42097P1_AE_RF_012968.pdf

National Aeronautics and Space Administration International Space Station Program Johnson Space Center Houston, Texas Contract No. ��������

International Space Station Program

Revision F

30 June 2011

Type 1 − NASA APPROVED

Space Station Program Pressurized Mating Adapter 2 & 3 To United States Pressurized Elements (Node Element 3 To Pressurized Mating Adapter 3) Interface Control Document, Part 1, Appendix E

SSP 42097, Part 1, Appendix E, Revision F 30 June 2011 ii

REVISION AND HISTORY PAGE

REV. DESCRIPTION PUB.

DATE

− Initial Release in accordance with DR VE 06 28 Sept 94

CHANGE 1, IRN 0001 (REFERENCE SSCD 000085 EFF. 05−05−95) 1−17−96

CHANGE 2, IRN 0002 (REFERENCE SSCD 000085 EFF. 05−05−95) 1−17−96

CHANGE 3, IRN 0003 (REFERENCE SSCD 000085 EFF. 05−05−95) 1−17−96

CHANGE 4, IRN 0004 (REFERENCE SSCD 000085 EFF. 05−05−95) 1−17−96

CHANGE 5, IRN 0005 (REFERENCE SSCD 000085 EFF. 05−05−95) 1−17−96

CHANGE 6, IRN 0014 (REFERENCE SSCD 000085 EFF. 05−05−95) 1−17−96

CHANGE 7, IRN 0015 (REFERENCE SSCD 000085 EFF. 05−05−95) 1−17−96

CHANGE 8, IRN 0023 (REFERENCE SSCD 000085 EFF. 05−05−95) 1−17−96

CHANGE 9, IRN 0024 (REFERENCE SSCD 000085 EFF. 05−05−95) 1−17−96

CHANGE 10, IRN 0026 (REFERENCE SSCD 000085 EFF. 05−05−95) 1−17−96

CHANGE 11, IRN 0028 (REFERENCE SSCD 000085 EFF. 05−05−95) 1−17−96

CHANGE 12, IRN 0030 (REFERENCE SSCD 000085 EFF. 05−05−95) 1−17−96

CHANGE 13, IRN 0031 (REFERENCE SSCD 000085 EFF. 05−05−95) 1−17−96

CHANGE 14, IRN 0033 (REFERENCE SSCD 000085 EFF. 05−05−95) 1−17−96

CHANGE 15, IRN 0034 (REFERENCE SSCD 000085 EFF. 05−05−95) 1−17−96

CHANGE 16, IRN 0035 (REFERENCE SSCD 000085 EFF. 05−05−95) 1−17−96

CHANGE 17, IRN 0036 (REFERENCE SSCD 000085 EFF. 05−05−95) 1−17−96

CHANGE 18, IRN 0007 (REFERENCE SSCD 000059 EFF. 07−14−95) 1−29−96

CHANGE 19, IRN 0007R1 (REFERENCE SSCD 000059 EFF. 07−14−95) 4−12−96

CHANGE 20, IRN 0008 (REFERENCE SSCD 000067 EFF. 11−27−95) 4−12−96

CHANGE 21, IRN 0028R1 (REFERENCE SSCD 000085 EFF. 05−05−95 ) 4−15−96

CHANGE 22, IRN 0011 (REFERENCE SSCD 000106 EFF. 1−23−96) 4−15−96

CHANGE 23, IRN 0004R1 (REFERENCE SSCD 000085 EFF. 05−05−95) 5−29−96

CHANGE 24, IRN 0028R2 (REFERENCE SSCD 000085 EFF. 05−05−95) 5−29−96

CHANGE 25, IRN 0007R2 (REFERENCE SSCD 000059 EFF. 07−14−95) 5−29−96

CHANGE 26, IRN 0008R1 (REFERENCE SSCD 000067 EFF. 11−27−95) 5−29−96

iii

REVISION AND HISTORY PAGE − Continued

REV. DESCRIPTION PUB.

DATE

CHANGE 27 IRN 0009 (REFERENCE SSCD 00070 EFF. 11−06−95) 5−29−96

CHANGE 28, IRN 0011R1 (REFERENCE SSCD 000106 EFF. 1−23−96) 5−29−96

CHANGE 29, IRN 0063 (REFERENCE SSCD 000064 EFF. 08−28−94) 6−24−96

CHANGE 30, IRN 0145 (REFERENCE SSCD 000145 EFF. 10−31−96) 6−24−96

CHANGE 31, IRN 0010 (REFERENCE SSCD 000102 EFF. 11−04−94) 10−30−96

CHANGE 32, IRN 0042 per CCR 000151 12−05−96

CHANGE 33, IRN 0012 per CCR 000169 12−10−96

CHANGE 34, IRN 0045 per CCR 000263 02−11−97

A Revision A per CCR 000475 10−13−97 Block update to incorporate the following IRN’s:

42097−0001 (Auth. IFM BP/95−0098, 4/5/95) 42097−0023 (Auth. IFM BP/95−0101, 4/6/95) 42097−0030 (Auth. IFM BP/95−0101, 4/6/95) 42097−0012 (Auth. IFM BP/96−0623, 8/7/96) 42097−0145 (Auth. IFM BP/96−0623, 8/7/96) 42097−0008 (Auth. IFM BP/95−0249, 7/20/95) 42097−0009 (Auth. IFM BP/96−0623, 8/7/96) 42097−0010 (Auth. IFM BP/96−0623, 8/7/96) 42097−0011 (Auth. IFM BP/96−0623, 8/7/96) 42097−0040 (Auth. IFM BP/96−0623, 8/7/96) 42097−0041 (Auth. IFM BP/96−0623, 8/7/96) 42097−0042 (Auth. IFM BP/96−0623, 8/7/96) 42097−0045 (Auth. IFM BP/95−0098, 4/5/96) 42097−0047 (Auth. IFM BP/96−0623, 8/7/96) 42097−0049 (Auth. IFM BP/96−0623, 8/7/96)

For Information: The PIRNs rolled into Revision A by previously released IRNs, or as a part of Revision A, are noted below with their associated SSCN.

PIRN 42097−0001 IRN 0001 SSCN 000085

PIRN 42097−0002 IRN 0002 SSCN 000085

PIRN 42097−0003 IRN 0003 SSCN 000085

PIRN 42097−0004 IRN 0004R1 SSCN 000085

PIRN 42097−0005 IRN 0005 SSCN 000085

PIRN 42097−0014 IRN 0014 SSCN 000085

PIRN 42097−0015 IRN 0015 SSCN 000085

PIRN 42097−0023 IRN 0023 SSCN 000085

PIRN 42097−0024 IRN 0024 SSCN 000085

PIRN 42097−0026 IRN 0026 SSCN 000085

PIRN 42097−0028 IRN 0028R2 SSCN 000085

PIRN 42097−0030 IRN 0030 SSCN 000085

PIRN 42097−0031 IRN 0031 SSCN 000085

PIRN 42097−0033 IRN 0033 SSCN 000085

iv

REVISION AND HISTORY PAGE − Continued

PIRN 42097−0034 IRN 0034 SSCN 000085

PIRN 42097−0035 IRN 0035 SSCN 000085

PIRN 42097−0036 IRN 0036 SSCN 000085

PIRN 42097−0043B IRN 0007R2 SSCN 000059

PIRN 42097−0061 IRN 0008R1 SSCN 000067

PIRN 42097−0059C IRN 0011R1 SSCN 000106

PIRN 42097−0060B IRN 0009 SSCN 000070

PIRN 42097−0063C IRN 0063 SSCN 000064

PIRN 42097−0050D IRN 0145 SSCN 000145

PIRN 42097−0054C IRN 0010 SSCN 000102

PIRN 42097−0055C IRN 0010 SSCN 000102

PIRN 42097−0056D IRN 0010 SSCN 000102

PIRN 42097−0057D IRN 0010 SSCN 000102

PIRN 42097−0058C IRN 0010 SSCN 000102

PIRN 42097−0064D IRN 0010 SSCN 000102

PIRN 42097−0065 IRN 0010 SSCN 000102

PIRN 42097−0068A IRN 0042 SSCN 000151

PIRN 42097−0048C IRN 0012 SSCN 000169

PIRN 42097−0049B IRN 0012 SSCN 000169

PIRN 42097−0067 IRN 0040 SSCN 000116

PIRN 42097−0066C IRN 0041 SSCN 000239

PIRN 42097−0006D IRN 0045 SSCN 000263

PIRN 42097−0008 IRN 0045 SSCN 000263

PIRN 42097−0010B IRN 0045 SSCN 000263

PIRN 42097−0011A IRN 0045 SSCN 000263

PIRN 42097−0012E IRN 0045 SSCN 000263

PIRN 42097−0016A IRN 0045 SSCN 000263

PIRN 42097−0017 IRN 0045 SSCN 000263

PIRN 42097−0018B IRN 0045 SSCN 000263

PIRN 42097−0019B IRN 0045 SSCN 000263

PIRN 42097−0020A IRN 0045 SSCN 000263

PIRN 42097−0021A IRN 0045 SSCN 000263

PIRN 42097−0022B IRN 0045 SSCN 000263

PIRN 42097−0025 IRN 0045 SSCN 000263

PIRN 42097−0029D IRN 0045 SSCN 000263

PIRN 42097−0032D IRN 0045 SSCN 000263

PIRN 42097−0037A IRN 0045 SSCN 000263

PIRN 42097−0038A IRN 0045 SSCN 000263

PIRN 42097−0039A IRN 0045 SSCN 000263

PIRN 42097−0044B IRN 0045 SSCN 000263

PIRN 42097−0045A IRN 0045 SSCN 000263

PIRN 42097−0046A IRN 0045 SSCN 000263

PIRN 42097−0047A IRN 0045 SSCN 000263

PIRN 42097−0075A IRN 0047 SSCN 000241

PIRN 42097−0077 IRN 0049 SSCN 000299

PIRN 42097−0078 IRN 0049 SSCN 000299

PIRN 42097−0079 IRN 0049 SSCN 000299

v

REVISION AND HISTORY PAGE − Continued

PIRN 42097−0070 IRN N/A SSCN 000475

PIRN 42097−0071 IRN N/A SSCN 000475

PIRN 42097−0072 IRN N/A SSCN 000475

PIRN 42097−0073 IRN N/A SSCN 000475

PIRN 42097−0074 IRN N/A SSCN 000475

PIRN 42097−0080 IRN N/A SSCN 000475

PIRN 42097−0081 IRN N/A SSCN 000475

PIRN 42097−0082 IRN N/A SSCN 000475

PIRN 42097−0083 IRN N/A SSCN 000475

PIRN 42097−0084 IRN N/A SSCN 000475

Note: IRNs 0040, 0041, 0047, and 0049 were never released, but were cancelled as changes were rolled into Revision A.

