0205 2.5 0.005 1/1 0343 5.0 0.009 1/1 0622 7.5 0.017 1/1 0930 10.0 0.029 1/1 1041 12.6 0.040 4

1/1 1246 15.0 0.108 1/1 1349 17.3 0.165 l

1/1 1630 17.3 0.184 1/1 2000 15.1 0.184 1/1 2249 12.5 0.171 3

1/2 0153 9.8 0.350 1/2 1458 5.1 0.112 1/2 1802 2.5 0.097 1/2 2114 0

0.080 i

TABLE 5-16

SUMMARY

OF DATA FOR TRANSDUCER H-16 V

(Psig)

Displacement 4

Date Time Pressure (inches) 1/1 0000 0

0.000 1/1 0205 2.5 0.004 1/1 0343 5.0 0.009 1/1 0622 7.5 0.014 1/1 0930 10.0 0.019 1/1 1041 12.6 0.024 1/1 1246 15.0 0.044 1/1 1349 17.3 0.051 d

1/1 1630 17.3 0.056 1/1 2000 15.1 0.055 i

1/1 2249 12.5 0.051 1/2 0153 9.8 0.046 1/2 1458 5.1 0.037 1/2 1802 2.5 0.032 1/2 2114 0

0.026 O

DH-105 5-23 1

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

. _ -. - -.. _ - - _. _ _ _ _. - - _ _ _. _ - = -

)

TABLE 5-17

SUMMARY

OF DATA FOR TRANSDUCER H-17 (Psig)

Displacement Date Time Pressure (inches) 1/1-0000 0

0.000 1/1 0205 2.5 0.005 1/1 0343 5.0 0.010 1/1 0622 7.5 0.015 1/1 0930 10.0 0.021 1/1 1041 12.6 0.027 1/1 1246 15.0 0.060 1/1 1349 17.3 0.075 1/1 1630 17.3 0.082 1/1 2000 15.1 0.081 1/1 2249 12.5 0.075 1/2 0153 9.8 0.067 1/2 1458 5.1 0.054 1/2 1802 2.5 0.047 1/2 2114 0

0.039 TABLE 5-18

SUMMARY

OF DATA FOR TRANSDUCER H-18 i

(Psig)

Displacement Date Time Pressure (inches) 1/1 0000 0

0.000 1/1 0205 2.5 0.003 1/1 0343 5.0 0.006 1/1 0622 7.5 0.009 4

1/1 0930 10.0 0.013 1/1 1041 12.6 0.016 1/1 1246 15.0 0.038 1/1 1349 17.3 0.058 1/1 1630 17.3 0.074 1/1 2000 15.1 0.072 1/1 2249 12.5 0.068 1/2 0153 9.8 0.064 1/2 1458 5.1 0.056 1/2 1802 2.5 0.051 1/2 2114 0

0.046 O

DH-105 5-24 i

-,---,,-..,v.r,n,,-,-.-

e -, -, - ----

--w--.---.

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

i TABLE 5-19

SUMMARY

OF DATA FOR TRANSDUCER H-19 i

(Psig)

Displacement Date Time Pressure (inches) 1/1 0000 0

0.000 1/1 0205 2.5 0.004 i

1/1 0343 5.0 0.008 1/1 0622 7.5 0.013 i

1/1 0930 10.0 0.025 j

1/1 1041 12.6 0.041 1/1 1246 15.0 0.123 1/1 1349 17.3 0.182 l

1/1 1630 17.3 0.201 1/1 2000 15.1 0.193 1/1 2249 12.5 0.177 j

1/2 0153 9.8 0.157 1/2 1458 5.1 0.118 1/2 1802 2.5 0.096 1/2 2114 0

0.074 i

i Final Adjusted Recovery value: 0.068 1

I TABLE 5-20 l

SUMMARY

OF DATA FOR TRANSDUCER H-20 i

(Psig)

Displacement Date Time Pressure (inches) 1/1 0000 0

0.000 1/1 0205 2.5 0.003 1/1 0343 5.0 0.008

}

1/1 0622 7.5 0.013 1/1 0930 10.0 0.021 1/1 1041 12.6 0.042 1/1 1246 15.0 0.176 1/1 1349 17.3 0.255 1/1 1630 17.3 0.271 4

1/1 2000 15.1 0.258 1/1 2249 12.5 0.231 1/2 0153 9.8 1/2 1458 5.1 0.144 1/2 1802 2.5 0.117 1/2 2114 0

0.091 i

Final Adjusted Recovery Value: 0.100

• Invalid Reading - Out of Scale O

DH-105 5-25 4

]

-,,__._---y--

--e.-

_y,

,_pr.-

.,____g,----_y-.

