ML20217A854

Test Plan 70, Model 660 Series Type B Transport Tests

ML20217A854
Person / Time
Site:	07109033
Issue date:	09/17/1997
From:	AMERSHAM CORP.
To:
Shared Package
ML20217A852	List: ML20217A848 ML20217A854
References
PROC-970917, NUDOCS 9709230024
Download: ML20217A854 (87)

Text

SENTsNEL TEST PLAN NO. 70 iTEST PLAN COVER SilEET TEST TITLE:

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ENGINEERING APPROVAL:

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QUALITY ASSURANCE APPROVAL:

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REGULATORY AFFAIRS APPROVAL:

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Ms. Cathleen Roughan -

Regulatory Affairs and Safety Manager Amersham Corporation 40 North Avenue Burlington, MA 01803

SUBJECT:

Review of Amersham Test Plan #70, dated 9/17/97

Reference:

Letter, Cathleen Roughan, Amersham Corporation, to Gary Clark, Packaging Technology, Inc., dated Juno 10,1997.

Dear Ms. Roughan:

In accordance with the referenced letter, PacAaging Technology has reviewed the subject test plan for the Model 660 package, Based on our independent review, we have determined that the test plan provides the required details to ensure that packaging testing performed in accordance with this test plan will comply with the requirements of Title 10, Code of Federal Regulations, Part 71 (10 CFR 71),

Very Truly Yours, Packaging Technology. Inc.

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Gary l.. Clark, P.E.

Vice President i

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SENTINEL Test Plan #70 Amersham Corporation September 17,1997 Burlington, Massachusetts Pagei Contento Li st o f Fi g u re s a n d Tab l e s................................................................................................ I y Amersham Test Plan #70 1.0 Tra nsport Pac k a ge O ve rvie w.m.....m........m....................mm........

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omooo momm 2 3.0 Syst e m Fail u res of I n terest........................................................................................ 3

3. I S hield M a ve me n t or Fract ure.......................................................................... 3 3.2 Loc k A s se mbly S c re w s.................................................................................... 3 3.3 Shipping Plug and Source Tube Connection................................................... 3 3.4 F.n d - Pla te A t t ac hme nt Sc re ws........................................................................ 3 3.5 Ot h e r S yst e m Fail u re s...................................................................................... 4 4.0 Construction and Conditlon of Test Speeimens...................................................... 4 5.0 M a i e rial a n d Eq u i p me n t List................................................................................... 7 6.0 Tes t P r oc ed u re............................................................... m..............................m... 8 6.1 Roles a nd Respon sibilities............................................................................... 8 6.2 Test Specimen Preparation and Inspect 10n.................................................... 0 6.3 Compression Test (10 CFR 71.71(c)(9))......................................................... 9 6.3.1 Compre ssion Test S e t up......................................................................... 9 6.3.2 Com pre ssion Te st A sse ssme nt.............................................................., 1 1 6 A Penetration Test ( 10 CFR 71.71 (c)( 10))........................................................, 12 6.4.1 Pe ne tration Test S e t u p.......................................................................... 12 6.4.2 Specimen A Orientation for Penetration Test.......................................

13 6.4.3 Specimen B Orientation for Penetration Test....................................... 14 6.4.4 Specimen C Orientation for Penetration Test...................................... 15

I SENTINEL Test Plan #70 Amersharn Corporation September 17,1997 Durhngton, Massachusetts Page il 6.4.5 Spccimen D Orientation for Fenetration Test........................................ I6 6.4.6 Pe ne tration Te st A s se s sment................................................................. I 7 6.5 Four foot Free Drop Test (10 CFR 71.71(c)(7))............................................. I 8 6.5.1 Fou r foot Free Drop Se t u p.................................................................... I 8 6.5.2 Specimen A Orientation for Four foot Free Drop................................ 19 6.5.3 Specimen B Orientation for Four foot Free Drop................................ 20 6.5.4 Specimen C Orientation for Four. foot Free Drop................................ 21 6.5.5 Specimen D Orientation for Four foot Free Drop................................ 22 6.5.6 Four foot Free Drop Assessment.......................................................... 23 6.6 First Intermedlate Test Inspection................................................................ 23 6.7 30. foot Free Drop Test (10 CFR 71.73(c)(1))............................................... 24 6.7.1 30 foot Free Drop Se t up....................................................................... 24 6.7.2 Specimen A Orientation for the 30 foot Free Drop.............................. 25 6.7.3 Spccimen 11 Orientation for the 30-foot Free Drop.............................. 26 6.7.4 Specimen C Orientation for the 30-foot Free Drop............................. 27 6.7.5 Specimen D Orientation for the 30 foot Free Drop.............................. 28 6.7.6 30 foot Free Drop Test Assessment...................................................... 29 6.8 Puneture Test (10 CFR 71,73(c)(3)).............................................................. 30 6.8.1 Pu n e t u te Te st S e t u p.............................................................................. 3 0 6.8.2 Specimen A Orientation for the Puncture Test.....................................

31 6.8.3 Specimen B Orientation for the Puncture Test..................................... 32 6.8.4 Specimen C Orientation for the Puncture Test..................................... 33 6.8.5 Specimen D Orientation for the Puncture Test..................................... 34 6.8.6 Ptmet u re Test Assess ment................................................................... 3 5 6.9 Seeond Intermedlate Test Inspection............................................................ 35 6.10 Thermal Test ( 10 CFR 71.73(c)(4))........................................................... 36 6.10.1 Therm al Te st..................................................................................... 3 8 6.10.2 Orie nt at i on..................................................................................... 3 8 6.10.3 The rmal Te st Asse ss ment................................................................... 3 8 6.1 I Fi nal Test i n s pec t i o n.................................................................................. 3 9

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SENTINEL Test Plan #70 i

j Amarsham Corporation September 17.1997 Buriington. Massachusetts Page ill i

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i 7.0 W o rks hee ts............................................................................................................... 40 i

Equipme nt List 1 : Compression Test.................................................................. 40

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Chec k li st 1 : Com pre ssion Test............................................................................ 41 l

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Equipmcnt List 2: Pcnetration Test Equipment..................................................

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Chec klist 2: Pc ne t ration Te s t............................................................................... 4 3 1

Equipment List 3: Four foot Free Drop Equipment List.................................... 46 Checklist 3: Fou r foot Free Drop......................................................................... 4 6

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Equipment List 4: 30-foot Free Drop Equipment List........................................

49 Chec klist 4 : 30- foot Free Drop............................................................................ 50 a

i Equipmcnt List 5: Punetunc Test Equipment...................................................... 53 1

Ch e c kli s t 5 : Pu n e t u te Te s t................................................................................... 5 3 Equipment List 6: Thermal Test Equipmcn1..................................................... 56 Ch e c kli s t 6: The rmal Te st.................................................................................... 5 7 4

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SENTINEL Test Plan #70 Amersham Corporation September 17,1997 Burlington, Massachusetts Page tv List of Figures and Tables Figure 1: Side View of a Model 660 Series Projector........................................................ I 4

Table 1 : M ode 1 660 Se ries Variation s............................................................................... 5 Figure 2: Specimen Orientation for the Compression Test............................................. 10 Figure 3: Specimen A Orientation for the Penetration Test............................................ 13 Figure 4: Specimen H Orientation for the Penetration Test.............................................

14 Figure 5: Specimen C Orientation for the Penetration Test.............................................

15 Figute 6: Specimen D Orientation for the Penetration Test............................................. I6 j

Figure 7: Specimen A Orientation for the Four foot Free Drop......................................

19 Figurc 8: Specimen B Oricntation for the Four foot Free Drop...................................... 20 3

Figure 9: Specimen C Orientation for the Four foot Free Drop...................................... 21 Figure 10: Specimen D Orientation for the Four-foot Free Drop.................................... 22 Figure 11: Specimen A Orientation for the 30 foot Free Drop....................................... 25 Figure 12: Specimen B Orientation for the 30-foot Free Drop........................................ 26 -

Figure 13: Specimen C Orientation for the 30-foot Free Drop........................................ 27 Figure 14: Specimen D Orientation for the 30-foot Free Drop....................................... 28 Figure 15: Specimen A Orientation for the Puncture Test.............................................. 3 i Figure 16: Specimen B Orientation for the Puncture Test............................................... 32 Figure 17: Specimen C Oricntation for the Puneture Test............................................... 33 Figure 18: Specimen D Orientation for the Puncture Test.............................................. 34 i

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SENTINEL Test Flan #70 Amersham Corporation September 17,1997 Burlington, Massachusetts Page 1 of $9 Amersham Test Plan #70 This document describes the package design test plan for Sentinel Model 660 Series projectors to meet NRC requirements for Type ll(U) packages (10 CFR 71.71 and 10 CFR 71.73). 'lhe test plan also covers the criteria ststed in I AEA, Safety Series 6 (1985, as amended 1990).

Quality Assurance will be involved si. sll aspects of this test plan and its execution.

The Model 660 Series includes the following models: 660,660A,66011,660E,660AE, and 66011E. Reference Certificate of Compliance 9033.

This document omiines the testing scenario, justifies the package orientations for the difTerent test specimens, and provides test worksheets to record key steps in the testing sequence.

1.0 Transport Package Overview 1he Model 660 Series projector consists of a source tube enclosed in a depleted uranium shleid, an end plate with a lock assembly, a second end plate with a storag plug assembly, four steel connecting rods, a sheet metal shcIl and foam packing material (Figure 1).

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SENTINEL Test Plan #70 Amersham Corporation September 17,1997 Durlington, Massachusotts Pago 2 of $9 The shield consists of a 1/2 inch outside diameter source tube with its mid section set in depleted uranium. One end of the source tube is inserted into a 1/2 inch deep hole of the lock assembly at the rear end plate. 'lhe other end of the shield's source tube is inserted into another 1/2 inch deep hole of the shipping plug at the front end-plate. Iloth 1/2 inch deep holes allow enough radial clearance for a slip fitting attachment. There is approximately 1/8 inch axial clearance at the front end for assembly.

1he source is contained in a special fonn, encapsulated capsule assembly which is attached to the source wire assembly. This source wire assernbly is secured in the package by the lock assembly. The lock assembly, in turn, is attached to the rear end plate by four #10-32 U.N.C.

stainless steel screws.1here are two versions of the lock assembly used on the Model 660 series projectors. The sire, material and location of the end plate attachment screws are identical on both versions.

'the shield, end plates and the sheet metal shell are connected by four 3/8 inch thick stecI rods w hich are threaded at each end to accept 1/4 inch screws securing the end plates to the rals.

A polyurethane foam is used to Gil the space around the shield and fill void within the sheet metal shell.1he foam acts as an impact absorber.

The depleted-uranium shield provides the primary radiation protection for the Model 660 Series projector. The shield accomplishes this by limiting the transmission of gamma rays to a dose level at or below 200 mler at the package surface and limiting the dose level at or below 10 mlUhr at one meter from the surface of the package. A fracture of the shield could compromise this protection.

%e location of the source relative to its stored position in the shield is also an important safety element. A large displacement of the source relative to its stored position could elevate the dose at the surface of the package above regulatory limits.

There are two possible scenarios to displace the source relative to its stored position:

The shield could move away from the source if the source tubes were bent or frac-tured during testing.