B Revision B per SSCN 001252. This revision incorporates the following PIRNs associated with the appropriate SSCNs. 10/08/98

PIRN 42097−0097A IRN 0064 SSCN 000391

PIRN 42097−0100 IRN 0046 SSCN 000253

PIRN 42097−0105 IRN 0054 SSCN 000557

PIRN 42097−0114 IRN 0065 SSCN 000561

PIRN 42097−0129 IRN N/A SSCN 001252

PIRN 42097−0095 IRN N/A SSCN 001252

PIRN 42097−0096A IRN N/A SSCN 001252

PIRN 42097−0098A IRN 0064 SSCN 000391

PIRN 42097−0099 IRN 0064 SSCN 000391

PIRN 42097−0101 IRN 0046 SSCN 000253

PIRN 42097−0102 IRN 0046 SSCN 000253

PIRN 42097−0103 IRN 0046 SSCN 000253

PIRN 42097−0104 IRN 0046 SSCN 000253

PIRN 42097−0106A IRN 0054 SSCN 000557

PIRN 42097−0107A IRN 0054 SSCN 000557

PIRN 42097−0108A IRN 0054 SSCN 000557

PIRN 42097−0115A IRN 0066 SSCN 000702

PIRN 42097−0116 IRN 0067 SSCN 000600

PIRN 42097−0117 IRN 0067 SSCN 000600

PIRN 42097−0118 IRN 0067 SSCN 000600

PIRN 42097−0119B IRN N/A SSCN 001252

PIRN 42097−0120A IRN N/A SSCN 001252

PIRN 42097−0121B IRN N/A SSCN 001252

PIRN 42097−0122A IRN N/A SSCN 001252

PIRN 42097−0123A IRN N/A SSCN 001252

Note: IRNs 0064, 0046, 0054, 0065, 0066, and 0067 were never released, but were cancelled as rolled into Revision B.

Due to past history of this document, IRNs 0006, 0013, 0016 to 0022, 0025, 0027, 0029, 0032, 0037 to 0039, 0043, 0044, 0048, 0050 to 0053, and 0055 to 0062 have been retired without use. The only traceability that can be found is that the IRN number was withdrawn.

vi

REVISION AND HISTORY PAGE − Continued

C Revision C per SSCN 001465. 10/09/98

As of Rev. C, this Document was split into separate Appendixes to be tracked individually due to different Approval Requirements for each Document This revision incorporates the following PIRNs associated with the appropriate SSCNs.

PIRN 42097−0113 IRN N/A SSCN 001465

PIRN 42097−0128 IRN N/A SSCN 001465

PIRN 42097−0132 IRN N/A SSCN 001465

PIRN 42097−0137 IRN N/A SSCN 001465

IRN 0001 (PIRN 42097−NA−0011) incorporates SSCN 001594 10/09/98

IRN 0003 (PIRN 42097−NA−0026) incorporates SSCN 001481 10/09/98

IRN 0004 (PIRN 42097−NA−0032) incorporates SSCN 001555 10/09/98

D Revision D per SSCN 001665. 10/09/98 This revision incorporates the following PIRNs associated with the appropriate SSCNs.

PIRN 42097-0146 IRN N/A SSCN 001665

E Revision E per SSCN 008203 Rev A EFF (10−02−03) 07/25/05

Revision E incorporates the following PIRNs/IRNs with associated SSCNs:

PIRN 42097−0133B IRN 42097−0007 SSCN 001786

PIRN 42097−NA−0016B IRN 42097−1464 SSCN 001464

PIRN 42097−NA−0036A IRN 42097−0024 SSCN 001814

PIRN 42097−NA−0038A IRN 42097−0024 SSCN 001814

Revision D closes SSCN 002541 (IRN 0028), this change was rolled into Revision E.

F Revision F per SSCN 012968. EFF (10−26−11) 11−01−11

This Revision incorporates the following PIRNs/IRNs associated with the appropriate SSCNs:

PIRN No. IRN No. SSCN No.

42097−NA−0041 0027 003488

42097−NA−0043A 012968

42097−NA−0044A 000202

42097−NA−0045 0034 008444

42097−NA−0045 0035 008939

42097−NA−0045 0038 009111

42097−NA−0045 0033 009475

42097−NA−0045 0002 001662

42097−NA−0045 0006 001740

42097−NA−0045 0037 009993

42097−NA−0045 0013 001383

vii

PIRN No. IRN No. SSCN No.

42097−NA−0045 0012 001703

42097−NA−0045 0030 003404

42097−NA−0045 0036 009719

42097−NA−0045 0034 009086

42097−NA−0046 0039 012010

42097−NA−0047A 012968

Revision F closes SSCNs: 001711(IRN 0010), 002199(IRN 0021), 002820(IRN 0022), 003289(IRN 0025), 000929(IRN 0005), 009111(IRN 0038)

INTERNATIONAL SPACE STATION PROGRAM

PRESSURIZED MATING ADAPTER 2 & 3 TO U.S. PRESSURIZED ELEMENTS

(Appendix E − NODE ELEMENT 3 TO PRESSURIZED

MATING ADAPTER 3)

INTERFACE CONTROL DOCUMENT, PART 1

LIST OF CHANGES

x

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

SSCBD ENTRY DATE CHANGE PARAGRAPH(S)

001786 42097−0133B Preface NASA/ASI concurrence

ICWG concurrence E1.1, E1.2, E1.3, E2.0, E2.1, E2.2, E3.1.1, E3.1.1.1 E3.1.1.2, E3.1.1.3, E3.1.1.4.2, E3.1.1.5, E3.1.1.6 E3.1.2, E3.1.2.1, E3.1.2.2, E3.2.1, E3.2.1.2.1, E3.2.1.2.2, E3.2.1.2.3, E3.1.2.3.1, E3.1.2.3.2, E3.1.2.3.3, E3.2.1.2.3.4, E3.2.1.2.3.5, E3.2.1.2.3.6, E3.2.1.2.4, E3.2.1.2.4.1, E3.2.1.2.4.2, E3.2.1.2.5, E3.2.1.2.5.1, E3.2.1.2.6.1, E3.2.1.2.6.2 E3.2.1.3.1, E3.2.1.3.1.1, E3.2.1.3.1.1.2 E3.2.1.3.1.1.3, E3.2.1.3,2, E3.2.1.3.2.1, E3.2.1.3.2.1.2, E3.2.1.3.2.1.3, E3.2.1.3.2.2 (Deleted), E.3.2.1.3.2.3 (Deleted), E3.2.1.3.3, E3.2.1.3.3.1.2, E3.2.1.3.3.1.3, E3.2.1.3.3.1.4, E3.2.1.3.3.2, E3.2.1.3.4, E3.2.1.3.4.1, E3.2.1.3.4.1.1, E3.2.1.3.4.1.2, E3.2.1.3.5, E3.2.1.3.5.1, E3.2.1.3.5.1.1.

E3.2.1.3.5.1.2, E3.2.1.3.3.5, E3.2.1.4, E3.2.1.4.1, E3.2.1.4.1.1 E3.2.1.4.1.1.2, E3.2.1.5.1, E3.2.1.5.2.1, E3.2.1.5.2.2, E3.2.1.5.2.3, E3.2.1.5.2.4, E3.2.1.5.3, E3.2.1.5.3.1, E3.2.1.5.3.2 (Deleted), E3.2.1.5.3, E3.2.1.5.3.4 (Deleted), E3.2.1.5.4.1, E3.2.1.5.4.2, E3.2.1.7.1.1, E3.2.1.7.1.2, E3.2.1.7.1.3, E3.2.1.7.1.4, E3.2.1.7.1.5, E3.2.1.7.1.6, LIST OF CHANGES − Continued

SSCBD ENTRY DATE CHANGE PARAGRAPH(S)

xi

001786 42097−0133B E3.2.1.7.1.7, E3.2.1.7.2, E3.2.1.7.4.1, E3.2.1.7.4.2, E3.2.2.2.1, E3.2.2.2.2, E3.2.2.2.3, E3.2.2.2.3.1, E3.2.2.3.2, E3.2.2.3.3, E3.2.2.2.3.4, E3.2.2.2.3.5, E3.2.2.2.3.6, E3.2.2.2.4, E3.2.2.2.4.1, E3.2.2.2.4.2, E3.2.2.2.5, E3.2.2.2.5.1, E3.2.2.2.6.1, E3.2.2.2.6.2, E3.2.2.3.1, E3.2.2.3.1.1.3, E3.2.2.3.1.2 (Deleted), E3.2.2.3.2, E3.2.2.3.2.1, E3.2.2.3.2.1.2, E3.2.2.3.2.1.3, E3.2.2.3.2.2 (Deleted), E3.2.2.3.3, E3.2.2.3.3.1, E3.2.2.3.3.1.3, E3.2.2.3.3.1.4, E3.2.2.3.3.2 (Deleted), E3.2.2.3.4, E3.2.2.3.4.1.1, E3.2.2.3.4.1.2, E3.2.2.3.5, E3.2.2.3.5.1.1, E3.2.2.3.5.1.2, E3.2.2.4, E3.2.2.4.1, E3.2.2.4.1.1, E3.2.2.5.1, E3.2.2.5.2.1, E3.2.2.5.2.2, E3.2.2.5.2.3, E3.2.2.5.3.1, E3.2.2.5.3.2 (De-leted), E3.2.2.5.3.3 (Deleted), E3.2.2.5.3.4 (Deleted), E3.2.2.5.4.1, E3.2.2.5.4.2, E3.2.2.7.1.1, E3.2.2.7.1.2, E3.2.2.7.1.3, E3.2.2.7.1.4, E3.2.2.7.1.5, E3.2.2.7.1.6, E3.2.2.7.1.7, E3.2.2.7.4.1, E3.2.2.7.4.2 (Deleted)

