International Space Station Program Space Station Manned Base to

SSP 42003, Part 2, Revision A

National Aeronautics and Space AdministrationInternational Space Station ProgramJohnson Space CenterHouston, Texas

International Space StationProgram

Space Station Manned Base toMobile Servicing SystemInterface Control DocumentPart 2

Revision A,

MAY 22, 1997

Type 1Approved by NASA

SSP 42003, Part 2, Revision A SSMB to MSS ICDMay 22, 1997

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


i

PREFACE

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

/s/ Denny A. Kross 5–2–96

Program Manager, DateInternational Space Station


ii

NASA/CSA

INTERNATIONAL SPACE STATION PROGRAM

SPACE STATION MANNED BASE TO MOBILE SERVICING SYSTEMINTERFACE CONTROL DOCUMENT PART 2

DATE

Print Name

For NASA

C. A. Hatfield

/s/ C. A. Hatfield 3/11/96

DATE

Print Name

For CSA

R. G. Brown

/s/ R. G. Brown 3/6/96


iii



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

Michael A. Stager

/s/ Michael A. Stager

26940

3/11/96

Steve Cox

/s/ Steve Cox

26940

3/11/96

Howard Griffin

/s/ Howard Griffin

26940

3/11/96

Frank Monahan

/s/ Frank Monahan

OB–1

3/11/96

Freddie G. Young

/s/ Freddie G. Young

OB–5

10/23/97


iv

CONCURRENCE



Product Group–1 ICWG


SIGNATURE

PRINT NAME

DATE

SIGNATURE

PRINT NAME

DATE

Representative for Concurrence


SPAR

SIGNATURE

PRINT NAME

DATE


SIGNATURE

PRINT NAME

DATE



Lee Archibald

/s/ Lee Archibald 3/29/96

N/A

N/A

Ralph Thompson

/s/ Lowell E. Cook for Ralph Thompson 2/22/96

P. Chadwick

/s/ P. Chadwick 4/3/96


v


SPACE STATION MANNED BASE TO MOBILE SERVICING SYSTEM INTERFACE CONTROL DOCUMENT PART 2

LIST OF CHANGES

MAY 22, 1997

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

SSCBD ENTRY DATE CHANGE PARAGRAPH(S)

TABLE(S)

FIGURE(S)

APPENDIX(ES)

ADDENDA


vi

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 APPLICABLE DOCUMENTS 2 - 1. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

SECTION

SECTION A3 MOBILE TRANSPORTER TO MRS BASE SYSTEM INTERFACE A3 – 1. . . . . . . . . . . .

A3 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. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

A3.3 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 ANDVIDEO 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. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

A3.5 ENVIRONMENTS A3 – 3. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

A3.6 SOFTWARE INTERFACES A3 – 4. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

A3.7 EVA HARDWARE LOCATIONS A3 – 4. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

B3 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. . . . . . . . . . . . . . . . . . . . . . . . . . .

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. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .


vii

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 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 DELETED D3 – 2. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

D3.3 THERMAL INTERFACES D3 – 2. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

D3.4 ELECTRICAL INTERFACES D3 – 2. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

D3.4.1 POWER RETURN AND GROUNDING INTERFACES D3 – 2. . . . . . . . . . . . . . . . . . .

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 DELETED 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 – 3. . . . . . . . . . .

D3.4.4.1 USL DATA AND VIDEO CONNECTORS AND PIN ASSIGNMENTS D3 – 3. . . . . .

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

D3.4.4.3 JEM–PM 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. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

SECTION E3 PWP TO MBS INTERFACE E3 – 1. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

E3 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. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .


viii

E3.3 SOFTWARE INTERFACES E3 – 2. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

SECTION F SSMB LSA TO SSRMS INTERFACE F3 – 1. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

F3 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. . . . . . . . . . .

F3.5 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. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

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 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. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .


ix

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 – 2. . . . . . . . . . . . . . . .

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

H3.5 ENVIRONMENTS H3 – 3. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

H3.6 SOFTWARE INTERFACES H3 – 3. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

FIGURES

A3.2–1 DELETED A3 – 4. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

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










A3.2.1–1 MBS/MT INTERFACE HARNESS DESIGN A3 – 15. . . . . . . . . . . . . . . . . . . . . . . . . . . .

A3.4–1 MT/MBS POWER, RETURN AND GROUNDING DIAGRAM A3 – 16. . . . . . . . . . . . .

A3.4–2 MT/MBS ELECTRICAL INTEGRATED DIAGRAM A3 – 17. . . . . . . . . . . . . . . . . . . . . . .

A3.4–3 MBS EVA ELECTRICAL OUTLETS A3 – 18. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

A3.4.2–1 DELETED A3 – 19. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

A3.4.2–2 DELETED A3 – 20. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

A3.4.2–1 MBS EVA OUTLET #1 CONNECTOR AND PIN ASSIGNMENTS A3 – 21. . . . . . . . .

A3.4.2–2 MBS EVA OUTLET #2 CONNECTOR AND PIN ASSIGNMENTS A3 – 22. . . . . . . . .

A3.7–1 LOCATION OF EVA HARDWARE ON MBS A3 – 24. . . . . . . . . . . . . . . . . . . . . . . . . . . .



C3.2.1–1 INTERFACE CONTROL DRAWING OF AVU (NOT TO SCALE) C3–4. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

C3.2.1–2 INTERFACE CONTROL DRAWING OF AVU (NOT TO SCALE) C3–5. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

C3.4.1–1 PRIMARY AVU ELECTRICAL SYSTEM DIAGRAM C3–6. . . . . . . . . . . . . . . . . . . . .

C3.4.1–2 SECONDARY AVU ELECTRICAL SYSTEM DIAGRAM C3–7. . . . . . . . . . . . . . . . . .

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 DELETED D3 – 7. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

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


x

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. . . . . . . . .

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

D3.4–5 DELETED D3 – 12. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

D3.4–6 JEM–PM TO PDGF ELECTRICAL SYSTEM DIAGRAM D3 – 13. . . . . . . . . . . . . . . . .

D3.7–1 SSRMS EVA HARDWARE LOCATIONS 3D – 38. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

E3 – 3. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

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 – 7. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

F3.2–6 DELETED F3 – 8. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

F3.2–7 DELETED F3 – 9. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

F3.2–8 DELETED F3 – 10. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

F3.2–9 DELETED F3 – 11. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

F3.4–1 FSEGF TO USL ELECTRICAL SYSTEM DIAGRAM F3 – 12. . . . . . . . . . . . . . . . . . . .

F3.4–2 FSEGF TO USL ELECTRICAL SYSTEM DIAGRAM F3 – 13. . . . . . . . . . . . . . . . . . . .

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. . . . . . . . . . . . . . . . . . . . . . .

H3.2–2 VSC BRACKET H3 – 4. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

H3.2–3 VSC BRACKET H3 – 5. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

H3.4–1 TUS VSC ELECTRICAL DIAGRAM H3 – 6. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

TABLES

C3.1.3–1 LINEAR TOLERANCES C–3. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

C3.4.1.1–1 DETAILED ELECTRICAL DESCRIPTION OF AVU CONNECTOR J1 (POWER)C3–8

C3.4.1.1–2 DETAILED ELECTRICAL DESCRIPTION OF AVU CONNECTOR J2 (DATA) C3–9

C3.4.1.1–2 DETAILED ELECTRICAL DESCRIPTION OF AVU CONNECTOR J2 (DATA)(CONTINUED) C3–10. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

C3.4.1.1–3 DETAILED ELECTRICAL DESCRIPTION OF AVU CONNECTOR J3 (CURSORCONTROL DEVICE) C3–11. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

C3.4.1.1–3 DETAILED ELECTRICAL DESCRIPTION OF AVU CONNECTOR J3 (CURSORCONTROL DEVICE)(CONTINUED) C3–12. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

C3.4.1.1–4 DETAILED ELECTRICAL DESCRIPTION OF AVU CONNECTOR J4 (VIDEO) . C3–13

C3.4.1.1–4 DETAILED ELECTRICAL DESCRIPTION OF AVU CONNECTOR J4 (VIDEO)(CONTINUED) C3–14. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

D3.4.2.1–1 DETAILED ELECTRICAL DESCRIPTION OF LAB PDGF CONNECTOR J400 (PRIMEPOWER) (PAGE 1 OF 2) D3 – 14. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .


xi

D3.4.2.1–1 DETAILED ELECTRICAL DESCRIPTION OF LAB PDGF CONNECTOR J400 (PRIMEPOWER) (PAGE 2 OF 2) D3 – 15. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

D3.4.2.1–2 DETAILED ELECTRICAL DESCRIPTION OF LAB PDGF CONNECTOR J401(REDUNDANT POWER) (PAGE 1 0F 2) D3 – 16. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

D3.4.2.1–2 DETAILED ELECTRICAL DESCRIPTION OF LAB PDGF CONNECTOR J401(REDUNDANT POWER) (PAGE 2 0F 2) D3 – 17. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

D3.4.2.1–3 DETAILED ELECTRICAL DESCRIPTION OF LAB PDGF CONNECTOR J402 (BACKUPDRIVE POWER) D3 – 18. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

D3.4.2.2–1 DETAILED ELECTRICAL DESCRIPTION OF HAB PDGF CONNECTOR J400 (PRIMEPOWER) D3 – 19. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

D3.4.2.2–2 DETAILED ELECTRICAL DESCRIPTION OF HAB PDGF CONNECTOR J401(REDUNDANT POWER) D3 – 20. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

D3.4.2.2–3 DETAILED ELECTRICAL DESCRIPTION OF HAB PDGF CONNECTOR J402 (BACKUPDRIVE POWER) D3 – 21. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

D3.4.2.3–1 DETAILED ELECTRICAL DESCRIPTION OF JEM PDGF CONNECTOR J400 (PRIMEPOWER) D3 – 22. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

D3.4.2.3–2 DETAILED ELECTRICAL DESCRIPTION OF JEM PDGF CONNECTOR J401(REDUNDANT POWER) D3 – 23. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

D3.4.4.1–1 DETAILED ELECTRICAL DESCRIPTION OF LAB PDGF CONNECTOR J403 (1553 &VIDEO) (PAGE 1 OF 3) D3 – 24. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .





D3.4.4.1–3 DETAILED ELECTRICAL DESCRIPTION OF LAB PDGF CONNECTOR J405 (VIDEO)(PAGE 1 OF 1) D3 – 29. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

D3.4.4.1–4 DETAILED ELECTRICAL DESCRIPTION OF LAB PDGF CONNECTOR J406 (1553 &VIDEO) D3 – 30. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

D3.4.4.1–5 DETAILED ELECTRICAL DESCRIPTION OF LAB PDGF CONNECTOR J407 (1553 &VIDEO) D3 – 31. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

D3.4.4.2–1 DETAILED ELECTRICAL DESCRIPTION OF HAB PDGF CONNECTOR J403 (1553 &VIDEO) D3 – 32. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

D3.4.4.2–2 DETAILED ELECTRICAL DESCRIPTION OF HAB PDGF CONNECTOR J404 (1553 &VIDEO) D3 – 33. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

D3.4.4.2–3 DETAILED ELECTRICAL DESCRIPTION OF HAB PDGF CONNECTOR J405 (VIDEO) . D3 – 34

D3.4.4.3–1 DETAILED ELECTRICAL DESCRIPTION OF JEM PDGF CONNECTOR J403 (1553 &VIDEO) D3 – 35. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

D3.4.4.3–2 DETAILED ELECTRICAL DESCRIPTION OF JEM PDGF CONNECTOR J404 (1553 &VIDEO) D3 – 36. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

D3.4.4.3–3 DETAILED ELECTRICAL DESCRIPTION OF JEM PDGF CONNECTOR J405 (VIDEO) . D3 – 37

F3.4.2–1 DETAILED ELECTRICAL DESCRIPTION OF FSEGF TO USL CONNECTOR J300(PRIME POWER) F3 – 14. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

F3.4.2–2 DETAILED ELECTRICAL DESCRIPTION OF FSEGF TO USL CONNECTOR J301(REDUNDANT POWER) F3 – 15. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .


xii

F3.4.4–1 DETAILED ELECTRICAL DESCRIPTION OF FSEGF TO USL CONNECTOR J303 (1553& VIDEO) F3 – 16. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

F3.4.4–2 DETAILED ELECTRICAL DESCRIPTION OF FSEGF TO USL CONNECTOR J304 (1553& VIDEO) F3 – 17. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

F3.4.4–3 DELETED F3 – 18. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

G3.1.3–1 LINEAR TOLERANCES G3 – 1. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

G3.4.1.1–1 DETAILED ELECTRICAL DESCRIPTION OF AVU CCD CONNECTOR J1 (CURSORCONTROL DEVICE) G3 – 7. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

H3.4.2–1 DETAILED ELECTRICAL DESCRIPTION OF VSC ORU TO SSMB CONNECTOR J2(PRIME POWER) H3 – 7. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

H3.4.2–2 DETAILED ELECTRICAL DESCRIPTION OF VSC ORU TO SSMB CONNECTOR J3(REDUNDANT POWER) H3 – 8. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

H3.4.4–1 DETAILED ELECTRICAL DESCRIPTION OF VSC ORU TO SSMB CONNECTOR J1(FIBER OPTIC VIDEO CONNECTOR) H3 – 9. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

H3.4.4–2 DETAILED ELECTRICAL DESCRIPTION OF VSC ORU TO SSMB CONNECTOR J4(COPPER VIDEO CONNECTOR) H3 – 10. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

APPENDIX A: ABBREVIATIONS AND ACRONYMS A – 1. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

APPENDIX B: TBD LIST B – 1. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .


1 - 1

1.0 INTRODUCTION

1.1 PURPOSE AND SCOPE

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

1.2 PRECEDENCE

In the event of conflict between SSP 41000, Space Station System Specification, and thecontents 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 SpaceStation 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 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

SSQ 21635 Connectors and accessories, Electrical, Circular Miniature,IVA/EVA Compatible, Space Quality, General SpecificationFor

SSP 42000 Space Station Manned Base to Japanese Experiment ModuleRev J Interface Control Document11/7/95

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

SSP 30256:001 EVA Standard Interface Control DocumentRev E3 Oct 94

SSP 41000 Space Station System Specification

SSP 30245 Space Station Electrical Bonding Requirements

SSP 30459 International Space Station Interface Control Plan

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

SSP 30482 Electrical Power Specification and Standards, Volumes I and II

SSQ 21655 General Specifications for Cable Electrical, MIL–STD–1553,Data Bus, Space Quality

MIL–STD–1553 Digital Time Division Command/Response Multiplex Databus

CSA–SS–ID–0002 Canadian Space Vision System (CSVS) Interface ControlDocument (ICD) MRCS/AVU


A3 – 1

SECTION A3 MOBILE TRANSPORTER TO MRS BASE SYSTEM INTERFACE

A3 INTERFACE DEFINITION

A3.1 GENERAL

A3.1.1 INTERFACE DESCRIPTION

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

A3.1.2 INTERFACE RESPONSIBILITIES

CSA is responsible for development of the MBS. NASA is responsible for development of theMT. Interface responsibilities for the MT to MBS interface are as defined in SSP 42003 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 systemof inch pound (IP) units.