'lhe source could move away from the shield if the lock assembly became loose or

+

was removed from the end plate or if the end plates themselves became loose or were removed during testing.

'Ihe tests in this plan focus on damaging those components of the package which could cause the displacement of the source relative to its stored position within the shleid and which affect the integrity of the shield itself.

2.0 Purpose lhis purpose of this plan, which was developed in accordance with Amersham sop-E005, is to ensure the Model 660 Series projectors meet the Type 11 transport package requirements of 10 CFR 71.

The series includes these models: 660,660A,660B,660E,660AE, and 660BE. Refer to Appendix A for descriptive drawings of these models.

SENTINEL Test Plan #70 Amersham Corporation September 17,1997 Burlington, Massachusetts Page 3 of 69 1he Nonnal Conditions of Transport tests (10 CFR 71.71) to be perfonned are the compression i

test, penetration test and four foot free drop test.

1he water spray preconditioning of the package is not perfonned as the Model 660 projectors are constructed of waterproof materials throughout. The water spray would not contribute to any degradation in structural integrity.

1he llypothetical Accident Tests (10 CFit 71.73) to be perfonned are the 30-foot free drop, puncture test, and thennal test.

The crush test (10 CFR 71.73(c)(2))is not perfonned because the radioactive contents are special fonn radioactive material.

The immersion test and all other conditions specilled in 10 CFR 71 will be separately evaluated in accordance with Amersham Work Instruction Wi E08.

3.0 System Failures of Interest 1he possible system failures which could occur during test conditions and affect package integrity:

3.1 Shield Movement or Fracture Elevated dose levels and depleted uranium contamination may result if the shield were to move or break as a result of high shock loading.

3.2 Lock Assembly Screws Elevated dose levels may result if the lock assembly with source assembly attached were to be removed or damaged as a result of high impact loading.

Dispersal of special fonn contents is highly unlikely since the encapsulated source assembly meets the requirements of special form and is protected at the center of the shield.

3.3 Shipping Plug and Source Tube Connection A direct impact on the shipping plug could defonn the end plate in towards the shield An impact could also damage the source tube connection allowing the shield to move.

3.4 End-Plate Attachment Screws The loss of the rear end-plate would result in loss of the lock assembly as well and cause exposure of the source. The loss of the front plate may indicate that the loss of the rear plate is just as likely.

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SEN11NEL.

lest Plan #70 Amersham Corporation Septemt>er 17,1997 Burhngton, Massachusetts Page 4 of 69 3.5 Other System Failures Two other possible system failures were considered but rejected because damage to these components would not cause damage to safety related components.

4 Plunger Lock: *lhe lock mount containing the plunger lock functions as a locking index plunger for the selector ring, it does not hold the source wire assembly. Ifit were to fall, the source would continue to be secured in the lock assembly. 'the se-lector ring can only be rotated during operation, that is, aller removal of the ship-ping cap and depression of the anti rotation lugs.

Ca rrying Ilandle: The handle provides no safety features to the device. its prima-ry function is as a carrying or lifling feature.

4.0 Construction and Condition of Test Specimens The test specimens will be Model 6601) units constructed in accordance with Amersham Drawing D66010, Rev. C, modified per Drawing TP70, Rev. ll. The units specified in Drawing TP70, Rev. II, are in accordance with the NRC approved design.

Drawing TP70, Rev. ll, specifies the Model 660 Series in its worst case transport condition, that is, with supplemental lead added to the shield. The added welght induces higher loads during dynamic testing.

Except for the compression and thennal tests, the test temperature of the specimen must be below 40' C at the time of each test, a minimum temperature sequired by IAEA, Safety Series 6 (1985, as amended 1990). The low temperature represents the worst-case condition for the package because of the potential for brittle fracture of the shleid and the end-plate attachment scre ws.

Four test specimens, built to Drawing 'fP70, Rev. B, and the Amersham Quality Assurance Program, are to be tested, one for each possible failure mode:

Specimen A: Shield movement or fracture Specimen I3: Failure of the lock assembly attachment screws Specimen C: Loss of the connection between the storage plug and the source tube Specimen D: Failure of the end plate attachment screws NOTE:

Because each test is designed to add to damage inflicted on a specific component or assembly in the preceding test, it is important that each specimen maintain its identity throughout the battery of tests and that the setup instructions spec {fic to the specimen are strictlyfollowed Table I lists the differences between the test specimen and other 660 Series models.

SENTINEL Test Plan #70 I

Amersham Corporation September 17,1997 Burlington, Maasachusetts Page 6 of 69 Table 1: Model 660 Series Variations Test Specimen Feature per Drawing TP70, 660 Series Models Rev,11 Shell Material Stainless steel ne Models 660,660A,660AE and 660E can have either a carbon steel shell or a stainless steel shell.

All other models in the series use stainless steel.

Lock Asseinbly Posilok" ne Model 660 and 660E use a non Posilok lock assembly.

All other models feature the Posilok lock assembly.

Actuator Wirts No actuator wires and Models 660AE,660BE and 660E have wires and ccnnectors l

and Connecton connectors attached to ends plates for automatic actuation.

Models 660,660A and 660B do not have actuator wires and connectors.

Shield Capacity 140 Curie ne following models have 120-Curie capacity shields:

660,660A,660AE and 660E,

%e following models have 140-Curie capacity shields:

6608 and 660BE.

Body Width Standard width Some Model 660s and Model 660Es have a narrow body (51/4 inches) design (4 3/4 inches wide).

All other models only use the standard width body (51/4 inches).

Source Tube Titanium Prior to 1980, the Models 660,660A,660AE and 660E were Material manufactured with zircaloy source tubes,-

All other units have titanium source tubes.

Use of Lead Supplen entallead Prior to June 1992, some units in the Model 660 Series had added lead added to supplement the shielding, ne maximum amount of lead added was 3 pounds. De amount was also limited by a maximum shield weight of 40 pounds and a maximum package weight of 56 pounds, Weight 54 pounds it.inimum Over the last five years, the average package weight has been approximately 50 pounds. Earlier in the product history, the average weight was approximately 53 pounds.

SENTINEL Test Plan #70 Amersham Corporation September 17,1997 Burlington, Massachusetts Page G of 59 1he differences listed in Table I do not affect the radiological safety of the projector for the following reasons:

Shell Materials: 'ihe shell thickness is 1/16-inch for the carbon steel and stainless stect versions. The likelihood of a crack or brittle flaw increases with the thickness of the section and is a problem in sections greater than 1/8 inch. Additionally, the temperature for transition from ductile to brittle is lower for the thinner sections.

'ihe thicker carbon steel end plates will reach the ductile to brittle transition tem.

perature long before the shell does. 'the end plates are structural members, while the shell is not structurally significant.

Ieck Style: Damage to the Posilok lock assembly used on the test specimen would represent damage to any Model 660 Series lock assembly, including the non Posilok style assemblies used on the Model 660 and the Model 660lk

'Ihe internal components of both lock assemblies are protected by the same lock assembly cover and practically the same selector ring. The cover and selector ring raust be significantly dan. ged before an impact can disrupt the internal components' securement of the source. Because of the strength of the cover and the selector ring, damage to the source securement is more likely to occur from the failure of the lock assembly attachment screws. All models use the same type and size attachment screws in the same locations.

Actuator Wires and Connectors: 'Ihe additional parts used for automatic actua-tion provide no structural support.

Shield Capacity: 'ihe lower capacity shields are either lighter than or the same weight as the shield used on the Model 6600, making the 660!! the worst case for shield failures ofinterest in these tests.

Ilody Width: 'ihe end plates and shells of the narrow body versions of the Model 660 and the Model 660B would provide smaller impact surfaces than the standard-width plates and shell used in the test specimen. The smaller impact surfaces would result in greater surface defonnation and less deceleration on impact. As a result there would be less transfer ofimpact forces that could affect the integrity of the source securement.

Sou rce Tube Material: 'lhe Model 660 Series projectors have been manufactured with titanium source tubes exclusively since 1980. Because this represents our cur-rent manufacturing methods and because the majority of Model 660 Series units curTently in use have titanium source tubes, the test specimens will be manufac-tured with titanium source tutws, llased on an evaluation of the damage caused by the tests, we will assess the implications for previously fabricated packages which utilized zirealoy.

Note that r.1 hough listed on the descriptive drawings, stainless steel source tubes have never been used in the fabrication of Model 660 Series units, nor do we intend to use them in future fabrication.

SENTINEL Test Plan #70 Amorsham Corporation September 17,1997 Burlington, Massachusetts Page 7 of 69 Supplemental tendt Prior to June 1992, supplemental lead was used in the pro-duction of hiodel 660 Series projectors with the depleted. uranium shleid. Although the addition of supplemental lead is no longer a production technique, the TP70 test specimen will be fabricated with the supplemental lead to ensure the maximum de-Vice mass.

Package Weight Hecause of more emcient casting and the elimination of supple-mental lead shielding, the average weight of Model 660 units produced in the last Ove years is three pounds less than the average welght for units produced in the car-ly years of the series history. Two steps will be taken to build test specimens that will weigh at least 54 pounds:

lleavier depleted uranium shields will be fabricated.

Supplemental lead will be added to the shleid.

He TP70 will be consistent with current manufacturing procedures and will represent the heavier units in the Model 660 population. Ninety seven percent of all 660 units produced weigh 54 pounds or less.

5.0 Material and Equipment List The test worksheets in Section 7.0 list the key materials and equipment speelned in 10 CFR 71 and the necessary measurement instruments.

When video recording is specined in the following tests, select video cameras with the highest shutter speed practical to record testing.

Additional materials and equipment may be used to facilitate the tests.

SENTINEL Test Plan #70 Amersham Corporation September 17,1997 Durhngton, Massachusetts Pago 8 of 69 6.0 Test Procedure Four units are tested in parallel with the same sequence but with the focus on the transpon integrity of different components and assemblies for each sample, as described in Section 3.0.

The tests have the following sequence:

1. Test specimen preparation and inspection

2. Compression test (10 CFR 71.71(cX9))

3.

Penetration test (10 CFR 71.71(cXio))

4.

Four foot free drop (10 CFR 71.71(c)(7))

5.

First intennediate test inspection 6.

30 foot free drop (10 CFR 71.73(c)(1))

7.

!' uncture test (10 CFR 71.73(cX3))

8.

Second intermediate test inspection 9.

Thermal test (10 CFR 71.73(cX4))

10. Final test inspection 6.1 Roles and Responsibilities The responsibilities of the groups identified in this plan are:

Engineering executes the tests according to the test plan and summarizes the test results. Engineering also provides technical input to assist Regulatory Affairs and Quality Assurance as needed.

Regulatory Affairs monitors the tests and reviews test reports for compliance with regulatory requirements.

Quality Assurance oversees test execution and test report generation to ensure compliance with 10 CFR 71, other regulatory requirements and the Amersham Quality Assurance Program, Engineering, Regulatory Affairs and Quality Assurance are,lointly responsible for a

assessing test and specimen conditions relative to 10 CFR 71.

Quality Control, a function that reports directly to Quality Assurance, is responsl.

ble for measuring and recording test and specimen data throughout the test cycle.

He managers directly responsible for Engineering, Regulatory A(Tairs and Quality Assurance will identify and document personnel who are qualified to represent their departments in carrying out this test plan.