TABLE(S)

E3.2.1.2.3.3−1, E3.2.1.4.1.1.1−1, E3.2.2.2.3.3−1

FIGURE(S)

E3.1.1−1, E3.1.1−2, E3.1.1.3−1, E3.1.1.3−2, E3.2.1.2.4−1, E3.2.1.2.5−1, E3.2.1.4−1

001464 42097−NA−0016B (PARAGRAPH(S)

E3.2.1.7.4.2, E3.2.1.7.4.2.1, (Add) E3.2.1.7.4.2.2, (Add) E3.2.2.7.4.2(Add), E3.2.2.7.4.2.1, (Add) E3.2.2.7.4.2.2(Add)

SSCBD ENTRY DATE CHANGE PARAGRAPH(S)

xii

001464 42097−NA−0016B TABLE(S)

E.3.2.1.7.4.2.1−1 (Add) E.3.2.1.7.4.2.1−2 (Add) E3.2.1.7.4.2.2−1, E3.2.1.7.4.2.2−2 (Add), E3.2.1.7.4.2.2−3(Add)

FIGURE(S)

E3.2.1.7.4.2.1−1 (Add)

001814 NA−0036A E3.2.1.3.3.1.3, E3.2.2.3.3.1.3

001814 NA−0038A E3.2.1.3.3.1.3, E.3.2.1.3.3.1.4 (Deleted), E3.3.2.3.3.1.3, E3.3.2.3.3.1.4 (Deleted)

003488 06/11 NA−0041 E3.2.1.3.3.4.1.2, E3.2.2.3.3.4.1.2

012968 06/11 NA−0043A E3.2.1.5.2.2, E3.2.1.5.2.4 (Deleted)

000202 06/11 NA−0044A E.2.2 (Adds), E3.1.1.1.1, E3.1.1.1.2 (Adds)

TABLE(S)

E.3.1.1.1.1−1 (Add)

FIGURE(S)

E.3.1.1.1.1−1 (Add)

PARAGRAPH(S)

008444, 008939, 06/11 NA−0045 2.1

009111, 009475, 001662, 001740, 009993, 001383, 001703, 003404, 009719, 009086

012010 06/11 NA−0046 PARAGRAPH(S)

E3.1.1, E3.1.1.3

FIGURE(S)

E3.1.1−1, E3.1.1−2, E3.1.1.3−1, E3.1.1.3−2

012968 06/11 NA−0047A E3.1.1, E3.1.1.1, E3.1.1.2, E3.2.1.3.3,

E3.2.1.3.3.1.2, E3.2.1.3.3.1.3, E3.2.1.3.3.2, SSCBD ENTRY DATE CHANGE PARAGRAPH(S) xiii

E3.2.1.3.4, E3.2.1.3.4.1.1, E3.2.1.3.4.1.2, E3.2.1.3.5, E3.2.1.3.5.1, E3.2.1.3.5.1.1, E3.2.1.3.5.1.2, E3.2.1.5.1, E3.2.1.5.2.2, E3.2.1.5.2.3, E3.2.1.5.3, E3.2.2.3.3, E3.2.2.3.3.1.2, E3.2.2.3.3.1.3, E3.2.2.3.4, E3.2.2.3.4.1, E3.2.2.3.4.1.1, E3.2.2.3.4.1.2, E3.2.2.3.5, E3.2.2.3.5.1, E3.2.2.3.5.1.2, E3.2.2.5.1, E3.2.2.5.2.2, E3.2.2.5.3, FIGURE(S)

