SSP-41172_Rev_AD.docx

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Human Space Flight Technical Integration Contract (HSFTIC) Federal contract opportunity
Solicitation number
80JSC019R0023
Issued by
National Aeronautics and Space Administration Johnson Space Center

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This notice announces a forthcoming Request for Proposal for the Human Space Flight Technical Integration Contract. NASA/JSC plans to issue the RFP on or about November 1, 2019, with proposals due on or about December 11, 2019. The procurement is a total small business set-aside under NAICS code 541715 with a size standard of 1,250 employees. The contract will provide technical integration services for human space flight programs. Interested parties should monitor the specified websites for the RFP release and any amendments. All technical questions must be submitted in writing.

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SSP-41172 Rev AD

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Cage Code 2B945 National

Aeronautics and

Space

Administration International

Space

Station

Program Johnson

Space

Center Houston, T exas

NAS15-10000

International

Space Station Program Qualification and Acceptance Environmental T est Requirements

Revision

AD

28 April

Type 4 EXPORT CONTROLLED - The technology or software is subject to the Export Administration Regulations (15 C.F.R. Parts 730-774). Export, re-export or retransfer contrary to U.S. law is prohibited. EAR

/ECCN 9E002

SSP 41172 Revision AD

REVISION AND HISTORY PAGE

REV.
DESCRIPTION
PUB.DATE
SRR Version (Reference: SSCBD 00002)
01/24/94
A
Updated to reflect incorporation of approved exceptions taken by the Product Groups; Added Appendices A, B, and C that documents these exceptions.

Incorporates ECP 145 (SSCBD 000145, Effective 10/31/95) 11/21/95

B
Updated to reflect incorporation of approved exceptions taken by the Product Groups;

Incorporates ECP 217 (SSCBD 000217, Effective 02/26/96) 04/04/96

DCN 001 incorporates ECP 151 (SSCBD 000151, Effective 02/18/98)
03/19/98
DCN 002 incorporates ECP 263 (SSCBD 000263, Effective 10/03/97)
03/19/98
DCN 003 incorporates ECP 346 (SSCBD 000346, Effective 03/28/97)
03/19/98

The following DCNs have been cancelled. The contents of the SSCNs authorizing the release of the DCNs have been incorporated into Revision C.

DCN 006 (SSCN 000845) (Administrative Cancel) DCN 007 (SSCN 000671) (Administrative Cancel) DCN 008 (SSCN 000877) (Administrative Cancel) DCN 009 (SSCN 000915) (Administrative Cancel) DCN 010 (SSCN 000844) (Administrative Cancel) DCN 011 (SSCN 001029) (Administrative Cancel) DCN 012 (SSCN 001030) (Administrative Cancel) DCN 013 (SSCN 001051) (Administrative Cancel) DCN 014 (SSCN 001052) (Administrative Cancel) DCN 004 (SSCN 000290) (Administrative Cancel) DCN 015 (SSCN 000823) (Administrative Cancel) DCN 016 (SSCN 000673) (Administrative Cancel) DCN 017 (SSCN 001050) (Administrative Cancel) DCN 018 (SSCN 001056) (Administrative Cancel) DCN 019 (SSCN 001392) (Administrative Cancel) DCN 020 (SSCN 000672) (Administrative Cancel) DCN 021 (SSCN 000908) (Administrative Cancel) DCN 022 (SSCN 000909) (Administrative Cancel) DCN 023 (SSCN 001048) (Administrative Cancel) DCN 024 (SSCN 000809) (Administrative Cancel) DCN 025 (SSCN 000842) (Administrative Cancel) DCN 026 (SSCN 001085) (Administrative Cancel) DCN 027 (SSCN 001198) (Administrative Cancel) DCN 028 (SSCN 001182) (Administrative Cancel) DCN 029 (SSCN 001112) (Administrative Cancel) DCN 030 (SSCN 001391) (Administrative Cancel) DCN 031 (SSCN 000585) (Administrative Cancel) DCN 032 (SSCN 001047) (Administrative Cancel) DCN 033 (SSCN 000542) (Administrative Cancel) DCN 034 (SSCN 001276) (Administrative Cancel) DCN 035 (SSCN 001338) (Administrative Cancel) DCN 036 (SSCN 001506) (Administrative Cancel) DCN 037 (SSCN 001390) (Administrative Cancel) DCN 005 (SSCN 000333) (Administrative Cancel)

SSP 41172 Revision AD 28 April 2017

Export Controlled – EAR/ECCN 9E002 REVISION AND HISTORY PAGE - continued

REV.
DESCRIPTION
PUB.DATE
C
Revision C, Type 2

Incorporates SSCNs 000290, 000333, 000542, 000585, 000671, 000672, 000673, 000809, 000823, 000842, 000844, 000845, 000877, 000908, 000909, 000915, 001029, 001030, 001047, 001048, 001050, 001051, 001052, 001056, 001085, 001112, 001182, 001198, 001276, 001338, 001390, 001391, 001392, 001506, and 001073.

The following DCNs have been cancelled. The contents of the SSCNs authorizing the release of the DCNs have been incorporated into Revision D.

DCN 038 (SSCN 001268) (Administrative cancellation) DCN 039 (SSCN 000473) (Administrative cancellation) DCN 040 (SSCN 001410) (Administrative cancellation) DCN 041 (SSCN 001724) (Administrative cancellation) DCN 042 (SSCN 000640) (Administrative cancellation) DCN 043 (SSCN 000855) (Administrative cancellation) DCN 044 (SSCN 001088) (Administrative cancellation) DCN 045 (SSCN 001379) (Administrative cancellation) DCN 046 (SSCN 001520) (Administrative cancellation) DCN 047 (SSCN 001651) (Administrative cancellation) DCN 048 (SSCN 001747) (Administrative cancellation) DCN 049 (SSCN 001802) (Administrative cancellation) DCN 050 (SSCN 001933) (Administrative cancellation) DCN 051 (SSCN 001845) (Administrative cancellation) DCN 052 (SSCN 000890) (Administrative cancellation) DCN 053 (SSCN 001703) (Administrative cancellation) DCN 054 (SSCN 002171) (Administrative cancellation) DCN 055 (SSCN 002285) (Administrative cancellation) DCN 056 (SSCN 002394) (Administrative cancellation) DCN 057 (SSCN 002395) (Administrative cancellation) DCN 058 (SSCN 002172) (Administrative cancellation) DCN 059 (SSCN 002366) (Administrative cancellation) DCN 060 (SSCN 002016) (Administrative cancellation) DCN 061 (SSCN 002522) (Administrative cancellation) DCN 062 (SSCN 002389) (Administrative cancellation) 02/25/99

D
Revision D, Type 2

Incorporates SSCNs 000473, 000640, 000855, 000890, 001088, 001268, 001379, 001410, 001520, 001651, 001703, 001724, 001747, 001802, 001845, 001933, 002016, 002171, 002172, 002285, 002366, 002389, 002394, 002395, and 002522.

Revision D incorporates Non−Prime SSCNs 001200, 001250, 01306, 001348, 001350, 001382, 001487, 001595, 001628, 001763, 001851, 002013, 002157, 002201, 002373, 002374, and 002505.

10/15/99

DCN 063 incorporates SSCD 002398 Eff. 10/26/99
01/10/00

The following DCNs have been cancelled. The contents of the SSCNs authorizing the release of the DCNs have been incorporated into Revision E.

DCN 064 incorporates SSCN 002601 (Administrative cancellation) DCN 065 incorporates SSCN 002594 (Administrative cancellation) DCN 066 incorporates SSCN 002338 (Administrative cancellation) DCN 067 incorporates SSCN 002591 (Administrative cancellation)

DCN 068 incorporates SSCN 002593 (Administrative cancellation) DCN 069 incorporates SSCN 002767 (Administrative cancellation) DCN 070 incorporates SSCN 002768 (Administrative cancellation) DCN 071 incorporates SSCN 002582 (Administrative cancellation) DCN 072 incorporates SSCN 002585 (Administrative cancellation) DCN 073 incorporates SSCN 002640 (Administrative cancellation) DCN 074 incorporates SSCN 002216 (Administrative cancellation) DCN 075 incorporates SSCN 002592 (Administrative cancellation) DCN 076 incorporates SSCN 002442 (Administrative cancellation) DCN 077 incorporates SSCN 002757 (Administrative cancellation)

DCN 078 incorporates SSCN 002275 (Administrative cancellation) DCN 079 incorporates SSCN 002795 (Administrative cancellation) Notes: SSCNs 002275 and 002795 bring onto Prime the Non−Prime changes incorporated into Revision D

E
Revision E, Type 2

Incorporates SSCNs 002216, 002338, 002442, 002582, 002585, 002591, 002592, 002593, 002594, 002601, 002640, 002757, 002767, 002768, 002275, 002795, and 002620.