SENTINEL Test Plan #70 Amersham Corporation September 17,1997 Durlington. Massachusetts Page 9 of 69 6.2 Test Specimen Preparation and Inspection To prepare the test units:

1. Manufacture five standard [ oduction units with the changes indicated on Amersham Drawing TP70, lley,11. The fifth unit is a spare.

1

2. Measure and record the weight of the shield.

3. Measure and record the weight of the total package.

4.

Inspect the test units to ensure that:

All fabrication and inspection records are documented in accordance with the Amersham Quality Assurance Program.

'Ihc test units comply with the requirements of Drawing TP70, Itev.11.

5. Perfonn and record the radiation profile in accordance with Amersham Work Instruction Wl-Q05.

6,

!!ngineering,Itegulatory Affairs and Quality Asrurance wilijointly verify that the test specimen complies with Drawing TP70, Itev,11. and the Amersham Quality Assurance Program.

7. Measure and record the location of the dummy source from the front end using the source location tool (Amersham Drawing IIT10142, llev. A).

8.

Prepare the package for transport.

6.3 Compression Test (10 CFR 71.71(c)(9))

The first test is the compression test per 10 Cillt 71.7l(c)(9), in which the package is placed under a load of 280 to 290 pounds for at least 24 hours2.777778e-4 days <br />0.00667 hours <br />3.968254e-5 weeks <br />9.132e-6 months <br />.

Use Checklist 1: Compression Test on page 41 to date and initial all action items and to record required data.

NoTEt The worksheet identifies those steps which must be witnessed by Engineering.

Regulatory Afairs and Quality Assurance.

l The following describes the orientation of the test specimen during the compression test and the test assessment.

i 6.3.1 Compression Test Setup The same setup is used in the compression test for all test samples.

To prepare a specimen for the compression test:

1.

Iteview the setup shown in l'igure 2.

L.

SENTINEL Test Plan 870 Amersham Corporation September 17,1997 Durlington, Massachusotts Page 10 of 69 2.

Plaec the specimen upright on a concrete surface with only the feet of the package touching the Door.

'ihe package is oriented in its nonnal transport position.

3. Place 280 to 290 pounds unifonnly distributed onto the specirnen as shown in l'igure 2.

2 The weight is Ove tirnes the package weight and greater than 2 lbflin multiplied 2

by the vertically projected area (5.25" wide x 9.875" long x 2 lbflin = 104 lbf).

200 to 290 por-load evenly distributed Test specimen A,

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SENilNEL Test Plan #70 Amersham Corporatton September 17,1997 Burlington. Massachusetts Page 11 of 69 6.3.2 Compression Test Assessment Upon completion of the test, lingineering, llegulatory AfTairs and Quality Assurance team members will jointly perfonn the following:

Iteview the test execution to ensure that the test was performed in accordance with 10 CI:ll l.

Make a preliminary evaluation of the specimen relative to the requirements of 10 CFit 71.

Assess the damage to the specimen to decide whether testing of that specimen is to continue.

livaluate the condition of the specimen to determinu hat changes are necessary in package orientation in the penetration test to achieve maximum damage.

SENTINEL.

Test Plan #70 Amersham Corporation September 17,1997 Burington, Massachusetts Page 12 of 69 6.4 Penetration Test (10 CFR 71.71(c)(10))

l The compression test is followed by the penetration test per 10 CFR 71.7l(c)(10), in which a penetration bar is dropped from a height of at least 40 inches to impact a specified point on the package. The bar is dropped through free air.

Use ChecAllst 2 penetration Test on page 43 to ensure that test sequence is followed. Date and initial all action itens and record required data.

NOTEt The worksheet identifies those steps which must be witnessed by Engineering.

Regulatory MJisirs and Quality Assurance.

The following describes the orientation of each test specimen immediately before the bar is dropped and the test evaluation for the test.

6.4.1 Penetration Test Setup

'there is a specific orientation for each specimen so that the penetration bar is aimed at the component or assembly ofinterest.

NOTEt Because each test is designed to add to damage irtflicted on a specific component or anembly in the preceding test, it is important that each specimen maintain its identity throughout the battery oftests and that the setup instructions specific to the specimen are strictlyfollowed.

This test requires that the test specimen be at or below.40' C at the time of the penetration bar release. The worksheet calls for measuring and recording the specimen temperature before and after the test.

To set up a package for the penetration test:

1. Measure the specimen's internal and surface temperature to ensure that the package is at or twlow.40' C,

2. Place the specimen on the drop surface (Drawing AT10122, Rev. B) and position it according to the specimen specific orientation described below.

3. Use steel shims to position the package, if necessary.

4.

Position the penetration bar shown in Drawing HT10129, Rev. B, directly above the specified point ofimpact, and raise the bar 40 to 42 inches above the target.

' SENTINEL Test Plan #70 Arnersham Corporation September 17,1997 Burlington Massachusetts Page 13 of 69 6.4.2 Specimen A Orientation for Penetration Test The penetration target for Specimen A is the hit marker on the left side of the package (when facing the lock assembly), as shown in Figure 3. There are two objectives for this orientation:

Move the shield and thus disrupt the source tube connections at either end plate liracture the shield This setup was chosen because the depleted-uranium shield is closer to the exterior on the left side than it is in any other location.

I l

Ponetration Bar j

Drawing BT10129 Rov, B I

i I,

l 7

t l

40 to 42 inches Lock Assembly E

/'S Drop Surface fe Drawing AT10122 i

Shipping Plug Figure 3: Specimen A Orientationfor the Penetration Test

)

SENTINEL Test Plan #70 Amorsham Corporation September 17,1997 Durhngton, Massachusetts Page 14 of $9 6.4.3 Specimen B Orientation for Penetration Test

'Ihe setup for Specimen 11 (Figure 4) provides the greatest impact moment on the lock assembly j

with the penetration bar. The resulting damage could include loosening or shearing the lock assembly screws, disruption of the source tube end plate connection at either end, and movement of the source. Note that the point ofimpact is the outer edge of the lock selector ring.

l.

l Ponotration Bar Drawing BT10129. Rov. B l

4 l

i.

l.

l l

40 to 42 inches s

e i

Drop Surface Drawing AT10122, Impact Point:

Outer Edge of the Lock Rev.B s

Selector Ririg Figure 4: Specimen B Orientationfor the Penetration Test Other orientations that were considered, but not included in this test include:

Normal Transport: If the package were oriented in its normal transport position, the plunger lock mount would interfere.

Invertal: If the package were inverted, that is, positioned on its handle, the plunger lock mount would restrict the lock assembly movement, reducing the likelihood of shearing the screws, disrupting the source tube-end plate connections and moving of the source.

l SENTINEL Test Plan #70 Amersham Corporation September 17,1997 Burlington, Massachusetts Page 16 of 69 6.4.4 Specimen C Orientation for Penetration Test 1hc Specimen C setup attacks the shipping plug in much the same way as Setup 11 attacks the lock assembly.1his test causes an initial round of damage to the plug which is compounded by the two drop tests for the Specimen C.

The point of the penetration bar should impact a flat portion on the shipping plug fitting as close to the outer edge as possible (Figure 5),

+

l l

Penetration Bar Drawing BT10129, Rev. O I

4 I

i I

l.

Ie I

l 40 to 42 inches 4

s Drop Surface Impact Point:

Drawing AT10122, Flat Outer Edge of Shipping Plug Fitting Figure 3: Specimen C Orientationfor the Penetration Test

SENTINEL Test Plan #70 Amersham Corporation September 17,1997 Burlington, Massachusetts Page 16 of 59 6.4.5 Specimen D Orientation for Penetration Test ne object of the penetration test setup for Specimen D is to impact the end-plate attachment screw in the lower left corner of the rear end-plate (Figure 6), A hit marker indicates the target.

Damage that may result from the bar drop includes loosening or shearing of the end plate screws.

+

l.

I' 4

Penetration Bar Drawing BT10129, Rev. B li i

I 7

I 40 ta 42inchds Lock Assembly l

Hit Marker-Drop Surface Drawing AT'.0122, l/

Rev.B d

s Figure 6: Spec, men D Orientationfor the Penetration Test

_____.m._.__.

SENTINEL Test Plan #70 Amersham Corporation September 17,1997 Burlington, Massachuv tts Page 17 of 59 6.4.6 Penetration Test Assessment Upon completion of the test, Engineering, Regulatory AITairs and Quality Assurance team members willjointly perform the following:

- - Review the test execution to ensure that the test was perfonned in accordance with 10 CFR 71, Make a preliminary evaluation of the specimen relative to the requirements of 10 CFR 71.

Assess the damage tu the specimen to decide whether testing of that specimen is to continue.

Evaluate the condition of the specimen to determine what changes are necessary in package orientation in the 4 foot free drop to achieve maximum damage.

4 4

r

SENTINEL Test Plan #70 Amorsham Corporation September 17.1997 Burlington, Massachusetts Page 18 of 59 6.5 Four-foot Free Drop Test (10 CFR 71.71(c)(7))

The final Normal Transport Conditions test is the four foot free drop as described in 10 CFR 71.71(c)(7). This drop compounds any damage caused in the first two tests. Upon completion of this step, you will perfonn the first intermediate test inspections.

Use Checklist 3: Four-foot Free Drop on page 46 to ensure that the test sequence is fol lowed.

Date and initial all action items, and record required data on the worksheet.

NOTE:

The worksheet identifies those steps which must be witnessed by Engineering, Regulatory 4[ fairs and Quality An. trance.

6.5.1 Four-foot Free Drop Setup in this test, the package is released from a height of four feet and lands on the steel drop surface specified in Drawing AT10122, Rev. B. There is a specific orientation for each specimen so that the package lands on the componu or assembly ofinterest.

NOTE:

Because each test is designed to add to damage inflicted an a specific component or assembly in the preceding test, it is important that each specimen maintain its identity throughout the battery oftests and that the setup instructions specific to the specimen aoe strictlyfollowed.

This test requires that the test specimen be at or below -40 C at the time of the drop. Follow the Worksheet instructions for measuring and recording the specimen temperature before and after the drop.

To set up a package for the four-foot drop test:

1. Use the drop surface specified in Drawing AT10122, Rev B.

2. Measure the specimen's internal and surface temperature to ensure that the package is at or below-40 C.

3. Place the specimen on the drop surface and position it according to the specimen-specific orientation described below.

4.

Raise the package so that the impact target is 4.0 to 4.5 feet above the drop surface.

5. Align the selected center of gravity marker as shown in the referenced drawing.

SERTINEl.

Test Plan #70 Amersham Corporation -

September 17,1997 Burlington, Massachusetts Page 19 of 69 6.5.2 Specimen A Orientation for Four-foot Free Drop The impact points are the bottom edges of the two end plates as shown in Figure 7. Align the center of gravity marker on the sides of the packages with the middle of the drop surface.

His orientation attempts to break the connection between the source tube and the end plates, and move the shield away from the source. Each end plate provides a rigid structure which limits defonnation and directs the shock load to the source tube connections of the shield. The momentum of the shield toward the bottom of the package may cause the end plates to separate from the shell.

., C'4: 7 r.

y d,.?'6..y...

I y Center of Gravity a.

