ML20207D281
| ML20207D281 | |
| Person / Time | |
|---|---|
| Site: | 07106613, 07109187 |
| Issue date: | 02/28/1999 |
| From: | Claude E, Marrone N, Schlaseman C AEA TECHNOLOGY |
| To: | |
| Shared Package | |
| ML20207D229 | List: |
| References | |
| 81, NUDOCS 9903090291 | |
| Download: ML20207D281 (55) | |
Text
.
1 A64 TECHNOLOGY
'Q5A TEST PLAN NO. 8/
i w
~ TEST PLAN COVER SHEET.
TEST TITLE:
Mom Mz r/wnmrMerscr Tw3r2.9,Lsarev-res7s PRODUCT MODEL:
ORIGINATED BY DA
- . TEST PLAN REVIEW DATE:
ENGINEERING APPROVgA v7
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6VZ/
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QUALITY ASSURANCE APPROVAL:
DATE.
4
$d!~ Y.
NIN W REGULATORY APPROVAL:
.[
A DATE:Sy%d COMMENTS:
f I
l TEST RESULTS REVIEW -
ENGINEERING APPROVAL:
DATE:
QUALITY ASSURANCE APPROVAL:
DATE:
REGULATORY APPROVAL:
DATE:
SENTINEL 9903090291 990224 ~~
PDR,
Test Plan 81 Model 702 Transport Package Type B Transport Tests
/
February 1999 Prepared By: [
Date EEAisF6 C. SCHLASEMAN MPR Checked By:
Dat E. CLAUDE MPR Approved By:
Date J2 h5 99 N.MARRONE MPR
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~ AEA Technology Tsst PLIn 81 i
QSA. loc.
F;bruiry 22.1999 j
Burlington, Massachusetts Pagei l
i Contents i
6 Contents..................~.................................
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i List of Fige 's, Tables and Worksheets
............. ii 1
1.0
. Introduction..............
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i L 2.0 '
Transport Package Description ;
=2
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3.0 Regulatory Compliance...............................
.........5
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4.0 System Failures and Package Orientations.....
..........................6
' 5.0 Assessment of Package Conformance........
7 i
5.1 Regulatory Requirements.....-....................
-7 t
5.2 Test Package Contents.
7 i
I 6.0
~ Construction and Condition of Test Specimens..
-8 7.0 Material and Equipment List..............
=9 1
i 8.0 Test Procedure _.
. 10
........ ~.....
-. =
1 8.1 Roles and Responsibilities......
.... 10
)
8.2 Specimen Temperature Measurement-
........ 1 1.
83 Test Specimen Preparation and Inspection.
_11 8.4 Summary of Test Schedule.....................,......
12 j
'. 8.5 Compression Test (10 CFR 71.71(c)(9))..........
-14 8.5.1 Compression Test Setup.......................
- 14 8.5.2 ~
Compression Test Assessment _
15 8.6 Penetration Test (10 CFR 71.71(c)(10))-
........... 15 8.6.1 Penetration Test Setup -
- 15 1
i i
l 8.6.2 Penetration Test Orientation...........
- 16 1
8.63 Penetration Test Assessment...........................
- 17 8.7 1.2 Meter (4 Foot) Free Drop Test (10 CFR 71.71(c)(7)).........
- 17
)
8.7.1 1.2 Meter (4 Foot) Free Drop Test Setup......
17 8.7.2 1.2 Meter (4 Foot) Free Drop Test Orientation =
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..m AEA Technology Tsst PIIn 81 QSA, Inc.
February 22.1999 Curlington. Massachusetts Page li 8.7.3 1.2 Meter (4 Foot) Free Drop Test Assessment -
.... 18 8.8 First Intermediate Test Inspection :
19 8.9 9 Meter (30 Foot) Free Drop Test (10 CFR 71.73(c)(1)).....................
.I9 8.9.1 9 Meter (30 Foot) Free Drop Test Setup _--
- 19 8.9.2 9 Meter (30 Foot) Free Drop Test Orientation........
.... 20 8.9.3 9 Meter (30 Foot) Free Drop Test Assessment..
20 8.10 Puncture Test (16 CFR 71.73(c)(3))
.21 8.10.1
, Puncture Test Setup.
21 8.10.2 Puncture Test Orientation...............
...... 21 8.10.3 PunctureTest Assessment _.
- _22 8.11 Second Intermediate Test Inspection.....
.23 8.12 Thermal Test (10 CFR 71,73(c)(4)) :
........... 2 3 8.12.1 Test Specimen Orientation
-23 l
8.12.2 7hermalTest Setup
....... 23 I
8.12.3 Thermal Test Procedure--
24 8.12.4' Thermal Test Assessment........
- 24 f
8.13 Final Test inspection......
.... 25 9.0 Worksheets.....
. 26 '
Appendix A:
Drawing TP 81,' Revision A l
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February 22.1999 Burlington, Massachusetts Page lii List of Figures, Tables and Worksheets i
i Figure 1: Isometric View of Model 702 Package...
3 Figure 2: Side View of Model 702 Pack' age.
.4 i
4 Figure 3: Compression Test Setup.....
.. 15 Figure 4: Penetration Test Orientation 17 I
l Figure 5: 1.2 Meter (4 Foot) Free Drop Orientation, Specimen TP81(A)..
L19 1
Figure 6: 9 Meter (30 Foot) Free Drop Orientation, Specimen TP81(A)....
- 21
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Figure 7: Puncture Test Orientation.
_ 23 Specimen Preparation List.-.
. 28 Equipment List 1: Compression Test.-
29 Equipment List 2: Penetration Test -
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Equipment List 3: 1.2 Meter (4 Foot) Free Drop =
- 35 Equipment List 4: 9 Meter (30 Foot) Free Drop
.38 Equipment List 5: Puncture Test
.. 41 Equipment List 6: Thermal Test..
. 44 1
i Checklist 1: Compression Test.
30 J
1 Checklist 2: Penetration Test
_33 j
Checklist 3: 1.2 Meter (4 Foot) Free Drop :
.36 Checklist 4: 9 Meter (30 Foot) Free Drop.................. =
-.39 Checklist 5: Puncture Test..
-2 4
Checklist 6: Thermal Test.:
45 Data Sheet 1: Compression Test _
_ _31 Data Sheet 2: Penetration Test -
.34 Data Sheet 3: 1.2 Meter (4 Foot) Free Drop
- 37
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Data Sheet 4: 9 Meter (30 Foot) Free Drop..................
.40 i
Data Sheet 5: Puncture Test....
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Data Sheet 6: Thermal Test..-.....,
.46 i
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AP Technology C*,A.Inc.