DCN 080 (SSCN 002914) (Administrative cancellation) DCN 081 (SSCN 001586) (Administrative cancellation) DCN 082 (SSCN 002660) (Administrative cancellation) DCN 083 (SSCN 002982) (Administrative cancellation) DCN 084 (SSCN 002400) (Administrative cancellation) 04/11/00

F
Revision F, Type 2

Incorporates SSCNs 001586, 002400, 002660, 002914, 002982, and 003008.

DCN 085 (SSCN 002587) (Administrative cancellation) DCN 086 (SSCN 002964) (Administrative cancellation) DCN 087 (SSCN 002934) (Administrative cancellation) DCN 088 (SSCN 003255) (Administrative cancellation) DCN 089 (SSCN 003082) (Administrative cancellation) DCN 090 (SSCN 003571) (Administrative cancellation) DCN 091 (SSCN 003570) (Administrative cancellation) DCN 092 (SSCN 003569) (Administrative cancellation) DCN 093 (SSCN 003531) (Administrative cancellation) DCN 094 (SSCN 003532) (Administrative cancellation) DCN 095 (SSCN 003533) (Administrative cancellation) DCN 096 (SSCN 003682) (Administrative cancellation) DCN 097 (SSCN 003492) (Administrative cancellation) DCN 098 (SSCN 003683) (Administrative cancellation) DCN 099 (SSCN 003684) (Administrative cancellation) DCN 100 (SSCN 003511) (Administrative cancellation) DCN 101 (SSCN 003542) (Administrative cancellation) DCN 102 (SSCN 002586) (Administrative cancellation) DCN 103 (SSCN 003292) (Administrative cancellation) DCN 104 (SSCN 003293) (Administrative cancellation) DCN 105 (SSCN 003294) (Administrative cancellation) DCN 106 (SSCN 003572) (Administrative cancellation) DCN 107 (SSCN 003573) (Administrative cancellation) 01/16/01

DCN 108 (SSCN 003642) (Administrative cancellation) DCN 109 (SSCN 003654) (Administrative cancellation) DCN 110 (SSCN 003699) (Administrative cancellation) DCN 111 (SSCN 003701) (Administrative cancellation)

G
Revision G, Type 2

Incorporates SSCNs 002586, 002587, 002934, 002964, 003082, 003255, 003292, 003293, 003294, 003492, 003511, 003531, 003532, 003533, 003542, 003569, 003570, 003571, 003572, 003573, 003642, 003654, 003682, 003683, 003684, 003699, 003701, and 003702.

DCN 112 (SSCN 002689) (Administrative Cancellation) DCN 113 (SSCN 002793) (Administrative Cancellation) DCN 114 (SSCN 003123) (Administrative Cancellation) DCN 115 (SSCN 003074) (Administrative Cancellation) DCN 116 (SSCN 003034) (Administrative Cancellation) DCN 117 (SSCN 003700) (Administrative Cancellation) DCN 118 (SSCN 004064) (Administrative Cancellation) DCN 119 (SSCN 004296) (Administrative Cancellation) 01/16/01

H
Revision H, Type 2

Incorporates SSCNs 002689, 002793, 003034, 003074, 003123, 003700, 004064, 004296, and 001637.

DCN 120 (SSCN 003133) (Administrative Cancellation) DCN 121 (SSCN 003952) (Administrative Cancellation) DCN 122 (SSCN 002995) (Administrative Cancellation) DCN 123 (SSCN 003955) (Administrative Cancellation) DCN 124 (SSCN 003979) (Administrative Cancellation) DCN 125 (SSCN 003606) (Administrative Cancellation) DCN 126 (SSCN 003528) (Administrative Cancellation) DCN 127 (SSCN 003963) (Administrative Cancellation) DCN 128 (SSCN 003408) (Administrative Cancellation) DCN 129 (SSCN 003044) (Administrative Cancellation) DCN 130 (SSCN 001371) (Administrative Cancellation) DCN 131 (SSCN 003035) (Administrative Cancellation) DCN 132 (SSCN 004105) (Administrative Cancellation) DCN 133 (SSCN 001450) (Administrative Cancellation) DCN 134 (SSCN 003530) (Administrative Cancellation) DCN 135 (SSCN 004289) (Administrative Cancellation) DCN 136 (SSCN 004917) (Administrative Cancellation) DCN 137 (SSCN 004647) (Administrative Cancellation) DCN 138 (SSCN 003276) (Administrative Cancellation) DCN 139 (SSCN 003978) (Administrative Cancellation) DCN 140 (SSCN 004434) (Administrative Cancellation) DCN 141 (SSCN 003751) (Administrative Cancellation) DCN 142 (SSCN 004306) (Administrative Cancellation) DCN 143 (SSCN 004458) (Administrative Cancellation) DCN 144 (SSCN 004902) (Administrative Cancellation) DCN 145 (SSCN 003526) (Administrative Cancellation) DCN 146 (SSCN 003491) (Administrative Cancellation) DCN 147 (SSCN 004134) (Administrative Cancellation) 02/23/01

DCN 148 (SSCN 003887) (Administrative Cancellation) DCN 149 (SSCN 004509) (Administrative Cancellation) DCN 150 (SSCN 003599) (Administrative Cancellation)

J
Revision J, Type 2

Incorporates SSCNs 001371, 001450, 002995, 003035, 003044, 003133, 003276, 003408, 003491, 003526, 003528, 003530, 003599, 003606, 003751, 003887, 003952, 003955, 003963, 003978, 003979, 004105, 004134, 004289, 004306, 004434, 004458, 004509, 004647, 004902, 004917, and 003920.

DCN 151 (SSCN 004947) (Administrative Cancellation) DCN 152 (SSCN 005019) (Administrative Cancellation) DCN 153 (SSCN 003273) (Administrative Cancellation) DCN 154 (SSCN 004354) (Administrative Cancellation) DCN 155 (SSCN 004383) (Administrative Cancellation) DCN 156 (SSCN 002027) (Administrative Cancellation) DCN 157 (SSCN 003477) (Administrative Cancellation) DCN 158 (SSCN 004684) (Administrative Cancellation) DCN 159 (SSCN 004287) (Administrative Cancellation) DCN 160 (SSCN 005281) (Administrative Cancellation) DCN 161 (SSCN 004309) (Administrative Cancellation) DCN 162 (SSCN 003775) (Administrative Cancellation) DCN 163 (SSCN 004485) (Administrative Cancellation) DCN 164 (SSCN 003953) (Administrative Cancellation) DCN 165 (SSCN 003655) (Administrative Cancellation) DCN 166 (SSCN 003434) (Administrative Cancellation) DCN 167 (SSCN 003608) (Administrative Cancellation) DCN 168 (SSCN 003825) (Administrative Cancellation) DCN 169 (SSCN 004457) (Administrative Cancellation) DCN 170 (SSCN 004644) (Administrative Cancellation) DCN 171 (SSCN 002486) (Administrative Cancellation) DCN 172 (SSCN 003877) (Administrative Cancellation) DCN 173 (SSCN 004948) (Administrative Cancellation) DCN 174 (SSCN 005271) (Administrative Cancellation) DCN 175 (SSCN 004433) (Administrative Cancellation) DCN 176 (SSCN 003529) (Administrative Cancellation) 05−18−01

K
Revision K, Type 2

Incorporates SSCNs 002027, 002486, 003273, 003434, 003477, 003529, 003608, 003655, 003775, 003825, 003877, 003953, 004287, 004309, 004354, 004383, 004433, 004457, 004485, 004644, 004684, 004947, 004948, 005019, 005271, 005281, and 005124.