A3.2 STRUCTURAL/MECHANICAL INTERFACES

MBS structurally attaches to the MT via a four fastener interface. The MT side of the MBS toMT mechanical interface will be as shown in Figures A3.2–2 through A3.2–7 (Figure A3.2–1has been deleted). The MBS side of the MBS to MT interface will be as shown in FiguresA3.2–8 through A3.2–11.


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 inFigure A3.2.1–1.

A3.3 THERMAL INTERFACES

The MT side of the MBS to MT thermal interface implementation will be as defined in FiguresA3.2–2 through A3.2–7. The MBS side of the MBS to MT thermal interface implementationwill 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 beachieved by an assembly procedure to allow sufficient time between initial capture of the MT bythe MBS capture latch and the attachment of four fasteners by Extravehicular Activity (EVA).

A3.4 ELECTRICAL INTERFACES

The Space Station Manned Base (SSMB) will provide power, data, and PFM copper videointerfaces to the MBS via the MT and Trailing Umbilical System (TUS) as defined in FiguresA3.4–1 and A3.4–2. The MBS will provide EVA electrical outlets for SSMB tools withelectrical 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 asdefined in Figure A3.4–1. For detailed electrical schematic and connectivity diagram, includingthe 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 connectorpanel 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 andA3.4.2–2.

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

The SSMB will support 1553 data and PFM sync and control and video interfaces between theSSMB and the MBS via the MT and TUS. PFM copper video will be carried between the MBSand 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 asdefined in Figures A3.2.1–1.

A3.4.3.2 MSS VIDEO PROVISIONS

During SSRMS or MBS POA operations, the MSS will provide, via the MBS, PFM sync andcontrol and video capability as defined in SSP 42004, Part 2, Table A3.4.4–1.

The External Video Switches (VSW(E)) will provide to the MBS via TUS A and TUS B, threevideo channels.

The External Video Switches (VSW(E)) will provide to the MBS, via TUS A and TUS B, twosimultaneous PFM sync and control signals.

A3.5 ENVIRONMENTS

The MBS to MT electromagnetic, grounding and bonding interface implementation will be asdefined in Figures A3.2–2 through A3.2–7 for the MT side of the interface and A3.2–8 throughA3.2–11 for the MBS side of the interface.


A3 – 4

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 andA3.7–3.


A3 – 5

FIGURE A3.2–1 DELETED


A3 – 6

Reference Astro Drawing S606955 Sheet 2 of 10

FIGURE A3.2–2 MBS TO MT MECHANICAL INTERFACE


A3 – 7




A3 – 8




A3 – 9




A3 – 10




A3 – 11



SSMB to MSS ICDSSP 42003, Part 2

May 22, 1997

A3 – 12

(Reference SPAR Drawing 51800–0011, Sheet 1 of 5)



May 22, 1997

A3 – 13




May 22, 1997

A3 – 14




May 22, 1997

A3 – 15




May 22, 1997

A3 – 16


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


A3 – 17

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

SS

P 42003, P

art 2, Revision A

SS

MB

to MS

S IC

DM

ay 22, 1997

A3 – 18

RPDASSBA

SSBA

RPDA

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

Figure A3.2.1–1.

SS Buffer AmplifierBus CouplerBus TerminatiotionRemote Power Distribution Assembly

SSBA:

RPDA:

Legend

FIGURE A3.4–2 MT/MBS ELECTRICAL INTEGRATED DIAGRAM


A3 – 19

MBS12A

RPCM(Prime)

J29 P1

EVA Load

MBS EVA Outlet #1

MBS12A

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 – 20

FIGURE A3.4.2–1 DELETED


A3 – 21

FIGURE A3.4.2–2 DELETED


A3 – 22

TABLE A3.4.2–1 MBS EVA OUTLET #1 CONNECTOR AND PIN ASSIGNMENTS

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁCONNECTOR ID(3)

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

MBSRef. Des: J29


Part Number: NZGL00T1717N6SN


SSMBRef. Des: P1


Part Number: Reserved

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

POWER SPECIFICATIONS

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

ContactID

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Signal Function ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

PeakPower(W)


MinimumVoltage(VDC)

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Current(4) (A)


EMCClass


Power(1)Quality Type


WireGauge

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

A

E

F

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

EVA Power

Return

Ground

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

500

500

500


113

113

113


12

12

12


EO

EO

EO


C

C

NA


12

12

12

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 – 23

TABLE A3.4.2–2 MBS EVA OUTLET #2 CONNECTOR AND PIN ASSIGNMENTS

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

CONNECTOR ID (3)ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

MBSRef. Des: J30

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Part Number: NZGL00T1717N6SN

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

SSMBRef. Des: P1

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Part Number: Reserved


POWER SPECIFICATIONSÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

ContactID

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Signal FunctionÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

PeakPower(W)


MinimumVoltage(VDC)


Current(4) (A)


EMCClass


Power(1)Quality Type


WireGauge


A

E

F

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

EVA Power

Return

Ground


500

500

500


113

113

113


12

12

12


EO

EO

EO


C

C

NA


12

12

12

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.


May 22, 1997

A3 – 24


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


May 22, 1997

A3 – 25




May 22, 1997

A3 – 26




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 U.S. Laboratory mated on–orbit configuration is shown inFigure C3.1.1–1. The structural and mechanical interface is at the plane between the twointerfacing units as documented herein. Utility interface planes exist at the connectors betweenthe 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 FurnishedEquipment (GFE). PG–3 is responsible for develoment of the U.S. Laboratory (U.S. Lab).Interface responsibilities for the AVU to U.S. Lab 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 systemof inch pound (IP) units. Implied tolerances on linear dimensions are defined in Table C3.1.3–1.

C3.2 STRUCTURAL/MECHANICAL INTERFACES

C3.2.1 GENERAL

AVU structurally attaches to the USL rack via a coldplate attachment system. The AVU tocoldplate 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 FigureC3.2.1–1, prefaced by the letter ”J”. The assigned reference designations for USL rack harnessconnectors 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 andU.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 INTERFACE(S)

Control of the detailed electrical interface between the AVU and the USL rack harness consistsof identifying the particular jack/plug pair, configuration, location, part number andfunctionality. Table C3.4.1.1–1 thru C3.4.1.1–4 define these controlling parameters for thepower, data, cursor control device, and video respectively. For Tables C3.4.1.1–1 throughC3.4.1.1–4, the following definitions apply:

Not Used – Pin location not used (by 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 thatcomplies with the requirements of SSP 30245. The AVU bonding is accomplished via sixteenthreaded fasteners that compress the AVU Electroless Nickel mounting surface against the USLcoldplate Stainless steel (CRES 347) mounting surface as defined in Figures C3.2.1–1 andC3.2.1–2.

C3.4.3 SOFTWARE INTERFACES

The AVU software interfaces to the Robotic Workstation (RWS) are as specified inCSA–SS–ID–0002.


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

SS

P 42003, P

art 2S

SM

B to M

SS

ICD

May 22, 1997

C3–5

DIMENSIONING & TOLERANCINGPER ANSI Y 14.5 M–1982

UNLESS OTHERWISE SPECIFIEDDIMENSIONS ARE IN INCHESTOLERANCES: ANGLES + 1DECIMALS .XX +.03DECIMALS .XXX +.010RIVET & BOLT EDGE MARGIN +.05BEND RADII +.01 ON .03 & .06+.03 ON .09 & GREATERSHEET METAL CORNER RADIIINTL .26 EXT .25 .22 .00DIMENSIONS AND SURFACE TEXTUREDESIGNATIONS APPLY BEFOREPLATING OR FINISH COATINGUNLESS 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 FORLAUNCH 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.

5.6

7 MASTER CONNECTOR KEYWAY LOCATION

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

75 PLACES

8 CONNECTORS ARE LOCATED ON ”FRONT” OF AVU

FIGURE C3.2.1–1 INTERFACE CONTROL DRAWING OF AVU (NOT TO SCALE)

SS

P 42003, P

art 2S

SM

B to M

SS

ICD

May 22, 1997

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

RPCMType V3.5 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 PlusVideo O/P #1 Minus

Video I/P #2 PlusVideo I/P #2 Minus


Sync I/P PlusSync I/P Minus

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


ControlElectronics

Unit(CEU)

CVIU

CVIU

Data Normal Lo (T Ball 1–)

D&CPanel*

A

B

C

D

E

910

11

12

15

17

21

22

MSS–PDGF LB B HI 22ga

MSS–PDGF LB B LO 22ga

8

RT address 2nd MSB

RT address MSB

RT address 3rd MSB

RT address 4th MSB

RT address LSB

Parity Bit

W1182P3

1

2

34

5

67

3736

3433

2726

2423

3029

32

65

5

6

11

12

13

16

14

15

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+)

18

17

Interface between DCP wire harness andAVU 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 InterfacePanel*

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

FIGURE C3.4.1–1 PRIMARY AVU ELECTRICAL SYSTEM DIAGRAM


C3–8

Secondary

AVU

RPCMType V3.5 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 PlusVideo O/P #1 Minus



Sync I/P PlusSync I/P Minus



ControlElectronics

Unit(CEU)

CVIU

CVIU

A

B

C

D

E

910

11

12

15

17

21

22

MSS–PDGF LB B HI 22ga

MSS–PDGF LB B LO 22ga

8

RT address 2nd MSB

RT address MSB

RT address 3rd MSB

RT address 4th MSB

RT address LSB

Parity Bit

1

2

34

5

67

3736

3433

2726

2423

3029

32

65

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

5

6

11

12

13

16

14

15

18

17

Interface between DCP wire harness and AVU CCDdefined in SectionG

Data Normal Hi (T Ball 1+)

Data Normal Lo (T Ball 1–)

D&CPanel*

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 InterfacePanel*

Note: * Rack Interface Panel and DCP informationis 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 AVU CONNECTOR J1(POWER)

CSANASA

AVUInterface Plane

J1P3

AVU

CONNECTOR

Insert ArrangementInsert 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 TABLECont

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 AVU CONNECTOR J2(DATA)

114

1521

22–X +X

–Y

+Y

CSANASA

AVUInterface Plane

J2P3

AVU

CONNECTOR

Insert ArrangementInsert 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

NumberNA

Ref. Des P3 Part Number NATC06G13N35SA Wire HarnessNumber

LAS5–W1182

LAP5–W1282

PIN FUNCTION TABLEContID

Signal Function EMCClass

AWG SignalSource

SignalDestination

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 AVU 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 AVU CONNECTOR J3(CURSOR CONTROL DEVICE)

CSANASA

AVUInterface Plane

J3P2

AVU

CONNECTOR

Insert ArrangementInsert 13–35 Per

SSQ 21635

1

15

22

21

14

+Y

+X

–Y

–X

CONNECTOR LOCATION

CONNECTOR ID – AVU (CURSOR CONTROL DEVICE)

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

NA

Ref. Des P2 Part Number NATC06G13N35SN Wire HarnessNumber

LAS5–W1186

LAP5–W1286



AWG SignalDestination

SignalSource

Notes

1 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–




10 NOT USED


C3–13

TABLE C3.4.1.1–3 DETAILED ELECTRICAL DESCRIPTION OF AVU 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–







19 RESERVED FOR ORBITER AP-PLICATION





C3–14

TABLE C3.4.1.1–4 DETAILED ELECTRICAL DESCRIPTION OF AVU CONNECTOR J4(VIDEO)

CSANASA

AVUInterface Plane

J4P2

AVU

CONNECTOR

Insert ArrangementInsert 15–35 Per

SSQ 21635

1

2131

+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



AWG SignalSource

SignalDestination

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 AVU 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 atthe Power Data Grapple Fixture (PDGF) Mounting Ring mounting surface at the Modules. Theutility interface plane (power, data and video) is defined between the PDGF harness and theModule connector panel. A Video Signal Converter (VSC) is required to convert the PFM fiberoptic video from the SSMB to PFM electrical video that is compatible with the PDGF andSpace Station Remote Manipulator System (SSRMS). The interfaces between the VSC and themodules 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 thePDGF and PDGF harness for the United States Laboratory (USL) and Hab. NASA isresponsible for development of the USL and Hab. National Space Development Agency ofJapan (NASDA) is responsible for development of the Japanese Experiment Module –Pressurized Module (JEM–PM) and procurement of the PDGF and PDGF harness for theJEM–PM.

D3.1.3 ENGINEERING UNITS AND TOLERANCES

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

D3.2 STRUCTURAL/MECHANICAL INTERFACES

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


D3 – 2

D3.2.1 USL MODULE PDGF LOCATION

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

D3.2.2 HAB MODULE PDGF LOCATION

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 JEM–PM at the location defined in SSP 42000, Figure3.8.1.1.1–1. The PDGF connector panel location on the JEM–PM will be as shown in SSP42000, Figure 3.8.2.1.1–1.

D3.2.4 DELETED

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 asdefined in Figures D3.4–1 through D3.4–6. The SSRMS Backup Drive power and datainterfaces are provided by USL and Hab modules only.

D3.4.1 POWER RETURN AND GROUNDING INTERFACES

The Modules will provide power return and grounding interfaces to the SSRMS via the PDGF asdefined in Figures D3.4–1 through D3.4–6.


D3 – 3

The Module PDGF external wiring diagram is defined in Figure D3.4.1–1.

D3.4.2 DELETED

D3.4.2.1 USL POWER CONNECTORS AND PIN ASSIGNMENTS

The PDGF harness power connectors and pin assignments for the USL module will be as definedin Tables D3.4.2.1–1 through D3.4.2.1–3.

D3.4.2.2 HAB POWER CONNECTORS AND PIN ASSIGNMENTS

The PDGF harness power connectors and pin assignments for the Hab module will be as definedin Tables D3.4.2.2–1 through D3.4.2.2–3.

D3.4.2.3 JEM–PM POWER CONNECTORS AND PIN ASSIGNMENTS

The PDGF harness power connectors and pin assignments for the JEM–PM will be as defined inTables D3.4.2.3–1 through D3.4.2.3–2.

D3.4.2.4 DELETED

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

The USL, Hab, and JEM–PM will support data, PFM sync and control and video interfacesbetween the SSMB and the SSRMS via the PDGF. PFM sync and control and video will betransmitted and received by copper lines between the VSC and the SSRMS. The PFM FiberOptic video from the Modules will be converted to copper for the PDGF by the VSC.

D3.4.4 DATA AND VIDEO CONNECTORS AND PIN ASSIGNMENTS

D3.4.4.1 USL DATA AND VIDEO CONNECTORS AND PIN ASSIGNMENTS

The PDGF harness data and video connectors and pin assignments for the USL module will beas defined in Tables D3.4.4.1–1 through D3.4.4.1–5.


D3 – 4

D3.4.4.2 HAB DATA AND VIDEO CONNECTORS AND PIN ASSIGNMENTS

The PDGF harness data and video connectors and pin assignments for the Hab module will be asdefined in Tables D3.4.4.2–1 through D3.4.4.2–3.

