SSP42003_P2_RevC.pdf

SSP 42003, Part 2, Revision C

National Aeronautics and Space Administration International Space Station Program Johnson Space Center Houston, T exas

International Space Station Program

Space Station Manned Base to Mobile Servicing System Interface Control Document Part 2

Revision C

May 22, 2007

SSP 42003, Part 2, Revision C SSMB to MSS ICD

REVISION AND HISTORY PAGE

REV. DESCRIPTION PUB.

DATE

− Initial Release (Reference per SSCD 000298, EFF. 05/08/96) 07−19−96

A Revision A (Reference per SSCD 000730, EFF. 10/23/97) 04−16−98

B Revision B (Reference per SSCD 006768, EFF. 09/27/02) 04−28−03

Revision B incorporates the following approved PIRNs/IRNs associated with the appropriate SSCNs.

PIRN IRN SSCN

42003−NA−2009 N/A 006768

42003−NA−2010A N/A 000600

42003−NA−2011 N/A 006768

42003−NA−2012E N/A 000737

42003−NA−2013C N/A 000737

42003−NA−2014H 0013 005411

42003−NA−2015 N/A 006768

42003−NA−2016A N/A 006768

42003−NA−2017A N/A 006768

42003−NA−2018A N/A 001283

42003−NA−2019C N/A 000737

42003−NA−2022 N/A 006768

42003−NA−2025 N/A 006768

42003−NA−2026D N/A 002691A

42003−NA−2027A N/A 001655/006768

42003−NA−2029A 0009 001988

42003−NA−2030C N/A 006768

42003−NA−2031C N/A 002623/006768

Revision B closes the following PIRNs/IRNs and associated SSCNs as they were withdrawn or overcome by events:

PIRN IRN SSCN

N/A 0002 001740

42003−NA−2020C 0003 001786

42003−NA−2021B 0003 001786

N/A 0004 001920 N/A 0005 002133 N/A 0006 002134 N/A 0007 002191 N/A 0008 002130 N/A 0010 003827 N/A 0011 003186 N/A 0012 003928

Revision B also closes the following SSCNs as they were withdrawn or overcome by events: 000554, 000567, 000583, 000585, 000588, 000591, 000673, 000773, 000823, 000832, 000844, 000845, 000877, 000889, 000894, 000915, 001026, 001481, 001594

Note: IRN 0001 has been retired without use. This IRN was assigned to SSCN 001662 but no update to the document was required by this SSCN.

REV. DESCRIPTION PUB.

DATE

C Revision C (Reference per SSCD 010615, EFF. 04/17/09) 04−28−09

Revision C incorporates the following approved PIRNs/IRNs associated with the appropriate SSCNs.

PIRN IRN SSCN

42003−NA−2032A 0014 006790

42003−NA−2033 N/A 010615

SSCN 210 was reviewed and determined to be overcome by previouse updates to the document.

SSCN 1344 was incorporated into Revision A of the document.

ERU: /s/Beth Mason 4−28−09 iv

PREFACE

SSP 42003, Space Station Manned Base to Mobile Servicing System Interface Control Document, Part 2, shall be implemented on all new Program contractural and internal activity and shall be included in any existing contracts through contract changes. This document is under the control of the Space Station Control Board (SSCB) with the concurrence of the respective International Partners, any changes or revisions will be approved by the SSCB and the respective International Partners.

See Directive

Program Manager, Date International Space Station v

NASA/CSA

INTERNATIONAL SPACE STATION PROGRAM

SPACE STATION MANNED BASE T O MOBILE SERVICING SYSTEM

INTERFACE CONTROL DOCUMENT PART 2

DATE

Print Name

For NASA

See Directive

DATE

Print Name

For CSA

See Directive vi

INTERNATIONAL SPACE STATION PROGRAM

SPACE STATION MANNED BASE T O MOBILE SERVICING SYSTEM

INTERFACE CONTROL DOCUMENT PART 2

CONCURRENCE

PREPARED BY:

CHECKED BY:

SIGNATURE

SUPERVISED BY (NASA):

PRINT NAME ORGN

DATE

SIGNATURE

PRINT NAME ORGN

DATE

SUPERVISED BY (BOEING):

SIGNATURE

PRINT NAME ORGN

DATE

SIGNATURE

PRINT NAME ORGN

DATE

DQA:

SIGNATURE

PRINT NAME ORGN

DATE

Warren England AG−92−J3ES

AG−92−J3ES

Dave Brueneman

OM/NASA

Quentin Henry

Chau Hong

AG−92−J3EHMerry Roberts

AG−92−J3ES

/s/ Warren England 11/1/07

/s/ Quentin L. Henry 11−6−07

/s/ David J. Brueneman 2/18/08

/s/ Chau Hong 10/31/07

/s/ Merry Roberts 2/18/08 vii

INTERNATIONAL SPACE STATION PROGRAM

SPACE STATION MANNED BASE T O MOBILE SERVICING SYSTEM

INTERFACE CONTROL DOCUMENT PART 2

LIST OF CHANGES

MAY 22, 2007

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

SSCBD ENTRY DATE CHANGE PARAGRAPH(S)

006790 5/22/07 NA−2032A A3.7

010615 5/22/07 NA−2033 2.2

SSCBD ENTRY DATE CHANGE FIGURE(S)

006790 5/22/07 NA−2032A A3.2−11, A3.2.1−1, A3.4−2, A3.7−1,

A3.7−2, A3.7−3, and A3.7−4 viii

TABLE OF CONTENTS

PARAGRAPH PAGE

1.0 INTRODUCTION 1 - 1

1.1 PURPOSE AND SCOPE 1 - 1

1.2 PRECEDENCE 1 - 1

1.3 RESPONSIBILITY AND CHANGE 1 - 1

2.0 DOCUMENTS 2 - 1

2.1 APPLICABLE DOCUMENTS 2 - 1

2.2 REFERENCE DOCUMENTS 2 - 2

SECTION A3 MOBILE TRANSPORTER TO MRS BASE SYSTEM INTERFACE A3 − 1

A3.0 INTERFACE DEFINITION A3 − 1

A3.1 GENERAL A3 − 1

A3.1.1 INTERFACE DESCRIPTION A3 − 1

A3.1.2 INTERFACE RESPONSIBILITIES A3 − 1

A3.1.3 ENGINEERING UNITS AND TOLERANCES A3 − 1

A3.2 STRUCTURAL/MECHANICAL INTERFACES A3 − 1

A3.2.1 MBS/MT INTERFACE HARNESS DESIGN A3 − 2

A3.2.2 DELETED A3 − 2

A3.2.3 UTILITY INTERFACES A3 − 2

A3.2.4 BERTHING VISUAL CUES A3 − 2

A3.3 THERMAL INTERFACES A3 − 2

A3.4 ELECTRICAL INTERFACES A3 − 2

A3.4.1 POWER, RETURN AND GROUNDING INTERFACES A3 − 2

A3.4.2 POWER CONNECTORS AND PIN ASSIGNMENTS A3 − 3

A3.4.3 DATA AND PULSE FREQUENCY MODULATION (PFM) SYNC AND

CONTROL AND VIDEO INTERFACES A3 − 3

A3.4.3.1 DATA AND VIDEO CONNECTORS AND PIN ASSIGNMENTS A3 − 3

A3.4.3.2 MSS VIDEO PROVISIONS A3 − 3

A3.4.3.3 MT INTERFACE CONNECTORS A3 − 3

A3.5 ENVIRONMENTS A3 − 4

A3.6 SOFTWARE INTERFACES A3 − 4

A3.7 EVA HARDWARE LOCATIONS A3 − 4

SECTION B3 RESERVED B3 − 1

B3.0 RESERVED B3 − 1

SECTION C3 AVU TO USL INTERFACE C3 − 1

C3.0 INTERFACE DEFINITION C3 − 1

C3.1 GENERAL C3 − 1

C3.1.1 INTERFACE DESCRIPTION C3 − 1

C3.1.2 INTERFACE RESPONSIBILITIES C3 − 1

C3.1.3 ENGINEERING UNITS AND TOLERANCES C3 − 1

ix

TABLE OF CONTENTS (Continued)