DCN 177 (SSCN 003334) (Administrative Cancellation) DCN 178 (SSCN 005503) (Administrative Cancellation) DCN 179 (SSCN 003286) (Administrative Cancellation) DCN 180 (SSCN 002944) (Administrative Cancellation) DCN 181 (SSCN 002186) (Administrative Cancellation) 07−25−01

L
Revision L, Type 2

Incorporates SSCNs 002186, 002944, 003286, 003334, 005503, and 002341.

11−13−01

DCN 182 (SSCN 005612) (Administrative Cancellation) DCN 183 (SSCN 005727) (Administrative Cancellation) DCN 184 (SSCN 003479) (Administrative Cancellation) DCN 185 (SSCN 003493) (Administrative Cancellation) DCN 186 (SSCN 005939) (Administrative Cancellation) DCN 187 (SSCN 005896) (Administrative Cancellation)

M
Revision M, Type 2

Incorporates SSCNs 003479, 003493, 005612, 005727, 005896, 005939, and 005321.

DCN 188 (SSCN 006077) (Administrative Cancellation) DCN 189 (SSCN 005895) (Administrative Cancellation) DCN 190 (SSCN 001000) (Administrative Cancellation) DCN 191 (SSCN 006220) (Administrative Cancellation) DCN 192 (SSCN 004209) (Administrative Cancellation) DCN 193 (SSCN 006242) (Administrative Cancellation) 12/21/01

N
Revision N, Type 2

Incorporates SSCNs 001000, 004209, 005895, 006077, 006220, 006242, and 004996.

DCN 194 (SSCN 006347) (Administrative Cancellation) DCN 195 (SSCN 006359) (Administrative Cancellation) DCN 196 (SSCN 006438) (Administrative Cancellation) DCN 197 (SSCN 006392) (Administrative Cancellation) DCN 198 (SSCN 003517) (Administrative Cancellation) DCN 199 (SSCN 004383S) (Administrative Cancellation) DCN 200 (SSCN 003524) (Administrative Cancellation) 04-08-02

P
Revision P, Type 2

Incorporates SSCNs 003517, 003524, 004383S, 006347, 006359, 006392, 006438, and 006383.

DCN 201 (SSCN 006703) (Administrative Cancellation) DCN 202 (SSCN 004879) (Administrative Cancellation) 06-27-02

R
Revision R, Type 2

Incorporates SSCNs 004879, 006703, and 006681.

DCN 203 (SSCN 006890) (Administrative Cancellation) DCN 204 (SSCN 006243) (Administrative Cancellation) DCN 205 (SSCN 007021) (Administrative Cancellation) 10-07-02

T
Revision T, Type 2

Incorporates SSCNs 006243, 006890, 007021, and 007047.

DCN 206 (SSCN 005004) (Administrative Cancellation) DCN 207 (SSCN 006258) (Administrative Cancellation) DCN 208 (SSCN 007355) (Administrative Cancellation) 12-17-02

U
Revision U, Type 2

Incorporates SSCNs 005004, 006258, 007355, and 007356.

04-11-03

DCN 209 (SSCN 004099) (Administrative Cancellation) DCN 210 (SSCN 007720) (Administrative Cancellation) DCN 211 (SSCN 007721) (Administrative Cancellation) DCN 213 (SSCN 008182) (Administrative Cancellation)

V
Revision V, Type 2

Incorporates SSCNs 004099, 007720, 007721, 008182, and 004911.

The following DCNs have been cancelled. The contents of the SSCNs authorizing the release of the DCNs have been incorporated into Revision W.

DCN 212 (SSCN 007761) (Administrative Cancellation) DCN 214 (SSCN 009219) (Administrative Cancellation) DCN 215 (SSCN 008231) (Administrative Cancellation) DCN 216 (SSCN 009309) (Administrative Cancellation) 10−04−04

W
Revision W, Type 2

Incorporates SSCNs 007761, 009219, 008231, 009309 and 009125.

The following DCNs have been cancelled. The contents of the SSCNs authorizing the release of the DCNs have been incorporated into Revision Y.

DCN 217 (SSCN 009866) (Administrative Cancellation) DCN 218 (SSCN 009728) (Administrative Cancellation) DCN 219 (SSCN 009964) (Administrative Cancellation) DCN 220 (SSCN 009881) (Administrative Cancellation) DCN 221 (SSCN 004911S) (Administrative Cancellation) 12−12−05

Y
Revision Y, Type 2

Incorporates SSCNs 009866, 009728, 009964, 009881, 004911, and 009935.

The following DCNs have been cancelled. The contents of the SSCNs authorizing the release of the DCNs have been incorporated into Revision AA.

DCN 222 (SSCN 010676) (Administrative Cancellation) DCN 223 (SSCN 011013) (Administrative Cancellation) DCN 224 (SSCN 010801) (Administrative Cancellation) DCN 225 (SSCN 010791) (Administrative Cancellation) DCN 226 (SSCN 010471) (Administrative Cancellation) 07−30−07

AA
Revision AA

Incorporates SSCNs 010676, 011013, 010801, 010791, 010471, and 011498.

11−22−10

AB
Revision AB

Incorporates SSCN 013632.

09−19−13

AC
Revision AC

Incorporates SSCN 014318 and 014474.

06-29-15

AD
Revision AD

Incorporates SSCN 015572.

10-13-17

ERU: /s/Beth Mason 10-13-17

PREFACE

The contents of this document are intended to be consistent with the tasks and products to be prepared by the International Space Station Program Participants.

The Qualification and Acceptance Environmental Test Requirements shall be implemented on all new Space Station Program contractual and internal activities and shall be included in any existing contracts through contract changes.

This document is under the control of the Space Station Control Board (SSCB). Any future updates and/or revisions to this document has been delegated to the Multilateral Vehicle Control Board (MVCB) for approval with previous concurrence from the Requirement, Test and Verification Panel (RTVP).

This document establishes the minimum uniform requirements for qualification and acceptance environmental tests for Components, Structures, Assemblies and Flight Elements.

i Export Controlled – EAR/ECCN 9E002

NASA/ASI

INTERNATIONAL SPACE STATION PROGRAM

QUALIFICATION AND ACCEPTANCE ENVIRONMENTAL TEST REQUIREMENTS

28 April 2017

N/A

For NASA

DATE

N/A

For ASI

DATE

NASA/CSA

INTERNATIONAL SPACE STATION PROGRAM

N/A

For NASA

DATE

N/A

For CSA

DATE

Agreed to in principal subject to completion of detailed review by CSA and its contractor.

NASA/ESA

N/A

For NASA

DATE

N/A – No segment specification call out.

For ESA

DATE

NASA/JAXA

N/A

For NASA

DATE

N/A – No segment specification call out.

For JAXA Concurrence

DATE

NASA/ROSCOSMOS

N/A

For NASA

DATE

N/A – No segment specification call out

For RSA

DATE

CONCURRENCE

LIST OF CHANGES

28 April 2017

All changes to paragraphs, tables, and figures in this document are shown below:

SSCBD
ENTRY DATE
PARAGRAPH
Incorporation Action
015572
02-28-2017
Preface
Incorporated per SSCN 015572
015572
02-28-2017
1.4
Incorporated per SSCN 015572
015572
02-28-2017
2.0
Incorporated per SSCN 015572
015572
02-28-2017
2.1
Incorporated per SSCN 015572
015572
02-28-2017
3.3
Incorporated per SSCN 015572
015572
02-28-2017
4.1
Incorporated per SSCN 015572
015572
02-28-2017
4.2.2.3B
Incorporated per SSCN 015572
015572
02-28-2017
4.2.2.4
Incorporated per SSCN 015572
015572
02-28-2017
4.2.3.3B
Incorporated per SSCN 015572
015572
02-28-2017
4.2.3.3C
Incorporated per SSCN 015572
015572
02-28-2017
4.2.3.4
Incorporated per SSCN 015572
015572
02-28-2017
4.2.5.3
Incorporated per SSCN 015572
015572
02-28-2017
4.2.6.3
Incorporated per SSCN 015572
015572
02-28-2017
4.2.7.3
Incorporated per SSCN 015572
015572
02-28-2017
4.2.11.2A
Incorporated per SSCN 015572
015572
02-28-2017
4.2.11.2B
Incorporated per SSCN 015572
015572
02-28-2017
4.2.11.2F
Incorporated per SSCN 015572
015572
02-28-2017
4.2.11.2J
Incorporated per SSCN 015572
015572
02-28-2017
4.2.11.2K
Incorporated per SSCN 015572
015572
02-28-2017
5.1.2.3B
Incorporated per SSCN 015572
015572
04-25-2017
5.1.2.4
Incorporated per SSCN 015572
015572
02-28-2017
5.1.3.3B
Incorporated per SSCN 015572
015572
02-28-2017
5.1.3.3C
Incorporated per SSCN 015572
015572
04-25-2017
5.1.3.4
Incorporated per SSCN 015572
015572
02-28-2017
5.1.4.3A
Incorporated per SSCN 015572
015572
02-28-2017
5.1.4.3B
Incorporated per SSCN 015572
015572
02-28-2017
5.1.4.3C
Incorporated per SSCN 015572
015572
02-28-2017
5.1.5.3
Incorporated per SSCN 015572

LIST OF CHANGES − Continued

SSCBD
ENTRY DATE
PARAGRAPH
Incorporation Action
015572
02-28-2017
5.1.7.2
Incorporated per SSCN 015572
015572
02-28-2017
5.1.7.2A
Incorporated per SSCN 015572
015572
02-28-2017
5.1.7.2B
Incorporated per SSCN 015572
015572
02-28-2017
5.1.7.2F
Incorporated per SSCN 015572
015572
02-28-2017
5.1.7.2J
Incorporated per SSCN 015572
015572
02-28-2017
5.1.7.2K
Incorporated per SSCN 015572
015572
02-28-2017
5.1.8.3B
Incorporated per SSCN 015572
015572
02-28-2017
6.1.1A
Incorporated per SSCN 015572
015572
02-28-2017
6.1.1B
Incorporated per SSCN 015572
015572
02-28-2017
6.1.1C
Incorporated per SSCN 015572
015572
02-28-2017
6.1.1D
Incorporated per SSCN 015572
015572
02-28-2017
6.1.2.3B
Incorporated per SSCN 015572
015572
02-28-2017
8.2
Incorporated per SSCN 015572
015572
02-28-2017
10.2
Incorporated per SSCN 015572
015572
02-28-2017
10.3
Incorporated per SSCN 015572
015572
02-28-2017
4.2.1.2
DQA: Changed “leakage” to “leak”
015572
02-28-2017
4.4.3.3
DQA: Changed (MEFL) to MEFL
015572
2-28-2017
5.1.1.2
DQA: Changed “leakage” to “leak”

LIST OF CHANGES − Continued

SSCBD
ENTRY DATE
TABLES
Incorporation Action
015572
02-28-2017
3-1
Incorporated per SSCN 015572
015572
02-28-2017
4-1
Incorporated per SSCN 015572
015572
02-28-2017
5-1
Incorporated per SSCN 015572
015572
07-21-2017
9-1
Incorporated per SSCN 015572
015572
02-28-2017
9-2
Incorporated per SSCN 015572

LIST OF CHANGES − Continued

SSCBD
ENTRY DATE
FIGURES
Incorporation Action
015572
03-05-2017
5-2
Incorporated per SSCN 015572
015572
03-05-2017
5-3
Incorporated per SSCN 015572