Test Plin 81 Burlington, Massachusetts Fcbru:ry.1999 Page 1 of 46 AEA Technology /QSA Test Plan 81 1.0 Introduction This document describes Type B(U) transport package testing of the AEA Technology Model 702 Transport Package, Certificate of Compliance Number 6613. The purpose of the testing is to demonstrate that the package meets the NRC requirements for Type B(U) packages under Normal Conditions of Transport (10 CFR 71.71), and liypothetical Accident Conditions (10 CFR 71.73), and the criteria stated in
- IAEA Safety Series 6 (1985, as amended 1990).
The test plan specifies the test package configurations, testing equipment and scenarios, justifies the package orientations, and provides test worksheets to record key steps in the testing sequence.
Refer to Appendix A for a descriptive drawing of the package.
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AEA Technology Tcst Plan 81 QSA. Inc.
Fgbru1ry,1999 j
Burlington, Massachusetts Page 2 of 46 2.0 Transport Package Description ne Model 702 Transport Package is 20 inches high,21 inches long, and 19 inches wide in overall dimension. He gross weight of the package is 410 lb. He Model 702 Transport Package consists of the following components:
l Shiocine Cask: He Special Form source is contained in a shipping cask. The outer shell of e
the shipping cask is a 0.18 inch thick stainless steel cylinder with a 3/8 inch thick base, j
Welded to the shell are 24 cooling fins that measure 1/8 inch thick x % inch wide x 10.25 inch long. Inside the outer shell is a 196 lb. depleted uranium (DU) shield. The DU shield has an inner stainless steel liner that is welded at the top to the outer shell. For this test, the source cavity will be filled with a tungsten plug weighing approximately 9 lb., to bound the loaded device weight. '
i Cask Cover Assembiv: A cover assembly encloses the top ponion of the shipping cask. ne e
l cover assembly includes a 21 lb. DU shield encased in a stainless steel shell. The cover assembly flange is anchored to the inner liner of the shipping cask with six 3/8 inch diameter stainless steel bolts. A 1/16 inch thick neoprene rubber gasket is used to seal the cover assembly. The total weight of the cover assembly is approximately 30.lbs.
Skid: The skid consists primarily of % inch thick carbon steel, formed into a flat base with i
rolled " legs" on two sides of the skid. The legs have a height of approximately 4 inches.
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Plates of % inch and 1 inch thickness are welded to the formed skid to provide a mounting l
pedestal for the shipping cask. The shipping cask assembly is attached to the skid with four
% inch diameter bolts (stainless steel).
. Cask Hold Down Assembly: The shipping cask is further secured to the skid by a hold down assembly. The assembly consists of four % inch threaded stainless steel rods that are l
anchored to the skid through bottom " feet" that are welded to the skid. The rods clamp down on a hold down ring that fits on top of the shipping cask and around the cask cover.
Protective Cace: To protect personnel handling the package, a carbon steel cage is placed over the cask. The protective cage assembly is a frame constructed of 1.25 inch square tubing with a wall thickness of 0.120 inches. Perforated,0.047 inch thick steel b attached to the frame.
The frame is attached to the skid with four % inch diameter carbon steel bolts that attach to the skid at tapped holes.
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The Model 702 package is shown in the following figures (Figures I and 2).
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Febru;ry,1999 Burtinaton, Massachusetts Face 4 of 46 I
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Protective Cage (Carbon Steel)
. Hold Down Ring (Catton Steel)
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Hold Down Assembly (Stainless Steel)
Cask Cover Assembly (Stainless Steel and Depleted Uranium)
- Depleted Uranium Shield 4
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- Source Cavity Shipping Cask (Stainless Stee.t)
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kid (Carbon Steel) e s,
Figure 2: Side View of Model 702 Package
AEA Techn: logy Test Plin 81 QSA. Inc.
Febru:ry,1999 Burlington, Massachusetts Page 5 of 46 3.0 Regulatory Compliance The purpose of this plan, which was developed in accordance with AEAT/QSA SOP-E005, is to ensure that the Model 702 Transport Packege meets the Type B trmport package requirements of 10 CFR 71 and I AEA Safety Series No. 6 (1985, as amended 1990)..
j The Normal Conditions of Traraport tests (10 CFR 71.71) to be performed are the compression test, penetration test, and 1.2 meter (4 foot) free drop.
I Water spray preconditioning of the package is not performed es the Model 702 packages are constructed of 1
waterproof materials throughout. The water spray would not contribute to any degradation in structural integrity.
l The 11ypothetical Accident Tests (10 CFR 71.73) to be performed are the 9 meter (30 foot) free drop, puncture test, and themial test (if applicable).
The crush test (10 CFR 71.73(c)(2)) is not performed because the radioactive contents are special-form radioactive material.
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The immersion test and aD other conditions specified in 10 CFR 71 will be evaluated separately.
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FG bruIry.1999 Burhngton, Massachusetts Page 6 of 46 j
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4.0 System Failures and Package Orientations The tests in this plan focus on damaging those components of the package which could result in removal of the cover or which could affect the integrity of the shield.
System failures that could affect package integrity and cause radiological dose rates to exceed the regulatory limits include:
Failure of Cask Cover Bolts - During the free drop or puncture tests, failure of the cask cover bolts could result in the source becoming panially or completely exposed.
Failure of the Cask or Cover Assembly Shell - Failure (e.g., puncture) of the cask or cover assembly or failure of the inner liner to outer shell weld could expose the depleted uranium (DU) shield, which could oxidize during the thermal test.
Because significant damage to the cask itselfis unlikely, the most plausible failure mechanism is failure of the cask cover bolts or the inner liner weld. The cask cover flange is recessed in the top of the cask, and the cover-to-cask clearance is less than the bolt hole clearance. Consequently, the bolts cannot be loaded in shear. Therefore, the orientation considered most likely to cause serious damage during the drop test is a vertical top down orientation. Other orientations may cause failure of the skid or protective cage, or may cause detachment of the cask from the skid. This type of damage, however, would not effect shielding performance. The worst case temperature is the lower limit of-40*C due to embrittlement of the DU and carbon steel components.
In the vertical top down orientation, the maximum tensile load is applied to the cask cover bolts and inner liner weld. The strength of these bolts and the weld must be sufficient to resist the load due to deceleration of the cover assembly plus the tungsten plug. The impact loading due to deceleration of the entire unit is also likely to cause buckling and/or brittle failure of the protective cage structure. Detachment of the cask from the skid is possible due to thread failure of the tapped holes in the skid and brittle failure of the hold down assembly " feet"which are welded to the skid, if the cask becomes detached from the skid in the 30 foot drop test, the subsequent puncture test will be directed at impaning additional damage to the cask cover bolts.
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QSA, Inc.
Februiry,1999 Burlinoton, Massachusetts Page 7 of 46 l
5.0 Assessment of Package Conformance The Model 702 Transport Package must meet the Type B(U) transport package requirements of 10 CFR 71.