E3.1.1−2

TABLE OF CONTENTS

PARAGRAPH PAGE

xiv

E1.0 INTRODUCTION E1 - 1

E1.1 PURPOSE AND SCOPE E1 - 1

E1.2 PRECEDENCE E1 - 1

E1.3 RESPONSIBILITY AND CHANGE AUTHORITY E1 - 1

E2.0 DOCUMENTS E2 - 1

E2.1 APPLICABLE DOCUMENTS E2 - 1

E2.2 REFERENCE DOCUMENTS E2 - 4

E3.0 INTERFACES E3 - 5

E3.1 GENERAL E3 - 5

E3.1.1 INTERFACE DESCRIPTION E3 - 5

E3.1.1.1 NODE 3 DESCRIPTION E3 - 5

E3.1.1.1.1 NODE 3 / PMA−3 CABLE SUPPORT DESCRIPTION E3 - 5

E3.1.1.1.2 NODE 3 / PMA−3 EXTERNAL CABLE SUPPORT INTERFACE E3 - 8

E3.1.1.2 PRESSURIZED MATING ADAPTER−3 DESCRIPTION E3 - 8

E3.1.1.3 INTERFACE PLANE DESCRIPTION E3 - 8

E3.1.1.4 COORDINATE SYSTEM E3 - 8

E3.1.1.4.1 SPACE STATION E3 - 8

E3.1.1.4.2 INTERFACING ELEMENT E3 - 8

E3.1.1.5 NODE 3 INTERFACE FUNCTIONS E3 - 8

E3.1.1.6 PRESSURIZED MATING ADAPTER 3 INTERFACE FUNCTIONS E3 - 12

E3.1.2 INTERFACE RESPONSIBILITIES E3 - 12

E3.1.2.1 RESPONSIBILITY FOR NODE ELEMENT 3 E3 - 12

E3.1.2.2 RESPONSIBILITY FOR PRESSURIZED MATING ADAPTER 3 E3 - 12

E3.2 INTERFACE REQUIREMENTS E3 - 13

E3.2.1 NODE 3 INTERFACE REQUIREMENTS E3 - 13

E3.2.1.1 ENVELOPE REQUIREMENTS E3 - 13

E3.2.1.1.1 DELETED E3 - 13

E3.2.1.1.2 RESERVED VOLUMES E3 - 13

E3.2.1.2 STRUCTURAL/MECHANICAL ATTACHMENT E3 - 13

E3.2.1.2.1 STRUCTURAL/MECHANICAL INTERFACE PROVISIONS E3 - 13

E3.2.1.2.2 BERTHING/ATTACHMENT MECHANISM(S) E3 - 13

E3.2.1.2.3 INTERCONNECTING UTILITY HARDWARE E3 - 13

E3.2.1.2.3.1 ACCESSIBILITY E3 - 14

E3.2.1.2.3.2 ELECTRICAL CONNECTORS E3 - 14

E3.2.1.2.3.3 FLUID FITTINGS E3 - 14

E3.2.1.2.3.4 UTILITY CABLE SPECIFICATIONS E3 - 14

E3.2.1.2.3.4.1 AUDIO CHANNEL CABLE SPECIFICATIONS E3 - 14

E3.2.1.2.3.4.2 DELETED E3 - 15

E3.2.1.2.3.4.3 POWER CABLE SPECIFICATIONS E3 - 15

E3.2.1.2.3.4.4 DELETED E3 - 15

E3.2.1.2.3.5 ATTACHMENT BRACKETS E3 - 15

E3.2.1.2.3.6 REDUNDANT UTILITY INTERFACES E3 - 15

E3.2.1.2.4 THERMAL REQUIREMENTS AT THE PMA−3 INTERFACE PLANE E3 - 15

E3.2.1.2.4.1 PMA−3 PRESSURIZED E3 - 15

E3.2.1.2.4.2 PMA−3 UNPRESSURIZED E3 - 15

E3.2.1.2.5 ACCESS/PASSAGE WAYS E3 - 17

E3.2.1.2.5.1 EVA PRIMARY TRANSLATION PATH E3 - 17

E3.2.1.2.6 ATMOSPHERIC SEALS E3 - 17

E3.2.1.2.6.1 SEAL LEAKAGE E3 - 17

E3.2.1.2.6.2 SEAL MONITORING E3 - 17

E3.2.1.2.7 DELETED E3 - 17

TABLE OF CONTENTS − Continued

PARAGRAPH PAGE

xv

E3.2.1.2.8 MATERIALS AND FINISHES E3 - 17

E3.2.1.3 FLUID INTERFACES E3 - 17

E3.2.1.3.1 SUPPLY INTERMODULE ATMOSPHERE E3 - 17

E3.2.1.3.1.1 INTERMODULE ATMOSPHERE CHARACTERISTICS E3 - 19

E3.2.1.3.1.1.1 DELETED E3 - 19

E3.2.1.3.1.1.2 INTERMODULE ATMOSPHERE SUPPLY TEMPERATURE E3 - 19

E3.2.1.3.1.1.3 INTERMODULE ATMOSPHERE SUPPLY RATE E3 - 19

E3.2.1.3.2 RECEIVE RETURN INTERMODULE ATMOSPHERE E3 - 19

E3.2.1.3.2.1 INTERMODULE ATMOSPHERE CHARACTERISTICS E3 - 19

E3.2.1.3.2.1.1 DELETED E3 - 19

E3.2.1.3.2.1.2 INTERMODULE ATMOSPHERE RECEIVE RETURN TEMPERATURE E3 - 19

E3.2.1.3.2.1.3 INTERMODULE ATMOSPHERE RECEIVE RETURN RATE E3 - 19

E3.2.1.3.2.2 DELETED E3 - 19

E3.2.1.3.2.3 DELETED E3 - 19

E3.2.1.3.3 RECEIVE FUEL CELL WATER E3 - 19

E3.2.1.3.3.1 FUEL CELL WATER CHARACTERISTICS E3 - 20

E3.2.1.3.3.1.1 FUEL CELL WATER QUALITY E3 - 20

E3.2.1.3.3.1.2 FUEL CELL WATER RECEIVE TEMPERATURE E3 - 20

E3.2.1.3.3.1.3 FUEL CELL WATER RECEIVE PRESSURE E3 - 20

E3.2.1.3.3.1.4 DELETED E3 - 20

E3.2.1.3.3.2 FUEL CELL WATER SUPPLY AVAILABILITY E3 - 20

E3.2.1.3.4 RECEIVE RECHARGE OXYGEN E3 - 20

E3.2.1.3.4.1 RECHARGE OXYGEN CHARACTERISTICS E3 - 20

E3.2.1.3.4.1.1 RECEIVE RECHARGE OXYGEN TEMPERATURE E3 - 20

E3.2.1.3.4.1.2 RECEIVE RECHARGE OXYGEN PRESSURE E3 - 20

E3.2.1.3.5 RECEIVE RECHARGE NITROGEN E3 - 21

E3.2.1.3.5.1 RECHARGE NITROGEN CHARACTERISTICS E3 - 21

E3.2.1.3.5.1.1 RECEIVE RECHARGE NITROGEN TEMPERATURE E3 - 21

E3.2.1.3.5.1.2 RECEIVE NITROGEN RECHARGE PRESSURE E3 - 21

E3.2.1.4 ELECTRICAL INTERFACES E3 - 21

E3.2.1.4.1 SUPPLY POWER E3 - 21

E3.2.1.4.1.1 POWER OUTPUTS PMA3APASHTRS AND PMA3SHELLHTRS E3 - 22

E3.2.1.4.1.1.1 POWER QUALITY E3 - 22

E3.2.1.4.1.1.2 FAULT PROTECTION E3 - 22

E3.2.1.4.2 DELETED E3 - 22

E3.2.1.5 ELECTRONIC INTERFACES E3 - 22

E3.2.1.5.1 AUDIO CHANNEL E3 - 22

E3.2.1.5.2 COMMAND AND DATA HANDLING MIL−STD−1553B INTERFACE E3 - 23

E3.2.1.5.2.1 DATA BUS STANDARDS E3 - 23

E3.2.1.5.2.2 INTERFACE BUSSES E3 - 23

E3.2.1.5.2.3 PROVIDE OUTPUT AMPLITUDE E3 - 24

E3.2.1.5.2.4 DELETED E3 - 24

E3.2.1.5.3 VIDEO SIGNALS E3 - 24

E3.2.1.5.3.1 VIDEO CHANNEL SIGNAL CHARACTERISTICS E3 - 24

E3.2.1.5.3.2 DELETED E3 - 24

E3.2.1.5.3.3 DELETED E3 - 24

E3.2.1.5.3.4 DELETED E3 - 24

E3.2.1.5.4 INSTRUMENTATION INTERFACE E3 - 24

E3.2.1.5.4.1 PMA−3 SHELL AND APAS TEMPERATURE SENSORS E3 - 24

E3.2.1.5.4.2 GNC MODING INSTRUMENTATION SIGNALS E3 - 24

E3.2.1.6 SOFTWARE INTERFACES E3 - 25

E3.2.1.7 ENVIRONMENTS E3 - 25

PARAGRAPH PAGE

xvi

E3.2.1.7.1 ELECTROMAGNETIC EFFECTS E3 - 25

E3.2.1.7.1.1 ELECTROMAGNETIC COMPATIBILITY E3 - 25

E3.2.1.7.1.2 ELECTROMAGNETIC INTERFERENCE E3 - 25

E3.2.1.7.1.3 GROUNDING E3 - 25

E3.2.1.7.1.4 BONDING E3 - 25

E3.2.1.7.1.5 CABLE AND WIRE DESIGN E3 - 25

E3.2.1.7.1.6 ELECTROSTATIC DISCHARGE E3 - 26

E3.2.1.7.1.7 CORONA E3 - 26

E3.2.1.7.2 THERMAL E3 - 26

E3.2.1.7.3 ACOUSTIC E3 - 26

E3.2.1.7.4 STRUCTURAL LOADS E3 - 26

E3.2.1.7.4.1 INTERFACE LOADS E3 - 26

E3.2.1.7.4.2 ON−ORBIT THERMAL STRUCTURAL LOADS E3 - 27

E3.2.1.7.4.2.1 ON−ORBIT THERMALLY INDUCED STRUCTURAL LOADS E3 - 27

E3.2.1.7.4.2.2 ON−ORBIT THERMALLY INDUCED LOADS SPECTRA E3 - 30

E3.2.2 PRESSURIZED MATING ADAPTER 3 INTERFACE REQUIREMENTS E3 - 31

E3.2.2.1 ENVELOPE REQUIREMENTS E3 - 31

E3.2.2.1.1 DELETED E3 - 31

E3.2.2.1.2 RESERVED VOLUMES E3 - 31

E3.2.2.2 STRUCTURAL/MECHANICAL ATTACHMENT E3 - 32

E3.2.2.2.1 STRUCTURAL/MECHANICAL INTERFACE PROVISIONS E3 - 32

E3.2.2.2.2 BERTHING/ATTACHMENT MECHANISM(S) E3 - 32

E3.2.2.2.3 INTERCONNECTING UTILITY HARDWARE E3 - 32

E3.2.2.2.3.1 ACCESSIBILITY E3 - 32

E3.2.2.2.3.2 ELECTRICAL CONNECTORS E3 - 32

E3.2.2.2.3.3 FLUID FITTINGS E3 - 33

E3.2.2.2.3.4 UTILITY CABLE SPECIFICATIONS E3 - 33

E3.2.2.2.3.4.1 AUDIO CHANNEL CABLE SPECIFICATIONS E3 - 33

E3.2.2.2.3.4.2 DELETED E3 - 33

E3.2.2.2.3.4.3 POWER CABLE SPECIFICATIONS E3 - 33

E3.2.2.2.3.4.4 VIDEO DATA BUS CABLE SPECIFICATIONS E3 - 33

E3.2.2.2.3.5 ATTACHMENT BRACKETS E3 - 33

E3.2.2.2.3.6 REDUNDANT UTILITY INTERFACES E3 - 34

E3.2.2.2.4 THERMAL REQUIREMENTS AT THE PMA−3 INTERFACE PLANE E3 - 34

E3.2.2.2.4.1 PMA−3 PRESSURIZED E3 - 34

E3.2.2.2.4.2 PMA−3 UNPRESSURIZED E3 - 34

E3.2.2.2.5 ACCESS/PASSAGE WAYS E3 - 34

E3.2.2.2.5.1 EVA PRIMARY TRANSLATION PATH E3 - 35

E3.2.2.2.6 ATMOSPHERIC SEALS E3 - 35

E3.2.2.2.6.1 SEAL LEAKAGE E3 - 35

E3.2.2.2.6.2 SEAL MONITORING E3 - 35

E3.2.2.2.7 DELETED E3 - 35

E3.2.2.2.8 MATERIALS AND FINISHES E3 - 35

E3.2.2.3 FLUID INTERFACES E3 - 35

E3.2.2.3.1 RECEIVE INTERMODULE ATMOSPHERE E3 - 35

E3.2.2.3.1.1 INTERMODULE ATMOSPHERE CHARACTERISTICS E3 - 36

E3.2.2.3.1.1.1 DELETED E3 - 36

E3.2.2.3.1.1.2 INTERMODULE ATMOSPHERE RECEIVE TEMPERATURE E3 - 36