TABLE OF CONTENTS

PARAGRAPH
TITLE
PAGE
1.0INTRODUCTION1 – 1
1.1PURPOSE1 – 1
1.2SCOPE1 – 1
1.3PRECEDENCE1 – 1
1.4DELEGATION OF AUTHORITY1 – 1
2.0APPLICABLE DOCUMENTS2 – 1
2.1REFERENCE DOCUMENTS2 – 2
3.0GENERAL3 – 1
3.1REQUIREMENT FOR TEST3 – 1
3.2TEST CONDITION TOLERANCES3 – 1
3.3INTEGRATION AND VERIFICATION RECORDS3 – 4
4.0QUALIFICATION TESTING4 – 1
4.1ACCEPTANCE AND QUALIFICATION RELATIONSHIP4 – 1
4.2COMPONENT QUALIFICATION4 – 1
4.2.1FUNCTIONAL TEST, COMPONENT QUALIFICATION4 – 3
4.2.1.1PURPOSE4 – 3
4.2.1.2TEST DESCRIPTION4 – 3
4.2.1.3SUPPLEMENTARY REQUIREMENTS4 – 3
4.2.2THERMAL VACUUM TEST, COMPONENT QUALIFICATION4 – 4
4.2.2.1PURPOSE4 – 4
4.2.2.2TEST DESCRIPTION4 – 4
4.2.2.3TEST LEVELS AND DURATION4 – 4
4.2.2.4SUPPLEMENTARY REQUIREMENTS4 – 7
4.2.2.5DEPRESS/REPRESS VACUUM REQUIREMENTS4 – 8
4.2.2.5.1OPERATING4 – 8
4.2.2.5.2AUTOMATED POWER DOWN4 – 8
4.2.3THERMAL CYCLING TEST, COMPONENT QUALIFICATION4 – 9
4.2.3.1PURPOSE4 – 9
4.2.3.2TEST DESCRIPTION4 – 9
4.2.3.3TEST LEVELS AND DURATION4 – 9
4.2.3.4SUPPLEMENTARY REQUIREMENTS4 – 11
4.2.4SINUSOIDAL VIBRATION TEST, COMPONENT QUALIFICATION4 – 11
4.2.4.1PURPOSE4 – 11
4.2.4.2TEST DESCRIPTION4 – 11
4.2.4.3TEST LEVELS AND DURATION4 – 11
Table of Contents - continued
Paragraph
Title
Page
4.2.4.4SUPPLEMENTARY REQUIREMENTS4 – 12
4.2.5RANDOM VIBRATION TEST, COMPONENT QUALIFICATION4 – 12
4.2.5.1PURPOSE4 – 12
4.2.5.2TEST DESCRIPTION4 – 12
4.2.5.3TEST LEVELS AND DURATION4 – 12
4.2.5.4SUPPLEMENTARY REQUIREMENTS4 – 13
4.2.6ACOUSTIC VIBRATION TEST, COMPONENT QUALIFICATION4 – 13
4.2.6.1PURPOSE4 – 13
4.2.6.2TEST DESCRIPTION4 – 14
4.2.6.3TEST LEVELS AND DURATION4 – 14
4.2.6.4SUPPLEMENTARY REQUIREMENTS4 – 14
4.2.7PYROTECHNIC SHOCK TEST, COMPONENT QUALIFICATION4 – 14
4.2.7.1PURPOSE4 – 14
4.2.7.2TEST DESCRIPTION4 – 14
4.2.7.3TEST LEVELS AND EXPOSURE4 – 14
4.2.7.4SUPPLEMENTARY REQUIREMENTS4 – 15
4.2.8ACCELERATION TEST, COMPONENT QUALIFICATION4 – 15
4.2.8.1PURPOSE4 – 15
4.2.8.2TEST DESCRIPTION4 – 15
4.2.8.3TEST LEVELS AND DURATION4 – 15
4.2.8.4SUPPLEMENTARY REQUIREMENTS4 – 15
4.2.9HUMIDITY TEST, COMPONENT QUALIFICATION4 – 16
4.2.9.1PURPOSE4 – 16
4.2.9.2TEST DESCRIPTION AND LEVELS4 – 16
4.2.9.3SUPPLEMENTARY REQUIREMENTS4 – 16
4.2.10PRESSURE TEST, COMPONENT QUALIFICATION4 – 17
4.2.10.1PURPOSE4 – 17
4.2.10.2TEST DESCRIPTION4 – 17
4.2.10.3TEST LEVELS4 – 18
4.2.10.4SUPPLEMENTARY REQUIREMENTS4 – 18
4.2.11LEAK TEST, COMPONENT QUALIFICATION4 – 18
4.2.11.1PURPOSE4 – 18
4.2.11.2TEST DESCRIPTION AND ALTERNATIVES4 – 18
4.2.11.3TEST LEVELS AND DURATION4 – 25
4.2.11.4SUPPLEMENTARY REQUIREMENTS4 – 26
Table of Contents - continued
Paragraph
Title
Page
4.2.12ELECTROMAGNETIC COMPATIBILITY TEST, COMPONENT QUALIFICATION4 – 26
4.2.12.1PURPOSE4 – 26
4.2.12.2TEST DESCRIPTION4 – 26
4.2.12.3TEST LEVELS AND DURATION4 – 26
4.2.12.4SUPPLEMENTARY REQUIREMENTS4 – 26
4.2.13LIFE TEST, COMPONENT QUALIFICATION4 – 27
4.2.13.1PURPOSE4 – 27
4.2.13.2TEST DESCRIPTION4 – 27
4.2.13.3TEST LEVELS AND DURATION4 – 27
4.2.13.4SUPPLEMENTARY REQUIREMENTS4 – 28
4.2.14CORONA/ARCING TEST, COMPONENT QUALIFICATION4 – 28
4.2.14.1PURPOSE4 – 28
4.2.14.2TEST DESCRIPTION4 – 28
4.2.14.3TEST LEVELS AND DURATION4 – 28
4.2.14.4SUPPLEMENTARY REQUIREMENTS4 – 28
4.3STRUCTURAL QUALIFICATION TESTS4 – 29
4.3.1STATIC STRUCTURAL LOAD TEST4 – 29
4.3.1.1PURPOSE4 – 29
4.3.1.2TEST DESCRIPTION4 – 29
4.3.1.3TEST LEVELS AND DURATION4 – 29
4.3.1.4SUPPLEMENTARY REQUIREMENTS4 – 30
4.3.2MODAL SURVEY4 – 30
4.4FLIGHT ELEMENT QUALIFICATION TEST4 – 30
4.4.1FUNCTIONAL TEST, FLIGHT ELEMENT QUALIFICATION4 – 31
4.4.1.1PURPOSE4 – 31
4.4.1.2MECHANICAL FUNCTIONAL TEST4 – 31
4.4.1.3ELECTRICAL FUNCTIONAL TEST4 – 31
4.4.1.4SUPPLEMENTARY REQUIREMENTS4 – 32
4.4.2ELECTROMAGNETIC COMPATIBILITY TEST, FLIGHT ELEMENT QUALIFICATION4 – 32
4.4.2.1PURPOSE4 – 32
4.4.2.2TEST DESCRIPTION4 – 32
4.4.3ACOUSTIC VIBRATION TEST, FLIGHT ELEMENT
QUALIFICATION4 – 32
4.4.3.1PURPOSE4 – 32
Table of Contents - continued
Paragraph
Title
Page
4.4.3.2TEST DESCRIPTION4 – 32
4.4.3.3TEST LEVELS AND DURATION4 – 33
4.4.3.4SUPPLEMENTARY REQUIREMENTS4 – 33
4.4.4PRESSURE/LEAK TEST, FLIGHT ELEMENT QUALIFICATION4 – 33
4.4.4.1PURPOSE4 – 33
4.4.4.2TEST DESCRIPTION4 – 33
4.4.4.3TEST LEVELS AND DURATION4 – 33
4.4.4.4SUPPLEMENTARY REQUIREMENTS4 – 34
5.0ACCEPTANCE TESTING5 – 1
5.1COMPONENT ACCEPTANCE TESTS5 – 1
5.1.1FUNCTIONAL TEST, COMPONENT ACCEPTANCE5 – 3
5.1.1.1PURPOSE5 – 3
5.1.1.2TEST DESCRIPTION5 – 3
5.1.1.3SUPPLEMENTARY REQUIREMENTS5 – 3
5.1.2THERMAL VACUUM TEST, COMPONENT ACCEPTANCE5 – 4
5.1.2.1PURPOSE5 – 4
5.1.2.2TEST DESCRIPTION5 – 4
5.1.2.3TEST LEVELS AND DURATION5 – 4
5.1.2.4SUPPLEMENTARY REQUIREMENTS5 – 9
5.1.3THERMAL CYCLING TEST, COMPONENT ACCEPTANCE5 – 10
5.1.3.1PURPOSE5 – 10
5.1.3.2TEST DESCRIPTION5 – 10
5.1.3.3TEST LEVELS AND DURATION5 – 10
5.1.3.4SUPPLEMENTARY REQUIREMENTS5 – 12
5.1.4RANDOM VIBRATION TEST, COMPONENT ACCEPTANCE5 – 12
5.1.4.1PURPOSE5 – 12
5.1.4.2TEST DESCRIPTION5 – 12
5.1.4.3TEST LEVELS AND DURATION5 – 13
5.1.4.4SUPPLEMENTARY REQUIREMENTS5 – 14
5.1.5ACOUSTIC VIBRATION TEST, COMPONENT ACCEPTANCE5 – 14
5.1.5.1PURPOSE5 – 14
5.1.5.2TEST DESCRIPTION5 – 15
5.1.5.3TEST LEVELS AND DURATION5 – 16
5.1.5.4SUPPLEMENTARY REQUIREMENTS5 – 16
5.1.6PRESSURE TEST, COMPONENT ACCEPTANCE5 – 17
Table of Contents - continued
Paragraph
Title
Page
5.1.6.1PURPOSE5 – 17
5.1.6.2TEST DESCRIPTION5 – 17
5.1.6.3TEST LEVELS5 – 17
5.1.6.4SUPPLEMENTARY REQUIREMENTS5 – 17
5.1.7LEAK TEST, COMPONENT ACCEPTANCE5 – 18
5.1.7.1PURPOSE5 – 18
5.1.7.2TEST DESCRIPTION AND ALTERNATIVES5 – 18
5.1.7.3TEST LEVELS AND DURATION5 – 25
5.1.7.4SUPPLEMENTARY REQUIREMENTS5 – 25
5.1.8BURN−IN TEST, COMPONENT ACCEPTANCE5 – 25
5.1.8.1PURPOSE5 – 25
5.1.8.2TEST DESCRIPTION5 – 26
5.1.8.3TEST LEVELS AND DURATION5 – 26
5.1.8.4SUPPLEMENTARY REQUIREMENTS5 – 28
5.1.9OXYGEN COMPATIBILITY TEST, COMPONENT ACCEPTANCE5 – 29
5.1.9.1PURPOSE5 – 30
5.1.9.2TEST DESCRIPTION5 – 30
5.1.10CORONA/ARCING TEST, COMPONENT ACCEPTANCE5 – 31
5.1.10.1PURPOSE5 – 31
5.1.10.2TEST DESCRIPTION5 – 31
5.1.10.3TEST LEVELS AND DURATION5 – 31
5.1.10.4SUPPLEMENTARY REQUIREMENTS5 – 31
5.2FLIGHT ELEMENT ACCEPTANCE TESTS5 – 32
5.2.1FUNCTIONAL TEST, FLIGHT ELEMENT ACCEPTANCE5 – 32
5.2.1.1PURPOSE5 – 32
5.2.1.2MECHANICAL FUNCTIONAL TEST5 – 32
5.2.1.3ELECTRICAL FUNCTIONAL TEST5 – 33
5.2.1.4SUPPLEMENTARY REQUIREMENTS5 – 33
5.2.2ELECTROMAGNETIC COMPATIBILITY TEST, FLIGHT ELEMENT ACCEPTANCE5 – 33
5.2.3PRESSURE/LEAK TEST, FLIGHT ELEMENT ACCEPTANCE5 – 33
5.2.3.1PURPOSE5 – 33
5.2.3.2TEST DESCRIPTION5 – 34
5.2.3.3TEST LEVELS AND DURATION5 – 34
5.2.3.4SUPPLEMENTARY REQUIREMENTS5 – 34
Table of Contents - continued
Paragraph
Title
Page
5.2.4TOXIC OFF−GASSING TEST, FLIGHT ELEMENT
ACCEPTANCE5 – 35
5.2.4.1PURPOSE5 – 35
5.2.4.2TEST DESCRIPTION5 – 35
5.2.4.3TEST LEVELS AND DURATION5 – 35
5.2.4.4SUPPLEMENTARY REQUIREMENTS5 – 35
5.2.5ACOUSTIC NOISE GENERATION TEST FLIGHT ELEMENT ACCEPTANCE5 – 36
5.2.5.1PURPOSE5 – 36
5.2.5.2TEST DESCRIPTION5 – 36
5.2.6MASS PROPERTIES, FLIGHT ELEMENT ACCEPTANCE5 – 36
5.2.6.1PURPOSE5 – 36
5.2.6.2TEST DESCRIPTION5 – 36
5.2.6.3SUPPLEMENTARY REQUIREMENTS5 – 36
6.0PROTOFLIGHT TEST6 – 1
6.1USE OF QUALIFICATION ASSEMBLIES FOR FLIGHT
(PROTOFLIGHT)6 – 1
6.1.1ASSEMBLY/COMPONENTS PROTOFLIGHT TESTS6 – 1
6.1.2ASSEMBLY/COMPONENTS PROTOFLIGHT BURN−IN TESTS6 – 3
6.1.2.1PURPOSE6 – 3
6.1.2.2TEST DESCRIPTION6 – 3
6.1.2.3TEST LEVELS AND DURATION6 – 3
6.1.2.4SUPPLEMENTARY REQUIREMENTS6 – 5
6.1.3PROTOFLIGHT ASSEMBLY CERTIFICATION FOR FLIGHT6 – 6
6.2USE OF THE FLIGHT (PROTOFLIGHT) ELEMENT FOR QUALIFICATION6 – 6
6.2.1FLIGHT ELEMENT PROTOFLIGHT TESTS6 – 6
6.2.2FLIGHT ELEMENT CERTIFICATION FOR FLIGHT6 – 6
7.0USE OF THE QUALIFICATION TEST ARTICLE FOR FLIGHT7 – 1
8.0RETEST8 – 1
8.1GENERAL8 – 1
8.2SPECIAL CONSIDERATIONS FOR RANDOM VIBRATION
RETESTING8 – 2
8.2.1METHOD I8 – 3
8.2.2METHOD II8 – 6
9.0NONCRITICAL COMPONENT TESTING9 – 1
Table of Contents - continued
Paragraph
Title
Page
9.1DESCRIPTION9 – 3
9.1.1REQUIRED TESTS9 – 4
9.1.2HAZARD SCREENING9 – 4
9.1.3RELIABILITY SCREENING GUIDELINES9 – 4
10.0NOTES10 – 1
10.1GOVERNMENT−FURNISHED PROPERTY10 – 1
10.2DEFINITIONS10 – 1
10.3ABBREVIATIONS AND ACRONYMS10 – 10
APPENDIX
TITLE
PAGE
APG−1 APPROVED EXCEPTIONSA – 1
BPG−2 APPROVED EXCEPTIONSB – 1
CPG−3 APPROVED EXCEPTIONSC – 1
DGOVERNMENT−FURNISHED EQUIPMENT APPROVED
EXCEPTIONSD – 1
EBOEING HOUSTON APPROVED EXCEPTIONSE – 1
FCSA−FURNISHED EQUIPMENT APPROVED EXCEPTIONSF – 1