The conformance criteria are detailed in the following two sections.
l 5.1 Regulatory Requirements i
Normal Conditions of Transnort Tests (71.43(fi): There should be no loss or dispersal of e
radioactive contents, no significant increase in external surface radiation levels and no substantial red tetien in the effectiveness of the packaging.
HYDothetical Accident Conditions (71.51(aV2)): There should be no escape of radioactive materials greater than A in one week and no external dose rate greater than 2
1 R/hr at one meter from the external surface when the package contains its maximum design radioactive contents.
5.2 Test Package Contents The Model 702 is designed to carry Special Form Sources. Containment of the radioactive source is tested at manufacture. The source capsule design has been certified by the Competent Authority in accordance with the performance requirements for Special Form as specified in 10 CFR Part 71.75 and 49 CFR Part i
73.469.
The test plan therefore does not discuss /specify tests of the containment of the radioactive source. The purgiose of the tests is to demonst9.te that the shielding remains effective within the limits specified by the regulations.
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AEA Technology Tist PI:n 81 QSA. Inc.
Ftbrutry,1999 Burlington, Massachusetts Page 8 of 46 i
6.0 Construction and Condition of Test Specimens For this test plan, one Model 702 test specimen will be used with two protective cages.
l-As the number of 702 units is limited, the test units will be taken from the field population. This represents worst case, as a newly built 702 will have not undergone the abuse of a unit currently in use. If necessary, the unit will be modified to correspond to R-TP81 Rev A.
The Model 702 is not portable; therefore the unit will not be preconditioned prior to the hypothetical j
accident condition tests. Nevertheless, only one cask will be used for both the normal transport and the hypothetical accident condition tests. Following completion of the normal transport condition tests, the protective cage, which is expected to sustain some damage, will be. removed. The second cage will then be installed for the hypotheticaf accident condition tests.
For all Drop Test Cases the temperature of the specimen must be below -40*F at the time of each test, a minimum temperature required 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 carbon l
steel components.
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' AM Tenow Tsst Plan 81
,[, y Bu n on, Massachusetts 7.0 Material and Equipment List The equipment lists, checklists, and data sheets in Section 9.0 list the key materials and equipment specified in 10 CFR 71 and the necessary measurement instruments.
When video recording is specified, select video cameras with the highest shutter speed practical to record testmg.
Additional materials and equipment may be used to facilitate the tests.
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AEA Technology Test Plan 81 QSA, Inc.
F bruiry,1999 Burlington, Massachusetts Page 10 of 46 8.0 Test Procedure One specimen is to be tested to determine the transport integrity of the package. He testing sequence is shown below:
I 1.
Test specimen preparation and inspection 2.
Compression test (10 CFR 71.7)(c)(9))
3.
Penetration test (10 CFR 71.71(c)(10))
i 4.
1.2 Met,er (4 foot) free drop test (10 CFR 71.71(c)(7))
5.
First intermediate test inspection 6.
I.nstallation of second protective cage.
7.
9 Meter (30 foot) free drop test (10 CFR 71.73(c)(1))
8.
Puncture test (10 CFR 71.73(c)(3))
i 9.
Second intermediate test inspection
- 10. Thermal test (10 CFR 71.73(c)(4)) (if applicable - see section 8.12)
- 11. Finaltest inspection The specimen must be put through the entire test sequence. If test conditions such as the orientation at impact are not met during the test, the specimen may be replaced with a specimen of equivalent construction. The replacement must go through the entire test sequence.
If the shipping cask becomes detached from the skid during testing, the cask will be removed from the protective cage, and further testing will concentrate on damaging the cask cover bolts or adding to previous damage.
8.1 Roles and Responsibilities j
The responsibilities of the groups identified in this plan are:
Engineering executes the tests according to the test plan and summarizes the test results.
e Engineering also providea technical input to assist Regulatory Affairs and Quality j
Assurance as needed.
Regulatory Affairs monitors the tests and reviews test reports for compliance with e
regulatory requirements.
Quality Assurance oversees test execution and test report generation to ensure compliance with the AEAT/QSA Quality Assurance Program.
Engineering, Regulatory Affairs, and Quality Assurance arejointly responsible for l
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assessing test and specimen conditions relative to 10 CFR 71.
l Q tality Control, a function that reports directly to Quality Assurance, is responsible for measuring and recording test and specimen data throughout the test cycle.
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Fsbruiry,1999 l
Buriinaton. Massachusetts Page 11 of 46 l
8.2 Specimen Temperature Measurement The penetration, d:op, and puncture tests are to be carried out while the package is at or below -40*C.
l Temperature measurements will be made by positioning thermocouples on the outside surface of the cask j
and on the surface of the cage.
8.3 Test Specimen Preparation and Inspection l
Refer to the Specimen Preparation List in Section 9.0 to ensure that the test sequence is followed. Sign and l.
date the list when completed.
To prepare the test units:
i 1.
Inspect the test units to ensure that they comply with the requirements of Drawing l
TP 81, Revision A.
i l
2.
Weigh the shipping cask and the tungsten plug.
3.
Weigh the assembled test package with cage no.1. Weigh cage no. 2.
l 4.
Perform and record the radiation profile in accordance with AEAT/QSA Work l
Instruction Wl-Q09 for the unit with both cages.
l S.
Quality Control, Engineering, Regulatory Affairs, and Quality Assurance will jointly verify that the test specimens comply with Drawing TP 81, Revision A, and the AEAT/QSA Quality Assurance Program.
i 6.
Prepare the package for transport.
l 7.
Clearly and indelibly mark the units with identification.
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' AEATechnology Test Plan 81 1
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FebruIry,1999 Burhnaton Massachusetts Page 12 of 46 8.4 -
Summary of Test Schedule s
Test Paragraph Specimen Diagram j
Compression 71.71(c)(9)
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AEA Techn: logy Test Plin 81 QSA, Inc.
Burlinaton, Massachusetts Februtry,1999 p.g.33og4g Test Paragraph Specimen' Diagram 9 Meter (30 Foot) 71.73(cXI)
TP81(A)
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Februcry.1999 Burlington, Massachusetts Psoe 14 of 46 I
8.5
' Compression Test (10 CFR 71.71(c)(9))-
The first test is the compression test, per 10 CFR 71.71(c)(9), in which the package is placed under a load f
of at least 2080 pounds. This load is the greater of five times the maximum package weight or 2 lbf/in a multiplied by the vertically projected area:
i 5 x 410 lbf = 2050 lbf 21" wide x 19" long x 2 lbf/in: = 798 lbf Refer to Equipment List I for information about required tools. Use Checklist 1 to ensure that test sequence is followed. Use Data Sheet I to record testing results. Sign and date all action items and record required data on the appropriate worksheets.
