Text

Nuclear Component Qualification Test Rept Square D 9025-BCW-45 Thermal Switch
	ML20137Z827
Person / Time
Site:	Byron, Braidwood, Clinton, LaSalle, 05000000, Marble Hill
Issue date:	11/30/1984
From:	Bessey R, Scheidt D, Scott Wilson; SOUTHWEST RESEARCH INSTITUTE
To:	;
Shared Package
ML20137Z802	List: ML20137Z795; ML20137Z810; ML20137Z816; ML20137Z827;
References
	06-6073-TR116, 6-6073-TR116, NUDOCS 8512110416
	Download: ML20137Z827 (107)
	v • d • e

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b NUCLEAR COMPONENT C.UALIFICATION TEST REPORT r

i SQUARE D 9025-BCW-45 THERMAL SWITCH l

for STEWART & STEVENSON SERVICES, INC.

l P.O. Box 1637 Houston, Texas 77251 l

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SwRI Document No. 06-6073-TR116 O

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Southwest Research Institute i

6220 Culebra Road San Antonio, Texas 78284 i

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Copy No. 3 NUCLEAR COMPONENT QUALIFICATION Test ateoa1 O

SQUARE O 9025-BCW-45 THERMAL SWITCH n

For Stewart & Stevenson Services, Inc.

P. O. Box 1637 Houston, Texas 77251 By Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 Report No. 06-6073-TR116 O

November, 1984 1

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Steven K. Wilson Roger)L. Bessey

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Senior Technician Group Leader w

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Bruce Mabrito, Manager Quality Assurance mU

Test Report No.

TR116 IDENTIFICATION AND PLANT APPLICATIONS FOR QUALIFIED (M and IDENTIFICATION AND PLANT APPLICATIONS FOR ITEMS QUALIFIED O

SIMILARITY TO THE MASTER ITEM C.

SIMILAR ITEMS A.

PLANT APPLICATIONS B. MASTER ITEM

Serial Name of Utility and No.

Station Division / Unit Square D 9025-BCW-32 9025-BCW-35 CECO LaSalle Thermal Switches 1

Divisions I & 2 511, 513

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Square D 9025-BCW-35 9025-BCW-43 Thermal Switches 2

CECO LaSalle Division 3 513, 515 Sq'uare D Square D 9025-BCW-45 9025-BCW-42 Thermal Switch Thermal Switch 3

Illinois Power Company O

Clinton Divisions 1 5 2 516-47191-1 514 Square D 9025-BCW-35 Thermal Switch 4

Illinois Power Company

, Clinton Division 3 513 Square D 9025-BCW-32 Thermal Switch 5

CECO Byron /Braidwood Units 1 & 2 511 c'

5 Public Service Indiana Marole Hill, Units 1 & 2 i

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TABLE OF CONTENTS O

Page Section 1

1.0 PURPOSE 1

2.0 TEST ITEM IDENTIFICATION 1

2.1 Identification of Item to be Type Tested 1

2.2 Items Qualified by Similarity 1

3.0 SPECIFICATIONS AND STANDARDS 3

4.0 SEISMIC TEST FACILITY 3

4.1 Location 3

4.2 General Purpose 3

4.3 Mechanical Table Description 4

4.4 Associated Instrumentation 4

5.0 TEST EQUIfMENT IDENTIFICATION 4

6.0 CALIBRATION 6

7.0 TEST METHOD 6

O 7.1 Genere, 6

7.2 Functional Checks 7

7.3 Thermal Aging 7

7.4 Radiation Aging 7

7.5 Operational Aging 9

7.6 Vibrational Aging 9

7.7 Test Item Mounting 9

7.8 Resonance Search Tests 10 7.9 Preliminary Tests 10 7.10 Seismic Qualification Tests 12 7.11 Environmental Extremes Test 12 7.12 Sumary of Seismic Tests Performed 17 7.13 Analog Tape Logs 17 8.0 RESULTS AND CONCLUSIONS 19 9.0 PHOTOGRAPHS 26 10.0 RESONANCE SEARCH DATA 29 11.0 RESPONSE SPECTRUM DATA 56 12.0 SwRI LABORATORY DATA LOGS APPENDIX A - Basis for Required Response Spectrum Used in These Tests O

111

LIST OF FIGURES Page Figure No.

Sample from strip chart recorder used to monitor the 8

7.1 temperature of the test item during thermal aging 11 OBE and SSE shaker table drive 7.2 a

Circuit used to monitor the item's functionality 13 7.3 during seismic and the environmental extremes test Sample oscillograph record from test SSEYZ1 showing 7.4 the switch's contacts did not change states indicat-14 ing the switch was operating normally during test Sample calibration record showing the off (low) and 7.5 on (high) conditions showing how the trace would have deflected had the switch's contacts changed states 15 during the tests 20 9.1 thru thru Photographs 25 9.12 27 10.1 thru Resonance Search Data on Z-axis, X-axis, and Y-axis O

28 tnru 10.6 30 11.1 thru thru Response Spectrum Data 55 11.52 LIST OF TABLES g

Table No.

5 5.1 Equipment List Summary of Seismic Tests Performed with +10% Margin t

7.1 16 Added to the RRS c

16 7.2 Summary of Multiple Damping Plots 17 7.3 Analog Tape Log O

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TEST REPORT O

1.0 PURPOSE The purpose of this report is to describe the tests performed on a Square 0 9025-BCW-45 Thermal Switch for qualification as a Class 1E com-ponent for application in the nuclear generating stations listed in the The tests were identification matrix at the beginning of this report.

performed in accordance with the approved test plan, reference 3.7 and the The item was tested to qualification plans, references 3.8 through 3.12.

conform to the categorization listed in the NUREG Specification 058 Appendix E, Paragraph 2a. tion, operational and vibrational aging of the item Subsequent to end of service life condition plus 10% margin (44-years).

the applicable aging tests the item underwent a seismic qualification test to show that its Class IE function would not be impaired when exposed to The testing included a baseline func-the specified seismic environment.

tional check prior to the start of testing as well as functional c between tests.

Subsequent to all testing a post-test functional ronmental extremes test.The functional check procedures used along with the check was performed.

CFMA are contained in Appendices B and S, respectively of the test plan, reference 3.7.

2.0 TEST ITEM IDENTIFICATION 1dentificetioe of Item to be Tyne Tested O

2.1 Stewart & Stevenson One Square D 9025-BCW-45 Thermal Switch.

identification No. 516-47191-1.