I' 2:

Marker

~

)... d k:. j f

(7-- }. 3,. V L 3 i

n impact Sudaces:

Bottom Edges of the End Plates 4.0 to 4.5 feet i

U Drop Surface

)

Drawing AT10122' g

,g Rev.B Figure 7: Specimen A Orientationfor the Four-foot Free Drop As the bottom edges make contact with the drop surface, the plates rapidly decelerate while the downward momentum of the shield (the heaviest component in the package and the center of gravity) increases the likelihood of damaging the source tube-to-end plate connections. The shield may act as a wedge forcing the end plates apart. The downward momentum may also have the secondary efTect of mo ing the source.

A.

SENTINEL Test Plan #70 Amersham Corporation September 17.1997 Buriington, Massachusetts Page 20 of 59 6.5.3 Specimen B Orientation for Four-foot Free Drop The four foot drop setup for Specimen B is shown in Figure 8. The object of the drop is to shear or loosen the lock assembly screws and damage the connection with the shield.

The impact point is the outer edge of the lock assembly cover. It is important to position test specimen D so that its center of gravity is directly above the lock assembly.

The impact will add to any damage to the lock assembly caused by the penetration bar in the second test.

This orientation directs the maximum obtainable shear force to the lock assembly attachment screws in an attempt to move the lock and the source. Other orientations for attacking the lock assembly would not benefit from the center of gravity aligned with the impact position and/or would be limited by interference from the plate edges.

l

\\i j f'Y I Center of Gravity Marker i

5,1 //

g-QJU

-m(!

impact Surface: / '

Outer Edge of Lock Assembly 4.0 to 4.5 feet Cover V

Drop Surface g

)

~~

d Drawing AT10122,

.j Rev.B Figure 8: Specimen B Orientationfor the Four-foot Free Drop I

t SENTINEL '

Test Plan #70 Amersham Corporation September 17,1997 Burlington, Massachusetts Page 21 of 59 6.5.4 Specimen C Orientation for Four-foot Free Drop The setup for Specimen C is similar to the Specimen B orientation except that the point of impact is a flat outer edge on the shipping plug. The object in this drop is to disrupt the connection between the source tube and the shipping plug, which in turn could cause movement of the source. A secondary effect could be disruption of the connection between the source tube and the rear end-plate.

Figure 9 shows the Four foot Drop setup for Specimen C. Again, the center of gravity is directly above the point ofimpact and there is no interference from the plate edges or other package components.

Center-of Gravity U,<"

Marker i

.w Il' l x

w.

Impact Surface:

i A Flat Outer i

Edge of the l

Shipping Plug I,

4.0 to 4.5 feet U

5 Drop Surface Drawing AT10122,

• e Rev.B Figure 9: Specimen C OrientationJbr the Four-foot Free Drop

SENTINEL Test Plan #70 Amersham Corporation September 17,1997 Burlington, Massachusetts Page 22 of 59 6.5.5 Specimen D Orientation for Four-foot Free Drop The four foot drop setup for Specimen D (Figure 10) targets the bottom edge of the rear end-plate, liere, the objective is to loosen or shear the end-plate screws which hold the plate to the steel connecting rods. The bottom edge of the plate provides the greatest surface area for a direct hit, and thus the most rapid deceleration. Other locations were rejected as follows:

The top edge provides less than half the surface area of the bottom edge, and much of the load would be directed through the carrying handle.

The curved side edges would only provide a point impact.

The lock assembly and the shipping plug would interfere with a direct hit to the face of their respective end plates.

Dropping the package on any corner would absorb the impact energy by deforming the end plate into the foam.

Make sure the center of gravity is directly over the point ofimpact.

/\\

Conter-of Gravity g"%

6h Marker -

od'N NJ l

impact Surface: # I Bottom Edge of l

Rear End-Plate l

4.0 to 4.5 feet Y

)

Drop Surface

~*

Drawing AT10122, Rev.8 Figure 10: Specimen D Orientationfor the Four-foot Free Drop

SENTINEL Test Plan # 70 Amersham Corporation September 17,1997 Durlington, Massachusetts

. Page 23 of 59 6.5.6 Four-foot Free Drop Assessment Upon completion of the test, Engineering, Regulatory Affairs and Quality Assurance team members willjointly perform the following:

Review the test execution to ensure that the test was performed in accordance with 10 CFR 71.

Make a preliminary evaluation of the specimen relative to the requirements of 10 CFR 71, Assess the damage to the specimen to decide whether testing of that specimen is to continue.

Evaluate the condition of the specimen to determine what changes are necessary in package orientation in the 30-foot free drop to achieve maximum damage.

6.6 First Intermediate Test inspection Perform an intermediate test inspection afler the four-foot free drop test.

1.

Measure and record any damage to the test specimen.

2. Measure and record the location of the source from the front end-plate using the source location tool (Amersham Drawing BT10142, Rev. A).

3. Remove and assess the condition of the dummy source.

4 Reassemble the package using an active 424-9 source, making sure that the source wire position and the package configuration are the same as they were immediately afler the four-foot free drop.

5, Measure and record a radiation profile of the test specimen in accordance with Amersham Work Instruction WI-Q09.

6. Assess the significance of any change in radiation at the surface or at one meter from the package.

7.

Reassemble the package using the same dummy source used in the speci-men during the first three tests.

8.

Make sure that the source wire position and the package configuration are the same as they were immediately after the four-foot free drop.

Engineering, Regulatory Affairs, and Quality Assurance team members will make a final assessment of the test specimen andjointly determine whether the specimen meets the requirements of 10 CFR 71.71.

SENTINEL Tost Plan #70 l

Amersham Corporation September 17,1997 Burhngton, Massachusetts Page 24 of 59 -

6.7 30-foot Free Drop Test (10 CFR 71.73(c)(1))

The first flypothetical Accidents Test is the 30-foot free drop as described in 10 CFR 71.73(c)(1). This drop compounds any damage caused in the three Normal Conditions Tests.

Use Checklist 4:30-foot Free Drop on page 50 to ensure that the test sequence is followed. Date and initial all action items, and record required data on the worksheet.

NOTE:

The worksheet laemyles those steps which must be witnessed by Engineering, Regulatory Affairs and Quality Assurance.

Figure 11 through Figure 14 illustrate the orientations for the four test units, which are the same as those for the four-foot free drop except the package is raised 30 feet above the drop surface.

This test requires that the test specimen be at or below -40 C. at the time of the drop. Follow the worksheet instmetions for measuring and recording the specimen temperature before and after the drop.

6.7.1 30-foot Free Drop Setup To set up a package for the 30-foot drop test:

1. Use the drop surface specified in Drawing AT10122, Rev B.

2.

Measure and record the weight of test specimen.

3. Measure the specimen's internal and surface temperature to ensure that the package is at or below -40 C.

4.

Place the specimen on the drop surface and position it according to the specimen-specific orientation described below,

5. Raise the package so that the impact target is 30 to 32 feet above the drop surface.

6. Align the selected center-of-gravity marker as shown in the referenced drawing.

I

d 1

SENTINEL Test Plan #70 Amersham Corporation September 17,1997 Burhngton, Massachusetts Page 25 of 59 -

-6.7.2 Specimen A Orientation for the 30-foot Free Drop.

Figure 11 shows the package orientation for Specimen A.

I b

f

)

.. o(

)

Center of-Gravity o-Marker O.

(~D:/* S l

1 1

I impact Surface:

j Bottom Edges of the End Plates I

30 to 32 feet l

l l.

I*

u t

s Drop Surface Drawing AT10122, Figure 11: Specimen A Orientationfor the 30-foot Free Drop i

)

4 1

1

,y r,

SENTINEL Test Plan #70

- Amersham Corporation September 17,1997 Burkngton, Massachusetts Page 26 of 59 6.7.3 Specimen B Orientation for the 30-foot Free Drop Figure 12 shows the package orientation for Specirnen B.

LT Center-of-Gravity Marker

=. ~ -

'N 7'

Impact Surface:

j Outer Edge of the j

Lock Assembly Cover I

I l

30 to 32 feet I

l.

l s

Drop Surface Drawing AT10122, Figure 12: Specimen B Orientationfor the 30-foot Free Drop

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

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

SENTINEL Test Plan #70 Amersham Corporation September 17,1997 Burijngton, Massachusetts Page 27 of 59 6.7.4 Specimen C Orientation for the 30-foot Free Drop Figure 13 shows the package orientation for test specimen C.

7 Center-of Gravity-Marker 1I v

u impact Surface:

l Same Flat Outer Edge l

Targeted in the Four-foot Drop l

l l

30 to 32 feet t

I.

i l.

a f

s Drop Surface Drawing AT10122, Figure 13: Specimen C Orientationfor the 30-foot Free Drop a

l i

_.. _.. _ _ _ ~ _ _ _...

_.____...m SENTINEL Test Plan #70 Amersham Corporation September 17,1997 Burlington, Massachusetts Page 28 of 59 6.7.5 Specimen D Orientation for the 30-foot Free Drop i

Figure 14 shows the package orientation for test specimen D.

Center of-Gravity Marker I

l impact Surface:

i Bottom Edge of the.

l l

Rear End Plate l

l 30 to 32 feet I.

'l i.

i

.I 4

i i

n Drop Surface s

3 Drawing AT10122, Rev.B Figure 14: Specimen D Orientationfor the 30-foot Free Drop 1

i 4

1

l.

I SENTINEL Test Plan #70 Amersham Corporation September 17,1997

' Burhngton, Massachusetts Page 29 of 59 6.7.6 30-foot Free Drop Test Assessment Upon completion of the test, Engineering, Regulatory AITairs and Quality Assurance team members willjointly perform the following:

. Review the test execution to ensure that the test was performed in accordance with 10 CFR 71.

Make a preliminary evaluation of the specimen relative to the requirements of 10 CFR 71.

Assess the damage to the specimen to decide whether testing of that specimen is to continue.

Evaluate the condition of the specimen to determine what changes are necessary in

. package orientation in the puncture test to achieve maximum damage.

.--=

- - ~.

.... _ - ~ _ -

SENTINEL Test Plan #70 Amersham Corporation September 17,1997 Durbngton, Massachusetts Page 30 of 59 6.8 Puncture Test (10 CFR 71.73(c)(3))

The 30 foot free drop is followed by the puncture test per 10 CFR 71.73(c)(3), in which a package is dropped from a height of at least 40 inches onto the puncture billet specified in 4

Drawing CTl0119, Rev. C.

The billet is to be bolted to the drop surface used in the free drop tests (Figure 15).

Use Checklist 5: Pur.cture Test on page 53 to ensure that test sequence is followed. Date and initial all action items and record required data.

NOTE:

The worksheet identifies those steps which must be witnessed by Engineering.

Regulatory Affairs and Quality Assurance.

The following describes the orientation of each test specimen immediately before the package is dropped onto the billet and the test evaluation.

6.8,1 Puncture Test Setup There is a specific orientation for each specimen so that the package lands on the component or assembly ofinterest.

NOTE:

Because each test is designed to add to damage inflicted on a specific component or assembly in thepreceding test, it is important that each specimen maintain its identity throughout the trattery oftests and that the setup instructions specJic to the specimen are strictlyfollowed.

This test requires that the test specimen be at or below -40' C at the time of the test. The worksheet calls for measuring and recording the specimen temperature before and after the test, f

This test uses the 12-inch high puncture billet (Drawing CT10119, Rev. C). The billet meets the minimum height (8 inches) required in 10 CFR 71.73(c)(3). The specimen has no projections or overhanging members longer than 8 inches which could act as impact absorbers, thus allowing the billet to cause the maximum damage to the specimen.