TABLE OF CONTENTS – Continued

TABLES

TABLE

PAGE

3–1MAXIMUM ALLOWABLE TOLERANCES ON TEST
CONDITIONS3 – 2
4–1COMPONENT QUALIFICATION TESTS4 – 2
4–1aCORONA TEST VOLTAGE CRITERIA4 – 3
4–2FLIGHT ELEMENT QUALIFICATION TESTS4 – 31
5–1COMPONENT ACCEPTANCE TESTS5 – 2
5–a1CORONA TEST VOLTAGE CRITERIA5 – 3
5–1aOXYGEN COMPONENTS REQUIRING ACCEPTANCE
TESTING5 – 30
5–2FLIGHT ELEMENT ACCEPTANCE TESTS5 – 32
9–1NONCRITICAL HARDWARE QUALIFICATION
REQUIREMENTS9 – 2
9–2NONCRITICAL HARDWARE ACCEPTANCE
REQUIREMENTS9 – 3
GFE–144–1MDP Of Each ZoneD – 117

FIGURES

FIGURE
TITLE
PAGE
4–1COMPONENT THERMAL VACUUM QUALIFICATION TESTS4 – 6
5–1COMPONENT THERMAL VACUUM AND THERMAL CYCLE ACCEPTANCE TEST5 – 6
5–1aCOMBINED OPERATING/NON-OPERATING THERMAL VACUUM/CYCLE5 – 7
5–1bSEPARATE OPERATING/NON-OPERATING THERMAL VACUUM/CYCLE5 – 8
5–2COMPONENT WML5 – 15
5–3MASS ATTENUATED WORKMANSHIP VIBRATION SPECTRUM5 – 15

Export Controlled – EAR/ECCN 9E002 ix

INTRODUCTION

PURPOSE

This document establishes the minimum uniform requirements for qualification and acceptance environmental tests for components, structures, and flight elements.

SCOPE

These test requirements are applicable to the International Space Station (ISS) with the exception of the Attached Pressurized Module segment, the Russian segment, and the Japanese Experiment Module segment. These segments shall follow the testing standards of the following agencies: European Space Agency, Roscosmos, and Japan Aerospace Exploration Agency. However, it is expected that these standards meet or exceed the standards in this document. These test requirements specify component, assemblies, structures, and flight element qualification tests; component, assemblies, and flight element acceptance tests; and component, assemblies, structures, and flight element protoflight tests. Test procedures and margins are also specified. Any noncompliance to the requirements in this document will be documented and processed in accordance with SSP 41170.

PRECEDENCE

The verification requirements contained herein shall take precedence over any conflicting verification requirements, with the exception of the ISS System, Segment and End Item Specifications.

DELEGATION OF AUTHORITY

Where provisions are provided in this document for alternative strategies or requirements requiring ISS Program approval, the ISS RTVP shall be the designated approving authority.

Export Controlled – EAR/ECCN 9E002 1 – 1

APPLICABLE DOCUMENTS

The following applicable documents of the exact issue shown in the current issue of SSP 50257 form a part of this specification to the extent specified herein. Inclusion of applicable documents herein does not in any way supersede the order of precedence identified in 1.3. The references show where each applicable document is cited in this document.

DOCUMENT NO.
TITLE
D684−10020−1
Program Master Integration and Verification Plan

References: 3.3

JSC 20584
Spacecraft Maximum Allowable Concentrations for Airborne Contaminants

References: 5.2.4.4

JSC 62592
GFE EEE Part Assembly Level Power Cycle Burn−in

References: Table 9−2

MIL−STD−1474
Noise Limits for Army Material

References: 5.2.5.2

MSFC−PROC−404
Procedure Gases, Drying and Preservation Cleanliness Level and Inspection Methods

References: 5.1.9.2

NASA-STD-7001
Payload Vibroacoustic Test Criteria

References: Table 3-1, 5.1.4.3

NSTS 21000−IDD−ISS
International Space Station Interface Definition Document

References: PG1-86, PG1-92, PG1-136, PG1-155, PG1-236, PG1-237, PG1-240, PG2-66, PG2-156, PG2-157, PG2-158, PG2-166, PG3-103, GFE−156

SSP 30223
Problem Reporting and Corrective Action for the Space Station Program

References: 8.1

SSP 30234
Instructions for Preparation of Failure Modes and Effect Analysis and Critical Items List for Space Station

References: 3.1, 9.0

SSP 30237
Space Station Electromagnetic Emission and Susceptibility Requirements for Electromagnetic Compatibility

References: 4.2.12.2, 4.2.12.3, PG1-08, PG1-11, PG2-28, PG3-15, GFE-11

SSP 30238
Space Station Electromagnetic Techniques

References: 4.2.12.2, PG1-33, PG1-66, PG1-67, PG3-15

SSP 30243
Space Station Systems Requirements for Electromagnetic Compatibility References: 4.4.2.2
SSP 30559
Space Station Structural Design and Verification Requirements

References: 4.2.10.3B, 4.2.10.3C, 4.2.13.1, 4.3.1.2, 4.3.1.4, 4.4.4.3, 5.1.6.3, 5.2.3.3, 6.1.3, PG1-148, PG1-261, PG2-13, PG2-14, PG2-118, PG2-119, PG3-117, PG3-158, GFE-98, GFE-99, GFE-110, GFE-122, GFE-123, GFE-124, GFE-125

SSP 50507
NASA International Partners Plan for ISS Modules Pressure Integrity Verification

References: 5.2.3.2

SSP 52051, Volume 1
User Electric Power Specifications and Standards Volume 1: 120 Volt DC Loads

Reference: Table 9-1

REFERENCE DOCUMENTS

The following documents contain supplemental information to guide the user in the application of this document. These reference documents may or may not be specifically cited within the text of this document.