,,_--,__,,.,,_,,,, wry v

4,r3_.-.-

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

i i

\\

TABLE 5-21

SUMMARY

OF DATA FOR TRANSDUCER H-21 l

(Psig)

Displacement Date Time Pressure (inches) 1/1 0000 0

0.000 1/1 0205 2.5 0.003 1/1 0343 5.0 0.008 1/1 0622 7.5 0.014 1/1 0930 10.0 0.026 l

1/1 1041 12.6 0.036 1/1 1246 15.0 0.131 1/1 1349 17.3 0.185 1/1 1630 17.3 0.206 1/1 2000 15.1 0.206 1/1 2249 12.5 0.197 1/2 0153 9.8 0.183 1/2 1458 5.1 0.150 1/2 1802 2.5 0.131 1/2 2114 0

0.109 Final Adjusted Recovery Value: 0.020 i

O TABLE 5-22

SUMMARY

OF DATA FOR TRANSDUCER D-1 i

(Psig)

Displacement Date Time Pressure (inches) 1/1 0000 0

0.000 1/1 0205 2.5 0.008 1/1 0343 5.0 0.020 1/1 0622 7.5 0.035 1/1 0930 10.0 0.054 1/1 1041 12.6 0.069 1/1 1246 15.0 0.089 1/1 1349 17.3 0.106 1/1 1630 17.3 0.114 1/1 2000 15.1 0.114 1/1 2249 12.5 0.105 1/2 0153 9.8 0.090 1

1/2 1458 5.1 0.064 1/2 1802 2.5 0.051

+

I 1/2 2114 0

0.036 i

Final Adjusted Recovery Value: 0.017 i

O DH-105 5-26

. ~.

=_

}

TABLE 5-23

SUMMARY

OF DATA FOR TRANSDUCER D-2 (Psig)

Displacement Date Time Pressure (inches) 1/1 0000 0

0.000 1/1 0205 2.5 0.015 1/1 0343 5.0 0.026 1/1 0622 7.5 0.040 1/1 0930 10.0 0.056 j

1/1 1041 12.6 0.069 1/1 1246 15.0 0.091 j

1/1 1349 17.3 0.106 1/1 1630 17.3 0.112 1/1 2000 15.1 0.112 1/1 2249 12.5 0.106 1/2 0153 9.8 0.092 1/2 1458 5.1 0.067 1/2 1802 2.5 0.055 1/2 2114 0

0.043 Final Adjusted Recovery Value: 0.025 i

TABLE 5-24

SUMMARY

OF DATA FOR TRANSDUCER D-3 (Psig)

Displacement l

Date Time Pressure (inches) 1/1 0000 0

0.000 1/1 0205 2.5 0.000 1/1 0343 5.0 0.000 1/1 0622 7.5 0.012 i

1/1 0930 10.0 0.030 i

1/1 1041 12.6 0.039 1/1 1246 15.0 0.060 i

1/1 1349 17.3 0.073 1/1 1630 17.3 O.081 1/1 2000 15.1 0.080 I

1/1 2249 12.5 0.080 1/2 0153 9.8 0.073 1/2 1458 5.1 0.051 1/2 1802 2.5 0.051 1/2 2114 0

0.032 Final Adjusted Recovery Value:

0.014 O

DH-105 5-27 I

O TABLE 5-25

SUMMARY

OF DATA FOR TRANSDUCER V-3 (Psig)