To set up a package for the puncture test:

a 1.

Measure and record the weight of the package.

2.

Ensure that the package is at or below 40* C.

3.

Position it according to the specimen-specific orientation described below.

4.

Raise the package so that there is 40 to 42 inches between the package and the top of the puncture billet.

5. Check the alignment of the specified center-of-gravity marker with the tar-geted point ofimpact.

a w

.,-n

}

SENTINEL Test Plan #70 Amersham Corporation September 17,1997 Burhngton, Massachusetts Page 31 of 59 Figure 15 through Figure 18 illustrate the four package orientations for the puncture tests. The justification for each orientation is the same as the orientation for the specimen's free drops.

6.8.2 Specimen A Orientation for the Puncture Test The objective of the Specimen A orientation (Figure 15) is to puncture the shell and move the shield, The impact area is the bottom of the package, the largest flat surface on the shell. This surface will yield the greatest deceleration, while the momentum of the shield continues downward, Align the center of gravity marker on the side of the package with the center of the puncture billet.

[

] a

. -( = L Center-of Gravity Marker

^- y,

I impact Surface:

Bottom of the Package 40 to 42 inches Between the End Plates l

U Puncture Billet Drawing CT10119 Rev.C 5 E E

? Drop Surface Drawing AT10122 Figure 15: Specimen A Orientationfor the Puncture Test

SENTINEL Test Plan #70 Amersham Corporation September 17,1997 Burlington, Massachusetts Page 32 of 59 6.8.3 Specimen B Orientation for the Puncture Test E

The objective of the Specimen B setup (Figure 16) is to continue the damage inflicted on the lock arsembly caused by the penetration test and the two free drops. To achieve the same point of attack as the free G ops, you must align the center-of gravity marker over the lock assembly and ensure that the plunger lock clears the top of the billet.

G Center-of Gravity g

l Marker 1

(

l impact Surface:[ i.

Outer Edge of the l

Lock Assembly 40 to 42 inches Cover l

l 1I i

Puncture Billet l

Drawing CT10119 Rev.C rY V E E

Drop Surface

~

Drawing AT10122 Figure 16: Specimen B Orientationfor the Pwicture Test

(

l 7

y

6 Test Plan #70 Amersham Corporation September 17,1997 Burbngton, Massachusetts Page 33 of 59 6.8.4 Specimen C Orientation for the Puncture Test

%e objective of t'ne Specimen C setup (Figure 17) is to continue the damage inflicted on the shipping plug assembly caused by the penetration test and the two free drops. The impact point should be the sasne flat outer edge on the shipping plug targeted in the previous tests. Align the center-of gravity marker directly above the impact point on the shipping plug assembly, t

Center of Gravity Marker zf

\\r N

/t Impact Surface:

Same Flat Outer l

40 to 42 inches Edge of the Shipping Plug Target in l

l Free Drops t

Puncture Billet Drawing CT10119 Rev.O r@

2 5 E E

Drop Surface Drawing AT10122 Figure 17: Specimen C Orientationfor the Puncture Test I

.. ~...

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

SEtiTINEL Test Plan #70 Amersham Corporation September 17,1997 Burhngton, Massachusetts Page 34 of 59 6.8.5 Specimen D Orientation for the Puncture Test The Specimen D setup (Figure 18) targets the bottom edge of the rear end-plate to diston the end plate and loosen or shear the screws securing the end plate to the interior metal rods.

The bottom edge provides the largest, unobstructed flat surface on the plate. The impact will crush the bottom of the end plate into the polyurethane foam, the sollest material in the package, l

and cause the maximum distortion of the plate. Attacking the top edge was rejected because the flat surface area is less than half that of the bottom edge and the carrying handle would deflect much of the energy, r

q

/

~

Conter-of-Gravity rS

%)h

/

i

/

impact Surface:

l Bottom Edge of l

Rear End-Plate 40 to 42 inches l

F 4

Puncture Billet i

Drawing CT10119 Rev.C r@

91 sg a

Drop Surface y,' s l',*~

Drawing AT10122 M

Rev.B

~

Figure 18: Specimen D Orientationfor the Puncture Test 4

t

- - _ _ ~.. _

SENTINEL Test Plan #70 Amersham Corporation September 17,1997 Burlington, Massachusetts Page 35 of 59 6.8.6 Puncture Test Assessment Upon completion of the test, Engineering, Regulatory Affairs and Quality Assurance team members willjointly perform the following:

l Review the test execution to ensure that the test was performed in accordance with 10 CFR 71.

hiake a preliminary evaluation of the specimen relative to the requirements of 10 CFR 71.

Assess the damage to the specimen to decide whether testing of that specimen is to continue.

Evaluate the condition of the specimen to determir e the package orientation for the thermal test to achieve maximum damage.

As part of the evaluation, measure the weight of the specimen.

6.9 Second Intermediate Test inspection Perform a second intermediate test inspection aller the puncture test and before the thermal test.

1.

hicasure and record any damage to the test specimen.

2. hicasure and record the location of the source from the front end using the source location tool (Amersham Drawing B fl0142, Rev. A),

3. Remove and assess the condition of the dummy source.

4, Reassemble the package using an active 424-9 source, making sure that the source wire position and the package configuration are the same as they were immediately after the puncture test.

5. hieasure and record a radiation profile of the test specimen in accordance with Amersham Work Instruction WI-Q09.

4 6.

Reassemble the package using the same dummy source used in the speci-men during the first three tests.

7.

hiake sure that the source wire position and the package configuration are the same as they were immediately after the puncture test.

l A.

4

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

. - ~. --

.,-. -, ~.

SENTINEL Test Plan #70 Amersham Corporation September 17,1997 Burlington, Massachusetts Page 36 of 59

- 6.10 Thermal Test (10 CFR 71.73(c)(4))

i

%e final requirement is the thermal test specified in 10 CFR 71.73(c)(4).

To ensure sufficient heat input to the test specimens, each specimen will be pre-heated to a temperature of at least 800 C and held to at least that temperature for 30 minutes. This test condition provides heat input in excess of the requirements specified in 10 CFR 71.73(c)(4),

which does not include a pre-heat condition. The pre-heat condition assures equivalent heat input regardless of emissivity and absorptivity coefficients.

The test environment is a vented electric oven operating at 900 C. There will be sufficient air flow to allow combustion. Air will be forced into the oven at a minimum rate of 9.6 cubic feet per minute to ensure sufficient oxygen to fully combust all package materials that are capable of burning. This rate is based on the following analysis:

1. The only combustible material in the TP70 is the polyurethane foam.

2.

The chemical composition of polyurethane is [C 1I NO ]n.

26 33 i3

3. The products of combustion are carbon dioxide (CO ) and water (110) 2 2

and the molecular weights of the component materials are:

C = 12 11 = 1 O = 16 N = 14

4. The maximum mass of the polyurethane in a TP70 is 988 grams. The max-imum amounts of carbon and hydrogen present in the polyurethane are i

computed as follows:

Polyurethane C

II33 N

0:3 26 Molecular Weight (26x12) +

(33x1) +

(1x14) +

(13x16) 567 =

312 +

33 +

14 +

208 I

Percent by Mass 55.0 %

5.8%

2.5%

36.7 %

988 g =

543g +

$7g +

25g +

363g

5. The amount of oxygen required to fully combust the carbon to carbon di-oxide is computed as follows:

Carbon Dioxide C

-02 Molecular Weight (1x 12) +

(2x16)

=

44 =

12 +

32 For a given mass of carbon,32/12 = 2.67 times that mass of oxygen is required to fully combust the carbon to carbon dioxide. For a TP70 containing 543 grams of.

i carbon, full combustion would require 1450 grams of oxygen.

i

SENTINEL Test Plan #70 Amersham Corporation September 17.1997 Burlington, Massachusetts Page 37 of 59

6. The amount of oxygen required to fully convert the hydrogen to water is computed as follows:

Water 112 O

Molecular Weight (2x 1) +

16 18 =

24 16 For a given mass of hydrogen,16/2 = 8 times that mass of oxygen is required to fully convert the hydrogen to water. For a TP70 with 57 grams of hydrogen, full combustion would require 456 grams of oxygen.

7. The sum of these oxygen requirements (1450g + 456 g) less the oxygen supplied by the polyurethane (-363 g) equals 1543 grams of oxygen to as-sure suflicient oxygen to burn the polyurethane foam. At standard condi-i tions, the composition of air is 23.2% oxygen by mass. Therefore,6650 grams of air are required.

8.

The volume of air is computed at a density of 1.225 grams / liter to be 192 cubic feet:

3 3

6650g/1.225g/l = 54301 = 5.43m =19211 9.

A 50% safety factor is added and the volume is distributed over the 30-minute test period to determine a minimum air flow rate of 9.6 cubic feet per minute:

3 3

(192 ft )(1.5) / 30 min. = 9.6 fl / min.

The air will be introduced as compressed air passing through a flowmeter acd into the oven via metal tubing. A sufficient length of tubing will be inside the oven to ensure sufficient pre-heating.

The temperature of the package's exterior surface closest to the air entry point will be monitored throughout the test to ensure that the package remains above 800* C.

If the specimen is buming when it is removed, the unit is allowed to extinguish by itself and then cool naturally. The final evaluation of the package is performed when the specimen reaches ambient temperature.

1. Avallone, Eugene A. and Theodore Baumeister III, Editors, Afarks' Standard HandbooAfor Afechanical Engineers. Ninth Edition (New York: McGraw-Hill Book Company,1987), page 4-27

SENTINEL Test Plan #70 Amersham Corporation September 17,1997 Burlington, Massachusetts Page 38 of 59 6.10.1

-Thermal Test To perform the thermal test:

1. Ileat the oven to 900* C.

2. Attach thermocouples to the package's internal and external measurement locations,

3. place the package in the oven and close the door.

4.

When the internal temperature of the package goes above 800* C, start air flow and start a 30-minute timer.

5. Measure and record the oven temperature, test specimen internal and ex.

ternal temperatures and the air flow rate. Record whether there is any com-bustion.

6.

Monitor the specimen's internal and external temperatures, and the oven temperature throughout the 30-minute test period to ensure that all temper.

atures remain above 800* C.

7.

Monitor the airflow rate throughout the test period to ensure that it remains 3

above 9.6 ft / minute.

8.

At the end of the 30 minutes, repeat Step 5.

9.

Remove the test specimen from the oven,

10. Allow the package to self-extinguish and cool.

6.10.2 Orientation The orientation andjustification should be based on an assessment of the test specimen condition immediately aller the puncture test. Record, justify and approve the orientation for this test in accordance with Amersham SOP E005.

6.10.3 Thermal Test Assessment Upon completion of the test, Engineering, Regulatory Affairs and Quality Assurance team members willjointly perform the following:

Review the test execution to ensure that the test was performed in accordance with 10 CFR 71.

Make a preliminary evaluation of the specimen relative to the requirements of 10 CFR 71.

SENTINEL Test Plan #70 Amorsham Corporation September 17,1997 Durtington, Massachusetts Page 39 of 59 6.11 Final Test inspection Perfonn the following inspections aner completion of the thennal test:

1. Measure and record any damage to the test specimen.

2.