8.5.1 Compression Test Setup i
To prepare a specimen for the compression test:
1.
Review the setup shown in Figure 3.
1 2.
Place the specimen on a concrete surface oriented in its normal, upright transport position.
3.
Gradually place a minimum of 2080 pounds uniformly distributed onto the specimen l
as shown in Figure 3.
l 4.
Test specimen in accordance with Checklist 1.
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Buriinaton, Massachusetts Februlry.1999 Paos 15 of 46 l
8.5.2 Compression Test Assessment Upon completion of the test, Engineering, Regulatory Affairs, and Quality Assurance team members willjointly take the following actions:
1.
Review the test execution to ensure that the test was performed in accordance with 10 CFR 71.71.
2.
Make a preliminary evaluation of the specimen relative to the requirements of 10 CFR 71.
3.
Assess the damage to the specimen to decide whether testing of that specimen is to continue.
4.
Evaluate the condition of the specimen to determine if changes are necessary in the package orientation for the penetration test to achieve maximum damage.
8.6 Penetration Test (10 CFR 71.71(c)(10))
The compression test is followed by the penetration test, Mr 10 CFR 71.71(c)(10), in which a penetration bar is dropped frpm a height of at least 40 inches to impr t a specified point on the package. The bar is dropped through free air.
Refer to Equipment List 2 for information about required tools. Use Checklist 2 to ensure that the test sequence is followed. Use Data Sheet 2 to record testing results. Sign and date all action items and record required data on the appropriate worksheets.
8.6.1 Penetration Test Setup This test requires that the test specimen be at -40*C or below 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.
Place the specimen on the drop surface (Drawing AT10122, Revision B) and position it according to the orientation described in the next section.
2.
Position the penetration bar shown in Drawing BT10129, Revision B, directly above the specified point of impact, and raise the bar 40 to 42 inches above the target.
3.
Measure the specimen's surface temperature to ensure that the package is at the required temperature.
4.
Test specimen in accordance with Checklist 2.
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8.6.2 Penetration Test Orientation i
The Model 702 package is placed vertically, right side up on the drop surface specified in Drawing 5
l AT10122, Revision B. The desired impact point is on the perforated steel shell of the protective cage directly above the cask cover, l
PENETRATION BAR DWG8 T10129 N.T i
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WPACT PolNT AT Ib 40 [ f INCHES e
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Burlington, Massachusetts Februiry.1999
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Page 17 of 46 8.6.3 Penetration Test Assessment i
Upon completion of the test, Engineering, Regulatory Affairs, and Quality Assurance team members willjointly take the following actions:
i 1.
Review the test execution to ensure that the test was performed in accordance with 10 CFR 71.
2.
Make a preliminary evaluation of the specimen relative to the requirements of 10 CFR 71.
3.
Assess the damage to the specimen to decide whether testing of that specimen is to contimie.
l 4.
Evaluate the condition of the specimen to determine if changes are necessary in the package orientation for the 1.2 meter (4 foot) free drop test to achieve maximum damage.
8.7 1.2 Meter (4 Foot) Free Drop Test (10 CFR 71.71(c)(7))
He final Normal Transport Conditions test is the 1.2 meter (4 foot) free drop as described in 10 CFR 71.7)(c)(7). He drop compou ids any damage caused in the first two tests. Upon completion of this step, the first intermediate test inspection will be performed.
Refer to Equipment List 3 for information about required tools. Use Checklist 3 to ensure that the test sequence is followed. Use Data Sheet 3 to record testing results. Sign and date all action items and record required data on the appropriate worksheets.
8.7.1 1.2 Meter (4 Foot) Free Drop Test Setup In this test, the package is released from a heigi.t of four feet and lands on the steel drop surface specified in Drawing AT10122, Revision B.
This test requires that the test specimen be at -40*C or below at the time ofimpact. Follow the instructions in the appropriate checklist for measuring and recording the test specimen temperature i
before and after the drop.
To set up a package for the 1.2 meter (4 foot) free drop test-1.
Use the drop surface specified in Drawing AT10122, Rev. B.
j 2.
Measure and record the test specimen temperature to emue $at the package is at the specified temperature.
3.
Place the specimen on the drop surface and position it according to the orientation shown in Figure 5.
4.
Raise the package so that the impact target is 4.0 and 4.5 feet above the drop surface.
5.
Test specimen in accordance with Checklist J.
l
Test PL:n 81 Burhnaton, Massachusetts February,1999 Pace 18 of 46 8.7.2 1.2 Meter (4 Foot) Free Drop Test Orientation The impact surface of Specimen TP81(A) is the top of the protective cage as shown below.
TEST SPECNEN LIFT CABLE ATTACHMENT
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3
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7[1h.lN?!(
s wp bNI l$h
,m djj
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DROP SURFACE DWG8 T10122 4
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aa Figure 5.1.2 Meter (4 Foot) Free Drop Test Orientation, Specimen TP81(A) l l
i 8.7.3 1.2 Meter (4 Foot) Free Drop Test Assessment Upon completion of the test, Engineering, Regulatory Affairs, and Quality Assurance team members willjointly perform the following tasks:
4
Tcst Plin 81 Burlington. Massachusetts February,1999 Pace 19 of 46 1.
Review the test execution to ensure that the test was performed in accordance with 10 CFR 71.71.
2.
Make a preliminary evaluation of the specimen relative to the requirements of 10 CFR 71.71.
3.
Assess the damage to the specimen to decide whether testing of that specimen is to continue.
4.
Evaluate the condition of the specimen to determine if changes are necessary in package orientation for the 9 meter (30 foot) free drop to achieve maximum damage.
5.
Measur.e and record any damage to the test specimen.
6.
Perform and record the radiation profile in accordance with AEAT/QSA Work Instruction WI-Q09.
8.8 First Intermediate Test inspection Engineering, Regulatory Affairs, and Quality Assurance team members will make an assessment of the test specimen and jointly determine whether the specimen meets the requirements of 10 CFR 71.71.
8.9 9 Meter (30 Foot) Free Drop Test (10 CFR 71.73(c)(1))
The first Hypothetical Accident Conditions test is the 9 meter (30 foot) free drop as described in 10 CFR 71.73(c)(1). This drop uses the same orientation as the 1.2 meter (4 foot) free drop.
Refer to Equipment List 4 for information about required tools. Use Checklist 4 to ensure that the test sequence is followed. Use Data Sheet 4 to record testing results. Sign and date all action items and record required data on the appropriate worksheets.
8.9.1 9 Meter (30 Foot) Free Drop Test Setup In this test, the package is released from a height of thirty feet and lands on the steel drop surface specified in Drawing AT10122. Revision B.
This test requires that the test specimen be at -40*C or below at the time ofimpact. Follow the instructions in the appropriate checklist for measuring and recording the test specimen temperature before and after the drop.