Displacement Date

, Time Pressure (inches) 1/1 0000 0

0.000 1/1 0205 2.5 0.000 1/1 0343 5.0 0.000 1/1 0622 7.5 0.009 1/1 0930 10.0 0.009 1/1 1041 12.6 0.015 1/1 1246 15.0 0.023 1/1 1349 17.3 0.029 1/1 1630 17.3 0.031 1/1 2000 15.1 0.031 1/1 2249 12.5 0.031 1/2 0153 9.8 0.031 1/2 1458 5.1 0.027 1/2 1802 2.5 0.022 1/2 2114 0

0.017 Final Adjusted Recovery Value: 0.007 O

TABLE 5-26

SUMMARY

OF DATA FOR TRANSDUCER V-1 (Psig)

Displacement Date Time Pressure (inches) 1/1 0000 0

0.000 1/1 0205 2.5 0.000 1/1 0343 5.0 0.001 1/1 0622 7.5 0.005 1/1 0930 10.0 0.011 1/1 1041 12.6 0.013 1/1 1246 15.0 0.019 1/1 1349 17.3 0.024 1/1 1630 17.3 0.027 1/1 2000 15.1 0.027 1/1 2249 12.5 0.027 4

1/2 0153 9.8 0.024 1/2 1458 5.1 0.014 1/2 1802 2.5 0.011 1/2 2114 0

0.007 Final Adjusted Recovery Value: 0.003 O

DH-105 5-28

=_

1 i

TABLE 5-27 i

SUMMARY

OF DATA FOR TRANSDUCER V-4 (Psig)

Displacement Date Time Pressure (inches) 1/1 0000 0

0.000 i

1/1 0205 2.5 0.000

)

1/1 0343 5.0 0.004 I

1/1 0622 7.5 0.010 i

1/1 0930 10.0 0.016 j

1/1 1041 12.6 0.021 1/1 1246 15.0 0.027 1/1 1349 17.3 0.031 1/1 1630 17.3 0.034 1/1 2000 15.1 0.033 1/1 2249 12.5 0.033 1/2 0153 9.8 0.028 1/2 1458 5.1 0.018 1/2 1802 2.5 0.013 1/2 2114 0

0.008 Final Adjusted Recovery Value: 0.001 TABLE 5-28

SUMMARY

OF DATA FOR TRANSDUCER E-1 (Psig)

Displacement 1

Date Time Pressure (inches) 1/1 0000 0

0.000 1/1 0205 2.5 0.000 1/1 0343 5.0 0.009 1/1 0622 7.5 0.017 1/1 0930 10.0 0.031 1/1 1041 12.6 0.045 1/1 1246 15.0 0.145 1/1 1349 17.3 1/1 1630 17.3 0.233 1/1 2000 15.1 0.225 1/1 2249 12.5 1/2 0153 9.8 0.181 1/2 1458 5.1 0.137 1/2 1802 2.5 0.115 1/2

. 14 0

0.093 i

l

• Invalid Reading - Out of Scale l

O DH-105 5-29 I

-,__._,..,,.-m,,,-.c..r,

--,,,r.,

_r....

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

-... =. _,.

i 4

2 TABLE 5-29

SUMMARY

OF DATA FOR TRANSDUCER E-2 (Psig)

Displacement Date Time Pressure (inches) 1/1 0000 0

0.000 1/1 0205 2.5 0.005 1/1 0343 5.0 0.013 1/1 0622 7.5 0.022 1/1 0930 10.0 0.037 1/1 1041 12.6 0.052 1/1 1246 15.0 0.116 4

1/1 1349 17.3 0.213 1/1 1630 17.3 0.258 1/1 2000 15.1 0.228 1/1 2249 12.5 0.207 I

1/2 0153 9.8 0.183 1/2 1458 5.1 0.138 1/2 1802 2.5 0.110 1/2 2114 0

0.091 1

s TABLE 5-30

SUMMARY

OF DATA FOR TRANSDUCER E-3 (Psig)

Displacement Date Time Pressure (inches) 1/1 0000 0

0.000 1/1 0205 2.5 0.011 1/1 0343 5.0 0.022 1/1 0622 7.5 0.034 1/1 0930 10.0 0.051 l

1/1 1041 12.6 0.068

]

1/1 1246 15.0 0.156 1

1/1 1349 17.3 0.220 1/1 1630 17.3 0.224 1/1 2000 15.1 0.232 1/1 2249 12.5 0.209 1/2 0153 9.8 0.182 1/2 1458 5.1 0.134 1/2 1802 2.5 0.110 1/2 2114 0

0.085 t

l DH-105 5-30 i

-w-r--,~~--

+ -~

~

.,.e m -,

,_m,

,1,~-

=.. - -,.