2.2 Items Qualified by Similarity The following items are of similar construction and materials and differ in that the 30's series are SPDT switches and the 40's serie are DPDT switches., The only other differences between different models The items to be are the temperature set points and temperature ranges.

qualified by similarity to the item identified in Section 2.1 for theSquare D thermal applications listed in the id n tification matrix are: switches 9025-B 3.0 SPECIFICATIONS AND STANDARDS IEEE 323-1974, " Standard for Qualifying Class IE Equipment for 3.1 Nuclear Power Generating Stations," Nuclear Power Engineering Committee of the IEEE Power Engineering Society, 1974.

NUREG 0588, " Interim Staff Position of Environmental Qualifica-tion of Safety-Related Electrical Equipment," A. J. Szukiewicz, 3.2 1980.

O 1

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U.S. Nuclear Regulatory Commission, Regulatory Guide 1.100, 3.3

" Seismic Qualification of Electrical Equipment for Nuclear Power

^

Plant," Revision 1 August 1977.

p IEEE 344-1975, " Recommended Practices for Seismic Qualification 3.4 of Class 1E Equipment for Nuclear Power Generating Stations,"

Nuclear Power Engineering Committee of the IEEE Power Engineer-ing Society, 1975.

SwRI Division 06 Nuclear Projects Operating Procedure 3.5 XII-EE-101-3, " Calibration of Mechanical Sciences Dynamics Test Equipment," November 1981.

SwRI Division 06 Nuclear Projects Operating Procedure 3.6 XI-EE-101-2, " Seismic Tests of Electrical and Mechanical Components," November 1981.

SwRI Generic Test Procedure for the Qualification of Switches.

3.7 06-6073-TP-3.

All applicable revisions of Document No.

SwRI Nuclear Qualification Plan, Emergency Diesel Generator 3.8 System for Application in the Commonwealth Edison Company, Byron /Braidwood Units 1&2. Document No. 02-6073-005, dated January 1982.

SwRI Nuclear Qualification Plan, Emergency Diesel Generator 3.9 System for Application in the Commonwealth Edison Company,

/N LaSalle County Station Divisions 1&2. Document No. 02-6073-006, d

dated January 1982.

3.10 SwRI Nuclear Qualification Plan, Emergency Diesel Generator System for Application in the Illinois Power Company, Clinton Divisions 1&2. Document No. 02-6073-010, dated January 1982.

3.11 SwRI Nuclear Qualification Plan, Emergency Diesel Generator System for Application in the Commonwealth Edison Company, LaSalle County Station Division 3.

Document No. 02-6073-011, dated January 1982.

3.12 SwRI Nuclear Qualification Plan, Emergency Diesel Generator System for Application in the Illinois Power Company, Clinton Division 3.

Document No. 02-6073-012, dated January 1982.

c and the applicable portions of the following standards 3.13 EPRI NP-1558, "A Review of Equipment Aging Theory and Technology," Franklin Research Center, Carfagno, Gibson, September 1980.

3.14 IEEE 101-1972, "IEEE Guide for the Statistical Analysis of Thermal Life Test Data " IEEE Standards Coordinating Committee of Thermal Rating, 1972.

O 2

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Standard Criteria for Type Tests of Class 1E 3.15 IEEE 381-1977 Modules Used in Nuclear Power Generating Stations.

gQ Standard Criteria for Diesel-Generator Units 3.16 IEEE 387-1977 Applied as Standby Power Supplies for Nuclear Power Generating Stations.

3.17 IEEE 384-1981 Criteria for Independence of Class 1E Equipment and Circuits.

b 3.18 EPRI NP-2129, " Radiation Effects on Organic Materials in Nuclear Plants," Georgia Institute of Technology, November 1981.

4.0 SEISMIC TEST FACILITY 4.1 Location Southwest Research Institute Department of Engineering Mechanics 6220 Culebra Road San Antonio, TX 78284 4.2 General Purpose This facility has the capability of realistic simulation of an earthquake dynamic environment as well as all accepted standard approxima-It has been designed principally for quali-tions of such an environment.

O fication testins of traicei comPoneats to be used in auclear and conven-It is also particularly suited to the tional power generation stations.

It can study of structural scale model responses to seismic excitation.

further be used as a general purpose shaker facility within its range of operation, and therefore can simulate nuclear plant operating transients.

4.3 Mechanical Table Description A mounting surface of up to 6 by 6 feet can be excited with simultaneous vertical and horizontal motion that is arbitrary and indepen-dent along each ax'is. Extenders are utilized for mounting somewhat larger Maximum table payload capacity is 6,000 pounds specimens, when necessary.

dead weight.. Drive mechanisms are servo-controlled electrohydraulic, and having the following capabilities:

Horizontal Vertical

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0-250 Hz 0-250 Hz Frequency Range Force Capacity 10,000 lb 20,000 lb Maximum Stroke 8.0 in.

7.0 in.

Maximum Velocity 90 in./sec 22 in./sec Maximum Acceleration

10 g 10 g

At zero payload 3

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4-4.4 Associated Instrumentation O

Excitation signals are provided typically by function generators Table or actual seismic signals recorded on analog instrumentation tape.

displacement is accurately controlled at low to medium frequencies by

'l Deteriora-automatic feedback to respond to an arbitrary voltage signal.

tion in control is experienced at higher frequencies such that open-loop Table responses are monitored by operation is necessary in this range.

accelerometers whose outputs can be analyzed according to

+

t plotted within seconds by a Spectral Dynamics SD321 Shock Spectral Ana-Po parameters.

lyzer, or by a DEC 11/23 computer system.

computed by a Nicolet Scientific UA500A Real Time Analyzer or i

444A FFT Analyzer.

parameters are computed with a Saicor 43A Real Time Analyzer or with a i

Zonic multichannel FFT processor.

analog or digital tape, on oscillographs, or monitored on oscilloscopes.

l Large volumes of data are usually recorded first on ana i

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11/70 computer as its central processor.

1 I

5.0 TEST EQUIPMENT IDENTIFICATION i

The equipment used to perform the tests and obtain data during this qualification program is given in Table 5.1.

6.0 CALIBRATION O

Instrumentation calibration was performed in accordance with Engineering Sciences Division Nuclear Projects Operating Pro All accelerometers were calibrated using reference standard Kistler 808K/561T which is traceable to the National Bureau of Standards, l

A terminal peak sawtooth signal is used for calibrating the digital response spectrum subroutine used in the Division 06 DEC 11/23 computer i

i system comparing the results with the analytically known results.

The Hewlett-Packard Tape Recorder, Model 3964A was used solely as a signal source and was not calibrated on an absolute basis.

The Despatch Oven, Model LDB-1-69, does not require calibration.

Temperature was monitored using an Omega Model 199KC-A digital thermometer which was calibrated in accordance-with Division 06 cyclic calibration routine.

The output of the Omega Digital Thermometer Model 199KC-A was recorded on an Omega Model 141 Chart Recorder which was calibrated in accordance with Division 06 cyclic calibration routine.