D3.4.4.3 JEM–PM DATA AND VIDEO CONNECTORS AND PIN ASSIGNMENTS

The PDGF harness data and video connectors and pin assignments for the JEM–PM will be asdefined in Tables D3.4.4.3–1 through D3.4.4.3–3.

D3.4.4.4 DELETED

D3.5 ENVIRONMENTS

The PDGF to Modules electromagnetic, grounding and bonding interface implementation will beas defined in SSP 42004, Part 2, Figures A3.2–1 through A3.2–3.

D3.6 SOFTWARE INTERFACES

There are no software interfaces between the PDGF and the Modules.

D3.7 SSRMS EVA HARDWARE LOCATIONS

The SSRMS will provide EVA hardware locations as defined in Figure D3.7–1.

SS

P 42003, P

art 2, Revision A

SS

MB

to MS

S IC

DM

ay 22, 1997

D3 – 5

PDGF and ConnectorPanel Location

PDGF DATA

Radius = 90.6”Angle = 52.5o

12.00”36.20”

56.20”

USL Cof FWD MID Ring

Keel Pin

Forward

Nadir

Nadir

Starboard

FIGURE D3.2.1–1 PDGF LOCATION ON USL


D3 – 6

(TBD#8)

FIGURE D3.2.2–1 PDGF LOCATION ON US HAB


D3 – 7

FIGURE D3.2.4–1 DELETED


D3 – 8

MSS PDGF LB A INMSS PDGF LB A OUT

VIDEO PDGF – 1

VIDEO PDGF – 3

SYNC PDGF – 1

ÃÃÃÃ

J304

PDGF LOWERCONNECTOR PANEL

S0 / LAB / LDACONNECTOR PANEL

ÃÃ

J300

ÃÃÃ

ÃÃÃ

J302

ÃÃÃ

ÃÃÃ

J303

ÃÃÃ

ÃÃÃ

J301

PG–3

P111

P109

P110

P108

P454

P450

P453

P451

W9151

W9152

W9251

W9252

PG–1 CSAFWD PORTDEBRIS SHIELD

VIDEO PDGF – 2

SSRMS 1 Power & Return

(RIGID UMBILICAL)

MSS PDGF LB B OUT

NOTE: The Launch Deployment Assembly (LDA) is installed onthe Lab Cradle Assembly (LCA).

ÃÃÃJ407

ÃÃÃÃ

J404

ÃÃÃ

J400

ÃÃÃJ402

ÃÃÃ

ÃÃÃ

J403

ÃÃÃÃ

J401

ÃÃÃJ406

ÃÃÃÃ

J111

ÃÃÃÃ

J109

ÃÃÃÃ

J110

ÃÃÃÃ

J108

Ground

Ground

SYNC PDGF – 2

MSS PDGF LB B IN

P300

P301

P303

P304

vscORU

J1 J4

J1

J2

J3

J4

FSEGF

2

1

2

1

*Payload 1 Pwr and Rtn

P400

P401

P402

P403

P404

P407

P406


1 TSP

*1 TSP

1 Fiber

1 Fiber

1 Fiber

1 Fiber

1 Fiber

1 TSP

*1 TSP

*Payload 2 Pwr and Rtn

*SSRMS BUD Pwr and Rtn

*Ground

*2 TSP *3 TSP

6A1 – The FSEGFpower, data, and video utilities are routed from

the PG1 Rigid Umbilical via the Lab Fwd Port Debris Shield

LAB

LEGEND

* Unused in this configuration

J405J305*1 Fiber

*1 TSP MSS BUD LB A

Bus Coupler

& Terminator

Bus Coupler

& Terminator

*1 TSPMSS BUD LB B

Interface Plane

P1 P4

J2 J3

P2 P3

RPCM25A

Type VI

RPCM25A

Type VI

FIGURE D3.4–1 LAB EXTERNAL HARNESSES AND INTERFACES (FLIGHT 6A 1)

SSP 42003, Part 2, Revision A SSMB to MSS I CMay 22, 1997

D3 – 9

J304



J300

J302

J303

J301

PG–3

P109

P110

P450

P453

P451

W9151

W9152

W9251

PG–1FWD PORTDEBRIS SHIELD

(RIGID UMBILICAL)

NOTE: 6A2 – The SSRMS has walked on to the Lab PDGF. Removed & Stowed

LEGEND

ÃÃÃ

ÃÃÃ

J400

ÃÃÃJ407

ÃÃÃ

ÃÃÃ

J402

ÃÃÃJ403

ÃÃÃJ401

ÃÃÃJ406

ÃÃÃÃ

J109

ÃÃJ110

P1

P9

P11

P3

LAB


Ground

Ground


P108ÃÃJ108

2

1

2

1

P402

MSS PDGF LB A IN

MSS PDGF LB A OUT

VIDEO PDGF – 1

VIDEO PDGF – 3

SYNC PDGF – 1

1 TSP

1 Fiber

1 Fiber

*1 Fiber

P111 P454W9252

VIDEO PDGF – 2

MSS PDGF LB B OUT

ÃÃÃ

ÃÃÃ

J404ÃÃÃÃ

J111

SYNC PDGF – 2

MSS PDGF LB B IN

P71 Fiber

1 Fiber

1 TSP

1 TSP

P403

P404

*3 Fiber

*2 TSP

*2 Fiber

*2 TSP

*2 TSP *3 TSP

P407

P406

P400

P401

The Lab PDGF power, data, and video utilities are routed fromthe PG1 Rigid Umbilical.


1 TSP

*5 Power lines

*5 Power lines

J405P5 J305

*1 Fiber

*3 Power lines

*1 TSP

Interface Plane

RPCM25A

Type VI

RPCM25A

Type VI

VSCJ4

J1

BC#1

J5 LAB PDGF

MSS BUD LB B

BC#2

J6J8J7

1 TSP

2 TSP 2 TSP

1 TSP

To VSCJ2

To VSCJ3

FIGURE D3.4–2 LAB EXTERNAL HARNESS AND INTERFACES (FLT 6A 2 – 8A)


D3 – 10



J300

J302

PG–3

P111

P109

P110

P108

P454

P450

P453

P451

W9151

W9152

W9251

W9252

PG–1

FWD PORTDEBRIS SHIELD

SPARTO PDGF INTERFACE

(RIGID UMBILICAL)

*3 Fiber lines

*2 Fiber lines

NOTE: The Lab PDGF power and video utilities are routed from S0

ÃÃÃÃ

J111

ÃÃJ109

ÃÃÃÃ

J110

ÃÃJ108

ÃÃÃ

ÃÃÃ

J407

ÃÃÃ

ÃÃÃ

J400

ÃÃÃJ402

ÃÃÃ

ÃÃÃ

J406

P1

P11

LAB

Removed & Stowed

LEGEND


S0


Ground (Fault)

Payload 1 Power & Return

P400

J301ÃÃÃ

ÃÃÃ

J401P9


Ground (Fault)

Payload 2 Power & Return

P401

BUD Power & Return

*Ground (Fault)

P402

J304

J303

P7

P3

ÃÃÃÃ

J404

ÃÃÃ

ÃÃÃ

J403 P403

P404

*2 TSP

1 Fiber

1 Fiber

*1 Fiber

1 Fiber

1 Fiber

*2 TSP

VIDEO PDGF – 1

SYNC PDGF – 1

VIDEO PDGF – 2

SYNC PDGF – 2

MSS PDGF LB A IN

MSS PDGF LB A OUT

MSS PDGF LB B OUT

MSS PDGF LB B IN

MSS BUD LB A

1 TSP

1 TSP

1 TSP

1 TSP

1 TSP

P407

P406

1553 continues to be routed from the PG1 RigidUmbilical via the Lab

VIDEO PDGF – 3

P5 J405 J3051 Fiber

Interface Plane

MSS BUD LB B * 1 TSP

RPCM25A

Type II

RPCM12A

Type V

RPCM25A

Type II

FIGURE D3.4–3 LAB EXTERNAL HARNESSES AND INTERFACES (FLT 8A–AC)


D3 – 11

BCLB MSS – PDGF B 1 TSP

1 TSP

Sync and Control 2 1 Fiber Optic

1 Fiber OpticVideo Channel 2

Video Channel 3 1 Fiber Optic

S0Harnesses

and Connectors

HABHarnesses

and Connectors

SPDARPCM25A

Type II

SSRMS 1

Payload 1

8ga

8ga

2

2

18ga

Green Wire

12ga12ga

12ga12ga

2

2

2

2

12ga 1

RPCM12A

Type V

SPDA Backup Power 12ga2

20ga 2

LB MSS – PDGF A

Video Channel 1

Sync & Control 1

1 TSP

1 TSP

1 Fiber Optic

1 Fiber Optic

PDGF Harnessand Connectors

HAB

PDGFBC

RPCM25A

Type II

8ga

8ga

2

2

SSRMS 2

Payload 2

SPDA

12ga

12ga

12ga

12ga

2

2

2

2

18gaGreen Wire 12ga 1

HAB Connectors

CSA Connectors

PDGFConnector

Panel

HAB to PDGFInterface

Plane

NODE 1/HABInterface

Plane(See SSP 41140)

12ga

8 ga

8 ga

8 ga

8 ga

8 ga

8 ga

To VSC J2

ÉÉ

ÏÏÏÏÏ

ÏÏÏÏÏ

ÏÏÏÏ

ÏÏÏÏÏÏÏÏ

ÏÏÏÏÏÏ

1

Green Wire

VSC

To VSC J2

J5

To VSC J3

J2 J3Power In

J1 J4

J400

J401

J402

J403

J404

J7

J8

J6

To VSC J3

P102

P106

Hab/S0

S0 to HabInterface

Plane*

J102

P109 J109

J106

1 TSPLB MSS BD B

P104 J104

ÏÏ

P111 J111

J405

P107 J107

S0

S0

S0

S0

S0

S0

Node1

Node1

* See SSP 42137

FIGURE D3.4–4 US HAB TO PDGF ELECTRICAL SYSTEM DIAGRAM


D3 – 12

FIGURE D3.4–5 DELETED


D3 – 13

BCLB MSS – PDGF B 1 TSP

1 TSP

Sync and Control 2 1 Fiber Optic

1 Fiber OpticVideo Channel 2

1 TSP1 TSP

Video Channel 3 1 Fiber Optic

NODE 2Harnesses

and Connectors

JEM–PMHarnesses

and Connectors

SPDARPCM25A

Type II

SSRMS 1

Payload 1

8ga

8ga

2

2

18ga

12ga12ga

12ga12ga

2

2

2

2

12ga 1

20ga 2

LB MSS – PDGF A

Video Channel 1

Sync & Control 1

1 TSP

1 TSP

1 Fiber Optic

1 Fiber Optic

PDGF Harnessand Connectors

JEM

PDGF

BC

RPCM25A

Type II

8ga

8ga

2

2

SSRMS 2

Payload 2

SPDA

12ga

12ga

12ga

12ga

2

2

2

2

18gaGreen Wire 12ga 1

JEM–PM Connectors

CSA Connectors

JEM–PM/NODE 2Connector

Panel

PDGFConnector

Panel

JEM–PM to PDGFInterface

Plane

NODE 2/JEM–PMInterface

Plane(See SSP 42000)

8 ga

8 ga

8 ga

8 ga

8 ga

8 ga

To VSC J2

ÉÉ

ÏÏÏÏÏ

ÏÏÏÏÏ

ÏÏÏÏ

ÏÏÏÏÏÏÏÏ

ÏÏÏÏÏÏ

Green Wire

VSC

To VSC J2

J5

To VSC J3

J2 J3Power In

J1 J4

J400

J401

J402

J403

J404

J7

J8

J6

To VSC J3

ÏÏÏ

J405

FIGURE D3.4–6 JEM–PM TO PDGF ELECTRICAL SYSTEM DIAGRAM

SSMB to MSS ICDSSP 42003, Part 2, Revision A

May 22, 1997

D3–14

34

36

47

44

G

22 AWG

MSS LOCAL BUS B (L)

MSS LOCAL BUS B (H)

VIDEO COMPOSITE SYNC 2

VIDEO CHANNEL 3

36

35

34

44

47

VIDEO COMPOSITE SYNC 1

VIDEO CHANNEL 2

VIDEO CHANNEL 1

MSS LOCAL BUS A (H) MSS LOCAL BUS A (L)

SSRMS POWER BUS 2 RETURN

SSRMS POWER BUS 2


SSRMS POWER BUS 1

PAYLOAD POWER BUS 1

PAYLOAD POWER BUS 1 RETURN

PAYLOAD POWER BUS 2

PAYLOAD POWER BUS 2 RETURN12 AWG

12 AWG

12 AWG

12 AWG

35

52

51

50

49

22

21

201912 AWG

12 AWG 19

20

21

22

49

50

51

52

35

12 AWG

12 AWG

12 AWG

12 AWGPAYLOAD POWER BUS 2 RETURN

PAYLOAD POWER BUS 2

SSRMS POWER BUS 2


D

B

A

F

E

J3

W1P14

J2

C

PIN 51617–0044–1

W1P4

INTERFACE PLANEUSER TO PDGF

22 AWG

8 AWG

8 AWG

F

B

C

A

A

C

B

F

G

8 AWG

8 AWG

8 AWG

8 AWG

FIBER OPTIC

FIBER OPTIC

FIBER OPTIC

FIBER OPTIC

E A E ACW1P13

NOTES:1 INTERPRET DRAWING PER DOD–STD–100.