E3.2.2.3.1.1.3 INTERMODULE ATMOSPHERE RECEIVE RATE E3 - 36

E3.2.2.3.1.2 DELETED E3 - 36

E3.2.2.3.2 RETURN INTERMODULE ATMOSPHERE E3 - 36

E3.2.2.3.2.1 INTERMODULE ATMOSPHERE CHARACTERISTICS E3 - 36

PARAGRAPH PAGE

xvii

E3.2.2.3.2.1.1 DELETED E3 - 36

E3.2.2.3.2.1.2 INTERMODULE ATMOSPHERE RETURN TEMPERATURE E3 - 36

E3.2.2.3.2.1.3 INTERMODULE ATMOSPHERE RETURN RATE E3 - 36

E3.2.2.3.2.2 DELETED E3 - 37

E3.2.2.3.3 SUPPLY FUEL CELL WATER E3 - 37

E3.2.2.3.3.1 FUEL CELL WATER CHARACTERISTICS E3 - 37

E3.2.2.3.3.1.1 FUEL CELL WATER QUALITY E3 - 37

E3.2.2.3.3.1.2 FUEL CELL WATER SUPPLY TEMPERATURE E3 - 37

E3.2.2.3.3.1.3 FUEL CELL WATER SUPPLY PRESSURE E3 - 37

E3.2.2.3.3.1.4 DELETED E3 - 37

E3.2.2.3.3.2 DELETED E3 - 37

E3.2.2.3.4 SUPPLY RECHARGE OXYGEN E3 - 37

E3.2.2.3.4.1 RECHARGE OXYGEN CHARACTERISTICS E3 - 37

E3.2.2.3.4.1.1 SUPPLY RECHARGE OXYGEN TEMPERATURE E3 - 37

E3.2.2.3.4.1.2 SUPPLY RECHARGE OXYGEN PRESSURE E3 - 38

E3.2.2.3.5 SUPPLY RECHARGE NITROGEN E3 - 38

E3.2.2.3.5.1 RECHARGE NITROGEN CHARACTERISTICS E3 - 38

E3.2.2.3.5.1.1 SUPPLY RECHARGE NITROGEN TEMPERATURE E3 - 38

E3.2.2.3.5.1.2 SUPPLY RECHARGE NITROGEN PRESSURE E3 - 38

E3.2.2.4 ELECTRICAL INTERFACES E3 - 38

E3.2.2.4.1 RECEIVE POWER E3 - 38

E3.2.2.4.1.1 POWER INPUTS PMA3APASHTRS AND PMASHELLHTRS E3 - 38

E3.2.2.4.1.1.1 POWER QUALITY E3 - 38

E3.2.2.4.1.1.2 FAULT PROTECTION E3 - 39

E3.2.2.5 ELECTRONIC INTERFACES E3 - 39

E3.2.2.5.1 AUDIO CHANNEL E3 - 39

E3.2.2.5.2 COMMAND AND DATA HANDLING MIL−STD−1553B INTERFACE E3 - 39

E3.2.2.5.2.1 DATA BUS STANDARDS E3 - 39

E3.2.2.5.2.2 INTERFACE BUSSES E3 - 40

E3.2.2.5.2.3 PROVIDE OUTPUT AMPLITUDE E3 - 40

E3.2.2.5.3 VIDEO SIGNALS E3 - 40

E3.2.2.5.3.1 VIDEO CHANNEL SIGNAL CHARACTERISTICS E3 - 40

E3.2.2.5.3.2 DELETED E3 - 40

E3.2.2.5.3.3 DELETED E3 - 40

E3.2.2.5.3.4 DELETED E3 - 40

E3.2.2.5.4 INSTRUMENTATION INTERFACE E3 - 40

E3.2.2.5.4.1 PMA−3 SHELL AND APAS TEMPERATURE SENSORS E3 - 40

E3.2.2.5.4.2 GNC MODING INSTRUMENTATION SIGNALS E3 - 41

E3.2.2.6 SOFTWARE INTERFACES E3 - 41

E3.2.2.7 ENVIRONMENTS E3 - 41

E3.2.2.7.1 ELECTROMAGNETIC EFFECTS E3 - 41

E3.2.2.7.1.1 ELECTROMAGNETIC COMPATIBILITY E3 - 41

E3.2.2.7.1.2 ELECTROMAGNETIC INTERFERENCE E3 - 41

E3.2.2.7.1.3 GROUNDING E3 - 41

E3.2.2.7.1.4 BONDING E3 - 41

E3.2.2.7.1.5 CABLE AND WIRE DESIGN E3 - 41

E3.2.2.7.1.6 ELECTROSTATIC DISCHARGE E3 - 42

E3.2.2.7.1.7 CORONA E3 - 42

E3.2.2.7.2 THERMAL E3 - 42

E3.2.2.7.3 ACOUSTIC E3 - 42

E3.2.2.7.4 STRUCTURAL LOADS E3 - 42

E3.2.2.7.4.1 INTERFACE LOADS E3 - 42

PARAGRAPH PAGE

xviii

E3.2.2.7.4.2 ON−ORBIT THERMAL STRUCTURAL LOADS E3 - 42

E3.2.2.7.4.2.1 ON−ORBIT THERMALLY INDUCED STRUCTURAL LOADS E3 - 42

E3.2.2.7.4.2.2 ON−ORBIT THERMALLY INDUCED LOADS SPECTRA E3 - 42

E4.1 ABBREVIATIONS AND ACRONYMS E4 - 43

TABLE PAGE

TABLES

xix

E3.1.1.1.1−1 EVA CLAMP LOCATIONS E3 - 5

E3.2.1.2.3.3−2 FLUID FITTING SPECIFICATIONS E3 - 14

E3.2.1.4.1.1.1−1 ELECTRICAL INTERFACE PARAMETERS E3 - 22

E3.2.1.7.4.1−1 TRANSIENT LIMIT LOADS FOR NODE ELEMENT 3 TO PRESSURIZED

MATING ADAPTER 3 INTERFACES E3 - 26

E3.2.1.7.4.1−2 LOADS SPECTRUM FOR NODE ELEMENT 3 TO PRESSURIZED

MATING ADAPTER 3 E3 - 27

E3.2.1.7.4.2.1−1 ON−ORBIT THERMALLY INDUCED STRUCTURAL LOADS E3 - 28

E3.2.1.7.4.2.1−2 ACBM/PCBM INTERFACE BOLT LOCATIONS E3 - 29

E3.2.1.7.4.2.2−1 ON−ORBIT TRANSIENT THERMAL LOADS E3 - 30

E3.2.1.7.4.2.2−2 ON−ORBIT THERMALLY INDUCED LOADS SPECTRUM E3 - 31

E3.2.1.7.4.2.2−3 ON−ORBIT THERMALLY INDUCED MEAN BERTHING LOADS E3 - 31

E3.2.2.2.3.3−1 FLUID FITTING SPECIFICATIONS E3 - 33

FIGURE PAGE

FIGURES

xx

E3.1.1−1 NODE ELEMENT 3 TO PRESSURIZED MATING ADAPTER 3 ON−ORBIT

CONFIGURATION E3 - 6

E3.1.1−2 NODE ELEMENT 3 TO PRESSURIZED MATING ADAPTER 3 FUNCTIONAL

INTERFACE DIAGRAM E3 - 7

E3.1.1.1.1−1 NODE 3 NADIR ENDCONE MDPS PANELS W/TA CLAMP’S E3 - 9

E3.1.1.3−1 NODE ELEMENT 3 TO PRESSURIZED MATING ADAPTER 3

STRUCTURAL/MECHANICAL INTERFACE PLANE E3 - 10

E3.1.1.3−2 NODE ELEMENT 3 TO PRESSURIZED MATING ADAPTER 3 UTILITY

INTERFACE PLANE E3 - 11

E3.2.1.2.4−1 PMA−3 TO NODE 3 PASSIVE THERMAL INTERFACE E3 - 16

E3.2.1.2.5−1 NODE ELEMENT 3 TO PRESSURIZED MATING ADAPTER 3

ACCESS/PASSAGEWAY ENVELOPE E3 - 18

E3.2.1.4−1 NODE 3 TO PMA−3 ELECTRICAL INTERFACES E3 - 21

E3.2.1.7.4.2.1−1 ACBM/PCBM INTERFACE PLANE ATTACHMENT BOLT LOCATIONS E3 - 29

E1 - 1

E1.0 INTRODUCTION

E1.1 PURPOSE AND SCOPE

The purpose of this document is to provide definition of the physical and functional interface requirements between the Pressurized Mating Adapter (PMA)−3 and the Node Element 3 (Node 3).

The scope of this document covers the interface between PMA−3 and Node 3.

E1.2 PRECEDENCE

In the event of conflict between SSP 41000, International Space Station System Specification, and the contents of this Interface Control Document (ICD), the requirements of SSP 41000 shall take precedence.

E1.3 RESPONSIBILITY AND CHANGE AUTHORITY

This document is prepared and maintained in accordance with SSP 30459, International Space Station Interface Control Plan.

E2 - 1

E2.0 DOCUMENTS

E2.1 APPLICABLE DOCUMENTS

The documents in this paragraph are applicable to the extent specified herein. Inclusion of applicable documents herein does not in any way supersede the order of precedence identified in paragraph E1.3. The references show where each applicable document is cited in this document.

DOCUMENT NO. TITLE

683−16347 Revision F July 11, 1997

Fitting, Threaded Fluid

References Table: E3.2.1.2.3.3.−1, E3.2.2.2.3.3.–1

683−16348, Revision G

ADCN TBD (8444)

January 27, 1998

Coupling, Quick Disconnect, Fluid, Self Sealing, Internal

References Table: E3.2.1.2.3.3.−1, E3.2.2.2.3.3.–1

MIL−C−27500

Amendment February 23, 1990

General Specifications for Cable, Power, Electrical and Cable Amendment 1 Special Purpose, Electrical Shielded and Unshielded

References E3.2.1.2.3.4.1, E3.2.2.2.3.4.1

MIL−STD−1553

Revision B, CN−02 September 8, 1986

Digital Time Division Command/Response Multiplex Data Bus

References E3.2.1.5.2, E3.2.1.5.2.1, E3.2.1.5.2.3, E3.2.2.5.2, E3.2.2.5.2.1, E3.2.2.5.2.3

SSP 30219

Revision H June 1, 2005

Space Station Reference Coordinate Systems

References E3.1.1.4.1, E3.1.1.4.2

SSP 30233

Revision H August 21, 2007

Space Station Requirements for Materials and Processes

References E3.2.1.2.8, E3.2.2.2.8

E2 - 2

DOCUMENT NO. TITLE

SSP 30240

Revision C, DCN 010 September 30, 1998

Space Station Grounding Requirements

References E3.2.1.7.1.3, E3.2.2.7.1.3

SSP 30242

Revision E September 30, 1998

Space Station Cable/Wire Design and Control Requirements for Electromagnetic Compatibility

References E3.2.1.7.1.5, E3.2.2.7.1.5

SSP 30243

Revision E, DCN 003, 004 June 9, 1998

Space Systems Requirements for Electromagnetic Compatibility

References E3.2.1.7.1.1, E3.2.1.7.1.2, E3.2.1.7.1.6, E3.2.1.7.1.7, E3.2.2.7.1.1, E3.2.2.7.1.2, E3.2.2.7.1.6, E3.2.2.7.1.7

