Safety Analysis Report for the Models Sentry 110, Sentry 330 and 867 Transport Packages QSA Global, Inc. November 2015 - Revision 4 Burlington, Massachusetts Page 2-54 2.12.11 Test Plan 195 dated 30 June 2010 Document Number Revision •• Test Plan Cover Sheet TEST PLAN 195 SENTRY TRANSPORT PACKAGE STAN•DARD CONFIGURATION Type (B) Transport. Tests -rgnao 5.. Dat: es APRVL Page 1 o•" I. May :200.S : L F-E-I SOS-I RevO Page 1 of I May 2008 , TEST PLAN 19,5 SENTRY TRANSPORT PACKAGE STANDARD CONFIGURATION TYPE (B) TRANSPORT TESTS JUNE 2010 QSA 'GO~loc, Inc Jun 2010 Burlington. Massachusett~s Pagei SECTION 21ITRNPODU TION.......... PT. ON..................... ,..............; SECTION 3 REGULATORY COMPLIANCE........................................1t0 3.2 Normal Transport Condition Tests _.._-...,.......,..-.,.• ,•.. .. •,.....~ 10.. 3.2 .HypotheticalAccident Condition Tests ..........-. .......... ,,...,,..... ...-. _.. ... 10 13• Free Drop Height Akdjustment .,... ..... ,... .... _...• ..... ,...•............. .41 SECTION 4 DISCUSSiON ONSYSTEIM FAILURE MODES OF INTEREST,.;.12 41. Pass Criteria.....,...........- ...... ....... ,. ..... ,........... _:.........,......,,.....,...... .,. 12 , SECTION .S ASSESSMENT OF PACKAGE CONFORMANCE ............ 1......•3 5.1 Hypothetical Accident Conditions (71.51 (a)(2)).;..... .•,.,;,. ....... .. ,,. .......,...; 13 5.2 Transport Package: Contents..•....;...,.,,:,.-.•.,.,.•... ;,...,.......•. SECTION 6 CONSTRUCTION AND CONDITION OF TEST SPECIMENS......14 6.1 Test Specimen Justification. ..... ...... ~.............................. ........... .,1 6.2 S'tru ctural Mat erialJs of Test Spedm en.,.,..•......-.,............. .; .. ;;;;.15-. 6.3 Temperatutre Conditions: ..... ...........•.... .. •........ .- --........ 1.,,5.•.,......i 6.4 Pressure Conditions ... ...........,...............;...............................S..........1 •6.5: Vibration Conditions .... ............. ... .. .. ;....... .,.................... ... ,.... iS SECTION 7 M•ATERIAL AND EQUIPMENT LIST. ..... ................ ,. ... 16 SECTION 8 TEST PROCEDURE...,..,.•,...... ,....,;.•............... ,.,.-....,..1"7 5.1. Test Sequence ...................................................... ...... .......-.. ~...............17 8.2 Test Specimen preparation and InsPection-.•..•........................ .......-.... ....... 1..;...7 8.3" 9m Free Drop Tests per 10:R71.73(c) (1)------,--,.--.....---...-.....-......-.,....•.,.-17 i8.3.1 9 Meter :Free Drop Test Orientation Justification......................................... 18 •8.3.2 9m Free Dl'op Test Set-upts; ... ......... ;....... ....... ;.............-;-...... ......-.-.-......-...-.19 Tet .Plan 195 QSA Global, Inc Jun.2010, Burlingto, Massaht:setts •Page ii .19 &3,4 Pm Fret Drop Test Assessmemt.....,......,....-.. 8.4 Puncture Test per 10 CFR 71,73(). () ....... ,.... .. -.......-............. -..... 20 3.4.1 Puncture Test Orientation. .... ,...........-...... ... .. +...,..,,2 Puencture Test Set-nup,......+..-....,. ,..+....... ...-.......... ..... 21•,....,.,.$ 3.4.3 Punclture Test Assessment•-., .......... .....- ,.-,.+-.., ,....., -.. •,. 22 8.5 Pos't Test Inspection,..... .. +.. ,.,.,...,.. ... ,,.........,......,........... - ...--,.......... ThermelTest Assessment per 10 CF 71.73(c)() •, .+,-..•--, ,. ,,.,.+.-+.+ 23• •8.7 Test Specimen Stoage --......... •....,. ,-- ..-.--. ....... .... ,.. :..... .. , •2 SECTION+91 WORK<SHEETS..............,.............................. ,........,.....24 SENTINEL Test Plan 195 QSA Global, Inc June. 2010 Burlington., Ma~ssachst~tts "Page3 of 29 Test Plan No. 195 Section "1I|ntoduction rA review of the results of Test plan 180 report #2 raised the needi to perform another drop test sequence on~a test specimen built tO the special configuration of the SENTRY transport package. The special configuration, lis: identical tO ,the s•tandard configuration but without, the plastic .inserts assembled into the handling rib- assemblies. The additional testing inviolvies dropping a test 'specimen in the orientation With the rear plate access port ce down towards the drop pad, This orientation: does not provide much impact absorption with the handlinag ribs -attached. The drop test height shall be adjusted higher tha 10 CFR Part 71 drop height requirenientS to give the test specimen the impact energy equivalent to a -SENTRY uwansport package built to the maximum specifie weight of 780 Lbs. This test specimen built to the special configuration in the specified orientation at: :the adjusted height is the worst case test condition for the 'SENTRY transport .package built-to: the sthndardi configuration.. This plan will test the:SENTRY transport package in the special standard ,configuratiOn to :the. test" requiremenmtsor TypeB(U)-96 packages as