P

P

P

P

W1P12J4

B

C

H

D

J1W1P6

P

P

P

P

E1

E2

E3

E4

E8

E7

E5

E6

E9

E10

20A

WG

20A

WG

20A

WG

20A

WG

P P20 AWG

P

22AWG

22AWG

22AWG

22AWG

MATING CONNECTOR J403






A

FIBER OPTIC

BC#1

BC#2

39

40

W1P8

W1P2

SSRMS POWER BUS 1


PAYLOAD POWER BUS 1

PAYLOAD POWER BUS 1 RETURN

SSRMS GROUND

W1P10

W1P3

AB

CD

t

f

W1P5

W1P7

t

f

A

B

C

D

W1P1

W1P9

W1P11

BACKUP 1553 BUS (L)BACKUP 1553 BUS (H)22 AWG 42

46

E

F

SSRMS GROUND

P

N

d

P

P

P

P

VIDEO SIGNAL CONVERTER (VSC)

NDBC3B1A

NDBC3B1A

RD316

RD316

RD316

RD316

RD316

J7

J8

J6

J5

BACKUP POWER BUS

BACKUP POWER BUS RETURN

PDGF

W01–008A

W01–009A

W01–010A

W01–007C–WHTW01–007C–GRN

W01–110A

W01–109A

W01–107C–WHT

W01–107C–GRN

W01–001B–WHT

W01–001B–BLU

W01–001C–BLU

W01–001C–WHT

W01–002B–BLU

W01–002B–WHT

W01–002C–BLU

W01–002C–WHT

W01–101B–BLU

W01–101B–WHT

W01–101C–BLU

W01–101C–WHT

W01–102B–BLU

W01–102B–WHT

W01–102C–BLU

W01–102C–WHT

W01–103B–WHT

W01–003B–WHT

W01–102A–WHT

W01–102A–BLU

W01–103A–WHT

W01–104A–WHT

W01–104A–BLU

W01–101A–BLU

W01–101A–WHT

W01–003A–WHT

W01–002A–BLU

W01–002A–WHT

W01–001A–BLU

W01–001A–WHT

W01–108A–GRN

W01–108A–WHT

W01–107A–GRN

W01–107A–WHT

W01–107B–GRN

W01–107B–WHT

BUS STUB

BUS

W01–105A

W01–106A

W01–006A

W01–005A

W01–004A

W01–007B–WHT

W01–007B–GRN

VIDEO 1

SYNC A

SYNC B

VIDEO 3

VIDEO 2

CH

AS

SIS

GR

OU

ND

120V

RE

DU

ND

AN

T P

OW

ER

RE

TU

RN

120V

RE

DU

ND

AN

T P

OW

ER

CH

AS

SIS

GR

OU

ND

120V

PR

IME

PO

WE

R R

ET

UR

N

120V

PR

IME

PO

WE

R

VIDEO CHANNEL 1

VIDEO CHANNEL 2

SYNC CHANNEL 1

VIDEO CHANNEL 3

SYNC CHANNEL 2

W01–007A–WHT

W01–007A–GRNMSS LOCAL BUSPRIME (IN)

MSS LOCAL BUSPRIME (OUT)

VIDEO & SYNCCHANNELS



REDUNDANT (IN)MSS LOCAL BUS

REDUNDANT (OUT)MSS LOCAL BUS

1553 BUSSSRMS BACKUP DRIVE

SSRMS POWER(PRIME)

POWER (PRIME)SSRMS PAYLOAD

SSRMS GROUND(PRIME)

(REDUNDANT)SSRMS POWER

SSRMS PAYLOADPOWER (REDUNDANT)

SSRMS GROUND(REDUNDANT)

DRIVE POWERSSRMS BACKUP

W01

–103

C–W

HT

W01

–101

D–B

LU

W01

–101

D–W

HT

W01

–003

C–W

HT

W01

–001

D–B

LU

W01

–001

D–W

HT

BUS STUB

BUS PIN 51612–0002–1

DO NOT SCALE DRAWING

W01–108A–WHT

W01–108A–GRN

FIGURE D3.4.1–1 PDGF EXTERNAL WIRING DIAGRAM


D3 – 15

TABLE D3.4.2.1–1 DETAILED ELECTRICAL DESCRIPTION OF LAB PDGF CONNECTORJ400 (PRIME POWER) (PAGE 1 OF 2)

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

CONNECTOR LOCATIONÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

CONNECTOR ID PDGF (PRIME POWER)ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Ref. DesÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

J400ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Part NumberÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

NZGL77H2525LN7PPNÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

ReceptacleInstallationDrawingNumber

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

683–22090

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ


P400ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ


NZGL66G2525LN7SNÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Wire HarnessDrawingNumber


683–22091

ÁÁÁÁÁÁÁÁÁÁÁÁ

Ref. DesÁÁÁÁÁÁÁÁÁÁÁÁ

P450ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Part NumberÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

NZGL06G2525LN7SNÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ



1F75334–1








51618–1007

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁPIN FUNCTION TABLE (6A1 Configuration)ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Cont

ID (P450)

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Cont

ID (P400)


Signal Function

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

EMC

Class

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

AWG

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁNotes

ÁÁÁÁÁÁÁÁA ÁÁÁÁÁ

ÁÁÁÁÁA ÁÁÁÁÁÁÁÁ

ÁÁÁÁÁÁÁÁFAULT RTN ÁÁÁ

ÁÁÁEOÁÁÁÁÁÁÁÁ

8 ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁÁN/A ÁÁÁÁÁ

ÁÁÁÁÁE ÁÁÁÁÁÁÁÁ

ÁÁÁÁÁÁÁÁPDGFPL1LAB ÁÁÁ


8 ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁNOT USED IN P450

ÁÁÁÁÁÁÁÁN/A ÁÁÁÁÁ

ÁÁÁÁÁD ÁÁÁÁÁÁÁÁ

ÁÁÁÁÁÁÁÁPDGFPL1LAB RTN ÁÁÁ


8 ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁNOT USED IN P450


FÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

FÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

PDGFSSRMS1LAB

RTN

ÁÁÁÁÁÁÁÁÁ

EOÁÁÁÁÁÁÁÁÁÁÁÁ

8ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁÁG

ÁÁÁÁÁÁÁÁÁÁ

GÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

PDGFSSRMS1LABÁÁÁÁÁÁ

EOÁÁÁÁÁÁÁÁ

8ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ


D3 – 16

TABLE D3.4.2.1–1 DETAILED ELECTRICAL DESCRIPTION OF LAB PDGF CONNECTORJ400 (PRIME POWER) (PAGE 2 OF 2)

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

PIN FUNCTION TABLE 6A2 – 8A Configuration)


Cont

ID (P450)


Cont

ID (P1)

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Signal FunctionÁÁÁÁÁÁÁÁÁÁÁÁ

EMC

Class


AWG


Notes


A ÁÁÁÁÁÁÁÁÁÁ

A ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁFAULT RTN ÁÁÁ

ÁÁÁEO ÁÁÁÁÁÁ

8 ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁÁÁN/A ÁÁÁÁÁ

ÁÁÁÁÁB ÁÁÁÁÁÁÁÁÁ

ÁÁÁÁÁÁÁÁÁPDGFPL1LAB ÁÁÁ


8 ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

NOT USED IN P450ÁÁÁÁÁÁÁÁÁÁ

N/AÁÁÁÁÁÁÁÁÁÁ

CÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁPDGFPL1LAB RTN ÁÁÁ

ÁÁÁEOÁÁÁÁÁÁ


NOT USED IN P450ÁÁÁÁÁÁÁÁÁÁF

ÁÁÁÁÁÁÁÁÁÁF

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁPDGFSSRMS1LAB RTN

ÁÁÁÁÁÁEOÁÁÁÁÁÁ8ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ


GÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

GÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

PDGFSSRMS1LABÁÁÁÁÁÁÁÁÁ

EOÁÁÁÁÁÁÁÁÁ

8ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

PIN FUNCTION TABLE (8A – AC Configuration)ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Cont

ID (P1)


Cont

ID (P400)


Signal Function


EMC

Class

ÁÁÁÁÁÁÁÁÁÁÁÁAWG

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁNotesÁÁÁÁÁ


AÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

FÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

FAULT RTNÁÁÁÁÁÁÁÁÁ


8ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁÁÁB ÁÁÁÁÁ

ÁÁÁÁÁE ÁÁÁÁÁÁÁÁÁ




NOT USED IN P450


C ÁÁÁÁÁÁÁÁÁÁ

D ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁPDGFPL1LAB RTN ÁÁÁ




F ÁÁÁÁÁÁÁÁÁÁ

A ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁPDGFSSRMS1LAB RTN ÁÁÁ



ÁÁÁÁÁG ÁÁÁÁÁ

ÁÁÁÁÁG ÁÁÁÁÁÁÁÁÁ

ÁÁÁÁÁÁÁÁÁPDGFSSRMS1LAB ÁÁÁ




D3 – 17

TABLE D3.4.2.1–2 DETAILED ELECTRICAL DESCRIPTION OF LAB PDGF CONNECTORJ401 (REDUNDANT POWER) (PAGE 1 0F 2)



CONNECTOR ID – PDGF (REDUNDANT POWER)



J401ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Part NumberÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

NZGL77H2525LN7PPAÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ



683–22090



P401ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ


NZGL66G2525LN7SAÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ



683–22092



P451ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Part NumberÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

NZGL06G2525LN7SAÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ



1F75338–1








51618–1007


PIN FUNCTION TABLE (6A1 Configuration)ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Cont

ID (P451)

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Cont

ID (P401)

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Signal Function


EMC

Class


AWG


Notes



A ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

FAULT RTN ÁÁÁÁÁÁEO ÁÁÁÁÁÁ







NOT USED IN P451


N/A ÁÁÁÁÁÁÁÁÁÁ






F ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁPDGFSSRMS2LAB RTN ÁÁÁ









D3 – 18

TABLE D3.4.2.1–2 DETAILED ELECTRICAL DESCRIPTION OF LAB PDGF CONNECTORJ401 (REDUNDANT POWER) (PAGE 2 0F 2)

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

PIN FUNCTION TABLE 6A2 – 8A Configuration)


Cont

ID (P451)


Cont

ID (P9)


Signal FunctionÁÁÁÁÁÁÁÁÁÁÁÁ

EMC

Class


AWG


Notes



A ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁFAULT RTN ÁÁÁ




ÁÁÁÁÁB ÁÁÁÁÁÁÁÁÁ





N/AÁÁÁÁÁÁÁÁÁÁ

CÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁPDGFPL2LAB RTN ÁÁÁ

ÁÁÁEOÁÁÁÁÁÁ


NOT USED IN P451ÁÁÁÁÁÁÁÁÁÁF

ÁÁÁÁÁÁÁÁÁÁF

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁPDGFSSRMS2LAB RTN

ÁÁÁÁÁÁEOÁÁÁÁÁÁ8ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ



GÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

PDGFSSRMS2LABÁÁÁÁÁÁÁÁÁ




PIN FUNCTION TABLE (8A – AC Configuration)ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Cont

ID (P9)


Cont

ID (P401)


Signal Function


EMC

Class

ÁÁÁÁÁÁÁÁÁÁÁÁAWG

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁNotesÁÁÁÁÁ


AÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

FÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

FAULT RTNÁÁÁÁÁÁÁÁÁ


8ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁÁÁB ÁÁÁÁÁ





NOT USED IN P451


C ÁÁÁÁÁÁÁÁÁÁ






A ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁPDGFSSRMS2LAB RTN ÁÁÁ









D3 – 19

TABLE D3.4.2.1–3 DETAILED ELECTRICAL DESCRIPTION OF LAB PDGF CONNECTORJ402 (BACKUP DRIVE POWER)


CONNECTOR LOCATION

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

CONNECTOR ID – PDGF (BACKUP DRIVE POWER)ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Ref. DesÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

J402ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Part NumberÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

NZGL77H2525N19PPBÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ



683–22090


Ref. DesÁÁÁÁÁÁÁÁÁ



NZGL66G2525N19SBÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ


ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

683–22093





NZGL66G2525N19SBÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ



51618–1007

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

PIN FUNCTION TABLEÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

ContID

(P402)


ContID

(P11)


Signal FunctionÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

EMCClass


AWG*ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Notes

ÁÁÁÁÁÁÁÁ

N ÁÁÁÁÁÁ

P ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

SSRMS BUD PWRÁÁÁÁÁÁÁÁ

EO ÁÁÁÁÁÁÁÁ


ÁÁÁÁP ÁÁÁÁÁÁ

N ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

SSRMS BUD RTN ÁÁÁÁÁÁÁÁ

EO ÁÁÁÁÁÁÁÁ


ÁÁÁÁV ÁÁÁÁÁÁ

NAÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

FAULT RTN ÁÁÁÁÁÁÁÁ

EO ÁÁÁÁÁÁÁÁ

12 ÁÁÁÁÁÁÁÁÁÁÁÁ

not used in P11

* SPAR harness has 20 AWG wires


D3 – 20

TABLE D3.4.2.2–1 DETAILED ELECTRICAL DESCRIPTION OF HAB PDGF CONNECTORJ400 (PRIME POWER)



CONNECTOR ID PDGF (PRIME POWER)








683–22090








683–22091



P1 ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ





51618–1007


PIN FUNCTION TABLE


Cont

ID (P1)


Cont

ID (P400)

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Signal Function ÁÁÁÁÁÁÁÁÁ

EMC

ClassÁÁÁÁÁÁÁÁÁÁÁÁ

AWGÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Notes

ÁÁÁÁÁÁÁÁ

AÁÁÁÁÁÁÁÁÁÁ

FÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

FAULT RTNÁÁÁÁÁÁ

EOÁÁÁÁÁÁÁÁ

8ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁÁÁÁÁÁ

BÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

EÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

PDGFPL1HABÁÁÁÁÁÁÁÁÁ



ÁÁÁÁC ÁÁÁÁÁ

ÁÁÁÁÁD ÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁÁÁÁÁÁÁÁÁÁÁPDGFPL1HAB RTN ÁÁÁ



ÁÁÁÁF ÁÁÁÁÁ

ÁÁÁÁÁA ÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁÁÁÁÁÁÁÁÁÁÁPDGFSSRMS1HAB RTN ÁÁÁ



ÁÁÁÁG ÁÁÁÁÁ

ÁÁÁÁÁG ÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁÁÁÁÁÁÁÁÁÁÁPDGFSSRMS1HAB ÁÁÁ




D3 – 21

TABLE D3.4.2.2–2 DETAILED ELECTRICAL DESCRIPTION OF HAB PDGF CONNECTORJ401 (REDUNDANT POWER)

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁCONNECTOR LOCATIONÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

CONNECTOR ID – PDGF (REDUNDANT POWER)ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Ref. DesÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ


Part NumberÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

NZGL77H2525LN7PPAÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ



683–22090








683–22092








51618–1007



Cont

ID (P9)


Cont

ID (P401)

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Signal Function ÁÁÁÁÁÁÁÁÁÁÁÁ

EMC

Class


AWGÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Notes

ÁÁÁÁÁÁÁÁ


F ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

FAULT RTN ÁÁÁÁÁÁ

EOÁÁÁÁÁÁÁÁ


ÁÁÁÁB ÁÁÁÁÁ

ÁÁÁÁÁE ÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁÁÁÁÁÁÁÁÁÁÁPDGFPL2HAB ÁÁÁ








ÁÁÁÁF


AÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

PDGFSSRMS2HAB RTNÁÁÁÁÁÁ

EOÁÁÁÁÁÁÁÁ


ÁÁÁÁÁÁÁÁ


GÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

PDGFSSRMS2HABÁÁÁÁÁÁÁÁÁ




D3 – 22

TABLE D3.4.2.2–3 DETAILED ELECTRICAL DESCRIPTION OF HAB PDGF CONNECTORJ402 (BACKUP DRIVE POWER)


CONNECTOR LOCATIONÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

CONNECTOR ID – PDGF (BACKUP DRIVE POWER)



J402ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ


NZGL77H2525N19PPBÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ



683–22090





NZGL66G2525N19SBÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ



683–22093





NZGL66G2525N19SBÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ



51618–1007


PIN FUNCTION TABLEÁÁÁÁÁÁÁÁÁÁÁÁ

ContID (P402)


ContID (P11)



EMCClassÁÁÁÁÁÁÁÁÁÁÁÁ

AWG *ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Notes

ÁÁÁÁÁÁÁÁ

N ÁÁÁÁÁÁÁÁÁÁ

P ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

SSRMS BUD PWR ÁÁÁÁÁÁÁÁ

EO ÁÁÁÁÁÁÁÁ


ÁÁÁÁP ÁÁÁÁÁÁÁÁÁÁ

N ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

SSRMS BUD RTN ÁÁÁÁÁÁÁÁ

EO ÁÁÁÁÁÁÁÁ


ÁÁÁÁV ÁÁÁÁÁÁÁÁÁÁ

NA ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

FAULT RTN ÁÁÁÁÁÁÁÁ

EO ÁÁÁÁÁÁÁÁ


not used in P11

* SPAR harness has 20 AWG wires


D3 – 23

TABLE D3.4.2.3–1 DETAILED ELECTRICAL DESCRIPTION OF JEM PDGF CONNECTORJ400 (PRIME POWER)