PARAGRAPH PAGE

C3.2 STRUCTURAL/MECHANICAL INTERFACES C3 − 1

C3.2.1 GENERAL C3 − 1

C3.2.2 UTILITY INTERFACE(S) C3 − 1

C3.3 FLUID INTERFACE(S) C3 − 2

C3.4 ELECTRICAL INTERFACE(S) C3 − 2

C3.4.1 ELECTRICAL CONNECTIVITY C3 − 2

C3.4.1.1 DETAILED ELECTRICAL INTERFACE(S) C3 − 2

C3.4.2 ELECTRICAL BONDING C3 − 2

C3.4.3 SOFTWARE INTERFACES C3 − 2

SECTION D3 SSMB TO PDGF INTERFACE D3 − 1

D3.0 INTERFACE DEFINITION D3 − 1

D3.1 GENERAL D3 − 1

D3.1.1 INTERFACE DESCRIPTION D3 − 1

D3.1.2 INTERFACE RESPONSIBILITIES D3 − 1

D3.1.3 ENGINEERING UNITS AND TOLERANCES D3 − 1

D3.2 STRUCTURAL/MECHANICAL INTERFACES D3 − 1

D3.2.1 USL MODULE PDGF LOCATION D3 − 2

D3.2.2 HAB MODULE PDGF LOCATION D3 − 2

D3.2.3 JEM−PM PDGF LOCATION D3 − 2

D3.2.4 NODE 2 PDGF LOCATION D3 − 2

D3.3 THERMAL INTERFACES D3 − 2

D3.4 ELECTRICAL INTERFACES D3 − 2

D3.4.1 POWER RETURN AND GROUNDING INTERFACES D3 − 3

D3.4.2 DELETED D3 − 3

D3.4.2.1 USL POWER CONNECTORS AND PIN ASSIGNMENTS D3 − 3

D3.4.2.2 HAB POWER CONNECTORS AND PIN ASSIGNMENTS D3 − 3

D3.4.2.3 JEM−PM POWER CONNECTORS AND PIN ASSIGNMENTS D3 − 3

D3.4.2.4 NODE 2 POWER CONNECTION AND PIN ASSIGNMENTS D3 − 3

D3.4.3 DATA AND PFM SYNC AND CONTROL AND VIDEO INTERFACES D3 − 3

D3.4.4 DATA AND VIDEO CONNECTORS AND PIN ASSIGNMENTS D3 − 4

D3.4.4.1 USL DATA AND VIDEO CONNECTORS AND PIN ASSIGNMENTS D3 − 4

D3.4.4.2 HAB DATA AND VIDEO CONNECTORS AND PIN ASSIGNMENTS D3 − 4

D3.4.4.3 NODE 2 DATA AND VIDEO CONNECTORS AND PIN ASSIGNMENTS D3 − 4. . .

D3.4.4.4 DELETED D3 − 4

D3.5 ENVIRONMENTS D3 − 4

D3.6 SOFTWARE INTERFACES D3 − 4

D3.7 SSRMS EVA HARDWARE LOCATIONS D3 − 4

x

TABLE OF CONTENTS (Continued)

PARAGRAPH PAGE

SECTION E3 PWP TO MBS INTERFACE E3 − 1

E3.0 INTERFACE DEFINITION E3 − 1

E3.1 GENERAL E3 − 1

E3.1.1 INTERFACE DESCRIPTION E3 − 1

E3.1.2 INTERFACE RESPONSIBILITIES E3 − 1

E3.1.3 ENGINEERING UNITS AND TOLERANCES E3 − 1

E3.2 STRUCTURAL/MECHANICAL INTERFACES E3 − 1

E3.2.1 INTERFACE LOCATIONS E3 − 2

E3.3 SOFTWARE INTERFACES E3 − 2

SECTION F3 SSMB LSA TO SSRMS INTERFACE F3 − 1

F3.0 INTERFACE DEFINITION F3 − 1

F3.1 GENERAL F3 − 1

F3.1.1 INTERFACE DESCRIPTION F3 − 1

F3.1.2 INTERFACE RESPONSIBILITIES F3 − 1

F3.1.3 ENGINEERING UNITS AND TOLERANCES F3 − 1

F3.2 STRUCTURAL/MECHANICAL INTERFACES F3 − 1

F3.2.1 FSEGF AND FSE BRACKET LOCATION F3 − 1

F3.3 THERMAL INTERFACES F3 − 2

F3.4 ELECTRICAL INTERFACES F3 − 2

F3.4.1 POWER RETURN AND GROUNDING INTERFACES F3 − 2

F3.4.2 POWER CONNECTORS AND PIN ASSIGNMENTS F3 − 2

F3.4.3 DATA AND PFM SYNC AND CONTROL AND VIDEO INTERFACES F3 − 2

F3.4.4 DATA AND VIDEO CONNECTORS AND PIN ASSIGNMENTS F3 − 2

F3.4.5 FSEGF HARNESS LENGTH F3 − 3

F3.5 ENVIRONMENTS F3 − 3

F3.6 SOFTWARE INTERFACES F3 − 3

SECTION G3 AVU CCD TO RWS INTERFACE G3 − 1

G3.0 INTERFACE DEFINITION G3 − 1

G3.1 GENERAL G3 − 1

G3.1.1 INTERFACE DESCRIPTION G3 − 1

G3.1.2 INTERFACE RESPONSIBILITIES G3 − 1

G3.1.3 ENGINEERING UNITS AND TOLERANCES G3 − 1

G3.2 STRUCTURAL/MECHANICAL INTERFACES G3 − 1

G3.2.1 GENERAL G3 − 1

G3.2.2 ELECTRICAL CONNECTOR LOCATION G3 − 1

G3.3 FLUID INTERFACE(S) G3 − 2

G3.4 ELECTRICAL INTERFACES G3 − 2

G3.4.1 ELECTRICAL CONNECTIVITY G3 − 2

xi

TABLE OF CONTENTS (Continued)

PARAGRAPH PAGE

G3.4.1.1 DETAILED ELECTRICAL INTERFACE(S) G3 − 2

G3.4.2 ELECTRICAL BONDING G3 − 2

G3.4.3 SOFTWARE INTERFACES G3 − 2

SECTION H3 SSMB TO VSC INTERFACE H3 − 1

H3.0 REQUIRMENTS H3 − 1

H3.1 GENERAL H3 − 1

H3.1.1 INTERFACE DESCRIPTION H3 − 1

H3.1.2 INTERFACE RESPONSIBILITIES H3 − 1

H3.1.3 ENGINEERING UNITS AND TOLERANCES H3 − 1

H3.2 STRUCTURAL/MECHANICAL INTERFACES H3 − 1

H3.3 THERMAL INTERFACES H3 − 2

H3.3.1 PASSIVE THERMAL INTERFACES H3 − 2

H3.3.2 ACTIVE THERMAL INTERFACES H3 − 2

H3.4 ELECTRICL INTERFACES H3 − 2

H3.4.1 POWER RETURN AND GROUNDING INTERFACES H3 − 2

H3.4.2 POWER CONNECTORS AND PIN ASSIGNMENTS H3 − 2

H3.4.3 PFM SYNC AND CONTROL AND VIDEO INTERFACES H3 − 3

H3.4.4 DATA AND VIDEO CONNECTORS AND PIN ASSIGNMENTS H3 − 3

H3.5 ENVIRONMENTS H3 − 3

H3.6 SOFTWARE INTERFACES H3 − 3

xii

TABLE OF CONTENTS (Continued)

FIGURES

FIGURES PAGE

A3.2−1 DELETED A3 − 4

A3.2−2 MBS TO MT MECHANICAL INTERFACE A3 − 5

A3.2−3 MBS TO MT MECHANICAL INTERFACE A3 − 6

A3.2−4 MBS TO MT MECHANICAL INTERFACE A3 − 7

A3.2−5 MBS TO MT MECHANICAL INTERFACE A3 − 8

A3.2−6 MBS TO MT MECHANICAL INTERFACE A3 − 9

A3.2−7 MBS TO MT MECHANICAL INTERFACE A3 − 10

A3.2−8 MBS TO MT STRUCTURAL INTERFACES A3− 11

A3.2−9 MBS TO MT STRUCTURAL INTERFACES A3− 12

A3.2−10 MBS TO MT STRUCTURAL INTERFACES A3 − 13

A3.2−11 MBS TO MT STRUCTURAL INTERFACE A3 − 14

A3.2−12 MBS TO MT STRUCTURAL INTERFACES A3 − 15

A3.2−13 MBS TO MT MECHANICAL INTERFACE A3 − 16

A3.2.1−1 MBS/MT INTERFACE HARNESS DESIGN A3 − 17

A3.4−1 MT/MBS POWER, RETURN AND GROUNDING DIAGRAM A3 − 18

A3.4−2 MT/MBS ELECTRICAL INTEGRATED DIAGRAM A3 − 19

A3.4−3 MBS EVA ELECTRICAL OUTLETS A3 − 20

A3.4.2−1 DELETED A3 − 21

A3.4.2−2 DELETED A3 − 21

A3.4.3.3−1 MT/MBS INTERFACE CONNECTOR LOCATION A3 − 22

A3.4.3.3−2 MT/MBS CONNECTOR LOCATION A3 − 23

A3.7−1 LOCATION OF EVA HARDWARE ON MBS A3 − 27

A3.7−2 LOCATION OF EVA HARDWARE ON MBS A3 − 28

A3.7−3 LOCATION OF EVA HARDWARE ON MBS A3 − 29

A3.7−4 LOCATION OF EVA HARDWARE ON MBS A3 − 30

C3.1.1−1 MSS RACK CONFIGURATION (FRONT VIEW) C3 − 3

C3.2.1−1 INTERFACE CONTROL DRAWING OF AVU (NOT TO SCALE) C3 − 5

C3.2.1−2 INTERFACE CONTROL DRAWING OF AVU (NOT TO SCALE) C3 − 6

C3.4.1−1 PRIMARY AVU ELECTRICAL SYSTEM DIAGRAM C3 − 7

C3.4.1−2 SECONDARY AVU ELECTRICAL SYSTEM DIAGRAM C3 − 8

D3.2.1−1 PDGF LOCATION ON USL D3 − 5

D3.2.2−1 PDGF LOCATION ON US HAB D3 − 6

D3.2.4−1 PDGF LOCATION ON NODE 2 D3 − 7

D3.4−1 LAB EXTERNAL HARNESSES AND INTERFACES (FLIGHT 6A1) D3 − 8

D3.4−2 LAB EXTERNAL HARNESS AND INTERFACES (FLT 6A2 − 8A) D3 − 9

D3.4−3 LAB EXTERNAL HARNESSES AND INTERFACES (FLT 8A−AC) D3 − 10

xiii

TABLE OF CONTENTS (Continued)