To set up a package for the 9 meter (30 foot) free drop test:
1.
Install the second protective cage on the skid in accordance with Drawing TP 81, Revision A.
2.
Use the drop surface roccified in Drawing AT10122, Rev. B.
3.
Measure and record the test specimen temperature to ensure that the package is at the specified temperature.
4.
Place the specimen on the drop surface and position it according to the orientation shown in Figure 6.
5.
Raise the package so that the impact target is 30 and 31 feet above the drop surface.
e
Test Plan 81 Burlington, Massachusetts Ftbrurry.1999 Paos 20 of 46 6.
Test the specimen in accordance with Checklist 4.
8.9.2 9 Meter (30 Foot) Free Drop Test Orientation l
The impact surface of Specimen TP81(A) is the top of the protective cage as shown below.
l TEST SPECIMEN l
uFT CAsLE l
[
LIFT CABLE I
ATTACHMENT
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" 9 %\\ug:'
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f IMPACT SURFACE 30,
FEET rop SURFACE DWG8 T10122 8
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l Figure 6. 9 Meter (30 Foot) Free Drop Orientation, Specimen TP81(A) 1 l
l 8.9.3 9 Meter (30 Foot) Free Drop Test Assessment Upon completion of the test, Engineering, Regulatory Affairs, and Quality Assurance team members'willjointly perform the following tasks:
l 1.
Review the test execution to ensure that the test was performed in accordance with i
10 CFR 71.73, and in accordance with the impact orientation and other conditions specified in this plan.
i
-~~ _
T1st PLin 81 Burhnaton, Massachusetts F1brutry,1999 Pace 21 of 46 2.
Make a preliminary evaluation of the specimen relative to the requirements of 10 CFR 71.
1 3.
Assess the damage to the specimen and take one of the following actions based on
{
the assessment:
If the cask does not detach from the skid, evaluate the condition of the specimen e
to determine if changes are necessary in package orientation for the puncture test to achieve maximum damage.
If the cask detaches from the skid, remove the cask from the protective cage. If there is any visible damage to the cask, orient the cask so that puncture testing adsis to the prior damage. If there is no obvious damage, then concentrate on damaging the cask cover bolts.
i l
8.10 Puncture Test (10 CFR 71.73(c)(3))
The 9 meter (30 foot) free drop is followed by the puncture test, per 10 CFR 71.73(c)(3), in which the package is dropped from a height of at least 40 inches onto the puncture 1:illet specified in the Drawing CT10119, Revision C.
The billet is to be bolted to the drop surface used in the free drop tests. The 12-inch high puncture billet meets the minimum height (8 inches) required in 10 CFR 71.73(c)(3). The specimen has no projections or i
overhanging members longer than 8 inches, which could act as impact absorbers, thus allowing the billet to cause the maximum damage to the specimen.
I Refer to Equipment List 5 for information about required tools. Use Checklist 5 to ensure that the test sequence is followed. Use Data Sheet 5 to record testing results. Sign and date all action items and record required data on the appropriate worksheets.
This test requires that the test specimen be at -40*C or below at the time ofimpact. Follow the instructions in the appropriate checklist for measuring and recording the test specimen temperature before and after the drop.
8.10.1 Puncture Test Setup To set up a test specimen for the puncture test:
1.
Measure and record the test specimen temperature to ensure that the package is at the specified temperature.
2.
Position the unit according to the orientation shown in Figure 7 or as assessed above.
3.
Check the alignment of the specified center-of-gravity with the targeted point of impact.
4.
Raise the package so that there are 40 to 42 inches between the package and the top of the puncture billet.
5.
Test the specimen in accordance with Checklist 5.
i 8.10.2 Puncture Test Orientation l
l
Test Plan 81 Buriinaton. Massachusetts Fsbrutry.1999 Page 22 of 46 The 702 package is dropped vertically, top down onto the puncture billet specified in Drawing CT10119, Revision C. He orientation of the package is shown below. The desired impact point is on the perforated steel of the protective cage, directly below the cask cover.
.s kI)
CENTER OF GRAVITY p
h 4PN hf
't
'4 TEST SPECIMEN e
i IMPACT SURFACE 40 [ 2 INCHES PREVIOUS 8
l PENETRATION IMPACT PUNCTURE BILLET U
DWG# T10119 (4) ATTACHMENT BOLTS DROP SURFACE DWG# T10122 5
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3 Figure 7. Penetration Test Orientation 8.10.3 Puncture Test Assessment Upon completion of the test, Engineering, Regulatory Affairs, and Quality Assurance team members willjointly perform the following tasks:
1.
Review the test execution to ensure that the test was performed in accordance with 10 CFR 71.73, and in accordance with any other conditions specified in this plan.
2.
Make a preliminary evaluation of the specimen relative to the requirements of 10 CFR 71.73.
i l
1 AEA Technology Test PLIn 81 QSA. inc.
F4 brut ry,1999 Burlington, Massachusetts Pace 23 of 46 3.
Assess the damage to the specimen to decide whether testing of the specimen is to continue.
8.11 Second Intermediate Test inspection Perform a second intermediate test inspection of specimen after the puncture test and befbre the thermal test.
1.
Measure and record any damage to the test specimen.
2.
Reassemble the package using an active source.
3.
Measure and record a radiation profile of the test specimen in accordance with AEAT/QSA Work Instruction WI-Q09.
4.
Reassemble the package using the same simulated source used in the specimen during the previous tests.
5.
Make sure that the source position and the package configuration are the same as they were immediately after the puncture test.
6.
Weigh the package.
7.
Review all results and decide whether a thermal test should be performed.
8.12 Thermal Test (10 CFR 71.73(c)(4))
e -
The final deitement is the thermal test specified in 10 CFR 71.73(c)(4). The thermal performance of the package may be evaluated by analysis rather than by testing depending on the damage sustained by the package following the puncture test. The assessment as to whether to continue with the thermal test will be documented in the secend intermediate test inspection described above.
Refer to Equipment List 6 for information about required tools. Use Checklist 6 to ensure that the test sequence is followed. Use Data Sheet 6 to record testing results. Sign and date all action items and record required data on the appropriate worksheets.
8.12.1 Test Specimen Orientation The decision to perform thermal testing will be based on an assessment of the damage sustained by the package following the puncture test. The thermal test orientation will also be determined based on an assessment of the test specimen condition.
8.12.2 Thermal Test Setup To ensure suflicient heat input to the test specimens, the oven will be pre-heated to a temperature of not less than 810*C. This temperature, above the required 800*C, includes an allowance for measurement uncertainty.
The test environment is a vented electric oven capable of creating a time weighted average temperature of 800*C.