CONNECTOR ID PDGF (PRIME POWER)








TBD








TBD



P1 ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ





51618–1007


PIN FUNCTION TABLE


Cont

ID (P1)


Cont

ID (P400)

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ


EMC

ClassÁÁÁÁÁÁÁÁÁÁÁÁ


Notes

ÁÁÁÁÁÁÁÁ

AÁÁÁÁÁÁÁÁÁÁ

FÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

FAULT RTNÁÁÁÁÁÁ

EOÁÁÁÁÁÁÁÁ


ÁÁÁÁÁÁÁÁ

BÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

EÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

PDGFPL1HABÁÁÁÁÁÁÁÁÁ








ÁÁÁÁF ÁÁÁÁÁ

ÁÁÁÁÁA ÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁÁÁÁÁÁÁÁÁÁÁPDGFSSRMS1HAB RTN ÁÁÁ



ÁÁÁÁG ÁÁÁÁÁ

ÁÁÁÁÁG ÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁÁÁÁÁÁÁÁÁÁÁPDGFSSRMS1HAB ÁÁÁ




D3 – 24

TABLE D3.4.2.3–2 DETAILED ELECTRICAL DESCRIPTION OF JEM PDGF CONNECTORJ401 (REDUNDANT POWER)


CONNECTOR ID – PDGF (REDUNDANT POWER)ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ



Part NumberÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

NZGL77H2525LN7PPAÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ



TBD








TBD








51618–1007



Cont

ID (P9)


Cont

ID (P401)

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ


EMC

Class



Notes

ÁÁÁÁÁÁÁÁ


F ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ


EOÁÁÁÁÁÁÁÁ


ÁÁÁÁB ÁÁÁÁÁ

ÁÁÁÁÁE ÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁÁÁÁÁÁÁÁÁÁÁPDGFPL2HAB ÁÁÁ








ÁÁÁÁF


AÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

PDGFSSRMS2HAB RTNÁÁÁÁÁÁ

EOÁÁÁÁÁÁÁÁ


ÁÁÁÁÁÁÁÁ


GÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

PDGFSSRMS2HABÁÁÁÁÁÁÁÁÁ




D3 – 25

TABLE D3.4.4.1–1 DETAILED ELECTRICAL DESCRIPTION OF LAB PDGF CONNECTORJ403 (1553 & VIDEO) (PAGE 1 OF 3)

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁCONNECTOR LOCATIONÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

CONNECTOR ID – PDGF (1553 & VIDEO)ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ




NZGL77H2525N43PPC4ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ



683–22090





NZGL06G2525N43SCÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ



1F75336–1





NZGL66G2525N43SCÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ



683–22094








51618–1007


D3 – 26


ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

PIN FUNCTION TABLE (6A1 Configuration)

ÁÁÁÁÁÁÁÁÁ

ContID

(P453)


ContID

(P403)




AWGÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Notes

ÁÁÁÁÁÁÁÁÁ

AÁÁÁÁÁÁÁÁÁÁÁÁ

AÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

LB MSS PDGF A HI (IN)ÁÁÁÁÁÁÁÁÁÁÁÁ

RFÁÁÁÁÁÁÁÁÁÁÁÁ

22ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁBÁÁÁÁÁÁÁÁ

B ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

LB MSS PDGF A LO (IN) ÁÁÁÁÁÁÁÁ

RFÁÁÁÁÁÁÁÁ

22 ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁCÁÁÁÁÁÁÁÁ

C ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

LB MSS PDGF A HI (OUT) ÁÁÁÁÁÁÁÁ

RFÁÁÁÁÁÁÁÁ


ÁÁÁDÁÁÁÁÁÁÁÁ

D ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

LB MSS PDGF A LO (OUT)ÁÁÁÁÁÁÁÁ

RFÁÁÁÁÁÁÁÁ


ÁÁÁEÁÁÁÁÁÁÁÁ

E ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

LB MSS BUD A HI ÁÁÁÁÁÁÁÁ

RFÁÁÁÁÁÁÁÁ


not used in this configurationÁÁÁÁÁÁ

FÁÁÁÁÁÁÁÁ

FÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

LB MSS BUD A LOÁÁÁÁÁÁÁÁ

RFÁÁÁÁÁÁÁÁ


not used in this configurationÁÁÁÁÁÁtÁÁÁÁÁÁÁÁt

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁVIDEO PDGF–1

ÁÁÁÁÁÁÁÁN/A

ÁÁÁÁÁÁÁÁFO

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁÁÁÁ

fÁÁÁÁÁÁÁÁÁÁÁÁ

fÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

SYNC PDGF–1ÁÁÁÁÁÁÁÁÁÁÁÁ

N/AÁÁÁÁÁÁÁÁÁÁÁÁ

FOÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁxÁÁÁÁÁÁÁÁ

x ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

VIDEO PDGF–3 ÁÁÁÁÁÁÁÁ

N/AÁÁÁÁÁÁÁÁ

FO ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ


PIN FUNCTION TABLE (6A2 – 8A Configuration)ÁÁÁÁÁÁÁÁÁÁÁÁ

ContID

(P453)


ContID

(P3)



EMCClass


AWGÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Notes

ÁÁÁÁÁÁ

AÁÁÁÁÁÁÁÁ

A ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁLB MSS PDGF A HI (IN) ÁÁÁÁ

ÁÁÁÁRF ÁÁÁÁÁÁÁÁ



BÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁLB MSS PDGF A LO (IN)

ÁÁÁÁÁÁÁÁ

RFÁÁÁÁÁÁÁÁ

22ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁCÁÁÁÁÁÁÁÁC

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁLB MSS PDGF A HI (OUT)

ÁÁÁÁÁÁÁÁRF

ÁÁÁÁÁÁÁÁ22


ÁÁÁÁÁÁ

DÁÁÁÁÁÁÁÁÁÁÁÁ

DÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

LB MSS PDGF A LO (OUT)ÁÁÁÁÁÁÁÁÁÁÁÁ




E ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁLB MSS BUD A HI ÁÁÁÁ



Reserved

ÁÁÁÁÁÁ

FÁÁÁÁÁÁÁÁ

F ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁLB MSS BUD A LO ÁÁÁÁ



ReservedÁÁÁÁÁÁ

tÁÁÁÁÁÁÁÁ

t ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁVIDEO PDGF–1 ÁÁÁÁ

ÁÁÁÁN/A ÁÁÁÁÁÁÁÁ

FO ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁfÁÁÁÁÁÁÁÁ

f ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁSYNC PDGF–1 ÁÁÁÁ



ÁÁÁxÁÁÁÁÁÁÁÁN/A


ÁÁÁÁÁÁÁÁN/A

ÁÁÁÁÁÁÁÁFO

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁnot used in P3


D3 – 27



PIN FUNCTION TABLE (8A – AC Configuration)

ÁÁÁÁÁÁÁÁÁ

ContID

(P3)


ContID

(P403)




AWG ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Notes

ÁÁÁÁÁÁÁÁÁ


ZÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ




ÁÁÁB ÁÁÁÁÁÁÁÁ

Y ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

LB MSS PDGF A LO (IN) ÁÁÁÁÁÁÁÁ

RF ÁÁÁÁÁÁÁÁ



X ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁLB MSS PDGF A HI (OUT) ÁÁÁÁ




W ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁLB MSS PDGF A LO (OUT) ÁÁÁÁ




V ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁLB MSS BUD A HI ÁÁÁÁ



ÁÁÁFÁÁÁÁÁÁÁÁ

UÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁLB MSS BUD A LO

ÁÁÁÁÁÁÁÁ

RFÁÁÁÁÁÁÁÁ

22ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁtÁÁÁÁÁÁÁÁt


ÁÁÁÁÁÁÁÁN/A

ÁÁÁÁÁÁÁÁFO


ÁÁÁÁÁÁ

fÁÁÁÁÁÁÁÁÁÁÁÁ





ÁÁÁN/AÁÁÁÁÁÁÁÁ

x ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁVIDEO PDGF–3 ÁÁÁÁ



not used in P3


D3 – 28







NZGL77H2525N43PPD4ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ



683–22090





NZGL06G2525N43SDÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ



1F75340–1





NZGL66G2525N43SDÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ



683–22096








51618–1007

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

PIN FUNCTION TABLE (6A1 Configuration)


ContID

(P454)

ÁÁÁÁÁÁÁÁÁ

ContID

(P404)




AWGÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Notes

ÁÁÁÁÁÁÁÁA

ÁÁÁÁÁÁAÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁLB MSS PDGF B HI (IN)

ÁÁÁÁÁÁÁÁRF

ÁÁÁÁÁÁÁÁ22


ÁÁÁÁÁÁÁÁ

BÁÁÁÁÁÁÁÁÁ

BÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

LB MSS PDGF B LO (IN)ÁÁÁÁÁÁÁÁÁÁÁÁ


22ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁÁC ÁÁÁÁÁÁ


LB MSS PDGF B HI (OUT)ÁÁÁÁÁÁÁÁ

RFÁÁÁÁÁÁÁÁ

22 ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁÁD ÁÁÁÁÁÁ


LB MSS PDGF B LO (OUT)ÁÁÁÁÁÁÁÁ

RFÁÁÁÁÁÁÁÁ

22 ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁÁE ÁÁÁÁÁÁ

N/AÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

LB MSS BUD B HI ÁÁÁÁÁÁÁÁ

RFÁÁÁÁÁÁÁÁ

22 ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Not used in P404ÁÁÁÁÁÁÁÁ

F ÁÁÁÁÁÁ

N/AÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

LB MSS BUD B LO ÁÁÁÁÁÁÁÁ

RFÁÁÁÁÁÁÁÁ


Not used in P404ÁÁÁÁÁÁÁÁt

ÁÁÁÁÁÁtÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁVIDEO PDGF–2

ÁÁÁÁÁÁÁÁN/A

ÁÁÁÁÁÁÁÁFO


ÁÁÁÁÁÁÁÁ

fÁÁÁÁÁÁÁÁÁ






D3 – 29



PIN FUNCTION TABLE (6A2 – 8A Configuration)


ContID

(P454)

ÁÁÁÁÁÁÁÁÁ

ContID

(P7)





Notes


AÁÁÁÁÁÁÁÁÁ

AÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

LB MSS PDGF B HI (IN)ÁÁÁÁÁÁÁÁÁÁÁÁ


22ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁÁB ÁÁÁÁÁÁ

B ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

LB MSS PDGF B LO (IN) ÁÁÁÁÁÁÁÁ

RF ÁÁÁÁÁÁÁÁ

22 ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ




RF ÁÁÁÁÁÁÁÁ





RF ÁÁÁÁÁÁÁÁ


ÁÁÁÁt ÁÁÁÁÁÁ

t ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ


N/AÁÁÁÁÁÁÁÁ

FO ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁÁfÁÁÁÁÁÁ

fÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

SYNC PDGF–2ÁÁÁÁÁÁÁÁ

N/AÁÁÁÁÁÁÁÁ

FOÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁÁEÁÁÁÁÁÁN/AÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁLB MSS BUD B HI

ÁÁÁÁÁÁÁÁRF

ÁÁÁÁÁÁÁÁ22

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁNot used in P7ÁÁÁÁ

ÁÁÁÁÁÁÁÁ

FÁÁÁÁÁÁÁÁÁ

N/AÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

LB MSS BUD B LOÁÁÁÁÁÁÁÁÁÁÁÁ


22ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Not used in P7



ContID

(P7)


ContID

(P404)



EMCClass


AWGÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Notes

ÁÁÁÁÁÁ

AÁÁÁÁÁÁÁÁ

Z ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

LB MSS PDGF B HI (IN) ÁÁÁÁÁÁÁÁ

RF ÁÁÁÁÁÁÁÁ





RF ÁÁÁÁÁÁÁÁ


ÁÁÁCÁÁÁÁÁÁÁÁX

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁLB MSS PDGF B HI (OUT)

ÁÁÁÁÁÁÁÁRF

ÁÁÁÁÁÁÁÁ22


ÁÁÁÁÁÁ

DÁÁÁÁÁÁÁÁÁÁÁÁ

WÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

LB MSS PDGF B LO (OUT)ÁÁÁÁÁÁÁÁÁÁÁÁ



ÁÁÁt ÁÁÁÁÁÁÁÁ



N/AÁÁÁÁÁÁÁÁ


ÁÁÁf ÁÁÁÁÁÁÁÁ

f ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

SYNC PDGF–2 ÁÁÁÁÁÁÁÁ

N/AÁÁÁÁÁÁÁÁ



D3 – 30

TABLE D3.4.4.1–3 DETAILED ELECTRICAL DESCRIPTION OF LAB PDGF CONNECTORJ405 (VIDEO) (PAGE 1 OF 1)


CONNECTOR LOCATIONÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

CONNECTOR ID – PDGF (1553 & VIDEO)





NZGL07T2525N29PEÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ



683–22090








683–22097





NZGL66G2525N29SEÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ



51618–1007



ContID

(P5)


ContID

(J405)


Signal Function ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

EMCClass



Notes

ÁÁÁÁÁÁ

d ÁÁÁÁÁÁ

fÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ


N/AÁÁÁÁÁÁÁÁ

FO ÁÁÁÁÁÁÁÁÁÁÁÁ


D3 – 31

TABLE D3.4.4.1–4 DETAILED ELECTRICAL DESCRIPTION OF LAB PDGF CONNECTORJ406 (1553 & VIDEO)


CONNECTOR ID – PDGF (VIDEO)ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ







683–22090








1F75336–1








683–22094

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁPIN FUNCTION TABLEÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

ContID

(P453)


ContID

(P406)



EMCClass



Notes

ÁÁÁÁÁÁÁÁ

AÁÁÁÁÁÁ

AÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

LB MSS PDGF A HI (IN)ÁÁÁÁÁÁÁÁ

RFÁÁÁÁÁÁ


ÁÁÁÁÁÁÁÁ

BÁÁÁÁÁÁÁÁÁ

BÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

LB MSS PDGF A LO (IN)ÁÁÁÁÁÁÁÁÁÁÁÁ

RFÁÁÁÁÁÁÁÁÁ



CÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

LB MSS PDGF A HI (OUT) ÁÁÁÁÁÁÁÁ

RF ÁÁÁÁÁÁ



DÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

LB MSS PDGF A LO (OUT)ÁÁÁÁÁÁÁÁ

RF ÁÁÁÁÁÁ


ÁÁÁÁE ÁÁÁÁÁÁ

EÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

LB MSS BUD A HI ÁÁÁÁÁÁÁÁ

RF ÁÁÁÁÁÁ


ReservedÁÁÁÁÁÁÁÁ

F ÁÁÁÁÁÁ

FÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

LB MSS BUD A LO ÁÁÁÁÁÁÁÁ

RF ÁÁÁÁÁÁ


ReservedÁÁÁÁÁÁÁÁ

tÁÁÁÁÁÁ

N/AÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

VIDEO PDGF–1ÁÁÁÁÁÁÁÁ

N/AÁÁÁÁÁÁ

FOÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Not used in P406ÁÁÁÁÁÁÁÁÁÁÁÁ

fÁÁÁÁÁÁÁÁÁ

N/AÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ


N/AÁÁÁÁÁÁÁÁÁ


Not used in P406

ÁÁÁÁÁÁÁÁ

x ÁÁÁÁÁÁ



N/A ÁÁÁÁÁÁ


Not used in P406


D3 – 32

TABLE D3.4.4.1–5 DETAILED ELECTRICAL DESCRIPTION OF LAB PDGF CONNECTORJ407 (1553 & VIDEO)