DOCUMENT NO.
TITLE
ASTM E493/493M-11
Standard Test Methods for Leaks Using Mass Spectrometer Leak Detector in the Inside−Out Testing Mode

References: 4.2.11.2O, 5.1.7.2O

ASTM E1066/E1066M-12
Ammonia Colorimetric Leak Testing

References: 4.2.11.2D, 5.1.7.2D

JSC 49908
ARED Instrumentation EEE Parts Report

References: GFE−146, GFE−149

MA2−00−057
Mechanical System Safety Letter

References: 4.2.13.3, CSA-001, CSA-002

MIL−STD−883
Test Method Standard Microcircuits, Department of Defense

References: 4.2.11.2O, 5.1.7.2O, PG1-161, PG1-218, PG1-219, PG1-220, PG1-221

MIL−STD−1553
Digital Time Division Command/Response Multiplex Data Bus

References: PG1-66, GFE−152, GFE-154

MSFC-STD-531
High Voltage Design Criteria

References: 4.2.14.4, 5.1.10.4

MSFC−SPEC−3024
Prime Item Development Specification for the Water Processor Assembly

References: GFE−139

NASA-HDBK-8739.19-4
Estimation and Evaluation of Measurement Decision Risk. NASA Measurement Quality Assurance Handbook –

ANNEX 4

References: 3.2, 5.2.6.3

NASDA-ESPC-2857
HTV Cargo Standard Interface Requirements Document

References: 4.2.5.3, 4.2.6.3, 6.1.1

NSTS−21000−IDD−MDK
Middeck Interface Definition Document

References: GFE−156

SOEC.1849
OHT Mechanism Analysis Report

References: CSA−003

SPX-00036031
FRAM Payloads Interface Requirements document (IRD)

References: 4.2.5.3, 4.2.6.3, 4.2.7.3, 6.1.1

SSP 30482
Electric Power Specifications and Standards

References: 10.2

SSP 41170
Configuration Management Requirements

References: 1.2

SSP 41173
Space Station Quality Assurance Requirements

References: 3.1, 10.2

SSP 50835
Pressurized Volume Hardware Common Interface Requirements Document

References: 4.2.5.3, 4.2.6.3, 4.2.7.3

SSP 57000
Pressurized Payloads Interface Requirements Document

References: 4.2.11.2, 5.1.7.2

Export Controlled – EAR/ECCN 9E002 2 – 3

GENERAL

REQUIREMENTS FOR TEST

All qualification, acceptance, and protoflight tests shall, as a minimum, comply with the test requirements of this document. If a requirement exists in another document (e.g., the applicable development specification) to perform a test that is not identified in this document as a required test, then the test shall be performed in the manner specified in this document. Hardware classified as criticality 1 or 2 from Failure Modes and Effects Analysis (FMEA) performed in accordance with SSP 30234 shall be tested in accordance with sections 4, 5 or, for protoflight, 6 of this document. Hardware classified as criticality 3 or 2N based on an integrated FMEA assessment by the Reliability and Maintainability Panel or its designee may be tested in accordance with section 9 of this document.

The objective of these requirements is to specify reasonable, prudent, and technically meaningful tests. Planned tests shall be evaluated to assure they meet these criteria.

The tests specified herein should only be conducted by personnel formally trained to conduct the applicable test(s). It is recommended that formal certification of personnel knowledge and skills for conducting the tests specified herein be maintained.

TEST CONDITION TOLERANCES

Test condition tolerances shall be applied to the nominal test values specified in this document. Unless otherwise specified, the following maximum allowable tolerances shown in Table 3−1 on test conditions shall apply:

TABLE 3–1 MAXIMUM ALLOWABLE TOLERANCES ON

TEST CONDITIONS/PARAMETERS

Condition/Parameter
Tolerance Bands
Temperature
Hot + 5.4/-0 degrees F

(+3.0/-0 degrees C) Cold + 0/-5.4 degrees F (+0/-3.0 degrees C)

OR

+/-5.4 degrees F (+/- 3.0 degrees C) provided that 50% or more of the time during functional/performance testing at each temperature extreme is at or beyond the target test temperature.

Pressure

Above 133 Pascals (Pa) (>1 Torr)

0.133 to 133 Pa (0.001 to 1 Torr) Less than 0.133 Pa (<0.001 Torr) +/− 10 percent +/− 25 percent +/− 80 percent

Relative Humidity
+/− 5 percent
Acceleration
+/− 10 percent

Vibration Frequency

25 Hz and above Below 25 Hz +/− 5 percent +/− 1/4 Hz

Sinusoidal Vibration Amplitude
+/− 10 percent
Static Load
+/− 5 percent
Time
+/− 2 percent

TABLE 3–1 MAXIMUM ALLOWABLE TOLERANCES ON

TEST CONDITIONS/PARAMETERS - Continued

Random Vibration Power Spectral Density (PSD)

20 to 500 Hz (25 Hz or narrower) 500 to 2000 Hz (50 Hz or narrower) Random overall grms Duration +/− 1.5 dB +/− 3.0 dB +/− 1.5 dB +10/−1 percent

Sound Pressure Levels (SPL) (1)

1/3−Octave Midband Frequencies

31.5 to 40 Hz 50 to 2000 Hz 2500 to 10000 Hz Test Duration Overall SPL +/− 5.0 dB +/− 3.0 dB +/− 4.0 dB +/− 1.5 dB +10/−1 percent +/- 1.0 dB

Shock Response Spectrum (Peak Acceleration, Q = 10) (2) Natural Frequencies Spaced at 1/6−Octave Intervals

At or below 5000 Hz Above 5000 Hz +/− 3.0 dB +9.0/−6.0 dB

Notes:
(1)The statistical degrees of freedom shall be at least 100.
(2)At least 50 percent of the spectrum values must be greater than the nominal test specification.
(3)The Measurement & Test Equipment (MTE) calibration records and its measurement accuracy shall be compliant with SSP 41173, paragraph 3.8. For the test parameters determined as critical in the specifications, the measurement uncertainty analysis shall be done in accordance with NASA-HDBK-8739.19-4.

(4) Tolerances for PSD and SPL match NASA-STD-7001.

INTEGRATION AND VERIFICATION RECORDS

D684−10020−1 shall be used to provide a record of disposition pertaining to the integration and verification of ISS related hardware. D684−10020−1 and associated Program Implementation Instructions (PII) referenced in D684−10020−1 contain the process, required instructions, and blank forms for the following Test and Verification approving documents: Requirements Interpretation Agreement, Reverification Assessment, Test Article Configuration Variance, Test Objectives Agreement, and Test Requirements Change Notice. The PII documents are utilized in the Test and Verification process for tracking issues of hardware testing that require documentation and traceability as they pertain to the International Space Station. These documents are binding agreements between responsible hardware owners, contractors, and National Aeronautics and Space Administration (NASA) responsible subsystems. These agreements are formalized through the RTVP.

Export Controlled – EAR/ECCN 9E002 3 – 4

QUALIFICATION TESTING

This paragraph provides the minimum requirements for qualification tests and the application of those tests to components, structures, and flight elements.

QUALIFICATION AND ACCEPTANCE TESTING RELATIONSHIP

Qualification test levels and duration shall in all cases envelope worst−case service life environments including acceptance test levels and duration (including test tolerances) and accommodate acceptance retesting. Acceptance testing, including functional and environmental, shall be conducted on all test articles as the first phase of the qualification tests.