Thermocouples will be attached to the specimen top, bottom, and two side surfaces. The external thermocouples will be shielded from the radiant heat of the oven so that the surface temperature of the transport package can be accurately measured.
eV1
Test Picn 81 Burfington, Massachusetts Fcbru ry,1999 Page 24 of 46 When the oven has been pre-heated to greater than 810*C, the package will be placed in the oven in the orientation determined to be worst case. When the surface temperature has risen to no less than 510*C, the test will start. The package will remain in the oven for a period of 30 minutes after the start of the test.
To allow for combustion, the oven door will remain slightly open. It has been determined that a gap of one inch at the top and bottom of the oven door allows airflow into the oven and allows the oven to maintain its temperature. The oven door is 36 inches long. As a result, there will be about a 36 square inch opening at voth the top and bottom of the furnace door. 'Ihis allows for the natural convection of air into the furnace.
If the specimen is burning when the oven is opened, the unit will be allowed to extinguish by itself and then cool naturally. Appropriate measures should be taken to avoid the radiological risks associated with this potential hazard. The final evaluation of the package is performed when the specimen reaches ambient temperature.
8.12.3 Thermal Test Procedure
(
To perform the thermal test:
1.
Attach the thermocouples to the top, bottom and sides (180* apart) of the test specimen.
2.
Preheat the oven temperature to not less than 810*C.
3.
When the oven temperature is stable at above 810*C, place the specimen in the oven, 4
and partially close the door.
4.
When the temperature of the all surfaces of the specimen rise above 810*C, stan the 30-minute time interval.
5.
Throughout the test, measure and record the oven and the test specimen temperatures.
6.
At the end of the 30 minute time interval, open the oven door and shut off the oven.
WARNING: If the package is burning, appropriate safety measures must be in place to avoid the risks associated with burning depleted uranium. Consult with the oven operator and other appropriate personnel 7.
Allow the package to self-extinguish and cool.
8.
Record any damage to the package and make a photographic and radiographic record of shield position and damage.
8.12.4 Thermal Test Assessment Upon completion of the test, Engineering, Regulatory Affairs, and Quality Assurance team members willjointly perform the following task:
I.
Review the test execution to ensure that the test was performed in accordance with 10 CFR 71.73 and the test conditions specified in this plan.
...~...- _..
~.. ~... _
Tstt Plan 81 i
Buriington, Massachusetts Ftbrutry,1999 Page 25 of 46 2.
Make a preliminary evaluation of the specimen relative to the requirements of 10 1
CFR 71.
j 8.13 Final Test inspection I
Perform the following inspections after completion of all the required testing:
l.
Measure and record any damage to the test specimen, i
2.
Measure and record a radiation profile of the test specimen in accordance with AEAT/QSA Work Instmetion W1-Q09.
3.
Document and assess the radiation level at one meter from the surface of the package.
)
4.
Determine whether it is necessary to dismantle the test specimen for inspection of hidden component damage or failure.
5.
If proceeding with the inspection, record and photograph the process of removing any component.
6.
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 te'st specimen, andjointly determine whether the specimen meets the requirements of 10 CFR 71.73.
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I 4
Test Plan 81 Bur 16naton, Massachusetts February,1999 Pace 26 of 46 9.0 Worksheets Use the following worksheets for executing these tests. There are three worksheets for each' test: an equipment list, a checkUst, and a data sheet.
Use the equipment list to record the serial number of each measurement device used. Attach a copy of the relevant inspection report or calibration certificate after verifying the range of 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 i
ensure the testing is performed in accordance with this test plan and 10 CFR 71.
l Make copies of the forms for* additional attempts. Maintain records of all attempts.
Note: Equipment List 6, Checklist 6, and Data Sheet 6 will only be required ifit is determined that i
damage to a specimen is sufficient w warrant a thermal test.
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1 AEA Technology Tott PLIn 81 QSA. inc.
FebruIry,1999 i
Burlington, Massachusetts Page 27 of 46 l
Specimen Preparation List l
Step TP81(A) 1.
Serial Number:
i 2.
Weight of tungsten plug (ib):
3.
Weight ofcask (lb):
4.
Total weight of package (Ib) with Cage 1:
5.
Total weight of package (Ib) with Cage 2:
6.
All fabrication and inspection records documented in accordance with the AEAT QA Program?
7.
Does the unit comply with the requirements of Drawing TP 81, Revision A?
8.
Has the radiation profile been recorded in accordance with AEAT QSA Work Instruments Wi-Q097 9.
Is the package prepared for transport?
Verified by:
Print Name:
Signature:
Date:
l Engineering Regulatory Affairs Quality Assurance J
l 1
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i I
l
I AM Tecno%y Test Plin 81 Bu on, Massachusetts
,g, f Equipment List 1: Compression Test Enter the Model and Serial Attach Inspection Description Number Repon or Calibration Certificate Weight Scale g
Record any additional tools used to facilitate the test and attach the appropriate inspection repon or calibration certificate.
Print Name:
Signature:
Date:
Completed by:
Verified by:
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f AEA Technology Test Plan 81 i
QSA, Inc.
Februiry,1999 Burlington, Massachusetts Pat.' 79 of 46 Checklist 1: Compression Test i
Step TP81(A) j 1.
Position the specimen on concrete surface, per the appropriate drawing.
Figure 3 j
2.
. Measure the ambient temperature.
Note the instrument used 3.
Apply a uniformly distributed weight of at least 2080 pounds on the top of the i
protective cage for a period of 24 hours2.777778e-4 days <br />0.00667 hours <br />3.968254e-5 weeks <br />9.132e-6 months <br />.
i Record the actual weight:
1 Note me instrument used:
Record start time and date:
4.
After 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 time and date:
S.
Measurethe ambient temperature.
Note the instrument used:
1 6.
Photograph the test specimen and record any damage on Data Sheet 1.
j 7.
Engineering, Regulatory Affairs and Quality Assurance make a preliminary assessment relative to 10 CFR 71. Record the assessment on Data Sheet 1.
Determine what changes are necessary in package orientation for the penetration j
test to achieve maximum damage.