described in the Code of Federal Regulations, 10"CFR. Part71,. revised as of March 31!, 1999,. The test plan also covers the criteria stated in the LIAEA Regulations~forthe Safe Transport of Radioactive Material, ,Safety Series No.6 1985 Edition (As Amended 1990). This documentdescribes the test specimen, testing: equipment, testing scenario, justifies the pack~oe orientati'on and prov ides test worksheets tO record key steps in the testing sequence. .Roles end Responsibilities: o .Engineering executes the tests according to the test plan and summr'izes the test results. oRegulatory Affairs monitors. the" tests and reviews test-reports for. compliance with regulatory requiremments. oQuality Assuran•e oversees test execution and test report generat ion to assure, compliance, with .the QSA Global Quality Assurance Program. Engineering, Regulatory Affairs and Quality Assurance are jointly re sponsible for assessing test and specimen conditions relative to 10 CFR. 71 and [ABA TS-R- l 1996. QSA Globa Inc Jne•2010 ThuriingtOn,M n~ssazhuseutS Page of29 SectIon 2 TranSpor PackageDescription The SENTRY transport packge• is• a tbmily-of packages', 'consiStinig of 2 ,different:model' numbers. Model. 860 refers to the SENTRY projector- serie~s and Model 867 refers to the :SENTRY source changer•. ,The Moe~lo 860 SENTRY Projector series is fnhrbroken down into 2 pro~jetors types defin~ed by kir ~rated caact for coba]k-60, the SENTRY.330• and SENTRY' •1 0 projectors.• Eazch projector type is available in. either• a standard or basic tanport package configurtion. The standard configurtin will mos likely be the most commonly used version of thet~rasort package. The •basic~confluaion is the sae• aste tndr configuration but"without the array. of remaovable handling .rib assemblies. The Model S67 SE•NTRY source hager is rtdat 3.30 c•urios of cobalt-60. :Similar o te projectors, the. sourcecanger is avaiable in beth a standar•dadbasic configuraton. Figur 2.1 .is a schenmatic o0verview• ofth'eSENTRY transport package conzfiguaion ree. SENTINEL Test Pln 195 QAGObal Inc June 201I0 Page 5 of29 Table 2.1 is a refeuc table comparing the various SETY:~ o akaecnjtwas ** SENTRY 33O 42465-9 & 60011& 78 .&3 Projetor- Stmidard Ys 42465-10 60012 78 2. 30 SENTRY 330 N 42465-9 & 60011& 70 .&3 Projctor-Basic 42465-10 60012 SENTRY 110 p~• m,.IYes 42465-8 60011 580 2.2 110 SENTRY 110 P~tr-Bsc No 4246541 60011 500 2.3 110 smm ore42465-8, 601& SNYSoreiYes 42465-9 & 60011.2&330 C_______-_Standard _ 42465-10 6001230 SENTRY Soturce j24N-8, 60011& 70&. 3 Chager - asic 42465-910 60012 **Indicates configutrion but without plastic imacaU to be tested in this teat pli.. SE1qTIKE TestPlan 195 QSA Globa, n June 2010 Pae6 of 29 Fiue23.SNR Tasoi akg Bai Caigrtln t .... •mjg.2 WcKM.Y *IWW1 Aa. FIgure 2.4 SENTRY Transport Package Comm.. Components All cofgran inld a deplted uaium shield completely encased and fully supported in a cylindrically shaped, stinlems steel, welded body (See Figure 2.4). The weldedx body, also calld.th hel includes two. tube shpd a~cces portos integraly welded on opposite sides of the main body. A twin set of shield mounting barn, one on each side of thea shield, ar welded to the bac~k piat of each aces or tub. Hev dut, SENTINELQSA Global. Inc TestJ•une'2i01 Plan 195, Burlington, Massachusetts Page 7 of29 titanium, shield pins pass through the shield and into bothl shield mounting bars.;ThiS creates.twO positive shield attachmentpoints to :the welded body¢. The shield source tube ends are also inserted into holes in each of the access part back plate. In additio0n.to th1is, the shield is captured and centrally located between the top-and bottom endplates, This combinationi of' shield securing features provide tor a robust Shield support system' within the welded bodly.. .. The inner cavity of the weldedbody, around the shield, is filled with polyurethlane'.foam. The foam_ prevents contamninaticn to and from the depletd uanum shield. Previous thermal tests have shown .charred polyuethnefoam will inhibit the flow of oxygen to the shield and prevent oxidation from-occurring during a. fire as long as the foam remains confined. This is shown on QSA Global test Plan results number 70. Previous test have also shown thle charred foam will not sup.port the shield at temperatures at r above'800 0C. Therefore, the SENTRY relies primarily on thle shield Support system inside the welded body to hold the shielId in place-during the thermal test where temperatures~reach 8000'C., Atitanium source 'tube, cast intO the• center,of the shield, provides:a, conduit for the source wire assembly within, the shield. The source tube of thle SENTFRy projector allows the. source assembly to pas through, the shied. l~owever, .the source tube'of thle SENTRY source changer