O 4

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TABLE 5.1 EQUIPMENT LIST LIST APR-13-94 REV-4 ENGINEERING MECHANICS DYNAM'CS EQUIPMENT

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MAAE MCDEL SERIAL REMARKE C,i NO ITEM 111C FC 3 OECADE SW p

4 SWEEF CSCILLATOR SSECTRAL DYNAM SD104A-5 FC 3 DECADE SW 5 5 WEEP CSCILLATOR SPECTRAL DYNAM SD104A-5 1E5e 557 FC 5-1CW H:

SERVC MONITCR EPECTRAL DYNAM SD105A 925 FC 1-5W H

- cERVC MCNITCR ScECTRAL DYNAM SD105C-1 10 PCWER AMDLIFIER TEAM 1528 1C2 FC PILCT VALVE II ACCELERCMETER ENDEVCC 22:1D JC 15 DU 1-5000 HZ 14 ACCELERCMETER ENDEVCD 2221D JC 18 DU 1-5000 HZ 15 ACCELERCMETER ENDEVCC 22:1D JE 66 DU 1-500C HZ I

17 ACCELERCMETER ENDEVCC 22:1D XB-7e DU 1-5000 H 34 ACCELERCMETER DELL & HCWELL 4-202-0001 24292 6M VERT. TABLE 444 DU TRACKING SPECTRAL DYNAM SD131L 56/250 DU 2 CHANNEL Si FILTER 52 DYNAMIC ANALYZER SDECTRAL DYNAM SD120/122L 1420 BU ANALOG 54 X-Y RECORCER HEWLETT #ACKAR 70059 1734A01580 DU ANALOG 55 X-Y RECCRDER HEWLETT-PACKAR 7045A 13e BU ANALCG CANS.

57 CP.

AMA.

MANIFCL ANALOG DEVICES 194 e5 ACCELERCMETER DELL & HCWELL 4-202-0001 19742 6M HrRI-TADLE e7 CCNTRCLLER TEAM 1522 104 6M MCRI. TAL.E 2

6M VERT TADLE e5 CCNTROLLER SWRI 450-O!!11 1Y PEDICD/FREG.

HEWLETT-PACKAR 5512A 4442 1204 1Y DATT PWR El CCUNTER 35 DIGITAL MULTIMET WESTON 1716A01910 1Y 4 1/2 DIGIT 3466A se DIGITAL MULTIMET HEWLETT-PACKAR 102 6M W/ TEAM 1522 1564 57 DIGITAL SERVC DI TEAM 1C; AMPLIFIER ENDEVCC 2721A DJCS 3U CHARGE 104 C3CILLCSCCPE TEKTRONIX 3111 D131937 1Y STCRAGE ICS SCCPE PLUG-IN TRKTRONIX

'5A14N 3074473 1Y 4-CHAN 10e SCCPE PLUG-IN TEKTRCNIX 5A14N D074477 1Y 4-CHAN

C7 SCCPE PLUG-IN TEKTRCNIX SD12N DO77663 1Y DUAL TIME DAEE

CV MEGGER ASSCO. RES.

2001 5:17 l 's 500 VDC ic2540:016 2U 4-CWAN

.15 'sDE *ECOc0E8 wEWLE?' 8ACK 3064A n

116 pCWER SUPDLv KEPCC ATE 150-7M F32789 FC 150V-7A

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11E DIGITAL TEMP CMEGA 2166A 2000547755 1Y TYDE K 119 ENVIRON CHAMDER TENNEY TR-40 102:5 6M TEMP / HUMID 120 C4EN OESPATCH LDS 1-69 1CE013 FC ACO DEGREES

E3 CAMAC STANDARD ENGR. PS3742 2315 1Y HI-DAV EYSTEM

IC CCMPUTER CEC 11/23 WF17625 FC HI-GAY SYSTEM 13: TERMINAL TEKTRCNIX 4006-1 DC36557 FC GRAPHICS 132 HARD CCPY TEnTRCNIX 4631 3164635 FC TmERMAL 152 DIGITAL TEMA CMEGA 199KC-A 25e94 1Y WITH #120 170 AMPLIFIER ENCEVCC 27213 CE 15 DU CHARGE 135 RECCRLER CMEGA 141 303OC2 1Y 1-CHAN

s? r-Y RECORCER HEWLETT #ACKAR 7044D 2129AOCB31 DU ANALCG 13C DIGITAL MULTIMET HEWLETT-P ACKAR 34ebA 1716A17650 1Y 4 1/2 DIGIT 1:0 TAFE REOCROER TEAC XR-50 17:399 iv AC/DC

? RECORDER SCLTEC 5L47 3C70074 1Y 15-CNAN

Se OIGITAL FLLAE 77 339314o 1Y HANO MELD In addition the following equiDment was also used:

OSCILLOSCOPE TEKTRONIX 455 B055592 lY 2-CHAN

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3M135A FC DAYTON GEARMOTOR & CAM ASSEMBLY 10 AMP FC SwRI VARIAC & DC POWER SUPPLY ELECTRODYNAMIC UNHOLTZ-DICKIE 56 203 FC SHAKER AUTOMATIC INTEGRATING PIC0 AMMETER HAR$ HAW 2000-B 1234 lY THERM 0LUMINESENCE DETECTOR HARSHAW 2000-C 258 1Y p

V iLD CHIP 005IMETERS HAR$ HAW 5

The Harshaw Automatic Integrating Picoammeter and Thermoluminescence

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Detector are routinely calibrated in accordance with the Fuel and Lubricants Research Division calibration procedures.

B The additional equipment listed in Table 5.1 is covered under the current revision of the Southwest Research, NQAPM.

7.0 TEST METHOD i

7.1 General The test item identified in Section 2.1 was aged in accordance with the test plan, reference 3.7 and the qualification plans, references 3.8 through 3.12 to a 40-year end of service life condition plus 10%

The testing used to precondition the item prior to margin (44-years).

The data for seismic testing is described in Sections 7.2 through 7.6.

state-of-the-art determination of synergistic effects from reference 3.18 shoss that these effects are not relevant for organic materials at radia-rads. Therefore for the tests described in 4

tion dosage levels below 10 Sections 7.3 and 7.4 the synergistic effects are not relevant to this test The seismic test procedure is described in Sections 7.7 through item.

Subsequent to seismic testing an environmental extremes test was 7.10.