Verified by:
Print Name:
Signature:
Date:
1 Engineering Regulatory Affairs Qcalitv Assurance i
i l
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.. -. -... ~ - - -. _ -
i AM Techno%y Test Plon R1 OSA. 384 -
February,1999 Burlington. Massachusetts Pane 30 of 46 l
i Data Sheet 1: Compression Test i
\\
Test Unit Model and Serial Number:
Test Specimen:
TP 81 (A)
J l
l Test Date:
Test Time:
Test Plan 81 Step No.: 8.5 Describe test orientation and setup:
l l
Describe on-site inspection (damage, broken parts, etc.):
l l
l On-site assessment 1
l l
l l
l-Engineering:
Regulatory:
QA:
Describe any post-test disassembly and inspection:
Describe any change in source position:
Describe results of any pre-or post-test radiography:
Completed by:
Date:
)
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t AEA Technology Test Plin 81 QSA. Inc, Februiry,1999 l
Burlington, Massachusetts Pace 31 of 46 l
l i
Equipment List 2: Penetration Test l
l Enter the Modeland Serial Attach inspection Report or Description Number Calibration Certificate Penetration Bar Drawing BT10129, Rev. B l
l Drop Surface Drawing AT10122, Rev. B i
l Thermometer Thermocouple t
i l
Thermocouple Record any additional tools used to facilitate the test and attach the appropriate inspection report or calibration certificate.
l 1
[
l Print Name:
Signature:
Date:
Conipleted by:
Verified by:
i
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AEA Technology Test Plan 81 QSA, Inc.
i FebnCry,1999 Burlington, Massachusetts Page 32 of 46 Checklist 2: Penetration Test Step TP81(A) l 1.
Immerse specimen in dry ice or cool in freezer to bring specimen below -40*C.
2.
Position the package as shown in the referenced figure.
Figure 4 3.
Begin video recording of the test.
4.
Inspect the orientation setup and verify the bar height.
t J
5.
Photograph the set-up in at least two perpendicular planes.
6.
Measure the ambient temperature and the specimen's surface temperature. Ensure that the specimen is at the specified temperature.
Record the ambient temperature:
Note the instrument used:
Record the specimen's surface temperatures:
No'tethe instrument used:
7.
Drop the penetration bar.
8.
Check to ensure that penetration bar hit the specified area.
9.
Measure the specimen's surface temp. Ensure that specimen is at specified temp.
Note the instrument used:
- 10. Photograph the test specimen and record any damage on Data Sheet 2.
j l 1.
Engineering, Regulatory Affairs and Quality Assurance make a preliminary assessment relative to 10 CFR 71. Record the assessment on Data Sheet 2.
Determine what changes are necessary in package orientation for the 1.2 meter (4 foot) free drop to achieve maximum damage.
Verified by:
Print Name:
Signature:
Date:
Engineering Regulatory Affairs Quality Assurance o
l
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/5.A Technology QSA, Inc.
Test PI:n 81 Burlington Massachusetts Fcbru::ry. F99 Page 33 of 46 l
Data Sheet 2: Penetration Test l
Test Unit Model and Serial Number:
Test Specimen:
TP 81 (A)
Test Date:
Test Time:
Test Plan 81 Step No.: 8.6 L
f Describe test orientation and setup:
l l
Describe impact (location, rotation, etc.):
Describe on-site inspection (damage, broken parts, etc.):
i l
On-site assessment:
i l
1 1
Engineering:
Regulatory:
QA:
l Describe any post-test disassembly and inspection.
l i
1 Describe any change in source position:-
NOT APPLICABLE Describe results of any pre-or post-test radiography:
I Completed by:
Date:
f b
)
9 AEA Technology.
Test Pbn 81 QSA, Inc.
Ftbrutry,1999 Burlington, Massachusetts Page 34 of 46 Equipment List 3: 1.2 Meter (4 Foot) Free Drop Enter the Model and Serial Attach Inspection Description Number Report or Calibration Certificate Drop Surface Drawing AT10122, Rev. B Thermometer Thermocouple Thermocouple Record any additional tools used to facilitate the test and attach the appropriate inspection report or calibration certificate.
Print Name:
Signature:
Date:
Completed by:
Verified by: '
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l AEA Techn: logy Test Pun 81 QSA, Inc.
F:brutry.1999 Buriington, Massachusetts Page 35 of 46 Checklist 3: 1.2 Meter (4 Foot) Free Drop Step TP81(A)
~
1.
Immerse specimen in dry ice or cool in freezer to bring specimen below -40 C.
2.'
Measure the ambient temperature.
2 Note the instrument used:
3.
Attach the test specimen to the release mechanism.
4.
Begin video recording of the test.
5.
Measure specimen surface temperature. Ensure specimen is at specified temp.
Record the specimen's surface temperature:
Note the instrument used:
6.
Lifi and orient the test specimen as shown in the specified referenced figure.
Figure 5 7.
- Inspect the orientation setup and verify drop height.
8.
Photograph the set-up in at least two perpendicular planes.
9.
Release the test specimen.
- 10. Measure specimen surface temperature. Ensure specimen is at specified temp.
Record the specimen's surface temperatures:
Note the instrument used:
- 11. Photograph the test spechnen and record any damage on Data Sheet 3.
- 12. Measure and record a radiation profile of the test specimen in accordance with AEAT/QSA Work Instruction Wl-Q09.
- 13. Engineering, Regulatory Affairs and Quality Assurance make a preliminary assessment relative to 10 CFR 71. Record assessment on Data Sheet 3. Determine what changes are necessary in package orientation for the 9 meter free drop to achieve maximum damage.
Verified by:
Print Name:
Signature:
Date:
Engineering Regulatory Affairs Quality Assurance
Test Plin 81 February,1999 Burtington Massachusetts Page 36 of 46 Data Sheet 3: 1.2 Meter (4 Foot) Free Drop Test Unit Model and SerialNumber:
Test Specimen:
TP 81 (A)
Test Date:
Test Time:
Test Plan 81 Step No.: 8.7 Describe drop orientation and drop height:
Describe impact (location, rotation, etc.):
Describe on-site inspection (damage, broken parts, etc.):
l l
On-site assessment:
l Engineering:
Regulatory:
QA:
l Describe any post-test disassembly and inspection:
l l
Describe any change in source position:
NOT APPLICABLE Describe results of any pre-or post-test radiography:
Completed by:
Date:
~....-
AEA Technology T2st PLin 81 QSA, Inc.
FIbrutry,1999 l
Burlington, Massachusetts Page 37 of 46 l
Equipment List 4: 9 Meter (30 Foot) Free Drop Enter the Model and Serial Attach Inspection Description Number Report or Calibration Certificate Drop Surface Drawing AT10122, Rev. B Thermometer Thermocouple Thermocouple Record any additional tools used to facilitate the test and attach the appropriate inspection report or calibration certificate.
Print Name:
Signature:
Date:
Completed by:
Verified by:
{-
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t AEA Technology Test PtJn 81 QSA. Inc.
February.1999 Burlington, Massachusetts Pace 38 of 46 Checklist 4: 9 Meter (30 Foot) Free Drop Step TP81(A) 1.
Immerse specimen in dry ice or cool in freezer to bring specimen below -40*C.
- 2. ' Measure the ambient temperature.
Note the instrument used:
3.
Attach the test specimen to the release mechanism.
4.
Begin Video Recorfing of the test.
5.
Measure specimen's surface temperature. Ensure specimen is at the specified temperature.
Record the specimen's surface temperature:
Note the instrument used:
6.