FIGURES PAGE

D3.4−4 US HAB TO PDGF ELECTRICAL SYSTEM DIAGRAM D3 − 11

D3.4−5 DELETED D3 − 12

D3.4−6 DELETED D3 − 12

D3.4−7 NODE 2 TO PDGF ELECTRICAL SYSTEM DIAGRAM D3 − 13

D3.4.1−1 PDGF EXTERNAL WIRING DIAGRAM D3 − 14

D3.4.1−2 NODE 2 PDGF EXTERNAL WIRING DIAGRAM (1 0F 2) D3 − 15

D3.4.1−2 NODE 2 PDGF EXTERNAL WIRING DIAGRAM (2 0F 2) D3 − 16

D3.7−1 SSRMS EVA HARDWARE LOCATIONS D3 − 53

E3.2.1−1 PORTABLE WORK PLATFORM (PWP) STOWED ON MBS E3 − 3

F3.2−1 FSEGF TO SSMB LSA BOLT PATTERN F3 − 4

F3.2−2 FSEGF TO SSMB LSA BOLT PATTERN F3 − 5

F3.2−4 DELETED F3 − 6

F3.2−5 DELETED F3 − 6

F3.2−6 DELETED F3 − 6

F3.2−7 DELETED F3 − 6

F3.2−8 DELETED F3 − 6

F3.2−9 DELETED F3 − 6

F3.4−1 FSEGF TO USL ELECTRICAL SYSTEM DIAGRAM F3 − 7

F3.4−2 FSEGF TO USL ELECTRICAL SYSTEM DIAGRAM F3 − 8

G3.1.1−1 AVU CCD TO RWS ON−ORBIT CONFIGURATION G3 − 3

G3.2.1−1 AVU CCD VOLUMETRIC & MECHANICAL INTERFACES G3 − 4

G3.2.1−2 AVU CCD BOLT PATTERN AND PANEL CUTOUT G3 − 5

G3.4.1−1 RWS TO AVU CCD ELECTRICAL INTERFACES G3 − 6

H3.2−1 VSC MODULE MOUNTING BRACKET H3 − 4

H3.2−2 VSC MODULE MOUNTING BRACKET H3 − 5

H3.2−3 VSC TRUSS MOUNTING INTERFACE H3 − 6

H3.2−4 VSC TRUSS MOUNTING INTERFACE H3 − 7

H3.2−5 VSC TRUSS MOUNTING INTERFACE H3 − 8

H3.4−1 TUS VSC ELECTRICAL DIAGRAM H3 − 9

xiv

TABLE OF CONTENTS (Continued)

TABLES

TABLES PAGE

A3.4.3.3−1 MBS/MT INTERFACE CONNECTOR LOCATION FOR DATA AND VIDEO A3 − 4.

A3.4.2−1 MBS EVA OUTLET #1 CONNECTOR AND PIN ASSIGNMENTS A3 − 24

A3.4.2−2 MBS EVA OUTLET #2 CONNECTOR AND PIN ASSIGNMENTS A3 − 25

C3.1.3−1 LINEAR TOLERANCES C3−4

C3.4.1.1−1 DETAILED ELECTRICAL DESCRIPTION OF AVU CONNECTOR

J1 (POWER) C3−9

C3.4.1.1−2 DETAILED ELECTRICAL DESCRIPTION OF AVU CONNECTOR

J2 (DATA) C3−10

C3.4.1.1−3 DETAILED ELECTRICAL DESCRIPTION OF AVU CONNECTOR J3

(CURSOR CONTROL DEVICE) C3−12

C3.4.1.1−4 DETAILED ELECTRICAL DESCRIPTION OF AVU CONNECTOR

J4 (VIDEO) C3−14

D3.4.2.1−1 DETAILED ELECTRICAL DESCRIPTION OF LAB PDGF

CONNECTOR J400 (PRIME POWER) (PAGE 1 OF 2) D3 − 17

D3.4.2.1−2 DETAILED ELECTRICAL DESCRIPTION OF LAB PDGF

CONNECTOR J401 (REDUNDANT POWER) (PAGE 1 0F 2) D3 − 19

D3.4.2.1−3 DETAILED ELECTRICAL DESCRIPTION OF LAB PDGF

CONNECTOR J402 (BACKUP DRIVE POWER) D3 − 21

D3.4.2.2−1 DETAILED ELECTRICAL DESCRIPTION OF HAB PDGF

CONNECTOR J400 (PRIME POWER) D3 − 22

D3.4.2.2−2 DETAILED ELECTRICAL DESCRIPTION OF HAB PDGF

CONNECTOR J401 (REDUNDANT POWER) D3 − 23

D3.4.2.2−3 DETAILED ELECTRICAL DESCRIPTION OF HAB PDGF

CONNECTOR J402 (BACKUP DRIVE POWER) D3 − 24

D3.4.2.3−1 DELETED D3 − 24

D3.4.2.3−2 DELETED D3 − 24

D3.4.2.4−1 DETAILED ELECTRICAL DESCRIPTION OF NODE 2 PDGF

CONNECTOR J102 (PRIME POWER) D3 − 25

D3.4.2.4−2 DETAILED ELECTRICAL DESCRIPTION OF NODE 2 PDGF

CONNECTOR J104 (REDUNDANT POWER) D3 − 26

D3.4.2.4−3 DETAILED ELECTRICAL DESCRIPTION OF NODE 2 PDGF

CONNECTOR J107 (BACKUP DRIVE POWER) D3 − 27

D3.4.2.4−4 DETAILED DESCRIPTION OF NODE 2 PDGF CONNECTOR

J401 (PRIME POWER) D3 − 28

D3.4.2.4−5 DETAILED DESCRIPTION OF NODE 2 PDGF CONNECTOR

J402 (REDUNDANT POWER) D3 − 29

xv

TABLE OF CONTENTS (Continued)