A margin of +10% was added to conducted and is described in Section 7.11.

the applicable test parameters for all tests described above as called for in the test and qualification plans. A photograph of the test item taken prior to any testing is shown in Figure 9.1.

qV 7.2 Functional Checks The test item described in Section 2.1 was given a visual inspection upon receipt at SwRI which was witnessed by SwRI Quality The visual inspection verified that the item was not damaged Assurance.

during shipment to SwRI. The item was tagged with an acceptance tag and the findings of the inspection recorded on Q.A. form 21A. Subsequent to the receiving inspection and prior to testing a baseline functional check The baseline and post-test functional was performed on the test item.

checks were complete functional checks which were performed using the same test procedures in order to provide a comparison of the test item's func-tionality from the pre-to post-test condition. The data from the pre-and post-test functionals was used to determine if any degradation of the item's essential performance requirements had taken place. During and af ter each test partial functional checks were performed on the item in order to insure the item was still functioning properly. For many of the tests the post-test functional for one test was used as the pre-test c

All of the functional check procedures used functional for the next test.

In addition are described in Appendix B of the test plan, reference 3.7.

if the test item was monitored during a particular test, such as seismic, the functional check and monitoring will be covered in that section of The results of the post-test functional check at the this test report.

completion of all testing will be covered in the Results and Conclusions The Laboratory Data Logs in Section 12.0 in Section 8.0 of this report.

6

1 l

contain a chronological listing of all testing and function'l checks O

performed.

7.3 Thermal Aging The thermal aging of the test item listed in Section 2.1 was The tem-performed using a Despatch LDB 1-69 thermally controlled o The output of the Omega an Omega 199KC-A digital temperature indicator.

199KC-A was recorded using an Omega 141 strip chart recorder to provide a The test item was aged hard copy of the temperature during thermal aging.

at +125'C for 108 days to a simulated end of service life condition of The test item was not operated 40-years plus 10% margin (44-years).

during thermal aging and received a functional check prior to and at the The functional check at the conclusion of conclusion of thermal aging.

thermal aging indicated that the test item was functioning properly with A sample from the strip chart r narder used to mon-no degradation noted.

itor the temperature while thermally aging the test item is shown in The thermal aging calculations used to determine the time and Figure 7.1.

temperature used are given in Appendix C of the test plan, reference 3.7.

The methodology used to justify the time-temperature relationships is covered in the qualification plans, references 3.8 through 3.12.

7.4 Radiation Aging The test item identified in Section 2.1 was irradiated in the SwRI High Level Radiation Effects Facility using a number of Cobalt 60 sci.Irces which are arranged to give an even dosage rate to the test item.

O The test item was irradiated for 2.25 hours2.893519e-4 days 0.00694 hours 4.133598e-5 weeks 9.5125e-6 months and received an average dose The dosage received by the test item was measured 4

of 1.2 x 10 rads.

using Natural Lithium Fluoride Chip 00simeters and a Harshaw Automatic The test item Integrating Picoammeter and Thermoluminescence Detector.

was given a functional check at the conclusion of the radiation test and was found to be functioning normally. A photograph of the test item (indicated by arrow) being irradiated is shown in Figure 9.2.

7.5 Operational Aging The test item identified in Section 2.1 was operationally aged A Dayton gear motor and in accordance with the test plan, reference 3.7.

cam assembly were used to mechanically actuate the switch at a rate of 12 One set of the switch's normally open contacts were cycles per minute.

connected in series with a Kepco ATE 150-7M DC power supply set at 125 volts and a Potter & Brumfield MDR 138-8 relay as a load when the normally c

open contacts were closed. The pressure switch was operated for approxi-The test item mately 8.4 hours4.62963e-5 days 0.00111 hours 6.613757e-6 weeks 1.522e-6 months for a total of 6,120 cycles of operation.

functioned normally at the conclusion of the operational aging. A photo-graph of the test setup used to perform the operational aging is snown in Figure 9.3.

AV 7

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~~llorizontal Axis Qi by Cp Sliaker Control Monitor l'rel iminary 34 llands, 1/6 Octave Analog Run Data llorizontal Axin Stiakor Y~~

~~Tape Recoraler Vertical Axis~~

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~~linker Contro)~~

~~Vert l.~~

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llorizontal Axis gi Vertical Axi*

~~34 Hantis, 1/6 Octave l~~

~~Vertical Axi.s~~

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~~- Vertleal Motion Adjiistment figure 7.2 O!!E and SSE shaker table drive.~~

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~~The test data which was retained in the computer at the time of testing.~~

~~multiple damping plots were produced at values of 0.5, 1, 3 and 4% for the O"~~

~~0BE level tests and values of 0.5, 1, 2 and 4% for the SSE level tests.~~

~~p During the seismic qualification test the item was continuously monitored on an oscillograph capable of resolving a two-millisecond pulse.~~

~~The The circuit used to monitor the test item is shown in Figure 7.3.~~

circuit consists of a DC power supply set at 140 volts in series with the switch's normally closed contacts a 560 ohm load and a one ohm sense The normally closed contacts were monitored on oscillograph resistor.

~~The switch's thermal sensor was kept at channel #1 during the tests.~~

ambient temperature so that the normally closed contacts should not change state during the tests. Figure 7.4 is a sample oscillograph record from test SSEYZ1 which shows the switch's contacts did not change states indi-Figure 7.5 is a sample calibra-cating normal operation for the switch.

tion record which shows the off (low) and on (high) conditions indicating how the trace would have deflected had the contacts opened during the The bottom trace in Figure 7.4 is the horizontal acceleration time test.

~~The switch's contacts history which shows when the seismic test occurred.~~

~~There was did not change states for any of the seismic tests performed.~~

~~no physical damage as a result of the seismic tests performed.~~

~~7.11 Environmental Extremes Test Subsequent to seismic testing and post-seismic functional check-The test item was out, an environmental extremes test was conducted.~~

~~mounted as described in Section 7.7 and monitored using the same circuit sho a in risure 7.3.~~

~~The test item es pieced in en enviroementei chember O~~

and exposed to an environment of +153*F and 95% RH for a period of two hours after conditions in the chamber had stabilized. The monitoring cir-cuit was energized continually throughout the test and was monitored The item was monitored during the first and last 10 minutes of the test.

~~using the same oscillograph and channel setup as used for the seismic The test item functioned normally while being monitored during testing.~~

~~the environmental extremes test. A photograph of the test chamber and test setup is shown in Figure 9.12.~~

~~7.12 Summary of Seismic Tests Performed Table 7.1 lists a summary of the seismic tests performed with a~~

+10% margin added to the RRS and with damping values of 2% for the OBE level runs and 3% for the SSE level runs. Table 7.2 lists the multiple damping plots produced from the run information which was retained in the computer at the time testing was performed. The multiple damping plots e

~~show damping values of 0.5, 1, 3 and 4% for the OBE level runs and values In addition for the curves of 0.5, 1, 2 and 4% for the SSE level runs.~~

shown in Figures 11.1 through 11.26 the upper (enveloping) trace is the Test Response Spectrum (TRS) and the lower trace is the Required Response For the multiple damp-Spectrum (RRS) with +10% margin already included.