683–22090








1F75340–1








683–22096


PIN FUNCTION TABLE


ContID

(P454)


ContID

(P407)



EMCClass



Notes

ÁÁÁÁÁÁÁÁ

A ÁÁÁÁÁÁ

AÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

LB MSS PDGF B HI (IN) ÁÁÁÁÁÁÁÁ

RF ÁÁÁÁÁÁ


ÁÁÁÁB ÁÁÁÁÁÁ

BÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ


RF ÁÁÁÁÁÁ



CÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

LB MSS PDGF B HI (OUT) ÁÁÁÁÁÁÁÁ

RF ÁÁÁÁÁÁ



DÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ


RF ÁÁÁÁÁÁ


ÁÁÁÁEÁÁÁÁÁÁ


LB MSS BUD B HIÁÁÁÁÁÁÁÁ

RFÁÁÁÁÁÁ


Not used in P407ÁÁÁÁÁÁÁÁF

ÁÁÁÁÁÁN/AÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁLB MSS BUD B LO

ÁÁÁÁÁÁÁÁRF

ÁÁÁÁÁÁ22ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁNot used in P407ÁÁÁÁ

ÁÁÁÁÁÁÁÁ

tÁÁÁÁÁÁÁÁÁ

N/AÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

VIDEO PDGF–2ÁÁÁÁÁÁÁÁÁÁÁÁ

N/AÁÁÁÁÁÁÁÁÁ


Not used in P407

ÁÁÁÁÁÁÁÁ

f ÁÁÁÁÁÁ


SYNC PDGF–2 ÁÁÁÁÁÁÁÁ

N/A ÁÁÁÁÁÁ


Not used in P407


D3 – 33

TABLE D3.4.4.2–1 DETAILED ELECTRICAL DESCRIPTION OF HAB PDGF CONNECTORJ403 (1553 & VIDEO)









683–22090








683–22094








51618–1007


PIN FUNCTION TABLE

ÁÁÁÁÁÁÁÁÁ

ContID

(P3)


ContID

(P403)





Notes

ÁÁÁÁÁÁÁÁÁ







Y ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁLB MSS PDGF A LO (IN) ÁÁÁÁ












V ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁLB MSS BUD B HI ÁÁÁÁ



ÁÁÁFÁÁÁÁÁÁÁÁU

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁLB MSS BUD B LO

ÁÁÁÁÁÁÁÁRF

ÁÁÁÁÁÁÁÁ22


ÁÁÁÁÁÁ

tÁÁÁÁÁÁÁÁÁÁÁÁ

tÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ









D3 – 34

TABLE D3.4.4.2–2 DETAILED ELECTRICAL DESCRIPTION OF HAB PDGF CONNECTORJ404 (1553 & VIDEO)









683–22090








683–22096








51618–1007


PIN FUNCTION TABLE

ÁÁÁÁÁÁÁÁÁ

ContID

(P7)


ContID

(P404)





Notes

ÁÁÁÁÁÁÁÁÁ









RF ÁÁÁÁÁÁÁÁ



X ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ


RF ÁÁÁÁÁÁÁÁ



W ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ


RF ÁÁÁÁÁÁÁÁ





N/AÁÁÁÁÁÁÁÁ


ÁÁÁfÁÁÁÁÁÁÁÁf

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁSYNC PDGF–2

ÁÁÁÁÁÁÁÁN/A

ÁÁÁÁÁÁÁÁFO



D3 – 35

TABLE D3.4.4.2–3 DETAILED ELECTRICAL DESCRIPTION OF HAB PDGF CONNECTORJ405 (VIDEO)











683–22090








683–22097








51618–1007



ContID

(P5)


ContID

(J405)



EMCClass



Notes

ÁÁÁÁÁÁ

d ÁÁÁÁÁÁ



N/AÁÁÁÁÁÁÁÁ



D3 – 36

TABLE D3.4.4.3–1 DETAILED ELECTRICAL DESCRIPTION OF JEM PDGF CONNECTORJ403 (1553 & VIDEO)









TBD








TBD








51618–1007


PIN FUNCTION TABLE

ÁÁÁÁÁÁÁÁÁ

ContID

(P3)


ContID

(P403)





Notes

ÁÁÁÁÁÁÁÁÁ







Y ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁLB MSS PDGF A LO (IN) ÁÁÁÁ












V ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁLB MSS BUD B HI ÁÁÁÁ



ÁÁÁFÁÁÁÁÁÁÁÁU

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁLB MSS BUD B LO

ÁÁÁÁÁÁÁÁRF

ÁÁÁÁÁÁÁÁ22


ÁÁÁÁÁÁ

tÁÁÁÁÁÁÁÁÁÁÁÁ

tÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ









D3 – 37

TABLE D3.4.4.3–2 DETAILED ELECTRICAL DESCRIPTION OF JEM PDGF CONNECTORJ404 (1553 & VIDEO)









TBD








TBD








51618–1007


PIN FUNCTION TABLE

ÁÁÁÁÁÁÁÁÁ

ContID

(P7)


ContID

(P404)





Notes

ÁÁÁÁÁÁÁÁÁ









RF ÁÁÁÁÁÁÁÁ



X ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ


RF ÁÁÁÁÁÁÁÁ



W ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ


RF ÁÁÁÁÁÁÁÁ





N/AÁÁÁÁÁÁÁÁ


ÁÁÁfÁÁÁÁÁÁÁÁf

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁSYNC PDGF–2

ÁÁÁÁÁÁÁÁN/A

ÁÁÁÁÁÁÁÁFO



D3 – 38

TABLE D3.4.4.3–3 DETAILED ELECTRICAL DESCRIPTION OF JEM PDGF CONNECTORJ405 (VIDEO)











TBD








TBD








51618–1007



ContID

(P5)


ContID

(J405)



EMCClass



Notes

ÁÁÁÁÁÁ

d ÁÁÁÁÁÁ



N/AÁÁÁÁÁÁÁÁ



May 22, 1997

D3–39


FIGURE D3.7–1 SSRMS EVA HARDWARE LOCATIONS


E3 – 1

SECTION E3 PWP TO MBS INTERFACE

E3 INTERFACE DEFINITION

E3.1 GENERAL

E3.1.1 INTERFACE DESCRIPTION

The physical interface (mechanical, structural, thermal and environmental) plane is definedbetween the Worksite Interface Fixture (WIF) on the MBS and the EVA Portable Workplatform(PWP) probe.

There is no electrical interface between the EVA PWP and the MBS.

E3.1.2 INTERFACE RESPONSIBILITIES

The MBS WIF is supplied to CSA as GFE. NASA is responsible for development of the EVAPWP. Interface responsibilities for the EVA PWP to MBS WIF interface are as defined in SSP42003 Part 1, Section E and as described in SSP 42003 Part 2, Section E herein.

E3.1.3 ENGINEERING UNITS AND TOLERANCES

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

E3.2 STRUCTURAL/MECHANICAL INTERFACES

The EVA PWP probe attaches to the MBS WIF. Refer to Figure A3.7–1, A3.7–2, and A3.7–3for WIF locations on the MBS.

For structural and mechanical details of the WIF, refer to SSP 30256:001.


E3 – 2

E3.2.1 INTERFACE LOCATIONS

The location of the WIF on the MBS will be as defined in Figure A3.7–1, A3.7–2, and A3.7–3.

The physical orientation of the PWP in the WIF on the MBS will be as defined in FigureE3.2.1–1.

E3.3 SOFTWARE INTERFACES

There are no software interfaces between the EVA PWP and the MBS .


E3 – 3

FIGURE E3.2.1–1 PORTABLE WORK PLATFORM (PWP) STOWED ON MBS


F3 – 1

SECTION F3 SSMB LSA TO SSRMS INTERFACE

F3 INTERFACE DEFINITION

F3.1 GENERAL

F3.1.1 INTERFACE DESCRIPTION

The physical interface (mechanical, structural, thermal and environmental) plane is defined atthe Flight Support Equipment Grapple Fixture (FSEGF) and FSE brackets mounting surface atthe SSMB Launch Support Assembly (LSA). The utility interface plane (power, data and video)is defined between the FSEGF harness and the USL connector panel.

F3.1.2 INTERFACE RESPONSIBILITIES

CSA is responsible for development of the SSRMS, FSEGF, FSE brackets and FSEGF Harness.NASA is responsible for development of the SSMB LSA.

F3.1.3 ENGINEERING UNITS AND TOLERANCES

Unless otherwise noted herein, all dimensions are shown in the English system of IP units.

F3.2 STRUCTURAL/MECHANICAL INTERFACES

The FSEGF attaches to the SSMB LSA via eight fasteners.

The detailed mechanical interface between the SSMB LSA and the SSRMS via the FSEGF andFSE brackets is defined in Figures F3.2–1 and F3.2–2.

F3.2.1 FSEGF AND FSE BRACKET LOCATION

Two FSEGFs and four FSE brackets will be mounted on the SSMB LSA at the locations definedin Figures F3.2–1 and F3.2–2.


F3 – 2

F3.3 THERMAL INTERFACES

Reserved

F3.4 ELECTRICAL INTERFACES

The USL will provide power, data and PFM video interfaces to the SSRMS via the FSEGFharness as defined in Figures F3.4–1 and F3.4–2.

F3.4.1 POWER RETURN AND GROUNDING INTERFACES

The USL will provide power return and grounding interfaces to the SSRMS via the FSEGFharness as defined in Figures F3.4–1.

F3.4.2 POWER CONNECTORS AND PIN ASSIGNMENTS

The FSEGF harness power connectors and pin assignments for the SSMB connector panel willbe as defined in Tables F3.4.2–1 through F3.4.2–2.

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

The USL will support data and video interfaces between the SSMB and the SSRMS via theFSEGF harness. PFM sync and control and video will be transmitted and received by copperlines between the FSEGF and the SSRMS. The PFM Fiber Optic video from the SSMB will beconverted to copper for the FSEGF by the VSC located within the FSEGF.

F3.4.4 DATA AND VIDEO CONNECTORS AND PIN ASSIGNMENTS

The FSEGF harness data and video connectors and pin assignments for the SSMB connectorpanel will be as defined in Tables F3.4.4–1 and F3.4.4–2.


F3 – 3

F3.5 ENVIRONMENTS

The FSEGF to SSMB LSA electromagnetic, grounding and bonding interface implementationwill be as defined in Figures F3.2–1 and F3.2–2.

F3.6 SOFTWARE INTERFACES

There are no software interfaces between the FSEGF and the USL.


May 22, 1997

F3 – 4


FIGURE F3.2–1 FSEGF TO SSMB LSA BOLT PATTERN


May 22, 1997

F3 – 5


FIGURE F3.2–2 FSEGF TO SSMB LSA BOLT PATTERN


F3 – 6

FIGURE F3.2–4 DELETED


F3 – 7



F3 – 8



F3 – 9



F3 – 10



F3 – 11


SS

P 42003, P

art 2, Revision A

SS

MB

to MS

S IC

DM

ay 22, 1997

F3 – 12

P233To VSC (J2)20ga

12ga

12ga

12ga

12ga

12ga

2

2

2

2

1

2

2

1

8ga

8ga

8ga

2

2

1

8ga

8ga

8ga

SSRMS 1Pwr & Rtn

*Pyld 1 Pwr & Rtn

Ground

S0/Lab/LDAConnector Panel

InterfacePlane

FSEGFHarness &Connectors

LabHarness &Connectors J300 P300

J3

20gaP233To VSC (J2)

P344To VSC (J3)20ga

12ga

12ga

12ga

12ga

12ga

2

2

2

2

1

2

2

1

8ga

8ga

8ga

2

2

1

8ga

8ga

8ga

SSRMS 2

*Pyld 2 Pwr & Rtn

Ground

J301 P301

20gaP344To VSC (J3)

J4

28ga*SSRMS BUD Pwr & Rtn

8ga*Ground

J302

Note: Return lines not shown


FSEGF

Pwr & Rtn

RPCM25AType II

RPCM25AType II

FIG

UR

E F

3.4–1 FS

EG

F TO

US

L ELE

CT

RIC

AL S

YS

TE

M D

IAG

RA

M

SS

P 42003, P

art 2, Revision A

SS

MB

to MS

S IC

DM

ay 22, 1997

F3 – 13

Video Channel #1 CU PFM


Sync & Control #1 CU PFM

J4J1

J3J2

VSC

Power Connectors


Sync & Control #2 CU PFM

LB MSS–PDGF A In 22ga

22ga*LB MSS–PDGF A Out

Video PDGF #1

Video PDGF #3

Sync PDGF #1

Fo

Fo

Fo

FSEGFHarness &Connectors

InterfacePlane

Video PDGF #2

Sync PDGF #2

LB MSS–PDGF B In

*LB MSS–PDGF B Out

Fo

Fo

22ga

22ga

P303

P304

Fo

Fo

Fo

Fo

Fo

FSEGF

J1

J2

S0/Lab/LDAConnector Panel

J303

LabHarness &Connectors

Tsp

Tsp

J304

Tsp

Tsp

*1 Fo

J305

* Unused in this Configuration

Note: Backup Drive not wired to SSMB

BusCoupler &Terminator

BusCoupler &Terminator

FIG

UR

E F

3.4–2 FS

EG

F TO

US

L ELE

CT

RIC

AL S

YS

TE

M D

IAG

RA

M


F3 – 14

TABLE F3.4.2–1 DETAILED ELECTRICAL DESCRIPTION OF FSEGF TO USLCONNECTOR J300 (PRIME POWER)


CONNECTOR ID SSRMS LDA (PRIME POWER)ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ




NZGL07T2525LN7PNÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ



683–22091



P300ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ





51618–1130



Cont

ID



EMC

Class


AWGÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Notes

ÁÁÁÁÁÁ

A ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ


EO ÁÁÁÁÁÁ

8 ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁB ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

SSRMS LDAPL1LAB ÁÁÁÁÁÁ

EO ÁÁÁÁÁÁ


NOT USED IN P300

ÁÁÁÁÁÁ

C ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

SSRMS LDAPL1LAB RTN ÁÁÁÁÁÁ

EO ÁÁÁÁÁÁ


NOT USED IN P300ÁÁÁÁÁÁ

F ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

SSRMS LDASSRMS1LAB RTN ÁÁÁÁÁÁ

EO ÁÁÁÁÁÁ

8 ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁG ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

SSRMS LDASSRMS1LAB ÁÁÁÁÁÁ

EO ÁÁÁÁÁÁ



F3 – 15

TABLE F3.4.2–2 DETAILED ELECTRICAL DESCRIPTION OF FSEGF TO USL CONNECTORJ301 (REDUNDANT POWER)