SSP 30245

Revision D, DCN 004, 005, 006 June 4, 1998

Space Station Electrical Bonding Requirements

References E3.2.1.7.1.4, E3.2.2.7.1.4

SSP 30256:001

Revision H July 17, 2006

Space Station Program EVA Standard ICD

References E3.2.1.2.5.1, E3.2.2.2.5.1

SSP 30261:002

Rev J, IRNs 0060, 00063, 0068 April 1, 1998

International Space Station Multiplexer/Demultiplexer (SSMDM) Standard ICD

References E3.2.1.5.4.1, E3.2.1.5.4.2, E3.2.2.5.4.1, E3.2.2.5.4.2

SSP 30263:002

Revision N December 4, 1998

Remote Power Control Module (RPCM) Standard Interface Control Document

References Table: E3.2.1.4.1.1.1−1

SSP 30426

Revision D January 21, 1994

Space Station External Contamination Control Requirements

References E3.2.1.2.8, E3.2.2.2.8

E2 - 3

DOCUMENT NO. TITLE

SSP 30459

Revision F March 23, 1994

Space Station Interface Control Plan

References E1.3

SSP 41004

Rev H October 25, 2005

Common Berthing Mechanism to Pressurized Elements Interface Control Document, Part 1

References E3.2.1.1.2, E3.2.1.2.2, E3.2.2.2.2

SSP 41148

Revision D September 30, 1998

Active Common Berthing Mechanism to Passive Common Berthing Mechanism Interface Control

References E3.1.1.3, E3.2.1.2.2, E3.2.1.2.6.1, 3.2.1.2.6.2, E3.2.2.2.2, E3.2.2.2.6.1, E3.2.2.2.6.2

SSP 50005

Revision E, June 30, 2005

International Space Station Flight Crew Standard (NASA−STD−3000/T)

References E3.2.1.2.3.1, E3.2.1.2.3.3, E3.2.1.7.3, E3.2.2.2.3.1, E3.2.2.2.3.3, E3.2.2.7.2

SSP 50023

Revision Basic April 15, 1994

Space Station Program Thermal Control Plan Basic

References E3.2.1.7.2, E3.2.2.7.2

SSQ 21635

Revision H, DCN 001, 011, 012, 013, 014, 015 August 1, 1997

Connectors and Accessories, Electrical, Circular, Miniature, IVA/EVA Compatible, Space Station Quality, General Specifications for

References E3.2.1.2.3.2, E3.2.2.2.3.2

SSQ 21652

Revision E July 15, 1998

General Specification for Wire, Electric, Silicone Insulated, Nickel Coated Copper, Space Quality

References E3.2.1.2.3.4.3, E3.2.2.2.3.4.3

SSQ 21655

Revision E July 15, 1998

Cable, Electrical, MIL−STD−1553 Data Bus, Space Quality, General Specification for

References E3.2.2.2.3.4.4

E2 - 4

DOCUMENT NO. TITLE

SSQ 21656

Revision C, DCN 001, 002 April 25, 1996

Wire and Cable, Electric, Fluoropolymer−Insulated, Nickel Coated Copper or Copper Alloy, General Specification for

References E3.2.1.2.3.4.3, E3.2.2.2.3.4.3

E2.2 REFERENCE DOCUMENTS

The following documents are referenced in this ICD for context and user convenience.

DOCUMENT NO. TITLE

SSP 41000 International Space Station System Specification

Reference E1.2

9810ND003

Drawing

EXT Nadir Cone Installation

Reference Figure: E3.1.1.1.1−1

0000ND003

Drawing

Node 3 Assy

Reference Figure: E3.1.1.1.1−1

E3 - 5

E3.0 INTERFACES

E3.1 GENERAL

E3.1.1 INTERFACE DESCRIPTION

The Node 3 to PMA−3 on−orbit configuration is shown in Figure E3.1.1−1. The functional interfaces described in the following paragraphs are defined in Figure E3.1.1−2.

The only utility interfaces connected between Node 3 and PMA−3 are for intermodule ventilation, electrical power, and instrumentation. All other interfaces described in this ICD are scarred and not connected.

E3.1.1.1 NODE 3 DESCRIPTION

Node 3 is a pressurized element which provides living accommodations for on−orbit astronauts.

Node 3 contains a limited amount of powered hardware and provisions for storing crew necessities. Node 3 shall provide data, audio, video, air, sample structural/mechanical interfaces for PMA−3. Node 3 shall support a continuous Extravehicular Activity (EVA) primary translation path across Node 3−to−PMA−3 interface.

E3.1.1.1.1 NODE 3 / PMA−3 CABLE SUPPORT DESCRIPTION

Node 3 provides for external support of PMA−3 utility cables that will not violate EVA keepout/worksite areas or cover identification, instruction, or decal−type labels as specified in Table E3.1.1.1.1−1, EVA Clamp Locations.

TABLE E3.1.1.1.1−1 EVA CLAMP LOCATIONS

COORDINATES (mm)

MDPS PANEL X Y Z

CLAMP000 C202 −1903.6 −1309.4 +542.4

CLAMP001 C203 −1903.6 −542.4 +1309.5

CLAMP002 C203 −1841.2 −196.1 +1945

CLAMP003 C204 −1834.9 240.1 1974

CLAMP004 C204 −1903.6 +542.4 +1309.5

CLAMP005 C205 −1903.6 +1309.4 +542.4

E3 - 6

FIGURE E3.1.1−1 NODE ELEMENT 3 TO PRESSURIZED MATING ADAPTER 3

ON−ORBIT CONFIGURATION

NODE 3

PMA−3

NODE 3

PORT

ZENITH AFT

PORT

NODE 3

PMA−3

NODE 3

NODE 1

E3 - 7

FIGURE E3.1.1−2 NODE ELEMENT 3 TO PRESSURIZED MATING ADAPTER 3

FUNCTIONAL INTERFACE DIAGRAM

NODE 3 PMA−3

POWER

DATA (2)

AUDIO (1)

STRUCTURAL/MECHANICAL

VIDEO (1)

AIR

FUEL CELL WATER (1)

RECHARGE OXYGEN (1)

RECHARGE NITROGEN (1)

Notes:

(1) Interface is scarred only.

(2) Only instrumentation interface (P601/J103) is connected. Other data interfaces are scarred.

E3 - 8

E3.1.1.1.2 NODE 3 / PMA−3 EXTERNAL CABLE SUPPORT INTERFACE

The PMA−3 to Node 3 utility umbilicals support interface are external, releasable EVA cable clamps (Figure E3.1.1.1.1−1) located on Node 3 nadir panels C202, C203, C204, and C205 per Alenia drawings No. 9810ND003 and No. 0000ND003. (NCCS−EI−D−A−10−1 side mount type clamps)

E3.1.1.2 PRESSURIZED MATING ADAPTER−3 DESCRIPTION

PMA−3 shall provide a conditioned environment passageway for crew members and equipment when the orbiter is docked to the station.

PMA−3 shall provide power, air, instrumentation, and structural/mechanical interfaces to Node 3. PMA−3 shall scar data, audio, fuel cell water, recharge oxygen, and recharge nitrogen interfaces to Node 3.

E3.1.1.3 INTERFACE PLANE DESCRIPTION

The on−orbit structural/mechanical interface is between the Active Common Berthing Mechanism (ACBM) on Node 3 and the Passive Common Berthing Mechanism (PCBM) on PMA−3 as defined in Figure E3.1.1.3−1. The ACBM to PCBM interface is in accordance with SSP 41148, ACBM to PCBM ICD. The PMA−3/Node 3 external utility interface plane shall be located on the external Node 3 endring as defined in Figure E3.1.1.3−2. The PMA−3/Node 3 internal utility interface plane shall be located at the Node 3 bulkhead as defined in Figure E3.1.1.3−2.

E3.1.1.4 COORDINATE SYSTEM

E3.1.1.4.1 SPACE STATION

The space station coordinate system is defined in SSP 30219, Space Station Reference Coordinate Systems.

E3.1.1.4.2 INTERFACING ELEMENT

Node 3 coordinate system is defined in SSP 30219 Systems. PMA−3 coordinate system is defined in the core document.

E3.1.1.5 NODE 3 INTERFACE FUNCTIONS

Node 3 supports the following functions at the interface to PMA−3.

a. Structural/Mechanical Attachment

E3 - 9

Model edited for clarity.

FIGURE E3.1.1.1.1−1 NODE 3 NADIR ENDCONE MDPS PANELS W/TA CLAMP’S

b. Utility Distribution

c. Provide Passageway/Access

d. Provide Berthing/Mating Aids

e. Supply Power

f. Receive Recharge O2

g. Receive Recharge N2

h. Control Power

i. Supply Atmosphere

j. Receive Return Atmosphere

k. Receive Fuel Cell Water

l. Supply Data and Command

E3 - 10

FIGURE E3.1.1.3−1 NODE ELEMENT 3 TO PRESSURIZED MATING ADAPTER 3

STRUCTURAL/MECHANICAL INTERFACE PLANE

NODE 3

AFT

PORT

E3 - 11

ACTIVE COMMON

BERTHING MECHANISM

PASSIVE COMMON

BERTHING MECHANISM

INTERNAL UTILITY

INTERFACE PLANE

EXTERNAL UTILITY

INTERFACE PLANE

(Node 3 Endring)

PORT

AFT

NODE 3

FIGURE E3.1.1.3−2 NODE ELEMENT 3 TO PRESSURIZED MATING ADAPTER 3 UTILITY

INTERFACE PLANE

E3 - 12

m. Receive Data and Command

n. Supply Communications (Audio, Video)

o. Receive Communications (Audio, Video)

E3.1.1.6 PRESSURIZED MATING ADAPTER 3 INTERFACE FUNCTIONS

PMA−3 supports the following functions at the interface to Node 3:

a. Structural/Mechanical Attachment

b. Utility Distribution

c. Provide Passageway/Access

d. Provide Berthing/Mating Aids

e. Supply Recharge O2

f. Supply Recharge N2

g. Receive Power

h. Receive Atmosphere

i. Return Atmosphere

j. Supply Fuel Cell Water

k. Supply Data and Command

l. Receive Data and Command

m. Supply Communications (Audio, Video)

n. Receive Communications (Audio, Video)

E3.1.2 INTERFACE RESPONSIBILITIES

Node 3 and PMA−3 shall conform to the interfaces controlled by this document.