~~ing curves of Figures 11.27 through 11.52 the curves are shown in the same order as the damping values indicated at the right side of the plots.~~

~~OG 12~~

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~~O Test llem 516-47191-1 Honnally Closed Contacts Load 560 0 140 VDC Temperature Sensor at Anbient~~

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~~Oscillograpli Channel #1 3g~~

~~-O Circuit used to monitor the item's functionality figure 7.3 during seismic and the environmental extremes test.~~

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Table 7.1.
Summary of Seismic Tests Performed With +10% Margin Added to the RRS Axes of Test Level Horizontal Vertical Excitation and Number TRS TRS a
Y-Z OBE #1 Fig. 11.1 Fig. 11.2 Y-Z OBE #2 Fig. 11.3 Fig. 11.4 Y-Z OBE #3 Fig. 11.5 Fig. 11.6 Y-Z OBE #4 Fig. 11.7 Fig. 11.8 Y-Z OBE #5 Fig. 11.9 Fig. 11.10 Y-Z SSE #1 Fig. 11.11 Fig. 11.12 X-Z OBE #1 Fig. 11.13 Fig. 11.14 X-Z OBE #1A Fig. 11.15
' Fig. 11.16 X-Z OBE #2 Fig. 11.17 Fig. 11.18 X-Z OBE #3 Fig. 11.19 Fig. 11.20 X-Z OBE #4 Fig. 11.21 Fig. 11.22 X-Z OBE #5
. Fig. 11.23 Fig. 11.24 X-Z SSE #1 Fig. 11.25 Fig. 11.26 O
Table 7.2.
Summary of Multiple Damping Plots Axes of Test Level Horizontal Vertical Excitation and Number TRS TRS Y-Z OBE #1 Fig. 11.27 Fig. 11.28 Y-Z OBE #2 Fig. 11.29 Fig. 11.30 Y-Z OBE #3 Fig. 11.31 Fig. 11.32 Y-Z OBE #4 Fig. 11.33 Fig. 11.34 Y-Z OBE #5 Fig. 11.35 Fig. 11.36 Y-Z SSE #1 Fig. 11.37 Fig. 11.39 X-Z OBE #1 Fig. 11.39 Fig. 11.40 X-Z OBE #1A Fig. 11.41 Fig. 11.42 X-Z OBE #2 Fig. 11.43 Fig. 11.44 X-Z OBE #3 Fig. 11.45 Fig. 11.46 X-Z OBE #4 Fig. 11.47 Fig. 11.48 X-Z OBE #5 Fig. 11.49 Fig. 11.50 X-Z SSE #1 Fig. 11.51 Fig. 11.52 O
16
7.13 Analog Tape Log Table 7.3.
Analog Tape Log a
Tape Speed 3-3/4 ips Tape Channel Designation and Accelerometer Location Channel 1 - AH, Horizontal Table Accelerometer Channel 2 - AV, Vertical Table Accelerometer Data Tape Counter i
25 Sine Wave Calibration, 1 g peak 0 10 Hz OBEYZ1 94 151 OBEYZ2 206 OBEYZ3 260 OBEYZ4 316 OBEYZ5 374 SSEYZ1 446 OBEXZ1 512 OBEXZ1A 576 OBEXZ2 636 OBEXZ3 696 OBEXZ4 754 OBEXZ5 SSEXZ1 822 8.0 RESULTS AND CONCLUSIONS 0
Complete laboratory data notes are given in Section 12.0.
These include the notes from the thermal, radiation, operational and vibration aging notes as well as the seismic and environmental extremes test notes.
The Also included are the notes from all functional checks performed.
data logs are a chronological listing of all testing performed.
The test item received thermal, radiation, operational and vibration aging as required by the test procedure, reference 3.7.
The test item was successfully aged to a 40-year end of service life condition plus 10%
margin (44-years).
Resonance searches were performed in the frequency ranges of 10-200 Hz and 1-35 Hz for each of the item's three principal axes. There were resonances recorded in the X and Z-axis at 56 Hz and 173 Hz respectively.
The transmissibility plots for the X, Y and Z-axis resonance searches are shown in Figures 10.1 through 10.6.
c The aged test item underwent a seismic qualification test with a +10%
margin added to the RRS. The test item was monitored before, during and after each seismic event with no indication of abnormal operation for any of the tests conducted. The horizontal and vertical table motions for all random excitation tests are given in Section 11.0. Also given in Section 11.0 are the multiple damping plots produced from the test data retained in the computer at the time of testing.
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Subsequent to seismic testing the item underwent an environmental The item functioned normally while being monitored during
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the environmental extremes test.
A post-test functional check was performed at the conclusion of all testing and the results of this test were compared against the baseline functional check.
It is our conclusion that the item identified in Section 2.1 did pass the required qualification tests when tests were performed in accordance with the test procedure, reference 3.7 and the qualification plans, reference 3.8 through 3.12.