Lift and orient the test specimen as shown in the specified referenced figure.
Figure 6 7.
Inspect the orientation setup and verify drop height.
8.
Photograph the setup in at least two perpendicular planes.
9.
Release the test specimen.
- 10. Measure specimen's surfue temperatures. Ensure specimen is at specified
- temperature.
Record the specimen's surface temperature:
1 Note the instrument used:
1 1
~ l1. Photograph the test specimen and record any damage on Data Sheet 4.
- 12. Engineering, Regulatory Affairs and Quality Assurance make a prehmma.'/
assasment relative to 10 CFR 71. Record assessment on Data Sheet 4. Determ:ne,
what changes are necessary in package orientation for the puncture test to achieu l
maximum damage.
Verified by:
Print Name:
Signature:
Date:
. Engineering i
. Regulatory Affairs l-Quality Assurance l
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AEA Technology Test Pirn 81 QSA. Inc.
February.1999 Burlington, Massachusetts Pace 39 of 46 Data Sheet 4: 9 Meter (30 Foot) Free Drop Test Unit Model and SerialNumber:
Test Specimen:
TP 81 (A)
Test Date:
Test Time:
Test Plan 81 Step No.: 8.9 Describe drop orientation and drop height:
1 Describe impact (location, rotation, etc.):
Describe on-site inspection (damage, broken parts, etc.):
On-site assessment:
i J
Engineering:
Regulatory:
QA:
Describe any post-test disassembly and inspection:
j i
Describe any change in source position:
NOT APPLICABLE Describe results of any pre-or post-test radiography:
l Completed by:
Date:
l i
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9 l
Test P!In 81 Buriington, Massachusetts February.1999 Page 40 of 46 Equipment List 5: Puncture Test Enter the Model and Serial Attach inspection Description Number Report or i
i Calibration Certificate l.
Drop Surface Drawing AT10122, Rev. B i
Puncture Billet Drawing CT10119, Rev. C 1
Thermometer.
l Thennocouple Thermocouple 1
Record any additional tools used to facilitate the test and attsch the appropriate inspection report or calibration certificate.
Print Name:
Signatu:e:
Date:
Completed by:
Verified by:
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AEA Technology Test Ptn 81
- QSA, Inc.
February,1999 i
Buriington, Massachusetta Page 41 of 46 Checklist 5: Puncture Test Step TP81(A) i 1.
Immerse specimen in dry ice or cool in freezer to bring specimen temp, below -40*C.
+
2.
Measure the ambient temperature.
Note the instrument used:.
1 3.
Attach the test specimen to the release mechanism.
l 4.
Begin Video Recording of the test.,
5.
Measure specimen's surface temperature. Ensure that specimen is at specified temperature.
Record the specimen's surface temperature:
Note the instrument used:
l 6.
Lift and orient the test specimen as shown in the specified referenced figure.
Figure 7 7.
Inspect the orientation setup and verify drop height.
8.
Photograph the set-up in at least two perpendicular planes.
9.
Release the test specimen.
- 10. Measure the specimen's surface temperature.
Record the specimen's surface temperature:
Note the instrument used:
i 1.
Photograph the test specimen and record any damage on Data Sheet 5.
i i
- 12. Engineering, Regulatory Affairs and Quality Assurance make a preliminary assessment relative to 10 CFR 71. Record assessment on Data Sheet 5. Determine what changes are necessary in package orientation for thermal test to achieve maximum damage.
Verified by:
Print Name:
Signature:
Date:
1 I
Engineering Regulatory Affairs Quality Assurance i
i i
1.
L Ii t
AEA Techn11ogy QM Inc.
Test Plan 81 Burlington, Massachusetts February,1999 page 42 of 46 Data Sheet 5: Puncture Test Test Unit Model and Serial Number:
Test Specimen:
TP 81 (A)
Test Date:
Test Time:
Test Plan 81 Step No.: 8.10 Describe drop orientation and drop height:
Describe impact (location, rotation, etc.):
Describe on-site inspection (damage, broken parts, etc.):
On-site assessment:
Engineering:
Regulatory:
QA:
Describe any post-test disassembly and inspection:
Describe any change in source position:
NOT APPLICABLE 1
Describe results of any pre-or post-test radiography:
l
)
Completed by:
Date:
l
.... _. _ ~
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AEA Technology Tat Ptn 81 QM inc.
February,1999 Burbngton. Massachusetts page 43 of 46 Equipment List 6: Thermal Test Enter the Model and Serial Attach Inspection Description Number Report or Calibration Certificate Hermocouple 1 Hennocouple 2 Thermocouple 3 Oven Oven thermostat Record any additional tools used to facilitate the test and attach the appropriate inspection report or calibration certificate.
l Print Name:
Signature:
Date:
Completed by:
3 l
Verified by:
i l
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Test Plan 81 Burlington, Massachusetts February,1999 i
Page 44 of 46 l
Checklist 6: Thermal Test l
Step TP81(A) l 1.
Attach the thermocouples the specimen's measuring points.
)
1 2.
Preheat the oven to a temperature of 810 C.
l 3.
Place the package in the oven in the worst case orientation and partially close the oven door such that a 1 inch by 36 inch opening is provided. Record the time.
4.
When all of the test specimen's turface temperatures exceed 810*C, begin the 30-minute time interval. Record the time.
5.
Monitor and record the test specimen and the oven temperatures throughout the 30-minute period to ensure that they are above 810 C 6.
At the end of the 30-minute test period, shut off the oven and open the door.
Record the time.
7.
Describe combustion when door is opened to remove specimen:
NOTE: If specimen cortinues to burn, let it self-extinguish and cool naturally.
8.
Measure and record the ambient temperature.
9.
Photograph the test specimen and record any damage on Data Sheet 6.
- 10. If necessary, radiograph the unit to document its condition.
I 1.
Engineering, Regulatory Affairs and Quality Assurance make a preliminary assessment relative to 10 CFR 71. Record assessment on Data Sheet 6.
Verified by:
Print Name:
Signature:
Date:
Engineering Regulatory Affairs Quality Assurance I
i
- 7. -
1-AEA Technolo9Y Test Ptn 81 QSA, Inc.
Februcry,1999 Buriington, Massachusetts Page 45 of 46 l
Data Sheet 6: Thermal Test Test Unit Model and Serial Number:
Test Specimen:
TP 81 (A)
Test Date:
Test Time:
Test Plan 81 Step No.: 8.12 t
i Describe test orientation and setup-t i
Describe package during testing:
Describe on-site inspection (damage, broken parts, etc.):
On-site assessment:
l l
Engineering:
Regulatory:
QA:
Describe any post-test disassembly and inspection:
l Describe any change in source position:
NOT APPLICABLE Describe results of any pre-or post-test radiography:
Completed by:
Date:
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