TABLES PAGE

D3.4.2.4−6 DETAILED DESCRIPTION OF NODE 2 PDGF CONNECTOR

J403 (BACKUP DRIVE POWER) D3 − 30

D3.4.4.1−1 DETAILED ELECTRICAL DESCRIPTION OF LAB PDGF CONNECTOR

J403 (1553 & VIDEO) (PAGE 1 OF 3) D3 − 31

D3.4.4.1−2 DETAILED ELECTRICAL DESCRIPTION OF LAB PDGF CONNECTOR

J404 (1553 & VIDEO) (PAGE 1 OF 2) D3 − 34

D3.4.4.1−3 DETAILED ELECTRICAL DESCRIPTION OF LAB PDGF CONNECTOR

J405 (VIDEO) (PAGE 1 OF 1) D3 − 36

D3.4.4.1−4 DETAILED ELECTRICAL DESCRIPTION OF LAB PDGF CONNECTOR

J406 (1553 & VIDEO) D3 − 37

D3.4.4.1−5 DETAILED ELECTRICAL DESCRIPTION OF LAB PDGF CONNECTOR

J407 (1553 & VIDEO) D3 − 38

D3.4.4.2−1 DETAILED ELECTRICAL DESCRIPTION OF HAB PDGF CONNECTOR

J403 (1553 & VIDEO) D3 − 39

D3.4.4.2−2 DETAILED ELECTRICAL DESCRIPTION OF HAB PDGF CONNECTOR

J404 (1553 & VIDEO) D3 − 40

D3.4.4.2−3 DETAILED ELECTRICAL DESCRIPTION OF HAB PDGF CONNECTOR

J405 (VIDEO) D3 − 41

D3.4.4.3−1 DETAILED ELECTRICAL DESCRIPTION OF NODE 2 PDGF

CONNECTOR J106 (1553) D3 − 42

D3.4.4.3−2 DETAILED ELECTRICAL DESCRIPTION OF NODE 2 PDGF

CONNECTOR J807(1553) D3 − 43

D3.4.4.3−3 DETAILED ELECTRICAL DESCRIPTION OF NODE 2 PDGF

CONNECTOR J825 (1553) D3 − 44

D3.4.4.3−4 DETAILED ELECTRICAL DESCRIPTION OF NODE 2 PDGF

CONNECTOR J101 (VIDEO) D3 − 45

D3.4.4.3−5 DETAILED ELECTRICAL DESCRIPTION OF NODE 2 PDGF

CONNECTOR J103 (VIDEO) D3 − 46

D3.4.4.3−6 DETAILED ELECTRICAL DESCRIPTION OF NODE 2 PDGF

CONNECTOR J105 (VIDEO) D3 − 47

D3.4.4.3−7 DETAILED DESCRIPTION OF NODE 2 PDGF CONNECTOR

J404 (VIDEO) D3 − 48

D3.4.4.3−8 DETAILED DESCRIPTION OF NODE 2 PDGF CONNECTOR

J405 (VIDEO) D3 − 49

D3.4.4.3−9 DETAILED DESCRIPTION OF NODE 2 PDGF CONNECTOR

J406 (1553) D3 − 50

D3.4.4.3−10 DETAILED DESCRIPTION OF NODE 2 PDGF CONNECTOR

J407 (1553) D3 − 51 xvi

TABLE OF CONTENTS (Continued)

TABLES PAGE

D3.4.4.3−11 DETAILED DESCRIPTION OF NODE 2 PDGF CONNECTOR

J408 (1553) D3 − 52

F3.4.5−1 FSEGF HARNESS CABLE LENGTHS F3 − 3

F3.4.2−1 DETAILED ELECTRICAL DESCRIPTION OF FSEGF TO USL

CONNECTOR J300 (PRIME POWER) F3 − 9

F3.4.2−2 DETAILED ELECTRICAL DESCRIPTION OF FSEGF TO USL

CONNECTOR J301 (REDUNDANT POWER) F3 − 10

F3.4.4−1 DETAILED ELECTRICAL DESCRIPTION OF FSEGF TO USL

CONNECTOR J303 (1553 & VIDEO) F3 − 11

F3.4.4−2 DETAILED ELECTRICAL DESCRIPTION OF FSEGF TO USL

CONNECTOR J304 (1553 & VIDEO) F3 − 12

F3.4.4−3 DELETED F3 − 12

G3.1.3−1 LINEAR TOLERANCES G3 − 1

G3.4.1.1−1 DETAILED ELECTRICAL DESCRIPTION OF AVU CCD CONNECTOR J1

(CURSOR CONTROL DEVICE) G3 − 7

H3.4.2−1 DETAILED ELECTRICAL DESCRIPTION OF VSC ORU TO SSMB

CONNECTOR J2 (PRIME POWER) H3 − 10

H3.4.2−2 DETAILED ELECTRICAL DESCRIPTION OF VSC ORU TO SSMB

CONNECTOR J3 (REDUNDANT POWER) H3 − 11

H3.4.4−1 DETAILED ELECTRICAL DESCRIPTION OF VSC ORU TO SSMB

CONNECTOR J1 (FIBER OPTIC VIDEO CONNECTOR) H3 − 12

H3.4.4−2 DETAILED ELECTRICAL DESCRIPTION OF VSC ORU TO SSMB

CONNECTOR J4 (COPPER VIDEO CONNECTOR) H3 − 13

APPENDICES

APPENDIX PAGE

A ABBREVIATIONS AND ACRONYMS A − 1

B ISSUE SHEETS B − 1

C TBD LIST C − 1

1 - 1

1.0 INTRODUCTION

1.1 PURPOSE AND SCOPE

This Interface Control Document (ICD) Part 2 defines and controls the physical and functional interfaces between the United States On−Orbit Segment of International Space Station (ISS) and the Canadian Mobile Servicing System (MSS).

1.2 PRECEDENCE

In the event of conflict between SSP 41000, System Specification for the International Space Station, and the contents of this ICD, the requirements of SSP 41000 shall take precedence.

1.3 RESPONSIBILITY AND CHANGE

This document is prepared and maintained in accordance with SSP 30459, International Space Station Interface Control Plan. The National Aeronautics and Space Administration (NASA) shall delegate the responsibility for preparation and maintenance of this ICD Part 2.

2 - 1

2.0 DOCUMENTS

2.1 APPLICABLE DOCUMENTS

The following documents of the date and issue shown include specifications, models, standards, and form a part of this document to the extent specified herein.

DOCUMENT NO. TITLE

CSA−SS−ID−0002 Canadian Space Vision System (CSVS) Interface Control Document (ICD) MRCS/AVU

References C3.4.3

MIL−C−38999 Connectors, Electrical, Circular, Miniature, High Density, Quick Disconnect (Bayonet, Threaded, and Breech Coupling), Environment Resistant, Removable Crimp and Hermetic Solder contacts, General Specification For

References G3.4.1.1

MIL−STD−1553 Digital Time Division Command/Response Multiplex Databus References A3.4.3, C3.4.1.1, D3.4, D3.4.1, D3.4.4.1, D3.4.4.2, D3.4.4.3, F3.4.4, H3.4, Appendix C

SSP 30245 Space Station Electrical Bonding Requirements References C3.4.2, G3.4.2

SSP 30482, Vol. 1 Electrical Power Specification and Standards Volume 1:

Rev C EPS Electrical Performance Specifications 7 July 1997 References A3.4.2

SSP 30482, Vol. 2 Electrical Power Specification and Standards Volume 2:

Rev A, DCN−001, DCN−002, Consumer Constraints

DCN−003, DCN−004

1 Jan 1994 References A3.4.2

SSP 42000 Space Station Manned Base to Japanese Experiment Module Interface Control Document

References D3.2.3

SSP 42003, Part 1 Space Station Manned Base to Mobile Servicing System Interface Control Document, Part I

References C3.4.2, G3.4.2

SSP 42004, Part 2 Mobile Servicing System to User (Generic) Interface Control Document, Part 2

References A3.4.3.2, D3.2, D3.3, D3.5

2 - 2

SSQ 21635 Connectors and Accessories, Electrical, Circular Miniature, IVA/EVA Compatible, Space Quality, General Specification For

References A3.4.2, C3.4.1.1

SSQ 21655 Cable Electrical, MIL−STD−1553, Data Bus, Space Quality, General Specification For

References C3.4.1.1

2.2 REFERENCE DOCUMENTS

The following documents from a part of this ICD to the extent specified herein.

DOCUMENT NO. TITLE

SSP 30459 International Space Station Interface Control Plan Reference 1.3

SSP 41000 System Specification for the International Space Station Reference 1.2

SSP 30256:001 Extravehicular Activity (EVA) Standard Interface Control Document

Reference E3.2

2.3 REFERENCE DRAWINGS

51800−0011 Interface, MBS/MT, MBS MSS References A3.2, A3.2.1, A3.7

A3 − 1

SECTION A3 MOBILE TRANSPORTER T O MRS BASE SYSTEM INTERFACE

A3.0 INTERFACE DEFINITION

A3.1 GENERAL

A3.1.1 INTERFACE DESCRIPTION

The physical interface (mechanical, structural, thermal and environmental) plane is defined at the Mobile Remote Servicer (MRS) Base System (MBS) mounting surface at the Mobile Transporter (MT). The electrical power, data and video interface plane is defined between the MBS electrical harness and the MT connector panel.

A3.1.2 INTERFACE RESPONSIBILITIES

Canadian Space Agency (CSA) is responsible for development of the MBS. NASA is responsible for development of the MT. Interface responsibilities for the MT to MBS interface are as defined in SSP 42003 Space Station Manned Base to Mobile Servicing System Interface control Document, Part I, Section A and as described in SSP 42003 Part II, Section A herein.

A3.1.3 ENGINEERING UNITS AND TOLERANCES

Unless otherwise noted herein, all dimensions in this document are shown in the English system of inch pound (IP) units.

A3.2 STRUCTURAL/MECHANICAL INTERF ACES

MBS structurally attaches to the MT via a four fastener interface. The location of the MT changeout nuts and MBS bolt assemblies will be as shown in Table A3.2−1. The MT side of the MBS to MT mechanical interface will be as shown in the Figures A3.2−2 through A3.2−7, and A3.2−13 (Figure A3.2−1 has been deleted). The MBS side of the MBS to MT interface will be as shown in Figures A3.2−8 through A3.2−12. (MBS figures from SPAR Drawing 51800−0011)ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁD60694113−1

CHANGEOUT NUT

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ51800−2025−1

MBS BOLT ASSY

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁMBS/MT

LOCATION

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ S/N 006

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ S/N 204

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ −Y +Z

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ S/N 007

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ S/N 205

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ +Y +Z

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ S/N 008

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ S/N 206

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ −Y −Z

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ S/N 009

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ S/N 208

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ +Y −Z

A3 − 2

A3.2.1 MBS/MT INTERFACE HARNESS DESIGN

The MBS/MT interface harnesses design is shown in Figure A3.2.1−1.