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figure 9.10 Accelerometer location for the X-axis resonance search, i
accelerometer on front of switch as indicated by arrow.
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Figure 9.11 Accelerometer location for the Y-axis resonance search, l
accelerometer on side o.f switch as indicated by arrow.
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SECTION 10.0 i
RESONANCE SEARCH DATA i
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100 150..
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..L, 200 frequency,liz Figure 10.1 Resonance search from vibration testing, Z-axis, accelerometer on top of switch, input 0.1 g's peak, sweep 2.0 octaves / minute.
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60 100 150 200 f requency,11r Figure 10.2 Resonance search from vibration testing, X-axis, accelerometer on front of switch, input 0.1 g's peak, sweep 2.0 octaves / minute.
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$0 100 150 200 f requency,112 Figure 10.3 Resonance search from vibration testing. Y-axis, accelerometer on side of switch, input 0.1 g's peak, sweep 2.0 octaves / minute.
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ll lllI' lllllI ll ll ll-lll lll '}![IIl'll } l llll Yll (( \\ff ll'ljll 'IIjl [I! l lIl $l Fl ( 1 [ fl il ] 1 g . t.. .t . J O E o 4 3 l2 7 3 Ti NIIIIIII II lIlIl l ll li-b l l1 0'- 5 10 15 20 25 30 35 FREQUEllCY, HZ Figure 10.4 Resonance sea; ch, Z-axis, accelerometer on top of switch, input 0.2 g's' peak, sweep 1.0 octaves / minute. 8' t 6 J 3 s A $4 I 2 j 2 7;T 7
~~o. L Mllij ll lilli I l~~
I I ll l l l lli l 5 10 15 20 25 30 35 FREQUENCY, HZ Figure 10.5 Resonance search, X-axis, accelerometer on front of switch, input 0.2 g's peak, sweep 1.0 octaves / minute. 0 l{l '][' 6 = E O ~ 5 3 2 c -a m 0 lISb A! l1b .1 II I 5 10 15 20 25 30 35 FREQUENCY,llZ Figure 10.6 Resonance search, Y-axis, accelerometer on side of switch, input 0.2 g's peak, sweep 1.0 octaves / minute. 28
_w -e ~ -- k --sJ= A. a.-s Awa,. s a-- ..uM-nam A a-aaLAm i 0 i e i 4 6 6 { i 1 .i i 1 SECTION 11.0 RESPONSE SPECTRUM DATA O 4 1 } I i 1 l, i 4 1 ~ l i O 29 i l --,-n-,. n-.,-n,--,-----=-,,-_-,,,-.-.._
Figure 11.1 Run OBEYZ1 AH O >s 10 BETA = 0.020 4 I ZFA= 2.018 -;
~~a r.~~
~~r. i 1 4~~
~~10 i,~~
E i ~ 0 H 0 le r 4 i / G r .a 10_1 i gg 10 10 ' I G FREQUEtiCY - H: O i Figure 11.2 Run OBEYZ1 AV .4; to- ....6 BETA = 0.020 i 2P 5.= 4.23" a ~ i .1 i r r .1 t, F t. 0 3 10 r 1 1m G .r P 10,, g 0 1 39 10 10 ' FRE00EllCY - HZ 30 1 I c -,.. ~.- - -,,,, - -. ~ -,,. -,, - ~ -, - - - - -.... -.,,,. - - -.... -,,
Figure 11.3 Run OBEYZ2 AH 10- .....ri ....4 p E BETA = 0.020 3 Y
~~PA= 2.096 j c~~
~~T ~ e F t~~
10*
3 .g r r ~ 7 I ~ ) C N 0 10 / .~ G E I t e 10.g I 0 1 10 10 10 ' F:.EQUEHCY - H: O .i Figure 11.4 Run OBEYZ2 AV 10-g EETA= 0.020 3 5r PA= 4.040 ) ~ 4 C e t ] I 10* f ~f 4 F \\ \\ ,i 4 r; p it 0 J 10 / 44 e G f 3 1 10 3 -) 0 'e 1 10 - 10 5""EnCY - HI FP. 1
Figure 11.5 Run OBEYZ3 AH O 2 10 BETA = 0.020 ? ,5 ZFA= 2.164 i t s e. 7 10* c / N .l I s ) 0 1 H t r,0 43 / G -\\ ,0_t -i 1 10', 10 10 - F:.EGUEtiCY - H: O Figure 11.6 Run OBEYZ3 AV ...'.4 !Q BET 4= 0 020 i E ZPA= 4.333 r .4
~~10,'~~
a 4: F P C T t a g 'd ti 0 4 a-t0 r G P r. .g O le* to ' . to FREQUEtiCY - HI 32
Figure 11.7 Run OBEYZ4 AH O 10' ..>,g BETA = 0.020 m 2 pas 2.272 e 1 0 1 = I 3
~~10 r~~
2 ~5 P e i, h i 0 H 3 10 n ~ G 1 ~, a ,,,I ,0.; 1 10 ' 10'# 10 FFE00ENCY - HZ AV Figure 11.8 Run OBEYZ4 AV 10' ....3 EETA= 0.029 i e PA= 4.182 q a C. I e F ] ? 10 ' ? g Y m ,L i 9 s n ~ I r. 3 10'3 ai e r G V. 10.g 2 1 0 10 10 10 FREQUENCY - HZ 33
.] 1 1 Figure 11.9 Run OBEYZ5 AH ) \\ -...i >'.~r>; + 10-4 g ~ SETA= 0 020 t 5-2PA= 2.257 ~ t E ?. l. h 10 [ i R i I '. @Mf 'd N 10 1 0 ~ r J _g 0 g 10 10 10 ' FREGUENCY - H: i. O Figure 11.10 Run OBEYZ5 AV ..i>, t to- ...c., r EETA= 0.020 4 i e IPA = 4 055 i r r. e 0 4 j h 101 ? 4 1 f [ 5 = i J A ( s } u 10 3 0 M f t 0 10.g 4 1 10 10 10 ' FPEQUENCY - HI 34 a i