Measure and record the location of the source from the front end-plate using the source location tool (Drawing BT10142, Rev A).

3. Remove and assess the condition of the dummy source.

4.

Reassemble the package using an active 424-9 source, making sure that the source wire position and the package configuration are the same as they were immediately after the thermal test.

5.

%ure and record a radiation profile of the test specimen in accordance with Amersham Work Instruction WI-Q09.

6.

Assess the significance of any change in radiation at one meter from the package.

7.

Detennine whether it is necessary to dismantle the test specimen for in-spection of hidden component damage or failure.

8.

If you decide to proceed with the inspection, record and photograph the process of removing any component.

9.

Measure and record any damage or failure found in the process of dismantling the test specimen.

Engineering, Regulatory Affairs, and Quality Assurance team members will make a final assessment of the test specimen and jointly determine whether the specimen meets the requirements of 10 CFR 71.73

SENTINEL Test Plan #70 Amersham Corporation Septemoor 17,1997 Durlington, Massachusetts Page 40 of 59 7.0 Worksheets Use the fdlowing worksheets for executing these tests. There are two worksheets for each test:

an equipment list and a test procedure checklist.

Use the test equipment list to record the serial number ofcach measurement device used. Attach a copy of the relevant inspection report or calibration certi6cate after you have veri 6ed the range and accuracy of the equipment.

Quality Control will initial each step on the checklist as it is executed and record data as required. The Engineering, Regulatory Affairs and Quality Assurance representatives must witness all testing to ensure the testing is performed in accordance with this test plan and 10 CFR 71.

Make copies of the forms for additional attempts. Maintain records of all attempts.

Equipment List 1: Compression Test Enter the Model and Attach inspection Report or Description Serial Number Calibration Certincate

=-

Weight Scale Record any additional tools used to facilitate the test and attach the appropriate inspection report or calibration certiGcate, VerlGed by:

Signature Date Engineering Regulatory Affairs Quality Assurance

SENTINEL Test Plan #70 Amersham Corporation September 17,1997 Burlington, Massachusetts Page 41 of 59 Checklist 1: Compression Test Test location:

Attempt Number:

S ##i**"

S **i* "

S "*i*#"

b '" * ""

E E

E E

Stcp A

B C

D

1. Engineering, RA and QA confirm that test specimen complies with Drawing TP70, Rev. O, and the Amersham Quality Assurance Program.

2. Position specimen on concrete surface Figure 2 Figure 2 Figure 2 Figure 2 per the appropriate drawing.

3. Measure ambient temperature.

Record ambient temperature:

Note the instrument used:

4. Apply a uniformly distributed weight of 280 to 290 pounds on the top surface of the handle for a period of 24 hours2.777778e-4 days <br />0.00667 hours <br />3.968254e-5 weeks <br />9.132e-6 months <br />.

Record the actual weight:

Note the instrument used:

Record start time and date:

Steps I through 4 witnessed by:

Engineering Regulatory Affairs Quality Assurance

5. Afler 24 hours2.777778e-4 days <br />0.00667 hours <br />3.968254e-5 weeks <br />9.132e-6 months <br />, remove the weight.

Record end date:

Record end time:

6. Measure the ambient temperature.

Record the ambient temperature:

Note the instrument used:

7. Photograph the test specimen and any subsequent damage.

8. Record damage to test specimen on a separate sheet and attach.

SENTINEL Test Plan #70 Amersham Corporation September 17,1997 Budington, Massachusetts Page 42 of 59 Checklist 1: Compression Test (Continued)

Test Location:

Attempt Number:

P#CI* *"

b C#I**"

E

'St#P A

B C

D Steps 5 through 8 witnessed by:

Engineering Regulatory Affairs Quality Assurance

9. Engineering, Regulatory AiTairs and Quality Assurance make a preliminary assessment relative to 10 CFR 71. Record the assessment on a separate sheet and attach.

Determine what changes are necessary in package orientation for the penetration test to achieve maximum damage.

Test Data Accepted by:

l Signature Date Engineering: l Regulatory Affairs:

Quality Assurance: l

SENTINEL Test Plan #70 Amersham Corporation September 17,1997 Durlington, Massachusetts Page 43 of 59 L

Equipment List 2: Penetration Test Equipment Enter the Model and Attach inspection Report or Description Serial Number Calibration Certificate Penetration Bar, Drawing BT10129, Rey, B Drop Surface, Drawing AT10122. Rev. B Thennometer

'Ihermocouple ficxible probe Thermocouple surface probe Record any additional tools used to facilitate the test and attach the appropriate inspection report or calibration certificate.

Verified by:

Signature Date Engineering Regulatory Affairs Quality Assurance Checklist 2: Penetration Test Test Location:

Attempt Number:

Specimen Specimen Specimen Specimen 3,*E A

B C

D

1. Immerse the test specimen in dry ice as needed to bring specimen temperature below

-40 C.

Step I witnessed by:

Eng:neering Regulatory Affairs Quality Assurance

2. Remove the specimen from the dry ice, and Figure 3 Figure 4 Figure 5 Figure 6 position it as shown in the referenced figure.

SENTINEL Test Plan #70 Amorsham Corporation September 17,1997 Burlington, Massachusetts Page 44 of 69 Checklist 2: l'enetraflon Test (Continued) i Test Locationt Attempt Numbers j

)

Specimen Specimen Specimen Specimen 3,cp A

B C

D

3. Ilegin video recording of the test so that the j

impact is recorded.

4. Inspect the orientation setup and verify the bar height.

$. Measure the ambient tempeEure and the 5

test specimen internal and surface temperatures.

Ensure that specimen temperature is below

-4 0" C.

a Record ambient temperature:

Note the instrument used; Record the specimen Internal temperature:

Note the instrument used:

Record the specimen surface temperature:

Note the instrument used:

)

Steps 2 through

• wittiessed by:

l Engineering Regulatory AfTairs 4

j Quality Assurance

6. Drop the penetration bar onto the specified Figure 3 Figure 4 Figure 5 Figure 6 area shown in the referenced figure, f

7, Check to ensure that penetration bar hit the specified area.

8. Measure the test specimen's surface temperature. Ensure that specimen is below 40*C.

Record the specimen surface temperature:

Note the instrument used:

9. Pause the video recorder Ensure that the point ofimpact and orientr. don specified in the plan have been achieved sid recorded.

SENTINEL Test Plan #70 Amersham Corporation September 17.1997 Burlington, Massachusetts Page 45 of 69 i

J l

4 Checklist 2: l'enetration Test (Continued)

{

Test locationt Attempt Number:

l Specimen Specimen Specimen Specimen ggE A

11 C

D 1

l

10. Record damage to test specimen on a separate sheet and attach, Steps 6 through 10 witnessed by:

Engineering Regulatory Affairs I

Quality Assurance f

II. Engineering, Regulatory A(Tairs and Quality Assurance make a preliminary assessment relative to 10 CFR 71. Record the assessment on a separate sheet and attach.

4 Determine what changes are necessary in package orientation for the four foot free drop 1

i to achieve maximum damage.

l Test Data Accepted by:

signature Date 1

Engineering:

Regulatory Affairs:

Quality Assurance:

E 1

4 a

l

SENTINEL Test Plan #70 Amersham Corporation September 17,1997 Burlington, Massachusetts Page 46 of $9 Equipment List 3: Four foot Free Drop Equipment List Enter the Model and Attach inspection Report or Description Serial Number Calibration Certincate Drop Surface, Drawing AT10122, Rev. B Thermometer lhermocouple flexible prole lhermocouple surface prote Record any additional tools used to facilitate the test and attach the appropriate inspection report or calibration ecrt10cate, Verified by:

Signature Date Engineering Regulatory AfTairs Quality Assurance Checklist 3: Four-foot Free Drop Test lecation:

Attempt Number:

Specimen Specimen Specimen Specimen Step A

B C

D

1. Immerse the test specimen in dry ice as need to bring specimen temperature below 40'C.

j Step I witnessed by:

Engineering Regulatory Affairs Quality Assurance

2. Measure the ambient temperature, i

Record ambient temperature:

SENTINEL Test Plan #70 Amersham Corporation September 17,1997 Durhngton, Massachusotts Page 47 of 69 Checklist 3: Four foot Free Drop (Continued)

Test lx>eation:

Attempt Numl>cra S '"I**"

8 I*'"

S "I*'"

S I* *"

P P

P Step P

A 11 C

D Note the instrument used:

3. Attach the test specimen to the release mechanism.

4. Ilegin video recording of test so that impact is recorded,

5. Measure the temperature of the specimen.

Ensure that specimen is below -40' C.

Record the specimen internal temperature:

Note the instrument used:

Record the specimen surface temperature.

Note the instrument used:

6. Lif1 and orient the test specimen as shown Figure 7 Figure 8 Figure 9 Figure 10 in the referenced figure for the specimen.

7. Inspect the orientation setup and verify drop height.

8. Photograph the setup in at least two perpendicular planes.

Steps 2 through 8 witnessed by:

Engineering Regulatory Affairs Quality Assurance

9. Release the test specimen.

10. Measare the surface temperature of the test specimen.

Record the surface temperature:

Note the instrument used:

11. Pause the video recorder. Ensure that the point ofimpact and orientation specified in the plan have been achieved and recorded.

SENTINEL Test Plan #70 Amersham Corporation September 17,1997 Burlington, Massachusetts Page 48 of 69 Checklist 3: Four foot Free Drop (Continued)

Test Location:

Attempt Number:

3,,E Specimen Specimen Specimen Specimen A

D C

D

12. Record damage to test specimen on a separate sheet and attach.

Steps 9 through 12 witnessed by:

Engineering Regulatory Affairs Quality Assurance

13. Engineering, Regulatory AfTairs and Quality Assurance make a preliminary assessment relative to 10 CFR 71 Record the assessment on a separate sheet and attach.

Determine what changes are necessary in package orientation for the 30-foot free drop to achieve maximum damage.

Test Data Accepted by:

Signature Date Engineering:

Regulatory Affairs:

Quality Assurance:

l

_a

I SENTINEL Test Plan #70 Amersham Corporation September 17,1997 Durtington, Massachusetts Page 49 of 59 Equipment List 4: 30 foot Free Drop Equipment List Enter the Model and Attach inspection Report or Description Serial Number Calibration Certificate Drop Surface, Drawing AT10122. Rev.11 Weight Scale

'ihermometer Thermocouple flexible probe lhermoccuple surface probe Record any additional tools used to facilitate the test and attach the appropriate inspection report or calibration certificate, Verified by:

Signature Date Engineering Regulatory Affairs Quality Assurance i

?

., - - ~

- -. ~,

l SENTINEL Test Plan #70 i

Amersham Corporation September 17,1997

)

Durtington, Massachusetts Page 50 of 59 i

Checklist 4: 304oot Free Drop Test location:

Attempt Number:

Specimen Specimen Specimen Specimen 3tcp A

11 C

D

l. Measure and record test specimen weight.

Record the specimen's weight:

Note the instrument used:

2. Immerse the test specimen in dry lee u need to bring specimen temperature below

-40" C.

4 Steps 1 through 2 witnessed by:

l Engineering Regulatory Affairs Quality Assurance

3. Measure the ambient temperature.

Record ambient temperature:

l Note the instrument used:

4. Attach the test specimen to the release mechanism.

$, Begin video recording of test so that the impact is recorded.