A3.2.2 DELETED

A3.2.3 UTILITY INTERFACES

The assigned Electrical Reference Designations for MBS/MT harness connectors are shown in Figure A3.2.1−1.

A3.2.4 BERTHING VISUAL CUES

The MBS Berthing Visual Cues will be as shown in Figures A3.2−9, A3.2−11, and A3.2−12.

The MT Berthing Visual Cues will be as shown in Figure A3.2−13.

A3.3 THERMAL INTERFACES

The MT side of the MBS to MT thermal interface implementation will be as defined in Figures A3.2−2 through A3.2−7. The MBS side of the MBS to MT thermal interface implementation will be as defined in Figures A3.2−8 and A3.2−11.

The temperature differential will be equal to or lower than the maximum allowable. It will be achieved by an assembly procedure to allow sufficient time between initial capture of the MT by the MBS capture latch and the attachment of four fasteners by Extravehicular Activity (EVA).

A3.4 ELECTRICAL INTERF ACES

The Space Station Manned Base (SSMB) will provide power, data, and PFM copper video interfaces to the MBS via the MT and Trailing Umbilical System (TUS) as defined in Figures A3.4−1 and A3.4−2. The MBS will provide EVA electrical outlets for SSMB tools with electrical interfaces as defined in Figure A3.4−3.

A3.4.1 POWER, RETURN AND GROUNDING INTERFACES

The SSMB will provide power, return, and grounding interfaces to the MBS via the MT as defined in Figure A3.4−1. For detailed electrical schematic and connectivity diagram, including the harness, refer to Figure A3.2.1−1.

A3 − 3

A3.4.2 POWER CONNECTORS AND PIN ASSIGNMENTS

The prime and redundant harness power connectors and pin assignments for the MT connector panel will be as defined in Figure A3.2.1−1.

The MBS EVA outlet connectors and pin assignments will be as defined in Table A3.4.2−1 and A3.4.2−2.

A3.4.3 DATA AND PULSE FREQUENCY MODULA TION (PFM) SYNC AND CONTROL AND

VIDEO INTERFACES

The SSMB will support 1553 data and PFM sync and control and video interfaces between the SSMB and the MBS via the MT and TUS. PFM copper video will be carried between the MBS and the MT. For detailed electrical schematic and connectivity diagram, including the harness, refer to Figure A3.2.1−1.

A3.4.3.1 DATA AND VIDEO CONNECTORS AND PIN ASSIGNMENTS

The harness data and video connectors and pin assignments for the MBS/MT harness will be as defined in Figures A3.2.1−1.

A3.4.3.2 MSS VIDEO PROVISIONS

During Space Station Remote Manipulator System (SSRMS) or MBS POA operations, the MSS will provide, via the MBS, PFM sync and control and video capability as defined in SSP 42004, Mobile Servicing System to User (Generic) Interface Control Document, Part 2, Table A3.4.4−1.

The External Video Switches (VSW(E)) will provide to the MBS via TUS 1 and TUS 2, three video channels.

The External Video Switches (VSW(E)) will provide to the MBS via TUS 1 and TUS 2, two simultaneous PFM sync and control signals.

A3.4.3.3 MT INTERFACE CONNECTORS

The MT/MBS interface connectors located on the MT are defined in Table A3.4.3.3−1 and Fig-ures A3.4.3.3−1 and A43.4.3.3−2.

A3 − 4

TABLE A3.4.3.3−1 MBS/MT INTERFACE CONNECTOR LOCATION FOR DATA AND VIDEOÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁConnector Function

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁReference Designation

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁX

Coord

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁY

Coord

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁZ

Coord

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁConnector Axis LocationÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁMSS LB A

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁW0001J015

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ23.75

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ9.60

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ25.23

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ+Z Direction

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁMSS LB B

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁW0002J018

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ23.75

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ−9.60

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ25.23

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ+Z Direction

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ MBS−1

VIDEO/SYNC

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁB0014J017

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ24.42

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ−17.38

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ28.67

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁX−Y Plane, tilted 20 deg from X−axis

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ MBS−2

VIDEO/SYNC

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁB0004J016

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ24.42

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ17.38

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ28.67

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁX−Y Plane, tilted 20 deg from X−axis

Notes: 1. Coordinates are MT coordinates, except that X is measured from datum −A− of the Integrated Truss Rail underside (XMT = 66.13)

2. Coordinates provided are for center of receptacle mating face

A3.5 ENVIRONMENTS

The MBS to MT electromagnetic, grounding and bonding interface implementation will be as defined in Figures A3.2−2 through A3.2−7 for the MT side of the interface and A3.2−8 through A3.2−11 for the MBS side of the interface.

A3.6 SOFTWARE INTERFACES

There are no software interfaces between the MBS and the MT.

A3.7 EVA HARDWARE LOCATIONS

The MBS will provide EVA hardware at locations as defined in Figures A3.7−1, A3.7−2, A3.7−3, and A3.7−4.

FIGURE A3.2−1 DELETED

A3 − 5

Reference Astro Drawing S606955 Sheet 2 of 10

FIGURE A3.2−2 MBS TO MT MECHANICAL INTERFACE

A3 − 6

Reference Astro Drawing S606955 Sheet 3 of 10

FIGURE A3.2−3 MBS TO MT MECHANICAL INTERFACE

A3 − 7

Reference Astro Drawing S606955 Sheet 4 of 10

FIGURE A3.2−4 MBS TO MT MECHANICAL INTERFACE

A3 − 8

Reference Astro Drawing S606955 Sheet 5 of 10

FIGURE A3.2−5 MBS TO MT MECHANICAL INTERFACE

A3 − 9

Reference Astro Drawing S606955 Sheet 6 of 10

3.

2.

(2 .3

9) 7.

.0

FIGURE A3.2−6 MBS TO MT MECHANICAL INTERFACE

A3 − 10

Reference Astro Drawing S606955 Sheet 7 of 10

FIGURE A3.2−7 MBS TO MT MECHANICAL INTERFACE

SSMB to MSS ICDSSP 42003, Part 2, Revision C

A3 −11

(Reference SPAR Drawing 51800−0011, Sheet 1 of 6)

FIGURE A3.2−8 MBS TO MT STRUCTURAL INTERFACES

A3 −12

(Reference SPAR Drawing 51800−0011, Sheet 2 of 6)

FIGURE A3.2−9 MBS TO MT STRUCTURAL INTERFACES

A3 −13

(Reference SPAR Drawing 51800−0011, Sheet 3 of 6)

FIGURE A3.2−10 MBS TO MT STRUCTURAL INTERFACES

SSMB to MSS ICD SSP 42003, Part 2, Revision C May 22, 2007

A3 −14

Note: “For a detailed view of these drawings, refer to the VMDB under 51800−0011. Ref F. Sheet 4 of 6.”

FIGURE A3.2−11 MBS TO MT STRUCTURAL INTERFACE

A3 −15

(Reference SPAR Drawing 51800−0011, Sheet 6 of 6)

FIGURE A3.2−12 MBS TO MT STRUCTURAL INTERFACES

A3 −16

M

+Z

+Y

+X

+Y

NOTES; UNLESS OTHERWISE SPECIFIED

1. INTERPRET DRAWING PER DOD−STD AND ANSI Y14.5M−1982

MOBILE TRANSPORTER SIDE FACING SSRMS ELBOW CAMERA

VIEW B−B

MOBILE TRANSPORTER SIDE FACING EE CAMERA

MOBILE TRANSPORTER SIDE FACING KEEL CAMERA

VIEW A−A

DETAIL D

(0.265)

(0.876)

(Ø1.750)

DETAIL C

COLOR, BLACK 7 PL

W HITE 1 PL

2.00

2.00

1.00

0.20 A B M

B B

A A

4 6 .0 0

2 X 2 .2 2

4 SU R FAC ES

− A −

(46.000)

46.00

C O L O R : BL AC K

21.00

10.50

SEE D ETAIL C

SEE D ET AIL D

(46.000)

2 X 2 7 .5 0

2 4 .2 5

0.10 A B MM

0.10 A B MM

− B −

4 SU R FAC ES

−A −

0.10 A B MM

11.40

1.60

0.81 (0.876)

2x 2.22

(2.000)

0.10 A B MM

11.00

A BM M0.20

46.00

COLOR:

WHITE

COLOR:

BLACK

0.87 + 0.10

24.00 + 0.10

4X 0.50 + 0.05 4X (01.750)

0.50 + 0.05

22.80 + 0.05

22.00 + 0.05

FIGURE A3.2−13 MBS TO MT MECHANICAL INTERFACE

A3 − 17

Note: “For a detailed view of these drawings, refer to the VMDB under 51800−0011. Rev F. Sheet 5 of 6.”