,,,,_.m-.--w_nn

,,,-w

d Oi TABLE 5-31

]

SUMMARY

OF DATA FOR TRANSDUCER E-4 l

(Psig)

Displacement Date Time Pressure (inches) i 1/1 0000 0

0.000 1/1 0205 2.5 0.009 1/1 0343 5.0 0.019 1/1 0622 7.5 0.031 1/1 0930 10.0 0.053 1/1 1041 12.6 0.072 1/1 1246 15.0 0.134 1/1 1349 17.3 1/1 1630 17.3 0.213 1/1 2000 15.1 0.207 1/1 2249 12.5 1/2 0153 9.8 0.163 a

1/2..

1458 5.1 0.118 1/2 1802 2.5 0.096 1/2 2114 0

0.073 i

• Invalid Reading - Out of Scale j

l TABLE 5-32

SUMMARY

OF DATA FOR TRANSDUCER E-5 (Psig)

Displacement Date Time Pressure (inches) 1/1 0000 0

0.000 1/1 0205 2.5 0.000 1/1 0343 5.0 0.014 1/1 0622 7.5 0.026 1/1 0930 10.0 0.040 1/1 1041 12.6 0.059 1/1 1246 15.0 0.116 1/1 1349 17.3 0.166 q

1/1 1630 17.3 0.187 1/1 2000 15.1 0.187 1/1 2249 12.5 0.183 3~

1/2 0153 9.8 0.164 1/2 1458 5.1 0.128 1/2 1802 2.5 0.108 1/2 2114 0

0.088 O

DH-105 5-31 l

...--. --,,, n,, -,.

c.,, --.,,.. ---,

O TABLE 5-33

SUMMARY

OF DATA FOR TRANSDUCER E-6 (Psig)

Displacement Date Time Pressure (inches) 1/1 0000 0

0.000 1/1 0205 2.5 0.008 1/1 0343 5.0 0.014 4

1 1/1 0622 7.5 0.022 1/1 0930 10.0 0.036 1/1 1041 12.6 0.049 4

1/1 1246 15.0 0.104 1/1 1349 17.3 0.145 1/1 1630 17.3 0.167 1/1 2000 15.1 0.166 1/1 2249 12.5 0.153 1/2 0153 9.8 0.137 i

3 i

1/2 1458 5.1 0.106 l

1/2 1802 2.5 0.089 1/2 2114 0

0.072 TABLE 5-34

SUMMARY

OF DATA FOR TRANSDUCER E-7 j

(Psig)

Displacement Date Time Pressure (inches)

I 1/1 0000 0

0.000 1/1 0205 2.5 0.007 1/1 0343 5.0 0.014 1/1 0622 7.5 0.023 1/1 0930 10.0 0.037 i

1/1 1041 12.6 0.055 l

1/1 1246 15.0 0.117 1/1 1349 17.3 0.172 i

1/1 1630 17.3 0.200 1/1 2000 15.1 0.196 1/1 2249 12.5 0.177 i

1/2 0153 9.8 0.155 1/2 1458 5.1 0.116 1/2 1802 2.5 0.096 1/2 2114 0

0.076 i

O DH-105 5-32 i

a

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

l TABLE 5-35

SUMMARY

OF DATA FOR TRANSDUCER E-8 (Psig)

Displacement Date Time Pressure (inches) 1/1-0000 0

0.000 1/1 0205 2.5 0.009 1

1/1 0343 5.0 0.017 I

1/1 0622 7.5 0.027 1/1 0930 10.0 0.044 1/1 1041 12.6 0.062 1/1 1246 15.0 0.125 1/1 1349 17.3 0.184 1/1 1630 17.3 0.210 1/1 2000 15.1 0.200 1/1 2249 12.5 0.180 1/2 0153 9.8 0.155 1/2 1458 5.1 0.112 1/2 1802 2.5 0.090 1/2 2114 0