6. Measure the temperature of the specimen.

Ensure that specimen is below -40' C.

j Record the specimen internal temperature:

h Note the instrument used:

Record the specimen surface temperature.

Note the instrument used:

7. Lift and orient the test specimen as shown Figure 11 Figure 12 Figure 13 Figure 14 in the referenced figure for the specimen.

8. Inspect the orientation setup and verify drop height.

9. Photograph the setup in at least two perpendicular planes.

I SENTINEL Test Plan #70 Amersham Corporation September 17,1997 Durhngton. Massachusetts Page 61 of 69 Checklist 4130 foot Free Drop (Continued)

Test location:

Attempt Number:

Specimen Specimen Specimen Specimen Step A

11 C

D Steps 3 through 9 witnessed by:

Engineering Regulatory Affairs Quality Assurance

10. Release the test specimen.

11. Measure the surface temperature of the test specimen.

Record the surface temperature:

Note the instrument used:

12. Measure and record the test specimen's weight.

Record the specimen's weight:

Note the instrument used:

13. Pause the video recorder. Ensure that the point ofimpact and orientation specified in the plan have been achieved and recorded.

14. Recoid damage to test specimen on a separate sheet and attach.

Steps 10 through 14 witnessed by:

Engineering Regulatory Affairs Quality Assurance

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

l SENTINtEL Test Plan #70 l

Amersham Corporation September 17,1997 i

Durtington, Massachusetts Page 52 of 59

]

Checklist 4: 30-foot Free Drop (Continued)

Test Iecation:

Attempt Numl>cr Specimen Specimen Specimen Specimen Step A

11 C

D

~

15. Engineering, Regulatory AiTalrs and Quality Assurance make a preliminary assessment relative to 10 CFR 71. Record the assessment on a separate sheet and attach.

Determine what changes are necessary in package orientation for the puncture test to achles e maximum damage.

Test Data Accepted by signature Date Engineering:

Regulatory Affairs:

Quality Assurance:

2 4

1 d

t r

i

_m,.

.,m.,,

s-w-

-v'---

+---r---

'r-~-

' - - ~ - '

SENTINEL Test Plan #70 Amersham Corporation September 17,1997 Burlington, Massachusetts Page 53 of 69 Equipment List 5: Puncture Test Equipment Enter the Model and Attach inspection Repon or Description Serial Number Calibration Cert 10cate Drop Surface, Drawing AT10122 Rev. Il puncture lilllet, Drawing CT10119, Rev. C Weight Scale 1hermometer

'ihennocouple flexible probe lhermocouple surface probe Record any additional tools used to facilitate the test and attach the appropriate inspection report or calibration certificate.

Verined by:

Signature Date Engineering Regulatory A(Tairs Quality Assurance Checklist 5: Puncture Test Test Location:

Attempt Number:

Specimen Spec men Specimen Specimen SteE A

B C

D

1. Immerse the test specimen in dry ice as need to bring specimen temperature below

{

40'C.

Step I witnessed by:

Engineering Regulatory Affairs Quality Assurance

2. Measure the weight of the specirren.

SENTINEL Test f'lan #70 Amersham Corporation September 17,1997 Burlington, Massachusetts Page 54 of 69 Checklist 5: Puncture Test (Continued)

Test Location:

Atiempt Number Specimen Specimen Specimen Specimen Step A

11 C

D Record the specimen's weight:

Note instrument used:

3. Measure the ambient temperature.

Record ambient temperature:

Note the instrument used:

4. Attach the test specimen to the release mechanism.

5. Begin video recording of test so that the impact is recorded.

6. Measure the surface temperature of the specimen.

Ensure that specimen is below -40* C.

Record the specimen surface temperature.

Note the instrument used:

7. Lill and orient the test specimen as shown Figure 15 Figure 16 Figure 17 Figure 18 in the referenced figure for the specimen.

8. Inspect the orientation setup and verify drop height.

9. photograph the setup in at least two perpendicular planes.

Steps 2 through 9 witnessed by:

Engineering Regulatory AITairs Quality Assurance

10. Release the test specimen.

11. Measure the surface temperature of the test specimen.

Record the surface temperature:

Note the instrument used:

SENTINEL Test Plan 870 Amershem Corporation September 17,1997 Burhngton, Massachusetts Page SS of 59 Checklist 5: Puncture Test (Continued)

Test lecation:

Attempt Number:

Specimen Specimen Specimen Specimen

'q, E A

11 C

D

12. Measure and record the test specimen's weight.

Record the specimen's weight:

Note the instrument used:

13. Pause the video recorder Ensure that the point ofimpact and orientation specified in the plan have been achieved and recorded.

14. Record damage to test specimen on a separate sheet and attach.

5 steps 10 through 14 witnessed by:

Engineering Regulatory Affairs Quality Assurance

15. Engineering, Regulatory AfTairs and Quality Assurance make a preliminary assessment relative to 10 CFR 71. Record the assessment on a separate sheet and attach.

Determine the package orientation for the thermal test that will achieve maximum damage.

Test Data Accepted by:

Signature Date Engineering:

Regulatory Affairs:

Quality Assurance:

SENTINEL Test Plan 870 Amersham Corporation September 17,1997 Burlington, Massachusetts Page 56 of 69 Equipment I,lst 6t Thermal Test Equipment Enter the Model and Attach inspection Report or Description Serial Number Calibration Certificate Air Ilowmeter lhermocouple flexible probe lhermocouple surface probe Oven thermostat Record any additional tools used to facilitate the test and attach the appropriate inspection report or calibration certificate.

Verified by:

Signature Date Engineering Regulatory Affairs Quality Assurance i

4

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

SENTINEL Test Plan #70 Amersham Corporation September 17,1997 Durlington, Massachusetts Page 67 of 59 Checklist 6: Thermal Test Test leration:

Attempt Number:

b "i*'"

b "i*'"

b I**"

b I* *"

E E

E E

Step A

11 C

D

1. Pre-heat the oven to 900' C.

2. Attach the thennocouple the specimen's intemal measuring point.

3. Place the package in the osen and close the oven door.

Record date and time placed in oven.

4. When the specimen temperature exceeds 800* C, start the air now into the oven. Record time.

Steps I through 4 witnessed by:

lingineering Regulatory AfTairs Quality Assurance

5. Measure the oven tempeinture, the specimen's internal and external temperatures and the air How rate.

Record the oven temperature:

Note instrument used:

Record the specimen's internal temperature:

Note instrument used:

Record the specimen's external temperature:

Note instrument used:

Record airnow rate:

Note instrument used:

6. Monitor the specimen temperatures and oven temperature throughout the 30-minute period to ensure that they are above 800* C.

---ma

..__m._

SENTINEL Test Plan 870 Amersham Corporation September 17,1997 Burhngton, Massachusetts Page ES of 59 Checklist 6: Thermal Test (Continued)

Test lecation:

Attempt Number:

Specimen Specimen Specimen Specimen Step A

11 C

D 7, Monitor the airflow throughout the 30 minute period to ensure a rate of at least 3

9.6 A / min.

8. At the end of the 30-minute period, repeat step 5 using the same measurement devices.

Record the oven temperature:

Record the specimen;'s internal temperature:

Record the specimen's external temperature:

Record intake air flow velocity:

Steps 5 through 3 witnessed by:

Engineering Regulatory Affairs Quality Assurance

9. Remove test specimen from the oven.

Record time the specimen is removed.

Describe combustion when door is opened to remove specimen.

NOTE: If specimen continues to burn, let it self extinguish and cool naturally,

10. Measure the ambient temperature.

Record the ambient temperature:

Note the instrument u. d:

11, photograph the test specimen and any subsequent damage

12. Record damage to test specimen on a separate sheet and attach.

Steps 9 through 12 witnessed by:

Engineering Regulatory Affairs Quality Assurance

SENTINEL Test Plan 870 Amersham Corporation September 17,1997 Durtington, Massachusetts Page 69 of 69 Checklist 6: Thermal Test (Continued)

Test leention:

Attempt Numbert Specimen Specimen Specimen Specimen g,,P A

11 C

D

13. Engineering, Regulatory Affairs and Quality Assurance make a preliminary assessment relative to 10 CFR 71. Record the assessment on a separate sheet and attach.

Test Data Accepted by:

Signature Date Engineering:

Regulatory Affairs:

Quality Assurance:

SENTINEL Test Plan #70 Amesham CorporatKm September 17,1997 Duriirgion, Massachusotts Page 69of 59 Chccklist 6: Thermal Test (Continued)

Test letation:

Attempt Number Specimen Specimen Specimen Specimen g,,E A

B C

D

13. Engineering, Regulatory AfTalts and Quality Assurance make a preliminary assessment relative to 10 CFR 71. Record the assessment on a separate sheet and attach.

Test Data Accepted by:

Signature Date D pjneering:

R(,utatory AfTairs:

Quality Assurance:

c,

. ~. - ----

a SENTINEL Test Plan #70 l

Amersham Corporation September 17,1997 J

Burlington, Massachusetts Arpendix A Appendix A l

Drawings 4

j Model 660 Test Specimen j

TP70 Rev.B(1 shect) 1 Mbdel 660 Gamma Ray Projector Shipping Container Descriptive Assembly l

C66025, Rev. F(3 sheets) j Model 660 Gamma Ray Projector Shipping Container Descriptive Assembly i

C66025, Rev. B (4 sheets)

Model 660 Gamma Ray Projector Shipping Container Descriptive Assembly i

C66030, Rev. D (3 sheets) l Model 660 Gamma Ray Projector Shipping Container Descriptive Assembly j

C66030, Rev. A (3 sheets) j Model 660 Gamma Ray Projector Shipping Cor.tainer Descriptive Assembly i

C66030. Rev. -(4 sheets) i I

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SENTINEL Test Plan #70 Amersham Corporation September 17,1997 Burhngton, Masa Phusetts Appendix B Appendix B Referenced Material The following is an excefpt from Avallone, Eugene A., and Theodore Baumeister lit, Editors, Marks' Sfandard Handbookfor Mechanical Engineers, Ninth Edition (New York: McGraw-Hill Book Company,1987), page 4-27, p 415 Approaimate ines4an<urve Locus for Air for the elements C and H, the equations of complete com-bustion are

^ " * '

0 21 50 15 100 121 150 t?$ 200 225 C + O, = CO, H, + 40, = H,0 7' g (H2p 114 ll1 120 124 124 ell 137 143 149 121b + 321b = 441b 2tb + 16tb = 181b T*= " 453 641 629 617 606 394 382 568 555 544 For a combustible compound, as CH., the equation may be h, 250 273 300 325 350 373 400 425 432 written CH + s 0,

• y CO, + t H,0 g 52a 509 49 470 445 4:7 3:6 345 300 Taking. as a basis, I molecute of CH. and making a balance of the atoms on the two sides of the equation,it is seen that

_ ann = hre"" '""**' '""

y=1 t=2 2x== 2F t a or X=2 usa oue to Throtthng A throttimg p'ocess in a cycle of operations always introduces a loss of efliciency. If T. is the temperature corresponding to the back pressure, the loss of CH, + 20, = CO, + 2H,0 available energy is the product of T. and the increase of 16 lb + 64 lb = 44 lb + 36 lb cairopy during the throttling process. The following example The coemcients in the combustion equation give the combin-illustrates the calculation in the case of ammonia passing ing volumes of the gaseous components. Thus, in the last equa.

ihrough the capansion valve of a refrigerating machine, tion i ft' of CH. requires for combustion 2 ft' of oxygen and Es a.et s.