FIGURE A3.2.1−1 MBS/MT INTERFACE HARNESS DESIGN

A3 − 18

FIGURE A3.4−1 MT/MBS POWER, RETURN AND GROUNDING DIAGRAM

CRPCM

CRPCM

MBS

MBS

H − High (120 Vdc typical) G − Ground R − Voltage Return /// Structure Ground SPG − Single point ground

H

R

G

A3 − 19

RPDA

SSBA

SSBA

RPDA

4) For MBS/MT connector details refer to Figure A3.2.1−1

Figure A3.2.1−1.

SS Buffer Amplifier Bus Coupler Bus Termination Remote Power Distribution Assembly

SSBA:

RPDA:

Legend

MT/MBS

INTERFACE PLANE

(CONNECTORS)

MT MBS

Video A

Video B

MSS

Local Bus A Distribution

MSS

Local Bus B Distribution

50 ohm co−ax

50 ohm co−ax

−2

−1

UMA−1

UMA−2

5) This schematic applies during MT stationery operations.

FIGURE A3.4−2 MT/MBS ELECTRICAL INTEGRA TED DIAGRAM

A3 − 20

MBS

12A

RPCM

(Prime)

J29 P1

EVA Load

MBS EVA Outlet #1

MBS

12A

RPCM

(Redundant)

J30 P1

EVA Load

MBS EVA Outlet #2

EVA Connector

Notes: 1) For EVA outlets connector details refer to Tables A3.4.2−1 and A3.4.2−2.

FIGURE A3.4−3 MBS EVA ELECTRICAL OUTLETS

A3 − 21

FIGURE A3.4.2−1 DELETED

FIGURE A3.4.2−2 DELETED

A3 − 22

FIGURE A3.4.3.3−1 MT/MBS INTERFACE CONNECTOR LOCATION

A3 − 23

FIGURE A3.4.3.3−2 MT/MBS CONNECTOR LOCATION

A3 − 24

TABLE A3.4.2−1 MBS EVA OUTLET #1 CONNECTOR AND PIN ASSIGNMENTSÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁCONNECTOR ID(3)

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁMBS

Ref. Des: J29

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁPart Number: NZGL00T1717N6SNÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁSSMB Ref. Des: P1

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁPart Number: ReservedÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁPOWER SPECIFICATIONS ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁContact

ID

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁSignal Function

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁPeak Power (W)

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁMinimum Voltage

(VDC)

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁCurrent(4) (A)

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁEMC

Class

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁPower(1) Quality Type

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁWire GaugeÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

A

E

F

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ EVA Power

Return

Ground

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

EO

EO

EO

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

C

C

NA

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Notes:

1) The Transient Voltage Limits & Time Duration are as defined in SSP 30482, Electrical Power Specification and Standards, volume 1: EPS Electrical Performance Specifications, Volume 2: Consumer Constraints.

2) Table reflects the design to peak power requirement and the associated minimum voltage at the interface plane.

3) Connector specifications are per SSQ 21635, Connectors and Accessories, electrical, Circular Miniature, IVA/ EVA Compatible, Space Quality, General Specification for.

4) Rated output current capability of MBS Canadian Remote Power Control Module (CRPCM) providing power to EVA outlet.

A3 − 25

TABLE A3.4.2−2 MBS EVA OUTLET #2 CONNECTOR AND PIN ASSIGNMENTSÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁCONNECTOR ID (3)

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁMBS

Ref. Des: J30

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁPart Number: NZGL00T1717N6SNÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁSSMB Ref. Des: P1

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁPart Number: ReservedÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ POWER SPECIFICATIONS

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁContact

ID

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁSignal Function

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁPeak Power (W)

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁMinimum Voltage

(VDC)

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁCurrent(4) (A)

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁEMC

Class

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁPower(1) Quality Type

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁWire GaugeÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

A

E

F

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ EVA Power

Return

Ground

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

EO

EO

EO

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

C

C

NA

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Notes:

1) The Transient Voltage Limits & Time Duration are as defined in SSP 30482.

2) Table reflects the design to peak power requirement and the associated minimum voltage at the interface plane.

3) Connector specifications are per SSQ 21635.

4) Rated output current capability of MBS CRPCM providing power to EVA outlet.

A3 − 26

THIS PAGE INTENTIONALL Y LEFT BLANK

May 22, 2007SSP 42003, Part 2, Revision C

A3 − 27

Note: “For a detailed view of these drawings, refer to the VMDB under 51800−0001.Rev F. Sheet 1 of 4.”

FIGURE A3.7−1 LOCATION OF EVA HARDWARE ON MBS

A3 − 28

Note” “For a detailed view of these drawings, refer to the VMDB under 51800−0001. Rev F. Sheet 2 of 4.”

FIGURE A3.7−2 LOCATION OF EVA HARDWARE ON MBS

A3 − 29

Note: ”For a detailed view of these drawings, refer to the VMDB under 51800−0001.Rev F. Sheet 3 of 4.”

FIGURE A3.7−3 LOCATION OF EVA HARDWARE ON MBS

A3 − 30

Note: ”for a detailed view of these drawings, refer to the VMDB under 51800−0001. Rev F. Sheet 4 of 4.”

FIGURE A3.7−4 LOCATION OF EVA HARDWARE ON MBS

B3 − 1

SECTION B3 RESERVED

B3 RESERVED

C3 − 1

SECTION C3 AVU TO USL INTERFACE

C3.0 INTERFACE DEFINITION

C3.1 GENERAL

C3.1.1 INTERFACE DESCRIPTION

The Artificial Vision Unit (AVU) to United States Laboratory (USL) mated on−orbit configuration is shown in Figure C3.1.1−1. The structural and mechanical interface is at the plane between the two interfacing units as documented herein. Utility interface planes exist at the connectors between the AVU and the USL rack harness.

C3.1.2 INTERFACE RESPONSIBILITIES

CSA is responsible for procurement of the AVU for delivery to NASA as Government Furnished Equipment (GFE). PG−3 is responsible for develoment of the USL. Interface responsibilities for the AVU to USL interface are as defined in SSP 42003 Part I, Section C and as described in SSP 42003 Part II, Section C herein.

C3.1.3 ENGINEERING UNITS AND TOLERANCES

Unless otherwise noted herein, all dimensions in this document are shown in the English system of inch pound (IP) units. Implied tolerances on linear dimensions are defined in Table C3.1.3−1.

C3.2 STRUCTURAL/MECHANICAL INTERF ACES

C3.2.1 GENERAL

AVU structurally attaches to the USL rack via a coldplate attachment system. The AVU to coldplate fastener pattern will be as shown in Figures C3.2.1−1 and C3.2.1−2.

C3.2.2 UTILITY INTERFACE(S)

The assigned Electrical Reference Designations for AVU connectors are shown in Figure C3.2.1−1, prefaced by the letter ”J”. The assigned reference designations for USL rack harness connectors are prefaced by the letter ”P”.

C3 − 2

C3.3 FLUID INTERFACE(S)

N/A

C3.4 ELECTRICAL INTERFACE(S)

C3.4.1 ELECTRICAL CONNECTIVITY

The electrical interface(s) (Including Power, Data, & Video interfaces) between the AVU and U.S. Lab consists of a series of electrical connectors with associated cabling. The power, data, and video system interfaces are reflected in Figures C3.4.1−1 and C3.4.1−2.

C3.4.1.1 DETAILED ELECTRICAL INTERF ACE(S)

Control of the detailed electrical interface between the AVU and the USL rack harness consists of identifying the particular jack/plug pair, configuration, location, part number and functionality. Table C3.4.1.1−1 thru C3.4.1.1−4 define these controlling parameters for the power, data, cursor control device, and video respectively. For Tables C3.4.1.1−1 through C3.4.1.1−4, the following definitions apply:

Not Used − Pin location not used (by Orbital Replacement Unit (ORU) or wire harness).

Reserved − Pin used by ORU only.

Spare − Pin used by wire harness only.

C3.4.2 ELECTRICAL BONDING

The electrical bonding interface for the AVU is a Class R bond through the USL coldplate that complies with the requirements of SSP 30245, Space Station Electrical Bonding Requirements.

The AVU bonding is accomplished via sixteen threaded fasteners that compress the AVU Electroless Nickel mounting surface against the USL coldplate Stainless steel (CRES 347) mounting surface as defined in Figures C3.2.1−1 and C3.2.1−2.

C3.4.3 SOFTWARE INTERFACES

The AVU software interfaces to the Robotic Workstation (RWS) are as specified in CSA−SS−ID−0002, Canadian Space Vision System (CSVS) Interface Control Document (ICD)

MRCS/AVU.