CONNECTOR ID – SSRMS LDA (REDUNDANT POWER)ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ




NZGL07T2525LN7PAÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ



683–22092








51618–1130



Cont

ID

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ


EMC

Class


AWG ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Notes

ÁÁÁÁÁÁ

A ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ


EOÁÁÁÁÁÁÁÁ

8 ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁB ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

SSRMS LDAPL2LAB ÁÁÁÁÁÁ

EOÁÁÁÁÁÁÁÁ

8 ÁÁÁÁÁÁÁÁÁÁÁÁÁÁNOT USED IN P301

ÁÁÁÁÁÁ

C ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

SSRMS LDAPL2LAB RTN ÁÁÁÁÁÁ

EOÁÁÁÁÁÁÁÁ

8 ÁÁÁÁÁÁÁÁÁÁÁÁÁÁNOT USED IN P301

ÁÁÁÁÁÁ

F ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

SSRMS LDASSRMS2LAB RTN ÁÁÁÁÁÁ

EOÁÁÁÁÁÁÁÁ


ÁÁÁG ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

SSRMS LDASSRMS2LAB ÁÁÁÁÁÁ

EOÁÁÁÁÁÁÁÁ

8 ÁÁÁÁÁÁÁÁÁÁÁÁÁÁ


F3 – 16

TABLE F3.4.4–1 DETAILED ELECTRICAL DESCRIPTION OF FSEGF TO USL CONNECTORJ303 (1553 & VIDEO)


CONNECTOR ID – SSRMS LDA (1553 & VIDEO)ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ




NZGL07T2525N43SAÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ



683–22094





NZGL06G2525N43PAÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ



51618–1130



Cont

ID

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ


EMCClass



Notes

ÁÁÁÁÁÁ

A ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

LB MSS SSRMS LDA A HI (IN) ÁÁÁÁÁÁÁÁ

RF ÁÁÁÁÁÁÁÁ


ÁÁÁB ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

LB MSS SSRMS LDA A LO (IN) ÁÁÁÁÁÁÁÁ

RF ÁÁÁÁÁÁÁÁ


ÁÁÁC ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

LB MSS SSRMS LDA A HI (OUT) ÁÁÁÁÁÁÁÁ

RF ÁÁÁÁÁÁÁÁ



DÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

LB MSS SSRMS LDA A LO (OUT)ÁÁÁÁÁÁÁÁ

RFÁÁÁÁÁÁÁÁ

20ÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

NOT USED IN P303ÁÁÁÁÁÁqÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁVIDEO SSRMS LDA–1

ÁÁÁÁÁÁÁÁN/A

ÁÁÁÁÁÁÁÁFO

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁÁÁÁ

wÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

SYNC SSRMS LDA–1ÁÁÁÁÁÁÁÁÁÁÁÁ



ÁÁÁx ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

VIDEO SSRMS LDA–3 ÁÁÁÁÁÁÁÁ

N/A ÁÁÁÁÁÁÁÁ

FO ÁÁÁÁÁÁÁÁÁÁÁÁÁÁNote: MIL–STD–1553 wire is 22 AWG


F3 – 17

TABLE F3.4.4–2 DETAILED ELECTRICAL DESCRIPTION OF FSEGF TO USL CONNECTORJ304 (1553 & VIDEO)


CONNECTOR ID – SSRMS LDA (1553 & VIDEO)ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ




NZGL07T2525N43SBÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ



683–22096





NZGL06G2525N43PBÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ



51618–1130



Cont

ID

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ


EMCClass



Notes

ÁÁÁÁÁÁ

A ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

LB MSS SSRMS LDA B HI (IN) ÁÁÁÁÁÁÁÁ

RF ÁÁÁÁÁÁÁÁ


ÁÁÁB ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

LB MSS SSRMS LDA B LO (IN) ÁÁÁÁÁÁÁÁ

RF ÁÁÁÁÁÁÁÁ


ÁÁÁC ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

LB MSS SSRMS LDA B HI (OUT) ÁÁÁÁÁÁÁÁ

RF ÁÁÁÁÁÁÁÁ



DÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

LB MSS SSRMS LDA B LO (OUT)ÁÁÁÁÁÁÁÁ

RFÁÁÁÁÁÁÁÁ

20ÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

NOT USED IN P304ÁÁÁÁÁÁqÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁVIDEO SSRMS LDA–2

ÁÁÁÁÁÁÁÁN/A

ÁÁÁÁÁÁÁÁFO

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁÁÁÁ

wÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

SYNC SSRMS LDA–2ÁÁÁÁÁÁÁÁÁÁÁÁ


FOÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁNote: MIL–STD–1553 wire is 22 AWG


F3 – 18

TABLE F3.4.4–3 DELETED


G3 – 1

SECTION G3 AVU CCD TO RWS INTERFACE

G3.0 INTERFACE DEFINITION

G3.1 GENERAL

G3.1.1 INTERFACE DESCRIPTION

The Artificial Vision Unit (AVU) Cursor Control Device (CCD) to Robotic Workstation (RWS)mated on–orbit configuration for both primary (LAS 5) and secondary (LAP 5) configurationsare shown in Figure G3.1.1–1. The structural and mechanical interface plane is at the mountingsurface between the AVU CCD and the RWS bracket. Utility interface planes exist at theconnectors between the AVU CCD and the RWS harness.

G3.1.2 INTERFACE RESPONSIBILITIES

CSA is responsible for AVU CCD delivery to NASA as Government Furnished Equipment(GFE). NASA is responsible for development of the RWS. Interface responsibilities for theAVU CCD to RWS interface are as defined in SSP 42003 Part I, Section G and as described inSSP 42003 Part II, Section G herein.

G3.1.3 ENGINEERING UNITS AND TOLERANCES

Unless otherwise noted herein, all dimensions in this document are shown in English system ofinch pound (IP) units. Implied tolerances on linear dimensions are defined in Table G3.1.3–1.

TABLE G3.1.3–1 LINEAR TOLERANCES

English Dimensions Implied Tolerances (inches)

x.xx +/– 0.030

x.xxx +/– 0.010

G3.2 STRUCTURAL/MECHANICAL INTERFACES

G3.2.1 GENERAL

AVU CCD structurally attaches to the RWS mounting bracket as shown in Figure G3.2.1–1 andG3.2.1–2.

G3.2.2 ELECTRICAL CONNECTOR LOCATION

AVU CCD electrical connector location and configuration are as defined in Figure G3.2.1–1.


G3 – 2

G3.3 FLUID INTERFACE(S)

N/A

G3.4 ELECTRICAL INTERFACES

G3.4.1 ELECTRICAL CONNECTIVITY

The electrical interface(s) (including power and data interfaces) between the AVU CCD andRWS consists of an electrical connector with associated cabling. The power and data systeminterfaces are reflected in Figure G3.4.1–1.

G3.4.1.1 DETAILED ELECTRICAL INTERFACE(S)

Control of the detailed electrical interface between the AVU CCD and the RWS harness consistsof identifying the particular jack/plug pair, configuration, location, part number andfunctionality. Table G3.4.1.1–1 defines these controlling parameters for the power and data. ForTable G3.4.1.1–1 the following definitions apply:

Not Used – Pin location not used by ORU or wire harnessReserved – Pin used by ORU only.Spare – Pin used by wire harness only.

G3.4.2 ELECTRICAL BONDING

The electrical bonding interface for the AVU CCD is at the dedicated Class H–bond pin (22gauge) of the AVU J1 CCD Connector as identified in Table G3.4.1.1–1 (contact number one).This bonding interface shall comply with the electrical bonding requirements defined in SSP30245.

G3.4.3 SOFTWARE INTERFACES

N/A


G3 – 3

RWS Mounting Bracket

AVU CCD

FIGURE G3.1.1–1 AVU CCD TO RWS ON–ORBIT CONFIGURATION


G3 – 4

5.00”

1.320”

±0.0052.750”

±0.005

1.031”

1.031”

0.95”

1.75”

2.07”

2.32”3.19”

0.375”

#6–32 UNC 2B0.25” DEEP

(4 Places)

+0.06–0.00

0.375”

3.125”3.50”

Diameter

0.918”

3.125”

2.38”

1.75”

1.75”

3.250” ±0.005

Master Connector Keyway Location

0.125” ±0.005

+0.01–0.0

FIGURE G3.2.1–1 AVU CCD VOLUMETRIC & MECHANICAL INTERFACES


G3 – 5

1.375” +0.005

2.750” ±0.005

1.375” +0.005

2.750” +0.005

2.81”

2.380”

1.350”

1.640”

3.280”

0.172(4 Holes)

∅

∅

FIGURE G3.2.1–2 AVU CCD BOLT PATTERN AND PANEL CUTOUT


G3 – 6

11

3

9

1

6

12

13

NC

Power +5 VDC

Power Return

Structure

Data Norm Hi (+) (T Ball 1+)

Data Norm Lo (–) (T Ball 1–)

Spare (T–Ball 2+)

Spare (T–Ball 2–)

Spare (T–Ball 3+)


Spare (T–Ball 4+)


AVU

CCD

J1

11

3

9

1

6

12

13

5

7

2

10

4

8

NC

NC

NC

NC

NC

NC: No Connect

Indicates Twisted Shielded Pair

CCP01W07

Notes:

FIGURE G3.4.1–1 RWS TO AVU CCD ELECTRICAL INTERFACES


G3 – 7

TABLE G3.4.1.1–1 DETAILED ELECTRICAL DESCRIPTION OF AVU CCD CONNECTOR J1(CURSOR CONTROL DEVICE)

CSANASA

AVUInterface Plane

J01P01

AVU

CONNECTOR

Insert ArrangementSeries III Insert 11–35 Per

MIL–C–38999

+Y

+X

–Y

–X

CCD

1

2

3

4

5

67

8

9

10

11

1213

CONNECTOR LOCATION

CONNECTOR ID – AVU (CURSOR CONTROL DEVICE)

Ref. Des J01 Part Number D38999/20FB35PN Wire HarnessNumber

NA

Ref. Des P01 Part Number D38999/26FB35SN Wire HarnessNumber

W07CC



AWG SignalDestination

SignalSource

Notes

1 STRUCTURE ML 22 AVU CCD DCP

2 SPARE HO 22 AVU AVU CCD T Ball 3+

3 POWER +5 VDC ML 22 AVU CCD DCP

4 SPARE HO 22 AVU AVU CCD T Ball 4+

5 SPARE RF 22 AVU AVU CCD T Ball 2+

6 RESERVED Lamp supply

7 SPARE RF 22 AVU AVU CCD T Ball 2–

8 SPARE HO 22 AVU AVU CCD T Ball 4–

9 POWER RETURN ML 22 AVU CCD DCP

10 SPARE HO 22 AVU AVU CCD T Ball 3–

11 NOT USED

12 DATA NORM LO (–) RF 22 AVU AVU CCD T Ball 1–

13 DATA NORM HI (+) RF 22 AVU AVU CCD T Ball 1+


H3 – 1

SECTION H3 SSMB TO VSC INTERFACE

H3 REQUIRMENTS

H3.1 GENERAL

A VSC is an ORU that converts PFM fiber optic video to PFM copper video and converts PFMcopper video to PFM fiber optic video. VSC’s are mounted on the USL, Hab, and JEM–PMmodules near the PDGF’s in order to convert video signals for use by the PDGF and SSRMS.VSC’s are also mounted on the TUS reel assemblies on S0 to convert video signals for the TUScable.

H3.1.1 INTERFACE DESCRIPTION

For the VSC mounted on the module, the physical interface plane is at the VSC bracket tomodule mounting bracket. For the VSCs mounted on Truss Segment S0 the physical interfaceplane is at the VSC ORU assembly to truss mounting bracket. The electrical interface plane isbetween the VSC connectors and the harness connectors.

H3.1.2 INTERFACE RESPONSIBILITIES

CSA is responsible for development of the VSC. NASA is responsible for the procurement ofthe VSC bracket for the USL and the Hab. NASA is responsible for the procurement of the VSCMounting Hardware Kit for Truss Segment S0. NASDA is responsible for the development ofthe JEM–PM and procurement of the VSC and VSC bracket for the JEM–PM.

H3.1.3 ENGINEERING UNITS AND TOLERANCES

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

H3.2 STRUCTURAL/MECHANICAL INTERFACES

For a VSC mounted on a module, the VSC bracket will be a standard configuration as shown inFigure H3.2–1 (TBD). The VSC bracket bolt pattern available to the module will be the samefor each application.

For the VSCs mounted on the Truss Segment S0, the interface will be as shown in Figure H3.2–2and H3.2–3. For the VSCs mounted on Truss Segment S0, the VSC Mounting Hardware Kitwill be utilized.


H3 – 2

H3.3 THERMAL INTERFACES

Depending on the thermal environment, the VSC ORU can be passively controlled through theuse of thermal blankets and thermal conduction to the mating element. Conversely the VSCORU provides heaters and RTDs that can be utilized to actively control temperature of the VSCORU.

H3.3.1 PASSIVE THERMAL INTERFACES

The VSC ORU provides Cotherm strips to increase thermal conduction to the VSC bracket asshown in Figure H3.2–2.

H3.3.2 ACTIVE THERMAL INTERFACES

The VSC ORU provides two thermostatically controlled resistive heaters for active thermalcontrol.

H3.4 ELECTRICL INTERFACES

The modules will provide power and PFM video interfaces to the VSC as shown in FigureD3.4.1–1.

The Truss Segment S0 will provide power, RTD data and PFM video interfaces to the VSCs asshown in Figure H3.4–1.

The VSC does not support 1553 data bus interface.

H3.4.1 POWER RETURN AND GROUNDING INTERFACES

The modules will provide power return and grounding interfaces to the VSC as shown in FigureD3.4.1–1. The Truss Segment S0 will provide power return and grounding interfaces to the VSCas shown in Figure H3.4–1.

H3.4.2 POWER CONNECTORS AND PIN ASSIGNMENTS

The VSC ORU power connectors and pin assignments are defined in Tables H3.4.2–1 andH3.4.2–2.

H3.4.3 PFM SYNC AND CONTROL AND VIDEO INTERFACES

The modules will support PFM Fiber Optic video interfaces to the VSC ORU via the PDGFharness. The PDGF harness will provide both PFM Fiber Optic and PFM copper lines to the


H3 – 3

module mounted VSC ORU. The Truss Segment S0 will provide one RTD data interface, PFMFiber Optic (FO) and PFM copper interfaces to the VSC ORU.

H3.4.4 DATA AND VIDEO CONNECTORS AND PIN ASSIGNMENTS

The VSC ORU FO video connectors and pin assigments are defined in Table H3.4.4–1. TheVSC ORU copper video connector and pin assignments are defined in Table H3.4.4–2.

H3.5 ENVIRONMENTS

The VSC ORU to module electromagnetic, grounding, and bonding interface implementationwill be as defined in Figure H3.2–1. The VSC ORU to Truss Segment S0 electromagnetic,grounding, and bonding interface implementation will be as defined in Figure H3.2–2.

H3.6 SOFTWARE INTERFACES

There are no software interfaces between the VSC ORU and the module. There are no softwareinterfaces between the VSC ORU and the SSMB Truss.