0.068 TABLE 5-36

SUMMARY

OF DATA FOR TRANSDUCER E-9 (Psig)

Displacement Date Time Pressure (inches) 1/1 0000 0

0.000 1/1 0205 2.5 0.010 1/1 0343 5.0 0.022 1/1 0622 7.5 0.035 1/1 0930 10.0 0.055 1/1 1041 12.6 0.075 1/1 1246 15.0 0.144 1/1 1349 17.3 0.209 1/1 1630 17.3 0.235 1/1 2000 15.1 0.224 1/1 2249 12.5 0.200 1/2 0153 9.8 0.172 1/2 1458 5.1 0.121 1/2 1802 2.5 0.094 1/2 2114 0

0.068 i

4 DH-105 5-33 i

..-,-,_,-.--,.-.m..,.

_---._-._._-..,._-.,_-,,,m.,

j O~

TABLE 5-37

SUMMARY

OF DATA FOR TRANSDUCER E-10 1

(Psig)

Displacement Date Time Pressure (inches) 1/1 0000 0

0.000 1/1 0205 2.5 0.011 1/1 0343 5.0 0.021 1/1 0622-7.5 0.033 1/1 0930 10.0 0.050 1/1 1041 12.6 0.070 4

1/1 1246 15.0 0.129 1/1 1349 17.3 0.186 1/1 1630 17.3 0.205 1/1' 2000 15.1 0.192 1/1 2249 12.5 0.174 1/2 0153 9.8 0.152 i

1/2 1458 5.1 0.112 l

1/2 1802 2.5 0.090 1/2 2114 0

0.068 f'

TABLE 5-38 4

SUMMARY

OF DATA FOR TRANSDUCER E-11 O

(Psig)

Displacement Date Time Pressure (inches) 1 1/1 0000 0

0.000 1/1 0205 2.5 0.007 1/1 0343 5.0 0.015 1/1 0622 7.5 0.023 1/1 0930 10.0 0.033 1/1 1041 12.6 0.055 1/1 1246 15.0 0.117 1/1 1349 17.3 0.155 1/1 1630 17.3 0.173 1/1 2000 15.1 0.171 1/1 2249 12.5 0.159 1/2 0153 9.8 0.144 1/2 1458 5.1 0.116 1/2 1802 2.5 0.100 1/2 2114 0

0.082 t

!O

~

DH-105 5-34

1 I

l

[

4 TABLE 5-39

SUMMARY

OF DATA FOR TRANSDUCER E-12 i

l (Psig)-

Displacement i

Date Time Pressure (inches) i 1/1 0000 0

0.000

}

1/1 0205 2.5 0.006 1/1 0343 5.0 0.012 4

l 1/1 0622 7.5 0.020 l

l 1/1 0930 10.0 0.030 l

1/1 1041 12.6 0.046 1/1 1246 15.0 0.117 1/1 1349 17.3 0.152 i

1/1 1630 17.3 0.170 i

1/1 2000 15.1 0.168 l

I 1/1 2249 12.5 0.158 1

1/2 0153 9.8 0.145 1/2 1458 5.1 0.120 l!

1/2 1802 2.5 0.104 1/2 2114 0

0.087 f

I 3

l I

I ilO

}

t 1

4 i

i 1

l i

i I

a I

1 l

i DH-105 5-35 i

4 w e si -w ww- =&ve.-.na en-y e We-e w

.m w.

.m-e-e e

w-v-w,--

we m--

eev --*- - +-+

me----e--m-

-w-ww-e-n

--=- - + - * - -

new-='

i l

}

6.

REFERENCES h

l.

Final Safety Analysis Report, Grand Gulf Nuclear Station, j

Unit No. 1, Mississippi Power and Light Company.

f I

l 2.

Procedure QlM61-W-11302WKA, Containment Structural Integrity Test, Grand Gulf Nuclear Station Unit 1, Mississippi Power i.

and Light Company.

t Il' I

2 i

i i

l i

i i

I t

i i

l l

t I

t l

t DH-105 6-1

--~+++---*-irm ww

. w e w n

-e n-.

-en%-- > + +=*-

---