C3−3

Note: AVU Hard Drive not shown

FIGURE C3.1.1−1 MSS RACK CONFIGURATION (FRONT VIEW)

C3−4

TABLE C3.1.3−1 LINEAR TOLERANCES

English Dimensions Implied Tolerances (inches) x.xx +/− 0.030 x.xxx +/− 0.010

C3−5

DIMENSIONING & TOLERANCING

PER ANSI Y 14.5 M−1982

UNLESS OTHERWISE SPECIFIED

DIMENSIONS ARE IN INCHES

TOLERANCES: ANGLES + 1

DECIMALS .XX +.03

DECIMALS .XXX +.010

RIVET & BOLT EDGE MARGIN +.05

BEND RADII +.01 ON .03 & .06

+.03 ON .09 & GREATER

SHEET METAL CORNER RADII

INTL .26 EXT .25

.22 .00

DIMENSIONS AND SURFACE TEXTURE

DESIGNATIONS APPLY BEFORE

PLATING OR FINISH COATING

UNLESS OTHERWISE NOTED

ELECTROLESS NICKEL PLATE PER MIL−C−26074, CLASS 4, GRADE A

DENOTES ESTIMATED CENTRE OF GRAVITY

HARD DISK DRIVE SHOWN FOR REFERENCE ONLY: NOT INSTALLED FOR

LAUNCH CONFIGURATION: NOT INCLUDED FOR C OF G ESTIMATE.

ORU MOUNTING FASTENERS WILL BE TORQUED TO 25−30 IN. LBS.

NOTES:

CONNECTOR J5 NOT USED FOR ISS APPLICATION.

.6

7 MASTER CONNECTOR KEYWAY LOCATION

ALL CORNERS AND EDGES RADIUS OR CHAMFER TO .03 MIN.

5 PLACES

8 CONNECTORS ARE LOCATED ON ”FRONT” OF AVU

FIGURE C3.2.1−1 INTERFACE CONTROL DRAWING OF AVU

(NOT TO SCALE)

SSP 42003, Part 2, RevisionC

May 22, 2007

C3−6

FIGURE C3.2.1−2 INTERFACE CONTROL DRAWING OF AVU

(NOT TO SCALE)

C3−7

Data Normal Hi (T Ball 1+)

Primary

AVU

RPCM

Type V

3.5 A

AVU2 Power 16ga

AVU2 Return 16ga

MSS−PDGF LB A HI 22ga

MSS−PDGF LB A LO 22ga

Video O/P #2 Plus

CSA provided connectors

NASA provided connectors

J1

J2

J3

J4

W1186P2

W1181P3

W1187P2

J5

Video O/P #2 Minus

Video O/P #1 Plus Video O/P #1 Minus

Video I/P #2 Plus Video I/P #2 Minus

Video I/P #1 Plus Video I/P #1 Minus

Sync I/P Plus Sync I/P Minus

CEU Video O/P #1 Plus CEU Video O/P #1 Minus

CEU Video O/P #2 Plus CEU Video O/P #2 Minus

Control Electronics

Unit

(CEU)

CVIU

CVIU

Data Normal Lo (T Ball 1−)

D&C Panel*

A

B

C

D

E

MSS−PDGF LB B HI 22ga

MSS−PDGF LB B LO 22ga

RT address 2nd MSB

RT address MSB

RT address 3rd MSB

RT address 4th MSB

RT address LSB

Parity Bit

W1182P3

AVU Location Address (dec)

Address (binary)

Parity

Primary LAS 5 11 01011 0

Links

1&2,5&6, 11&12

RT Address Selection

Spare (T Ball 2+)

Interface between DCP wire harness and AVU CCD defined in Section G.

Spare (T Ball 2−)

Spare (T Ball 3+)

Spare (T Ball 3−)

Spare (T Ball 4+)

Spare (T Ball 4−)

Spare (T Ball 5+)

Spare (T Ball 5−)

Rack Interface Panel*

Note: * Rack Interface Panel and DCP information is included for reference only

FIGURE C3.4.1−1 PRIMARY AVU ELECTRICAL SYSTEM DIAGRAM

C3−8

Secondary

AVU

RPCM

Type V

3.5 A

AVU1 Power 16ga

AVU1 Return 16ga

MSS−PDGF LB A HI 22ga

MSS−PDGF LB A LO 22ga

Video O/P #2 Plus

CSA provided connectors

NASA provided connectors

Video O/P #2 Minus

Video O/P #1 Plus Video O/P #1 Minus

Video I/P #2 Plus Video I/P #2 Minus

Video I/P #1 Plus Video I/P #1 Minus

Sync I/P Plus Sync I/P Minus

CEU Video O/P #1 Plus CEU Video O/P #1 Minus

CEU Video O/P #2 Plus CEU Video O/P #2 Minus

Control Electronics

Unit

(CEU)

CVIU

CVIU

A

B

C

D

E

MSS−PDGF LB B HI 22ga

MSS−PDGF LB B LO 22ga

RT address 2nd MSB

RT address MSB

RT address 3rd MSB

RT address 4th MSB

RT address LSB

Parity Bit

AVU Location Address (dec)

Address (binary)

Parity

Secondary LAP 5 8 01000 0

Links

1&2,5&6, 7&8,9&10 , 11&12

RT Address Selection

J1

J2

J4

W1281P3

W1287P2

J5

W1282P3

J3

W1286P2

Interface between DCP wire harness and AVU CCD defined in SectionG

Data Normal Hi (T Ball 1+)

Data Normal Lo (T Ball 1−)

D&C Panel*

Spare (T Ball 2+)

Spare (T Ball 2−)

Spare (T Ball 3+)

Spare (T Ball 3−)

Spare (T Ball 4+)

Spare (T Ball 4−)

Spare (T Ball 5+)

Spare (T Ball 5−)

Rack Interface Panel*

Note: * Rack Interface Panel and DCP information is included for reference only

FIGURE C3.4.1−2 SECONDARY AVU ELECTRICAL SYSTEM DIAGRAM

C3−9

TABLE C3.4.1.1−1 DETAILED ELECTRICAL DESCRIPTION OF A VU CONNECTOR J1

(POWER)

CSANASA

AVU

Interface Plane

J1P3

A V U

C O N N E C T O R

Insert Arrangement Insert 15−5 Per SSQ 21635

A

B

CD

E

+X−X

+Y

−Y

CONNECTOR LOCATION

CONNECTOR ID AVU (POWER)

Ref. Des J1 Part Number D38999/20FD5PN Wire Harness Number NA

Ref. Des P3 Part Number NATC06G15N5SN Wire Harness Number LAS5−W1181

LAP5−W1281

PIN FUNCTION TABLE

Cont

ID

Signal

Function

Maximum

Pwr [W]

EMC

Class

AWG RPCM GND

Loc’n

Sig

Source

Notes

A Not used

B AVU1 Power 175 EO 16 3.5 amp MSS rack

Twisted with AVU 1

Return

C AVU1 Return 175 EO 16 3.5 amp MSS rack

Twisted with AVU 1

Power

D Reserved For Orbiter application

E Reserved For Orbiter application

C3−10

TABLE C3.4.1.1−2 DETAILED ELECTRICAL DESCRIPTION OF A VU CONNECTOR J2

(DATA)

22−X +X

−Y

+Y

CSANASA

AVU

Interface Plane

J2P3

A V U

C O N N E C T O R

Insert Arrangement Insert 13−35 Per SSQ 21635

*Note: For 1553B address and parity lines:

Closed loop equivalent to logic ’0’ Open loop equivalent to logic ’1’

CONNECTOR LOCATION

CONNECTOR ID − AVU (1553)

Ref. Des J2 Part Number D38999/20FC35PA Wire Harness

Number

NA

Ref. Des P3 Part Number NATC06G13N35SA Wire Harness Number

LAS5−W1182

LAP5−W1282

PIN FUNCTION TABLE

Cont

ID

Signal Function EMC Class

AWG Signal Source

Signal Destination

Notes

1 RT ADDRESS MSB N/A 22 AVU AVU Address*

2 GROUND FOR MSB N/A 22 AVU AVU Address*

3 RT ADDRESS 2ND MSB N/A 22 AVU AVU Address*

4 GROUND FOR 2ND MSB N/A 22 AVU AVU Address*

5 RT ADDRESS 3RD MSB N/A 22 AVU AVU Address*

6 GROUND FOR 3RD MSB N/A 22 AVU AVU Address*

7 RT ADDRESS 4TH MSB N/A 22 AVU AVU Address*

8 GROUND FOR 4TH MSB N/A 22 AVU AVU Address*

9 RT ADDRESS LSB N/A 22 AVU AVU Address*

C3−11

TABLE C3.4.1.1−2 DETAILED ELECTRICAL DESCRIPTION OF A VU CONNECTOR J2

(DATA) (CONTINUED)