E3.1.2.1 RESPONSIBILITY FOR NODE ELEMENT 3

ASI is responsible for the module primary structure and module outfitting interface requirements imposed on Node 3.

E3.1.2.2 RESPONSIBILITY FOR PRESSURIZED MATING ADAPTER 3

NASA is responsible for the module structure interface and module outfitting interface requirements imposed on PMA−3.

E3 - 13

E3.2 INTERFACE REQUIREMENTS

E3.2.1 NODE 3 INTERFACE REQUIREMENTS

E3.2.1.1 ENVELOPE REQUIREMENTS

E3.2.1.1.1 DELETED

E3.2.1.1.2 RESERVED VOLUMES

Volume shall be reserved at this interface for utility jumpers in accordance with SSP 41004, Common Berthing Mechanism to Pressurized Elements Interface Control Document, Part 1.

E3.2.1.2 STRUCTURAL/MECHANICAL ATTACHMENT

E3.2.1.2.1 STRUCTURAL/MECHANICAL INTERFACE PROVISIONS

Node 3 shall supply structural and mechanical provisions for the mechanical attachment of Node 3 to PMA−3 during on−orbit assembly, in accordance with the loads defined in Section E3.2.1.7.4.1−1.

E3.2.1.2.2 BERTHING/ATTACHMENT MECHANISM(S)

Node 3 ACBM shall provide alignment, capture, and rigidization mechanisms for the mechanical attachment of Node 3 to PMA−3 during on−orbit assembly.

Interfaces between the Common Berthing Mechanism and Node 3 shall be in accordance with

SSP 41004.

Node 3 shall provide the ACBM.

The ACBM of Node 3 shall support the capability to attach to and from a pressurized seal with PCBM on PMA−3 in accordance with SSP 41148.

E3.2.1.2.3 INTERCONNECTING UTILITY HARDWARE

The Node 3 interface design shall incorporate provisions for the mechanical connection of power, data, audio, video, air, and sample utilities between Node 3 and PMA−3 during on−orbit assembly. All external connections to PMA−3 shall be established prior to arrival of the Orbiter.

E3 - 14

E3.2.1.2.3.1 ACCESSIBILITY

The external utility interface design shall comply with SSP 50005, International Space Station Flight Crew Standard, requirements for accessibility by EVA suited crew members.

All internal utility interface connections between Node 3 and PMA−3 shall be designed to be manually mateable before opening of the hatch of Node 3 in the berthed configuration. Internal utility interface design shall comply with SSP 50005, requirements for Intravehicular Activity (IVA) accessibility, paragraph 12.3.1.

E3.2.1.2.3.2 ELECTRICAL CONNECTORS

The characteristics for electrical connectors shall be in accordance with SSQ 21635, General Specifications for Connectors and Accessories, Electrical, Circular, Miniature, IVA/EVA/Robot Compatible, Space Quality.

E3.2.1.2.3.3 FLUID FITTINGS

The fluid utility parts with service lines through them shall have mounted Type I Quick Disconnect (QD) valves which are self−sealing.

Fluid coupler requirements shall conform to SSP 50005, paragraph 11.10.3.1.

Fluid fittings/couplings used at interelement interfaces shall comply with the specifications shown in Table E3.2.1.2.3.3−2.

TABLE E3.2.1.2.3.3−2 FLUID FITTING SPECIFICATIONS

Quick Disconnect Fluid Internal 683-16348 Vestibule and module internal use only

Threaded Fitting Fluid Internal 683-16347 None

E3.2.1.2.3.4 UTILITY CABLE SPECIFICATIONS

E3.2.1.2.3.4.1 AUDIO CHANNEL CABLE SPECIFICATIONS

The audio data bus interconnect cables shall be twisted shielded pair wires that comply with the requirements of MIL−C−27500 for M27500−22T2N06 twisted shielded cable.

E3 - 15

E3.2.1.2.3.4.2 DELETED

E3.2.1.2.3.4.3 POWER CABLE SPECIFICATIONS

The 120 VDC utility power cables shall conform to SSQ 21652, General Specification for Wire, Electric, Silicone Insulated, Nickel Coated Copper, Space Quality and SSQ 21656, Wire and Cable, Electric, Fluoropolymer−Insulated, Nickel Coated Copper or Copper Alloy, General Specification for.

E3.2.1.2.3.4.4 DELETED

E3.2.1.2.3.5 ATTACHMENT BRACKETS

Node 3 shall provide attachment brackets for the vestibule closeouts.

E3.2.1.2.3.6 REDUNDANT UTILITY INTERFACES

Node 3 shall provide redundant utility interfaces for power distribution, thermal conditioning and element−to−element command and control and communications. Alternate or redundant functional paths shall be separated or protected at the interface such that a credible event which causes the loss of one functional path will not result in the loss of the alternate or redundant functional path(s).

E3.2.1.2.4 THERMAL REQUIREMENTS AT THE PMA−3 INTERFACE PLANE

The thermal interface between Node 3 and PMA−3 is depicted schematically in Figure E3.2.1.2.4−1. Heat is transferred between Node 3 and PMA−3 by conduction across the common berthing mechanism and by radiation between the Node 3 hatch and the interior of

PMA−3.

E3.2.1.2.4.1 PMA−3 PRESSURIZED

Node 3 shall maintain the temperature of the ACBM in the range of 60°F to 113°F without relying on heat transfer across the Common Berthing Mechanism (CBM) interface or radiation heat transfer with PMA−3.

E3.2.1.2.4.2 PMA−3 UNPRESSURIZED

Node 3 shall maintain the temperature of the ACBM berthing plate, and hatch plate in the range of 60°F to 113°F and shall account for the conduction and radiation heat transfer from Node 3 to PMA−3 resulting from the difference in the specified temperature ranges.

E3 - 16

Node 3 to ACBM thermal resistance, R1 = 0.0082 hr−F/Btu

ACBM to PCBM thermal resistance, R2 = 0.013 to 0.0925 hr−F/Btu

PCBM to PMA thermal resistance, R3 = 0.019 hr−F/Btu

NODE 3

FIGURE E3.2.1.2.4−1 PMA−3 TO NODE 3 PASSIVE THERMAL INTERFACE

E3 - 17

E3.2.1.2.5 ACCESS/PASSAGE WAYS

The Node 3 to PMA−3 access/passageway shall be as defined in Figure E3.2.1.2.5−1 after berthing and outfitting of the port. There shall be no protrusions into the passageway envelope.

E3.2.1.2.5.1 EVA PRIMARY TRANSLATION PATH

Node 3 shall provide EVA translation aids in support of a continuos primary translation path across Node 3−to−PMA−3 interface as defined in SSP 30256:001, Space Station Program EVA Standard ICD. Gaps in the path across the interface shall not exceed 24 inches. The diameter of the translation path corridor across the interface shall be a minimum of 43 inches. There shall be no protrusions into the corridor.

E3.2.1.2.6 ATMOSPHERIC SEALS

E3.2.1.2.6.1 SEAL LEAKAGE

Node 3 to PMA−3 atmosphere leakage interface requirements shall be in accordance with

SSP 41148.

E3.2.1.2.6.2 SEAL MONITORING

Node 3 to PMA−3 seal monitoring requirements shall be in accordance with SSP 41148.

E3.2.1.2.7 DELETED

E3.2.1.2.8 MATERIALS AND FINISHES

Materials and finishes at the hardware interface shall be compatible with the environment and with interfacing hardware per the requirements of SSP 30233, Space Station Requirements for Materials and Processes, paragraph 4.5.4. Materials located near sensitive hardware shall have lower outgassing rates as applicable per the requirements of SSP 30426, Space Station External Contamination Control Requirements, paragraph 3.2.2.3.

E3.2.1.3 FLUID INTERFACES

E3.2.1.3.1 SUPPLY INTERMODULE ATMOSPHERE

Node 3 shall supply intermodule air to PMA−3 through the open hatch and off nominally through the duct.

E3 - 18

12.00

50.00

FIGURE E3.2.1.2.5−1 NODE ELEMENT 3 TO PRESSURIZED MATING ADAPTER 3

ACCESS/PASSAGEWAY ENVELOPE

E3 - 19

E3.2.1.3.1.1 INTERMODULE ATMOSPHERE CHARACTERISTICS

E3.2.1.3.1.1.1 DELETED

E3.2.1.3.1.1.2 INTERMODULE ATMOSPHERE SUPPLY TEMPERATURE

Node 3 shall supply intermodule air to PMA−3 at a temperature range of 65oF to 85oF.

E3.2.1.3.1.1.3 INTERMODULE ATMOSPHERE SUPPLY RATE

Node 3 will supply a minimum of 125 cfm of intermodule air to PMA−3 through the open hatch.

E3.2.1.3.2 RECEIVE RETURN INTERMODULE ATMOSPHERE

Node 3 shall receive return air from PMA−3 through the duct.

E3.2.1.3.2.1 INTERMODULE ATMOSPHERE CHARACTERISTICS

E3.2.1.3.2.1.1 DELETED

E3.2.1.3.2.1.2 INTERMODULE ATMOSPHERE RECEIVE RETURN TEMPERATURE

Node 3 shall receive return respirable intermodule air from PMA−3 at a temperature range of 65oF to 85oF.

E3.2.1.3.2.1.3 INTERMODULE ATMOSPHERE RECEIVE RETURN RATE

Node 3 shall receive a minimum of 125 cfm of intermodule air from PMA−3 by providing a minimum suction pressure head of 0.10 inches of water.