J i Figure 11.11 Run SSEYZ1 AH w, BETA = 0.030 ZFAs 2.487 t ~ s. l E F
~~10 *,,~~
~~7 3 e i t i f. [ "i. L s ,,J H s 0 T 10 i - l.: i G l 5 t 10-1 [ 0 I i 10 10 10 FREQUENCY - HZ l t jlO 1 l Figure 11.12 Run SSEYZ1 ,AV l 10' .i.5 EETA= 0.030 4 E~~
~~PA= 4.406 i~~
4, e I w i 4 5 e ? -l ~ 1 10 \\ \\ g m q, ti ,00 s 4 i ( e i 2 5 m 1 i t s e f e e f e e_e. .a. ". j O 10 io 10 : e 1 ,,.EQuEnn - s: 35 i i . - _ ____..._..~
f Figure 11.13 Run OBEXZ1 AH r.r 4 ....3 0 h EETA= 0.020 ; IFks 2.174 -j .t i h 10I I f I rr r. ~. b [ s a i .nB i G P 10~,' 10 10 ' 10 - 0
~~FEQUENC'.' - HZ~~
~~' O Figure 11.14 Run OBEXZ1 AV 10' ..c., p BETA = 0.020 F 2P4= 3.972 0 r 4 d >y r I 1 s~~
~~10 r~~
+ F ~ A E. -t r a3 i = c 0 ] 9 0 10 .g / C 1 O .4 10 10 .10 '" 0 1 1 l F:EQUEHCY - HZ l 36 i I
s Figure 11.15 Run OBEXZ1A AH O i 10- .4 ip I BETA = 0.020 i ZPA= 2.511 { a P C Y LY ? ) 4 x i g g H I6 ? l / ? G .t 10 10 10 o g 1 FREQUENCY - HZ O Ficure 11.16 Run OBEXZ1A AV 10' ...g 4 ..43 BETA = 0.020 ? r 2PA= 3.742 n 6 W C 1, 0 1 i:
~~h. 10 a~~
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~~t to~~
~ FREQUEtiCY - HZ 37
Figure 11.17 Run OBEXZ2 AH ++i>; 10-BETA = 0.020 .....-ri 'oA= 2.279 ; 4 i C C I I I ) 10 e E I a E 1 L ~ b ) } te 0 7 10 7 .s f 3 G E 9 -1 ] ..] ,0_, 0 1 2 10 gg 10 FREQUENCY - H O Figure 11.18 Run OBEXZ2 AV 2 10 BETA = 0.020 ZPA= 4.260 1 } A C C 1 1 10 E i R ? 3 A f ~ 1 t 0 i H 0 9 10 i /
~~l i~~
r ei 'A n P W n ,_.e.,_! i.e...i. .g 2 2 O is 1e 1e ~ FREgEHCY-HZ
e4 ure 11.19 au, osexz3 As O 9 2 ..i.: 10 ....i BETA = 0.020 i ZPA= 2.334 r A C E b 101 7 r i R A I 5 2 I f s d 0 H 0 10 i G ~ ' ' ' ' '~'~ ' ' ' ' ' ~ ' ^ 10-I 0 1 10 10 10 ' FREGUENCY - HZ O Figure 11.20 Run OBEXZ3 AV 10- ...i BETA = 0.020 E ZPA= 3.806 1 A C C E h 101 1 f i x E A k 7 I 0 g 0 4 10 7 / g ~ ~ m i.v.v.e. 1 O le.g 0 I 2 10 10 10 FREQUENCY - HZ i 39 i ~,..,. - - -
Q Figure 11.21 Run OBEXZ4 AH ~''; 10- .>i.ii BETA = 0.020 i i ZPA= 2.506 C. p .u C E i.: h 101 r R E 2 A. n ~ I ~ 0 H 10 [ ] 0 G E 10 3 0 1 2 10 10 10 FREQUENCY - HZ O Run OBEXZ4 AV Ficure 11.22 ig-BETA = 0.020 j 2PA= 4.040 g 5 L. C. i l L 1 7_ 10 \\
~~i V~~
~~I. I c c H 10 I ) / i j W W i e~~
* + i.*-
,,,.1 q 'O 2 O i 10 1e 1e e FREQUENCY - HZ 40
Figure 11.23 Run OBEX 25 AH 2 gg BETA = 0.020 f IPA = 2.535 g A 7 C 7 C E h 10 i j 1 R 2 A l I [ E 0 N 0 3 10 i a. 4 G I 10.g[ 0 i 2 28 gg le FREQUENCY - HZ O Figure 11.24 Run OBEX 25 AV
~* ~a:
~ 6 a 10- .iri h BETA = 0.020 i E ZPA= 3.962 11 A C C E 1 1 10 E R \\ a T ? I I ~ 0 g 0 7 10 r / I r G r su .4 4 0 10.g 2 0 1 10 10 10 FREQUEHCY - HZ 41 1
Figure 11.25 Run SSEXZ1 AH 9 +' 10-m BET > e 43s : ZPM 2.535 C 7 h 10' r 1 T I ~ 0 M ti 0 10 e I G _g 0 1~ 2 I 10 gg 10 FREQUENCY - HZ O Figure 11.26 Run SSEXZ1 AV 10' ....ii BETA = 0.030 ZPA= 4.192 ~ a ~ C C g 1 ':: 10 2 ? .2 7 ~ 6 n 0 10 y / 4 ~ t -1 1 10_t i 0 1 2 10 10 10 O. FREQUENCY - HZ 42 l 1
Run OBEYZ1 AH Ficure 11.27 O 1@* i8 e 6 6 '6'&'6'l 3 J ~ A T 2PA= 2.02 C 7 BETA = 0.005 0.010 C 0.030 E 1. 1 0.040 ,E 3 10 P .A i A ? ~% 7 i T a N 3 10 3 -j .a l'_1 ) s 0 1 2 10 10 10 FREQUENCY - HZ O Figure 11.28 Run OBEYZ1 AV Ice r .I i A ZPA= 4.24 C 7 BETA = 0.005 0.010 c 0.020 I 1 0.040 ~4
~~10 l-e j~~
~~P. E 3 C ~ 14 e 10 -/ 3 ?/ j C E~~
J
-1 O e i 2 1e 1e te FREQUENCY - HZ 43
Figure 11.29 Run OBEYZ2 AH p 'd 10'
>ag 4
4 >i4i cPA= 2.10 4 C 7 BETA = 0.005 0.010 C 0.030 E 0.040 L 10'i a r e. i R A 7 0 -3 t4 0 ? 10 t 3 t. G =q g P 3 0 1 2 10 10 10 FREQUENCY - HZ O Figure 11.30 Run._0BEYZ2 AV 6 6 i.ig .4.i-10' 1 ~ E ZPA= 4.04 A ~ C 7 BETA = 0.005 0.010 C 0.030 E 0.040 L 1 E g 10 4 2 I f. i ~ i ~ l t 0 ti 0 10 7 2 g
~~5..~~
10-1 f 0 1 2 10 10 10 FREQUEHCY - HZ 44 l 1 i
i l l Figure 11.31 Run OBEYZ3 AH 10, .....i .~ 'T ZPA= 2.16 A C 7 EETA= 0.005 0.010 C 0.030 E 0.040 L
~~0'1 E~~
H F. a ? i I 0 p 0 10 G p ,,..a g.t O 10 10 '- 1 10 FREQUENCY - HZ i O Figure 11.32 Run OBEYZ3 AV 10' ...i A T ZPA= 4.33 7 C 7 BETA = 0.005 0.010 l C 0.030 i i E 0.040 L 1 19 ) 5 7 l T T I T, I I e o n 0 10 / W W d W m ' ' ~ ' ' ' ' ' ' ~ ' ' 0~I O O 1 2 10 10 10 FREQUENCY - HZ 45 I