10 GROUND FOR LSB N/A 22 AVU AVU Address*

11 PARITY BIT N/A 22 AVU AVU Address*

12 GROUND FOR PARITY

BIT

N/A 22 AVU AVU Address*

13 NOT USED

14 NOT USED N/A N/A

15 MSS PDGF LB B LO RF 22 N/A N/A 1553B per SSQ 21655

16 NOT USED

17 MSS PDGF LB A LO RF 22 N/A N/A 1553B per SSQ 21655

18 NOT USED

19 NOT USED

20 NOT USED

21 MSS PDGF LB B HI RF 22 N/A N/A 1553B per SSQ 21655

22 MSS PDGF LB A HI RF 22 N/A N/A 1553B per SSQ 21655

C3−12

TABLE C3.4.1.1−3 DETAILED ELECTRICAL DESCRIPTION OF A VU CONNECTOR J3

(CURSOR CONTROL DEVICE)

CSANASA

AVU

Interface Plane

J3P2

A V U

C O N N E C T O R

Insert Arrangement Insert 13−35 Per

SSQ 21635

+Y

+X

−Y

−X

CONNECTOR LOCATION

CONNECTOR ID − AVU (CURSOR CONTROL DEVICE)

Ref. Des J3 Part Number D38999/20FC35PN Wire Harness Number

NA

Ref. Des P2 Part Number NATC06G13N35SN Wire Harness Number

LAS5−W1186

LAP5−W1286

PIN FUNCTION TABLE

Cont

ID

Signal Function EMC Class

AWG Signal Destination

Signal Source

Notes

1 RESERVED For Orbiter Application

2 RESERVED For Orbiter Application

3 RESERVED For Orbiter Application

4 RESERVED For Orbiter Application

5 Data Normal Hi RF 22 AVU AVU CCD T Ball 1+

6 Data Normal Lo RF 22 AVU AVU CCD T Ball 1−

7 RESERVED For Orbiter Application

8 RESERVED For Orbiter Application

9 RESERVED For Orbiter Application

10 NOT USED

C3−13

TABLE C3.4.1.1−3 DETAILED ELECTRICAL DESCRIPTION OF A VU CONNECTOR J3

(CURSOR CONTROL DEVICE)(CONTINUED)

11 SPARE HO 22 AVU AVU CCD T BALL 2+

12 SPARE HO 22 AVU AVU CCD T BALL 2−

13 SPARE HO 22 AVU AVU CCD T BALL 3+

14 SPARE HO 22 AVU AVU CCD T BALL 3−

15 SPARE HO 22 AVU AVU CCD T BALL 4+

16 SPARE HO 22 AVU AVU CCD T BALL 4−

17 SPARE HO 22 AVU AVU CCD T BALL 5+

18 SPARE HO 22 AVU AVU CCD T BALL 5−

19 RESERVED FOR ORBITER AP-

PLICATION

20 RESERVED FOR ORBITER AP-

PLICATION

21 RESERVED FOR ORBITER AP-

PLICATION

22 RESERVED FOR ORBITER AP-

PLICATION

C3−14

TABLE C3.4.1.1−4 DETAILED ELECTRICAL DESCRIPTION OF A VU CONNECTOR J4

(VIDEO)

CSANASA

AVU

Interface Plane

J4P2

A V U

C O N N E C T O R

Insert Arrangement Insert 15−35 Per

SSQ 21635

+Y

+X

−Y

−X

CONNECTOR LOCATION

CONNECTOR ID − AVU (VIDEO)

Ref. Des J4 Part Number D38999/20FD35PA Wire Harness Number N/A

Ref. Des P2 Part Number NATC06G15N35SA Wire Harness Number LAS5−W1187

LAP5−W1287

PIN FUNCTION TABLE

Cont

ID

Signal Function EMC Class

AWG Signal Source

Signal Destination

Notes

1 NOT USED

2 CEU Video O/P #1 Minus RF 22 AVU CEU TSP 1

3 CEU Video O/P #1 Plus RF 22 AVU CEU TSP 1

4 NOT USED

5 CEU Video O/P #2 Minus RF 22 AVU CEU TSP 2

6 CEU Video O/P #2 Plus RF 22 AVU CEU TSP 2

7 Not used

8 Not used

9 Not used

10 Not used

11 Not used

12 Not used

13 Not Used

14 Not Used

C3−15

TABLE C3.4.1.1−4 DETAILED ELECTRICAL DESCRIPTION OF A VU CONNECTOR J4

(VIDEO) (CONTINUED)

15 Not Used

16 Not Used

17 Not Used

18 Not Used

19 Not Used

20 Not Used

21 Not Used

22 Not used

23 Video O/P #2 Minus RF 22 AVU CVIU TSP 3

24 Video O/P #2 Plus RF 22 AVU CVIU TSP 3

25 Not used

26 Video O/P #1 Minus RF 22 AVU CVIU TSP 4

27 Video O/P #1 Plus RF 22 AVU CVIU TSP 4

28 Not used

29 Sync I/P Minus RF 22 CVIU AVU TSP 5

30 Sync I/P Plus RF 22 CVIU AVU TSP 5

31 Not used

32 Not used

33 Video I/P #2 Minus RF 22 CVIU AVU TSP 6

34 Video I/P #2 Plus RF 22 CVIU AVU TSP 6

35 Not used

36 Video I/P #1 Minus RF 22 CVIU AVU TSP 7

37 Video I/P #1 Plus RF 22 CVIU AVU TSP 7

D3 − 1

SECTION D3 SSMB TO PDGF INTERFACE

D3 INTERFACE DEFINITION

D3.1 GENERAL

D3.1.1 INTERFACE DESCRIPTION

The physical interface (mechanical, structural, thermal and environmental) plane is defined at the Power and Data Grapple Fixture (PDGF) Mounting Ring mounting surface at the Modules.

The utility interface plane (power, data and video) is defined between the PDGF harness and the Module connector panel. A Video Signal Converter (VSC) is required to convert the PFM fiber optic video from the SSMB to PFM electrical video that is compatible with the PDGF and SSRMS. The interfaces between the VSC and the modules are as defined in SSP 42003, Section H.

D3.1.2 INTERFACE RESPONSIBILITIES

CSA is responsible for development of the PDGF. NASA is responsible for procurement of the PDGF and PDGF harness for the USL, Hab, and Node2. NASA is responsible for development of the USL and Hab. ASI/Alenia is responsible for development of Node 2.

D3.1.3 ENGINEERING UNITS AND TOLERANCES

Unless otherwise noted herein, all dimensions in this document are shown in the English system of inch pound (IP) units.

D3.2 STRUCTURAL/MECHANICAL INTERF ACES

The PDGF structurally attaches to the modules via a PDGF mounting ring. The PDGF mounting ring attaches to the Modules via eight fasteners. The bolt hole pattern and related mechanical installation details are defined in SSP 42004 Part 2, Figures A3.2−1 through A3.2−3.

D3 − 2

D3.2.1 USL MODULE PDGF LOCA TION

A PDGF will be mounted on the USL Module at the location defined in Figure D3.2.1−1. The PDGF connector panel location on the USL will be as shown in Figure D3.2.1−1.

D3.2.2 HAB MODULE PDGF LOCA TION

A PDGF will be mounted on the Hab Module at the location defined in Figure D3.2.2−1 (TBD#4). The PDGF connector panel location on the Hab will be as shown in Figure D3.2.2−1.

D3.2.3 JEM−PM PDGF LOCATION

A PDGF will be mounted on the Japanese Experiment Module−Pressurized Module (JEM−PM) at the location defined in SSP 42000, Figure 3.8.1.1.1−1. The PDGF connector panel location on the JEM−PM will be as shown in SSP 42000, Space Station Manned Base to Japanese Experiment Module Interface Control Document, Figure 3.8.2.1.1−1.

D3.2.4 NODE 2 PDGF LOCATION

A PDGF will be mounted on the Node 2 at the location in Figure D3.2.4−1.

D3.3 THERMAL INTERFACES

The PDGF to Modules thermal interface implementation will be as defined in SSP 42004 Part 2, Figures A3.2−1 through A3.2−3.

D3.4 ELECTRICAL INTERFACES

The Modules will provide power, data and PFM video interfaces to the SSRMS via the PDGF as defined in Figures D3.4−1 through D3.4−5 and D3.4−7. The SSRMS Backup Drive power and data interfaces are provided by USL, Hab, and Node 2 (Endcone Scar) modules only.

D3 − 3

D3.4.1 POWER RETURN AND GROUNDING INTERFACES

The Modules will provide power, return, and grounding interfaces to the SSRMS via the PDGF as defined in Figures D3.4−1 through D3.4−5 and D3.4−7.

The Module PDGF external wiring diagram (except Node 2) is defined in Figure D3.4.1−1.

The Node 2 PDGF external wiring diagram is defined in Figure D3.4.1−2.

D3.4.2 DELETED

D3.4.2.1 USL POWER CONNECTORS AND PIN ASSIGNMENTS

The PDGF harness power…