E3.2.1.3.2.2 DELETED

E3.2.1.3.2.3 DELETED

E3.2.1.3.3 RECEIVE FUEL CELL WATER

Node 3 shall be scarred to receive Fuel Cell Water (FCW) from PMA−3.

E3 - 20

E3.2.1.3.3.1 FUEL CELL WATER CHARACTERISTICS

E3.2.1.3.3.1.1 FUEL CELL WATER QUALITY

FCW quality shall be as specified in NSTS−SE−S−0073, Specification, Space Shuttle Fluid Procurement and User Control.

FCW free gas content will not exceed 10 percent peak by volume at 40oF and 20.7 psia.

E3.2.1.3.3.1.2 FUEL CELL WATER RECEIVE TEMPERATURE

Node 3 shall be scarred to receive FCW from PMA−3 at a temperature range of 65oF to 113oF.

E3.2.1.3.3.1.3 FUEL CELL WATER RECEIVE PRESSURE

Node 3 shall be scarred to receive FCW from the PMA−3 with a maximum design pressure of 35 psig.

E3.2.1.3.3.1.4 DELETED

E3.2.1.3.3.2 FUEL CELL WATER SUPPLY AVAILABILITY

Node 3 shall be scarred to receive FCW after the storage tanks are on−orbit.

E3.2.1.3.4 RECEIVE RECHARGE OXYGEN

Node 3 shall be scarred to receive recharge oxygen from PMA−3

E3.2.1.3.4.1 RECHARGE OXYGEN CHARACTERISTICS

E3.2.1.3.4.1.1 RECEIVE RECHARGE OXYGEN TEMPERATURE

Node 3 shall be scarred to receive recharge oxygen from PMA−3 at a temperature range of 25oF to 113oF.

E3.2.1.3.4.1.2 RECEIVE RECHARGE OXYGEN PRESSURE

Node 3 shall be scarred to receive recharge oxygen from PMA−3 at a pressure up to 1050 psia at a flow rate up to 16 lbm/hr.

E3 - 21

E3.2.1.3.5 RECEIVE RECHARGE NITROGEN

Node 3 shall be scarred to receive recharge nitrogen from PMA−3.

E3.2.1.3.5.1 RECHARGE NITROGEN CHARACTERISTICS

E3.2.1.3.5.1.1 RECEIVE RECHARGE NITROGEN TEMPERATURE

Node 3 shall be scarred to receive recharge nitrogen from PMA−3 at a temperature range of 25oF to 113oF.

E3.2.1.3.5.1.2 RECEIVE NITROGEN RECHARGE PRESSURE

Node 3 shall be scarred to receive recharge nitrogen from PMA−3 at a pressure up to 3400 psia at a flow rate up to 3 lbm/hr.

E3.2.1.4 ELECTRICAL INTERFACES

Node 3 to PMA−3 electrical interfaces are shown in Figure E3.2.1.4−1.

Node 3 PMA−3

PMA3SHELLHTRS

FIGURE E3.2.1.4−1 NODE 3 TO PMA−3 ELECTRICAL INTERFACES

E3.2.1.4.1 SUPPLY POWER

Node 3 shall supply power to the PMA−3 through the power circuits specified below.

E3 - 22

E3.2.1.4.1.1 POWER OUTPUTS PMA3APASHTRS AND PMA3SHELLHTRS

E3.2.1.4.1.1.1 POWER QUALITY

The steady state voltage over the interface operating current range shall be within the envelope shown in Table E3.2.1.4.1.1.1−1, Electrical Interface Parameters.

TABLE E3.2.1.4.1.1.1−1 ELECTRICAL INTERFACE PARAMETERS

Circuit Name

Interface Vrange

(Volts) Operating

Current (amps) Overcurrent Protection

Minimum Steady State Wire Rating

PMA3SHELLHTRS 114 to 126 0 to 0.7 3.5 Amp(1) 4.2A

(1) Protection is equivalent with SSP 30263:002, RPCM Standard ICD, Type V RPCM.

E3.2.1.4.1.1.2 FAULT PROTECTION

Node 3 shall provide protection as shown in Table E3.2.1.4.1.1.1−1.

E3.2.1.4.2 DELETED

E3.2.1.5 ELECTRONIC INTERFACES

E3.2.1.5.1 AUDIO CHANNEL

Node 3 shall be scarred to supply audio to PMA−3 for 4 full duplex, analog, electrical audio channels with the following characteristics:

A. Signal Type: The signal shall be balanced. The direct current (DC) resistance to signal ground shall exceed 1.0 megohm.

B. Signal Level: The signal level shall be 0.7 Vrms +/− 3.0 dB into 600 ohms.

C. Frequency Response: The audio signals shall have a frequency response from 200 Hz to 3000 Hz of +/− 3.0 dB referenced to the amplitude response with a 1000 Hz nominal input tone.

Node 3 shall be scarred to support audio reception from PMA−3 for 4 full duplex, analog, electrical audio channels with the following characteristics:

E3 - 23

A. Signal Type: The signal shall be balanced. The DC resistance to signal ground shall exceed 1.0 megohm.

B. Signal Level: The signal level shall be 0.7 Vrms +/− 3.0 dB into 600 ohms.

C. Frequency Response: The audio signals shall have a frequency response from 200 Hz to 3000 Hz of +/− 3.0 dB referenced to the amplitude response with a 1000 Hz nominal input tone.

Node 3 shall be scarred to support transmission of one discrete Page keying signal to PMA−3 with the following characteristics:

A. When keyed (on) the voltage shall be less than 0.3 volts with a maximum current of 2.0 milliamperes.

B. When keyed (off) the voltage shall be less than 7.0 volts +/− 1.0 volt with a maximum leakage current of 10 milliamperes.

Node 3 shall be scarred to support audio channel to channel isolation of greater than 54 dB.

Node 3 shall be scarred to support audio crosstalk of greater than 47 dB measured from the talk line of one channel to the listen line of another channel.

E3.2.1.5.2 COMMAND AND DATA HANDLING MIL−STD−1553B INTERFACE

E3.2.1.5.2.1 DATA BUS STANDARDS

The electrical characteristics and data transfer protocol for the Command and Data Handling (C&DH) MIL−STD−1553B interface shall conform to MIL−STD−1553B, Notice 2.

E3.2.1.5.2.2 INTERFACE BUSSES

The following busses shall be scarred at the Node 3 interface:

A. LB ORB−HAB−1 (2 places), B. LB ORB−HAB−2 (2 places).

C. LB SYS–FLY–1 (stub), D. LB SYS–FLY–2 (stub), Each bus shall be scarred to provide dual redundant data paths across each interface.

The data path interfaces for each bus shall conform to the redundancy requirements given in E3.2.1.2.3.6.

E3 - 24

E3.2.1.5.2.3 PROVIDE OUTPUT AMPLITUDE

Node 3 shall shall be scarred to provide a minimum signal amplitude of 3.6 volts, peak−to−peak, line−to−line at the PMA−3 interfaces for messages transmitted on Node 3 pass−through MIL−STD−1553 data busses.

E3.2.1.5.2.4 DELETED

E3.2.1.5.3 VIDEO SIGNALS

Node 3 shall be scarred to transmit and receive the video signals described in the following subparagraphs at the PMA−3 interface.

E3.2.1.5.3.1 VIDEO CHANNEL SIGNAL CHARACTERISTICS

The Baseband National Television Standards /System Committee (NTSC) video signal characteristics shall be in accordance with EIA/RS 170−A, EIA Industrial Electronics Tentative Standard No.1 − Color TV Studio Picture Line Amplifier Output Drawing.

E3.2.1.5.3.2 DELETED

E3.2.1.5.3.3 DELETED

E3.2.1.5.3.4 DELETED

E3.2.1.5.4 INSTRUMENTATION INTERFACE

E3.2.1.5.4.1 PMA−3 SHELL AND APAS TEMPERATURE SENSORS

Node 3 shall provide instrumentation signals to PMA−3 for the monitoring and control of PMA−3 shell and Androgynous Peripheral Assembly System (APAS) temperature sensors by Multiplexer /Demultiplexer (MDM) N3−2. The interface between the temperature sensors and the N3−2 MDM shall be in compliance with SSP 30261:002, International Space Station Multiplexer/Demultiplexer (SSMDM) Standard ICD.

E3.2.1.5.4.2 GNC MODING INSTRUMENTATION SIGNALS

Node 3 shall receive 8 discrete input signals from PMA−3 for the monitor of PMA−3 APAS capture/departure sensors by the N3−1 and N3−2 MDMs. The interface between the PMA−3

E3 - 25

APAS capture/departure sensors and the N3−1 and N3−2 MDMs shall be in compliance with

SSP 30261:002.

Node 3 shall provide four discrete output signals to PMA−3 for the control Guidance, Navigation and Control (GNC) Moding indicators by the N3−1 and N3−2 MDMs. The interface between the PMA−3 GNC moding indicators and the N3−1 and N3−2 MDMs shall be in compliance with

SSP 30261:002.

E3.2.1.6 SOFTWARE INTERFACES

N/A

E3.2.1.7 ENVIRONMENTS

E3.2.1.7.1 ELECTROMAGNETIC EFFECTS

E3.2.1.7.1.1 ELECTROMAGNETIC COMPATIBILITY

Node 3 to PMA−3 interface shall meet the requirements of SSP 30243, Space Systems Requirements for Electromagnetic Compatibility.

E3.2.1.7.1.2 ELECTROMAGNETIC INTERFERENCE

Node 3 to PMA−3 interface shall meet the requirements of SSP 30243.

E3.2.1.7.1.3 GROUNDING

Node 3 to PMA−3 interface shall meet the requirements of SSP 30240, Space Station Grounding…