Notes:

1. See Appendix C, PG3−81, for the exception to this paragraph.

COMPONENT QUALIFICATION

The component qualification tests that are a Program requirement are designated in Table 4−1 according to test category and component category. Where components fall into more than one category, the required tests for each category shall be applied. Subsequent paragraphs describe in detail the requirements for each test category. The word “required” means that, as a minimum, the component is required to be tested to the specific environment that it will experience during its life cycle.

Notes:

1.See Appendix A, PG1−221 and PG1−273, for exceptions to this paragraph.
2.See Appendix C, PG3−77, for the exception to this paragraph.

TABLE 4–1 COMPONENT QUALIFICATION TESTS

Test
Electronic or Electrical Equipment
Antennas
Moving Mechanical Assembly/Mechanism
Solar Panel
Batteries
Fluid or Propulsion Equipment
Pressure Vessels
Thermal Equipment
Optical Equipment
Functional (1)
R
R
R
R
R
R
R
R
R
Thermal Vacuum (4)
R(12)
R
R
R
R
R
−
R
R
Thermal Cycling
R(12)
R
ER
R
−
R
−
R(8)
R
Depress/Repress (5)
R
−
R
−
−
R(9)
R(9)
R(9)
R
Sinusoidal Vibration
−
−
−
−
−
−
−
−
−
Random Vibration (3)
R
R
R
−
R
R
R
R
R
Acoustic Vibration
R(3)
R(3)
−
R
−
−
−
−
−
Pyrotechnic Shock (10)
R
−
R
−
R
R
−
R
R
Acceleration
−
−
−
−
−
−
−
−
−
Humidity
−
−
−
−
−
−
−
−
−
Pressure
−
−
−
−
R(2)
R
R
−
−
Leak
R(2)
−
−
−
R(2)
R
R
R
R
EMI/EMC (11)
R
−
−
−
−
−
−
−
−
Life
−
−
R
−
−
−
−
−
−
Corona/Arcing (6) (7)
R
−
−
−
−
−
−
−
−
LEGEND:
R
=
REQUIRED
The ISS requires, as a minimum, that the article be tested if the subject environment is experienced during the article’s life cycle.
ER
=
EVALUATION

REQUIRED

Test requires an evaluation from the cognizant technical team and T&V representative.

Flag Notes:

(1)Functional tests shall be conducted prior to and following environmental test.
(2)Required only on sealed or pressurized equipment.
(3)Either random vibration or acoustic vibration test required with the other optional.
(4)External components only. For components that operate in a pressurized environment only, thermal vacuum testing is not required.
(5)Internal components only.
(6)Corona testing is not required for components with a sealed chassis or components which are powered on and operating under space vacuum conditions only.
(7)See Table 4−1a for component voltage criteria dictating corona/arcing testing.
(8)Thermal Cycling shall not be required for passive thermal equipment.
(9)A depress/repress test is not required if ultimate pressure testing provides a more severe differential pressure across the unit.
(10)Applicable if the hardware is exposed to a Pyro Shock environment.
(11)When multiple test articles exists, only one is required for the qualification of design.

(12) Minimum 140 degrees F (77.8 Degrees C) sweep is required. Caution must be exercised if at least one part of the component has a limit on its operational temperature.

TABLE 4–1a CORONA/ARCING TEST VOLTAGE CRITERIA

Peak Voltage (Volts(V)) (1)
Transient Duration

(microseconds) Corona Testing Required

< 150
Not Applicable (N/A)
No (N)
150 <= V < 190
< 250
N
150 <= V < 190
>= 250
Yes (Y)
>= 190
N/A
Y
Note:
(1)Applies to both steady−state and transient conditions. Also applies to input voltages, internal voltages, and output voltages.

FUNCTIONAL TEST, COMPONENT QUALIFICATION

PURPOSE

This test verifies that the functional performance of the component meets the operational requirements of the component specification (i.e., optical, thermal, etc.).

TEST DESCRIPTION

Electrical tests shall include application of expected voltages, impedance, frequencies, pulses, and waveforms at the electrical interfaces of the component, including all redundant circuits. Mechanical tests shall include application of torque, load, and motion as appropriate. These parameters shall be varied throughout their specification ranges and the sequences expected during its life cycle, and the component output shall be measured to verify the component performance to specification requirements. Functional performance shall also include electrical continuity, stability, response time, alignment, pressure, leak, or other special functional tests related to a particular component configuration.

SUPPLEMENTARY REQUIREMENTS

A functional test shall be conducted prior to each of the environmental tests to assure that performance meets the requirements of the particular specification. The same functional test shall be conducted after each environmental test. Functional tests shall not be required after application of ultimate loads during a structural loads test.

Notes:

1. See Appendix D, GFE−157, for an exception to this paragraph.

THERMAL VACUUM TEST, COMPONENT QUALIFICATION

PURPOSE

This test demonstrates the ability of the component to perform in a thermal vacuum environment that simulates the maximum and minimum predicted level temperature environment for the component.

Notes:

1. See Appendix F, CSA−003, for exceptions to this paragraph.

TEST DESCRIPTION

The component shall be mounted in a vacuum chamber on a thermally controlled heat sink or in a manner to simulate the flight environment.

With the chamber at the test−pressure level, radio frequency equipment shall be monitored to assure that multipacting does not occur. A temperature cycle begins with the chamber and component at ambient temperature. The temperature of the chamber is reduced to bring the component to the specified low qualification level and stabilized. Temperature stability has been achieved when the rate of change is no more than 5.4 degrees F/hour (3 degrees C/hour).

Components that operate on orbit shall be turned off, then started after a soak period sufficient to ensure the component internal temperature has stabilized at the specified temperature, and then functionally tested. With the component operating, the temperature of the chamber is increased to bring the component qualification temperature to the upper temperature level. After the component temperature has stabilized at the specified level, the component shall be turned off, then started after electrical circuits have been discharged. The temperature of the chamber and component shall then be reduced to ambient conditions. This constitutes one complete temperature cycle.

Notes:

1.See Appendix A, PG1−77 and PG1−87, for the exceptions to this paragraph.
2.See Appendix C, PG3−46, for the exception to this paragraph.

TEST LEVELS AND DURATION

A. Pressure. The pressure shall be reduced from atmospheric to below 0.0001 Torr (0.0133 Pa).

Notes:

1.See Appendix A, PG1−190, for the exception to this paragraph.
2.See Appendix B, PG2−109 and PG2−143, for exceptions to this paragraph.
3.See Appendix D, GFE−75, for the exception to this paragraph.

B. Temperature. The component shall be at the maximum acceptance limits plus a margin of 20 degrees F (11.1 degrees C) (maximum design temperature) during the hot portion of the cycle and at the minimum acceptance test level temperature minus a margin of 20 degrees F (11.1 degrees C) (minimum design temperature) during the cold portion of the cycle. The minimum limits shall be below 30 degrees F (−1.1 degrees C) where possible. See Figure 4−1. For electrical/electronic equipment where the minimum sweep (paragraph 5.1.3.3B) does not encompass the acceptance limits + and − the margin, the minimum sweep for qualification shall be 140 degrees F (77.8 degrees C). Caution must be exercised if at least one part of the component has a limit on its operational temperature.

Notes:

1.See Appendix A, PG1−75, PG1−172, PG1−183, PG1−209, and PG1−219, for the exceptions to this paragraph.
2.See Appendix B, PG2−39, PG2−40, PG2−59, PG2−65, PG2−82, PG2−86, PG2−87, PG2−89, PG2−98, PG2−120, PG2−133, and PG2−134, for the exceptions to this paragraph.
3.See Appendix C, PG3−84, PG3−100, and PG3−195, for the exceptions to this paragraph.
4.See Appendix D, GFE−101 and GFE−113, for the exceptions to this paragraph.

FIGURE 4–1 COMPONENT THERMAL VACUUM AND THERMAL CYCLING QUALIFICATION TESTS

C. Duration. A minimum of three temperature cycles shall be used. During each cycle, the component shall undergo a dwell period after stabilization at both the high and low temperature extremes. The dwell period shall be long enough for the component to reach internal thermal equilibrium for not less than 1 hour.

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