The I. quid ammonia at a temperature of 70*F pams the resulting gaseous products of combustion are i ft'of CO, sh,mish the valve into the bnne cat and 2 ft'of H,0. The coefficieats multiplied by the correspond-and the pressure a 48 21 pasa. The m,in which the temperators is 20 des aial enthalpy of time liquid ammo-bW u W W MW mh h m a, = 120 5. and therefors the 6aal enthalpy is An + s,au.

conveniently referred to I lb of the fuel. In the combustion of f

641 + ssi e, = t 20.5, =hence s, = 0101. The indial entropy is sn CH., for esa mple, I lb of CH. requires 64/16 = 4 lb of oxygen

= 0 254 The 6aal eniropy is sn + (s,a,,/ T ) = 0.344 + 0104 X for complete combustion and the products are 44/16 = 2.75 j

t 113 = 0 260 r = 20 + 460 = 480 hence the loss of refngeratiat Ib of CO, and 36/16 = 2.25 lb of H,0.

e egni a 4s0 x (0 260 - 0 2141 = 2.9 Bt*-

Air Required for Combuscon The composition of air is approximately 0.232 0,and 0 76: N,on a pound basis,or 0.21 O, and 0.79 N, by volume. For exact analyses,it may be nec-coa 480STION essary someti ~ to take account of the water vapor mixed stmani.cas Chisier, " Energy. Combustion and Environment,=

with the air, but ordinanly this may be neglected.

McGraw-Hill,1981 Campbell,"Thermodynanuc Analysis of Combes.

The minimum amount of air required for the combustion of iwa tagines." Wiley.1979 Glassman. "Comtmstion," Acadesuc Press, I lb of a fuelis the quantity of oAygen required,a4 found from Me Yuk.1917 Lefebvre," Gas Turbine Combust.on,"McGraw Hill, the combustion equation, divided by 0.232. Likewise, the min.

N4. Yarn.1981 Sirchlo=, "Combiistion Fondaawatals," McGrs=-

imum volume of air required for the combustion of I ft' of a Hill. New York,1984 Williams et al.," Fundamental Aspects of Solid Rockein." A edor'8P. tLA Oct.1969. Basic therniody.

fuel gas is the volume of osygen dmded by 0.21. For caample, Propetian t

4 names table type enformation needed in titis area es found im Giushko et in the combustion of CH the air required per pound of JH. is at, "Thermodynamec sad Thermophysical Properties of Combustion 4/0.232 = 17.24 lb and the volume of air per cubic foot of Products," Mosco=, and IPST translatica, Gordon, NASA Techsucal CH. is 2/0.21 = 9 52 ft'. Ordinanly, more air is provided than Paper 1906. 498 2,"J A N AF Thermachemical Tables " NSRDS-NBS.

is required for complete combustion. Let a denote the mini-

37. t914 mum amount required and xe the quantity of air admitted, Fue4e For special properties of various fuels, see Sec. 7. In then x - I is the esm.c.emrient.

general, fuels may be classed under three heads: (1) gaseous Products of Combustion The products arising from the fuels. (2) hquid fuels, and (3) solid fuels.

complete combustion of a fuel are CO,, H,0, and, if sulphur The tombumble elements that characterize fuels are car, bon, hydrogen, and. in some cases, sulphur. The complete com-is present, SO, Accompanying these are the nitrogen brought in with the air and the omygen in the excess of air. Hence the bumon of carbon gives as a product, carbon deonide, cog the combustion of hydrogen gives water, H,0 products of complete combustion are pnncipally CO,, H,0, N,, and O, The prmace erCo indicas incomp4m c.mbusuoa. In combustion of Geseous and Uquod Fuels simple calculations the reaction of nitrogen with oxygen to form nonious osides, often termed NO,. such as nitric oxide Combustion Equations The approximate molecular weights of the important elements and compounds entenng into cr m-(NO). nitrogen peroside (NO,) etc,is neglected. In practice, bustaun calculations are.

an automobile engine is run at a lower compression ratio to reduce NO, formation The reduced pollution is bought at the Manal C

11, O.,

N, CO CO, H,0 Cat.

C tt.

C,H.O S NO NO, SO, i

Moluntar weight 12 2 32 28 28 a4 18 16 28 da 32 30 46 64

SENTINEL Test Plan #70 Amersham Corporation September 17,1997 Burlington, Massachusetts Appendix A Appendix A Drawings Model 660 Test Specimen TP70, Rev. D (1 sheet)

Model 660 Gamma Ray Projector Shipping Container Descriptive Assembly C66025, Rev. F (3 sheets)

Model 660 Gamma Ray Projector Shipping Container Descriptive Assembly C66025, Rev. B (4 sheets)

Model 660 Gamma Ray Projector Shipping Container Descriptive Assembly C66030, Rev. D (3 sheets)

Model 660 Gamma Ray Projector Shipping Container Descriptive Assembly C66030, Rev. A (3 sheets)

Model 660 Gamma Ray Projector Shipping Container Descriptive Assembly C66030, Rev. -(4 sheets)

SENTINEL Test Plan #70 Amersham Corporation Snptembe r 17,1997 Buritngton, Massachus9tts Appendix 0 Appendix B Referenced Material Tlie following is an excerpt from Avallone Eugene A., and Theodore flaumeister lil, fiditors, Marks' s

Standard Handbookfor Mechanica/ Engineers, Ninth Edition (New York: McGraw liill flook Company,1987), page 4 27.

ggg Approntmate inversion Curve Locus for Air l'or the elements C and fl, the ecuations of complete com-bustion are

]%

0 25 SO 75 100 12S ISO 671 200 223 C + 0, = CO, 11, + 40, = II,0 ra g pille 114 117 t20 124 t2s 132 137 143 149 12 lb + 32 lb = 44 lb 2 lb + 16 lb = 18 lb g 60 641 629 617 606 594 582 568 $$$ $41 l'or a combustible compound, as Cile, the equation may be 7 ger 250 275 300 325 330 373 400 42$ 412

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06 164 173 184 197 ft! 2 10 26$ 100 g 524 509 491 4 70 441 417 386 341 300 Taking, as a basis, I molecule of Cil, and rnaking a balance f

of the atoms on the two sides of the equation,11 is seen that

.p,,

,melia im e h*I

,,y

,y go, ove to Throttimg A throtthng process in a cycle of operations alesys introduces a loss of efficiency, if T is the Cil + 20, = CO, 4 211,0 temperature corresponding to the back pressure, the loss of 16 lb + 64 lb = 44 lb 4 16 lb available energy is the product of T, and the increase of entropy during the throtthng process. The following c ample lhe cnefDcients in the combustion equation t,ive the combin-illustrates the calculation in the case of ammonia passing ing volumes of the gaseous components. Thus,in the last equa-through the espansion valve of a refrigerating machine, tion i It' of Cll, requires for combustion 2 ft' of onygen and the resulting gaseous products of combustion are I ft'of CO, E s wit The hquid ammonia at a temperature of 70'f. passes and 2 ft'of 110.1 he coefhcients multiphed by the correspond-emugh the vah, mio the brine calin which the temperature is 20 deg 3

and the precure i,48 21 psia The iminal en; hairy of the hquid amme in8 molecular weights give the combining wei hts. These are.

8 conveniently rsferred to I ib of the, fuel. In the combustion on ma n a i

• 120 5, and therefore the f nal emhairy is An + a3 f, r

A.

p 7 + $$) Ias = t 20 %, whence a = 0.101. The initial entropy is af, Cile, for etemple, I ib of Cil. requires 64/16 = 4 lb of oxygen s

0 25a The final entropy is sn+( 3 y/ Ta) = 0144 + 0101 x for complete combustion and the products are 44/16 = 2.75 a

1 Ol = 0 260 T. - 20 e 460 = 480, hence the kan of refriseratins Ib of CO and 36/16 = 2 25 lb of Il 0 i

erreciis 4:0 x to 260 - 0 2$41 = 2 9 Bau.

Ai, n, qui,,4 to, combustion The composition of air is epproximately 0 232 0,and 0 763 N on a pound basis,or 011 a

0, and 0 79 N, by volume l'or exact analyses,it may be nec-COM8UST40N estnry sometimes to take account of the water vapor mixed Rinao.us Chicier, *0nergy, Combustion and Environment,"

with the air, but ordinarily this may be neglected.

McGre.4hti,1981. Camptwit,"Thermixtynamic Analysis of Combus.

The minimum amount of air required for the combustion of uon Engines," Eley,1979 Glassman. " Combustion, Academic Press, i Ib of a fuelis the quantity of onygen required,as found from Nee York 197 7. Lefebvre,* Gas Turbine Combusuon," McGraw Hill, the combustion equation, divided by 0 232. LikcCse, the min.

Nee Yarn,1981 Strehico, " Combustion fundamentats," McGraw*

im m volume of air required for the combustion of I ft' of a Hilt. Nc. Yod. Its4 withants et al," fundamental Aspects of Sohd Propellant Ruckets." Ager#0grapA.114 Oct.1969. Basic thermody' fuel gas is the volume of on)sen d vided by 0.21. F'or example, name table egw informauon needed in this area is found in Olushko et in the combustion of Cll. the air required per pound of Clle is al., "Thermalynamic and Thermophysical Properties of Combustion 4/0 232 = 17.24 lb and the solume of air P'r cubic foot of Pruduen." Macow. and Ipsi translauon, Gordan. NASA Technical Cll. is 2/0.21 = 9 52 f t'. Ordinarily, more air is provided than Papes 1906,1982, "J AN Af Thermochemical Tables," NSRDS-Nits.

is required for complete wmbustion let a denote the mini-37,1971 mum amount required and so the quantity of air admitted, fuels Ior special properties of various fuels, see Sec. 7. In then 4 - 1 is the escas coerhcient.

general, fuels may be classed under three heads: (1) gaseous Products of Cornbust6on The products arising from the Itals,(2) liquid fuels, and (3) solid fuels.

complete combustion of a fuel are CO,11,0, and, if sulphur i

The combustible elements that characterize fuels are car, is present,SO, Accompanying these are the nitrogen brought ben, hydroten, and,in some cases, sulphur. The complete com in with the air and the otygen in the cacess of air. llence the busuon of carbon gives, as a product. c.arbon dioside, CO,: the products of complete combustion are principally CO,,11,O, combustion of bydrogen gives water.s,0.

N,, and O, The prnence of Co induates incomplete combustion. In Combustion of Osseous and liquid Fuele simple calculations the reaction of nitrogtn with otygen to form notious oxides, often termed NO,. such as nitric otide Combusbon Equations The approximate molecular weights (NO), nitrogen perotide (NO,), cic,is neglected. In practice, of the important elements and compounds entering into com-an automobile engine is run at a lower compression ratio to busuon calculations are:

reduce NO, formation The reduced pollution is bought at the Matertal C

it, 0,

N, CO CO, 11,0 Cif.

C,H.

Cdt.O 5 NO NO, SO, Molecutar weight 12 2 32 28 28 a4 18 16 28 46 32 30 46 64

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