Figure 11.33 Run OBEYZ4 AH 10' 4 +.c. ..i.i 1 cPA= 2.27 A C 7 BETA = 0.005 0.010 C 0.030 E 0.040 L 1 10 -e 1 R A ~ T 0 H 0 10 / -^ A: e" 10.g 1 2 0 10 10 19 FREQUENCY - HZ O Figure 11.34 Run OBEYZ4 AV 10-4.. D ~ A ZPA= 4.18 ~ C I BETA = 0.005 0.010 C E 0.030 0.040 L.pl E p e i 7 7, s 0 p 9 10 ea _t 0 1 2 10 10 10 FREQUEHCY - HZ 46 ) 1 l I i i l
Figure 11.35 Run OBEYZ5 An o 10- ...ia b 2PA= 2.26 2 4 C BETA = 0.005 C 0.010 0.030 E L 1 0.040 10 y E R A r P ~_ 0 -3 H 0 10 r f 3 G r I 1 10-g 0 1 2 10 10 10 FREQUENCY - HZ O Ficure 11.36 Run OBEYZ5 AV o 10- ...ia .>ri A 7 2PA= 4.05 C 7 BETA = 0.005 0.010 C 0.030 E L 1 0.040 10 -c E C A ~ ~ T, a i 4 0 c H 4 0 10 / 2 G r 4 v., t.t e...n_ 10.{ 0 1 2 10 10 10 FREQUEHCY - HZ 47 .,,,.m ,,y.- ,,ee- ,.w,.e ,,,,y --~r-r-----, -,.-..--..-+-,m ,q 9,9 y,-99q.n9--we .v y9.pg,, -g
1 i l l Figure 11.37 Run SSEYZ1 AH O~ 10- . s s >; s.sss a a a s F ] c 7 IPA = 2.49 C BETA = 0.005 0.010 C 0.020 E 0.040 ,0.! L r R, i F 0 H 0 10 i G _g 0 1 10 10 10 ' FREQUENCY - H:' Run SSEYZ1 A.V Ficure 11.38 10- .....i ~ A I ZPA= 4.41 ~ C BETA = 0.005 0.010 C 0.020 E 16.1 0.040 L 3 4 r e: C 3 F. i O i, ( e n 0 , 10 i C-C D 8 A D ' ' ' ~ ' ~ ' ~ ' 10"I ' ' '~'~'~ 0 I 2 10 10 10 FREQUEHCY - HZ 48 I
Figure 11.39 Run OBEXZ1 AH O 2 10 b ZPA= 2.17 A C T BETA = 0.005 0.010 C 0.030 E L 1 0.040 10 E R ? I A 7 7 I 0 N 0 10 l-i / C r 7 10-I ~ ' ' ' I O 1 10 *- 10 10 FREQUENCY - HZ O Figure 11.40 Run OBEXZ1 AV 10-E ZPA= 3.97 A C 7 BETA = 0.005 0.010 C 0.030 E 0.040 L Inl E R A i-T T I 1 0 c n 0 ~ 10 l-r -1 ._t_I f f i.I _ f _t_t _ eI e t t t 9 e 10 ' 8 I 2 10 10 10 FREGUENCY - HZ 49
) 4 Figure 11.41 Run OBEXZ1A AH 2 i O 1e ZPA= 2.51 ~ A SETA= 0.005 ~ C 0.010 C 0.030 E 0.040 1 L. 10 y R L p L 6 I 0 -~ N 0 10 i G = ~ .....,.i _t 1 2 0 10 10 10 FREQUENCY - HZ O Figure 11.42 Run OBEXZ1A AV 10' ...i5 ~ A ZPA= 3.74 ~ C BETA = 0.005 ~ 0.010 C 0.030 E L 1 0.040 10 R A r ~ ~ T, = Q = n c F i r. m n ' ' ' ~ ' ' ' ' ' '~'~'~' 0"I O 1 O 10 10 10 - FREQUEHCY - H7. 50
Figure 11.43 Run OBEXZ2 AH O 10' ..ii+ F ZPA= 2.33 2 g C BET A= 0.005 0.010 C 0.030 [ 10 t 0.040 -1 R 2 A s- ~ T ~ I ~ 0 a H 0 10 } G F 3 ..,..I 10_t 0 1 2 10 10 10 FREQUENCY - HZ O Figure 11.44 Run OBEXZ2 AV 10, i i >: 4 6 ....c3 .C 4 g ZPA= 4.26 C 7 BETA = 0.095 0.010 C j 0.030 E t-1 0.040 '9 E R A F 2 T [ I ( 0 ti 0 ~ 10 G [ 10 g 0 8 2 10 12 . te FREGUENCY - HZ i 51 i
Figure 11.45 Run OBEXZ3 AH 10- ~ A ZPA= 2.38 C BETA = 0.005 4 0.010 C 0.030 E 1 0.040 L. 10 H c R ? a T [ I 0 - ~ N 0 10 .~ G E ..,,,.i _g 0 1 2 10 10 10 FREQUENCY - HZ O Figure 11.46 Run OBEXZ3 AV 10,- i.3 F i A 7 2PA= 3.81 C 7 BETA = 0.005 0.010 C 0.030 E 1 0.040 L. 10 P i A F i T i, O H 10 1 / i G .t P g.g 0 1 1 18 10 10 ' FREQUENCY - H i 52 i ) r-- ,-s p,,-._p- --im w., ,..---e,-- =9-.., e*-%-.,ew ,----t-.-,-.m...e -.-r
i Figure 11.47 Run OBEXZ4 AH 10- ++c. ~ F ZPAs 2.51 i g BETA = 0.005 j C 0.010 C 0.030 E 0.040 t t y 10 = ~ E. h A E i T I [ 0 H 10 } 0 f C E. i i-10~g 0 1 2 10 10 10 FREQUENCY - HZ O Figure 11.48 Run OBEXZ4 AV d 10' 4 i.7 C Z?As 4.04 a C EETA= 0.005 0.010 C 0.030 r I 0.040 i 3
~~10 y~~
N 3 v' .a A r 6-T r_ c I 9 H 0 ~d 10 F ? 3 E -? r_ ~3 O 1,e 10 10 1 2 FREQUEHCY - HZ 53
Q Figure 11.49 Run OBEXZ5 AH 10 g T ZPA= 2.54 C 7 BET 4= 0.005 0.010 c 0.020 = [ 10 0.040 t y e a R f p b H 0 / g 10 i G 3 ~ ,,_1 0 1 2 10 10 10 FREQUENCY - HZ O Figure 11.50 Run OBEXZ5 AV o 10- ..ia F i A T ZPA= 3.96 7 ~ C 7 BETA = 0.005 0.010 C 0.030 E L 1 0.040 10 e P A ~ ~ T I c o tt 0 10 7 f -i G E S _1 O 10 10 LO ' 0 1 FREQUENCY - HZ 54
Figure 11.51 Run SSEXZ1 AH 10 . -...ia E ZPA= 2.54 ] C 7 BETA = 0.005 0.010 c 0.020 E i L 1 ~ 10 E I T 0 H 0 m 10 ~ / 4 G i-10_t J 0 1 2 10 10 10 FREQUENCY - HZ O Fic.ure 11.52 Run SSEXZ1 AV 10- .......3 b ZPA= 4.19 7 c. ~ C BETA = 0.005 0.010 C 0.020 E O.040 L 10' g E R 4 A e 1 T I 0 H 0 10 / 2 C M f T f f f f - t t! f f f 9 - f - f f "e O e 2 2 1e 10 10 FREQUEHCY - HZ 55 l -,7-r e

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1 m , a 0 1 1 l t 1 SECTION 12.0 SwRI LAB RAT RY DATA LOGS O 1 I 1 l \\ I O 56 \\
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ML20137Z827

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