H3 – 4

TBD

FIGURE H3.2–1 VSC MODULE MOUNTING BRACKET


May 22, 1997

H3 – 5


FIGURE H3.2–2 VSC TRUSS MOUNTING BRACKET


May 22, 1997

H3 – 6


FIGURE H3.2–3 VSC TRUSS MOUNTING BRACKET


H3 – 7

TUS VSC 1 Video 1 CoaxTUS VSC 1 Video 2 Coax

TUS VSC 1 Video 3 CoaxTUS VSC 1 Sync 1 Coax

TUS VSC 1 Sync 2 Coax

TUS VSC 2 Video 1 CoaxTUS VSC 2 Video 2 Coax

TUS VSC 2 Video 3 CoaxTUS VSC 2 Sync 1 Coax

TUS VSC 2 Sync 2 Coax

VSC 1

J4J1

J3J2

MDM

S0–1

VSW 1

VSW 2

VSW 3

TUS 1

VSC 2

J4 J1

J3 J2

MDM

S0–2

TUS 2

SPDA

S0–4B

SPDA

S0–3A

TUS VSC 1 Power 20 gaTUS VSC 1 Return 20 ga

TUS VSC 1 RTD HiTUS VSC 1 RTD Lo

TUS VSC 1 Heater 1 Power 20 gaTUS VSC 1 Heater 1 Return 20 ga

TUS VSC 1 Power 20 gaTUS VSC 1 Return 20 gaTUS VSC 1 Heater 2 Power 20 gaTUS VSC 1 Heater 2 Return 20 ga

RPCM

S0 4B–E

RPCM

S0 4B–F

RPCM

SO 3A–E

RPCM

S0 3A–F


TUS VSC 2 RTD HiTUS VSC 2 RTD Lo


TUS VSC 2 Video 1 FOTUS VSC 2 Video 2 FO

TUS VSC 2 Video 3 FOTUS VSC 2 Sync 1 FO

TUS VSC 2 Sync 2 FO

TUS VSC 1 Video 1 FOTUS VSC 1 Video 2 FO

TUS VSC 1 Video 3 FOTUS VSC 1 Sync 1 FO

TUS VSC 1 Sync 2 FO

FIGURE H3.4–1 TUS VSC ELECTRICAL DIAGRAM


H3 – 8

TABLE H3.4.2–1 DETAILED ELECTRICAL DESCRIPTION OF VSC ORU TO SSMBCONNECTOR J2 (PRIME POWER)


CONNECTOR LOCATIONÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

CONNECTOR ID VSC ORU (PRIME POWER)ÁÁÁÁÁÁÁÁ

Ref. DesÁÁÁÁÁÁ

J2ÁÁÁÁÁÁÁÁÁÁ

Part NumberÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

NZGL00T1513N98PNÁÁÁÁÁÁÁÁ


P14ÁÁÁÁÁÁÁÁÁÁ


NZGL06G1513N98SNÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

PIN FUNCTION TABLE

ÁÁÁÁÁÁÁÁÁ

Cont

ID

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Signal Function ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Maximum

Pwr [W]

ÁÁÁÁÁÁÁÁÁ

EMC

ClassÁÁÁÁÁÁÁÁÁ


Notes

ÁÁÁÁÁÁ

AÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Prime PowerÁÁÁÁÁÁÁÁÁÁ

17ÁÁÁÁÁÁ

EOÁÁÁÁÁÁ

20ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁÁÁÁ

BÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ


ÁÁÁÁÁÁÁÁÁ

ÁÁÁÁÁÁÁÁÁ


NOT USED

ÁÁÁÁÁÁ

C ÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Prime Power RTNÁÁÁÁÁÁÁÁÁÁ

17 ÁÁÁÁÁÁ

EO ÁÁÁÁÁÁ

20 ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁD ÁÁÁÁÁÁÁÁÁÁÁÁÁÁ


ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

NOT USED

ÁÁÁÁÁÁ

E ÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Chassis Ground ÁÁÁÁÁÁÁÁÁÁ

27 ÁÁÁÁÁÁ

EO ÁÁÁÁÁÁ


ÁÁÁÁÁÁ

F ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Heater Power 1

Return


27 ÁÁÁÁÁÁÁÁÁ

EO ÁÁÁÁÁÁÁÁÁ

20 ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁGÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Heater Power 1ÁÁÁÁÁÁÁÁÁÁ

27ÁÁÁÁÁÁ

EOÁÁÁÁÁÁ

20ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁÁÁÁ

HÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ


ÁÁÁÁÁÁÁÁÁ

ÁÁÁÁÁÁÁÁÁ


NOT USED

ÁÁÁÁÁÁ

J ÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Temp TransducerÁÁÁÁÁÁÁÁÁÁ

ÁÁÁÁÁÁ

ML ÁÁÁÁÁÁ


ÁÁÁÁÁÁ

K ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Temp Transducer

ReturnÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁÁÁÁÁÁÁ

ML ÁÁÁÁÁÁÁÁÁ



H3 – 9

TABLE H3.4.2–2 DETAILED ELECTRICAL DESCRIPTION OF VSC ORU TO SSMBCONNECTOR J3 (REDUNDANT POWER)

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁCONNECTOR LOCATIONÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

CONNECTOR ID VSC ORU (PRIME POWER)ÁÁÁÁÁÁÁÁ




NZGL00T1513N98PAÁÁÁÁÁÁÁÁ




NZGL06G1513N98SA


PIN FUNCTION TABLE

ÁÁÁÁÁÁÁÁÁ

Cont

ID

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Signal Function ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Maximum

Pwr [W]

ÁÁÁÁÁÁÁÁÁ

EMC

ClassÁÁÁÁÁÁÁÁÁ


Notes

ÁÁÁÁÁÁAÁÁÁÁÁÁÁÁÁÁÁÁÁÁPrime Power

ÁÁÁÁÁÁÁÁÁÁ17

ÁÁÁÁÁÁEOÁÁÁÁÁÁ20ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁÁÁÁ

BÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ


ÁÁÁÁÁÁÁÁÁ

ÁÁÁÁÁÁÁÁÁ


NOT USED

ÁÁÁÁÁÁ

C ÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Prime Power RTNÁÁÁÁÁÁÁÁÁÁ

17 ÁÁÁÁÁÁ

EO ÁÁÁÁÁÁ


ÁÁÁD ÁÁÁÁÁÁÁÁÁÁÁÁÁÁ



NOT USED

ÁÁÁÁÁÁ

E ÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Chassis Ground ÁÁÁÁÁÁÁÁÁÁ

27 ÁÁÁÁÁÁ

EO ÁÁÁÁÁÁ


ÁÁÁÁÁÁ

F ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Heater Power 2

Return


27 ÁÁÁÁÁÁÁÁÁ

EO ÁÁÁÁÁÁÁÁÁ

20 ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁGÁÁÁÁÁÁÁÁÁÁÁÁÁÁHeater Power 2

ÁÁÁÁÁÁÁÁÁÁ27

ÁÁÁÁÁÁEOÁÁÁÁÁÁ20ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁÁÁÁ

HÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ


ÁÁÁÁÁÁÁÁÁ

ÁÁÁÁÁÁÁÁÁ


NOT USED

ÁÁÁÁÁÁ

J ÁÁÁÁÁÁÁÁÁÁÁÁÁÁ



NOT USED

ÁÁÁÁÁÁ

K ÁÁÁÁÁÁÁÁÁÁÁÁÁÁ



NOT USED


H3 – 10

TABLE H3.4.4–1 DETAILED ELECTRICAL DESCRIPTION OF VSC ORU TO SSMBCONNECTOR J1 (FIBER OPTIC VIDEO CONNECTOR)


CONNECTOR ID VSC ORU (Fiber Video Connector)ÁÁÁÁÁÁÁÁ




NZGL00T1515N68SNÁÁÁÁÁÁÁÁ




NZGL06G1515N68PN

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

PIN FUNCTION TABLE

ÁÁÁÁÁÁÁÁÁ

Cont

ID




Notes

ÁÁÁÁÁÁAÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁSync B

ÁÁÁÁÁÁFOÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁÁÁÁ

BÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Sync AÁÁÁÁÁÁÁÁÁ

FOÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁC ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Video 2 ÁÁÁÁÁÁ

FO ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁD ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Video 1 ÁÁÁÁÁÁ

FO ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁE ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ


Not usedÁÁÁÁÁÁ

F ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ


Not usedÁÁÁÁÁÁ

GÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ


Not usedÁÁÁÁÁÁÁÁÁ

HÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Video 3ÁÁÁÁÁÁÁÁÁ



H3 – 11

TABLE H3.4.4–2 DETAILED ELECTRICAL DESCRIPTION OF VSC ORU TO SSMBCONNECTOR J4 (COPPER VIDEO CONNECTOR)


CONNECTOR ID VSC ORU (Fiber Video Connector)ÁÁÁÁÁÁÁÁ




NZGL00T1717N6PNÁÁÁÁÁÁÁÁ




NZGL06G1717N6SN

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

PIN FUNCTION TABLE

ÁÁÁÁÁÁÁÁÁ

Cont

ID




Notes

ÁÁÁÁÁÁAÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁSync Channel 1

ÁÁÁÁÁÁcoaxÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁÁÁÁ

BÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Video Channel 2ÁÁÁÁÁÁÁÁÁ

coaxÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁC ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ


Not used

ÁÁÁÁÁÁ

D ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Video Channel 1 ÁÁÁÁÁÁ

coaxÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁE ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Sync Channel 2 ÁÁÁÁÁÁ

coaxÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁF ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Video Channel 3 ÁÁÁÁÁÁ

coaxÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ


A – 1

APPENDIX A: ABBREVIATIONS AND ACRONYMS

A Ampere

Amp Ampere

APM Attached Pressurized Module

AVU Artificial Vision Unit

BDU Back–Up Drive Unit

BHD Bulkhead

C&C Command & Control

CCD Cursor Control Device

CETA Crew Equipment Translation Aid

CSA Canadian Space Agency

CL Centerline

dBm decibels meter

D&C Display and Control

dia diameter

EMI Electromagnetic Interference

ESA European Space Agency

EVA Extravehicular Activity

FRGF Flight Releasable Grapple Fixture

FSEGF Flight Support Equipment Grapple Fixture

ft feet

Hz Hertz

ICD Interface Control Document

in inch

IP International Partner


A – 2

ISS International Space Station

ITA Integrated Truss Assembly

IVA IntraVehicular Acivity

JEM–PM Japanese Experiment Module – Pressurized Module

kN–m kilo Newton–meter

kW kilowatt

lbs pounds

LSA Launch Support Assembly

m meter

MBS MRS Base System

MCE MSS Control Equipment

MRS Mobile Remote Servicer

MSC Mobile Servicing Center

MSS Mobile Servicing System

MT Mobile Transporter

N Newton

NASA National Aeronautics and Space Administration

NASDA National Space Development Agency of Japan

NSTS National Space Transportation System

oct Octave

ORU Orbit–Replaceable Unit

PDGF Power and Data Grapple Fixture

PFM Pulse Frequency Modulation

psia pounds per square inch absolute

PWP Portable Workplatform

Rad Radian


A – 3

Ref Reference

RMS Remote Manipulator System

RPCM Remote Power Control Module

RSS root sum squared

RWS Robotics Workstation

SPDM Special Purpose Dexterous Manipulator

SSCB Space Station Control Board

SSMB Space Station Manned Base

SSRMS Space Station Remote Manipulator System

Sync Synchronization

TBD To Be Determined

TBR To Be Resolved

TUS Trailing Umbilical System

ult Ultimate

US United States

USL United States Laboratory

V Volts

Vdc Volts, direct current

VSC Video Signal Converter

W Watts

WIF Worksite Interface Fixture


B – 1

APPENDIX B: ISSUE SHEETS


B – 2

SSMB to MSS ICD, 42003 Part 2 ISSUES – Date Febraury 21, 1997

ACTION NUMBER: 42003–P2–02 – Non–Compliant Connectors

ISSUE DESCRIPTION :

AFFECTED PARAGRAPHS :

ACTION PLAN :

DUE DATE :

Use of MIL–C–38999, Series III, connectors violates toxic outgassing requirements of the LabPIDS.

Table C3.4.1.1–1Table C3.4.1.1–2Table C3.4.1.1–3Table C3.4.1.1–4Table G3.4.1.1–1


B – 3

ISSUE FORM, SPACE STATION

Issue Title:

Issue No.

Initiator Name:Org/Company:

Phone:Mailcode:

Date:Initiator’s Issue No:Problem Category:

(Mandatory only)

Document ID:Title:Date:

Page #:Sec. #:

Para. #:Fig. #:

Description of Issue:

Recommendation:

Impact if Recommendation Not Implemented:

MT Connector Location

42003–02–04

B. LongfellowMcDonnell Douglas896–4909

3/06/97WL–04

SSP 42003SSMB to MSS ICD, Part 22/21/97

The ICD does not show the physical location of the MT electrical connectors.

Add a Figure or modify an existing Figure to show connectors and connector panellocation.

ICD reflects misleading information.


B – 1

APPENDIX C: TBD LIST

1 TABLE A3.4.2–1 MBS EVA OUTLET #1 CONNECTOR ANDPIN ASSIGNMENTS

A3–23 2–21–97

2 TABLE A3.4.2–2 MBS EVA OUTLET #2 CONNECTOR ANDPIN ASSIGNMENTS

A3–24 2–21–97

3 D3.2.1 USL MODULE PDGF LOCATION D3–2 2–21–97

4 D3.2.2 HAB MODULE PDGF LOCATION D3–2

5 D3.2.4 COLUMBUS APM MODULE PDGF LOCATION D3–2 2–21–97

6 D3.7 SSRMS EVA HARDWARE LOCATIONS D3–5 2–21–97

7 FIGURE D3.2.1–1 PDGF LOCATION ON USL D3–6 2–21–97

8 FIGURE D3.2.2–1 PDGF LOCATION ON US HAB D3–7

9 FIGURE D3.2.4–1 PDGF LOCATION ON APM D3–8 2–21–97

10 TABLE D3.4.2.1–1 DETAILED ELECTRICAL DESCRIPTIONOF LAB PDGF CONNECTOR J400 (PRIME POWER)(PAGE 1OF 2)

D3–16 2–21–97

11 TABLE D3.4.2.1–2 DETAILED ELECTRICAL DESCRIPTIONOF LAB PDGF CONNECTOR J401 (REDUNDANT POW-ER)(PAGE 1 OF 2)

D3–18 2–21–97

12 TABLE D3.4.2.1–3 DETAILED ELECTRICAL DESCRIPTIONOF LAB PDGF CONNECTOR J402 (BACKUP DRIVE POWER)

D3–20 2–21–97

13 TABLE D3.4.2.2–1 DETAILED ELECTRICAL DESCRIPTIONOF HAB PDGF CONNECTOR J400 (PRIME POWER)(PAGE 1OF 2)

D3–21 2–21–97

14 TABLE D3.4.2.2–2 DETAILED ELECTRICAL DESCRIPTIONOF HAB PDGF CONNECTOR J401 (REDUNDANT POW-ER)(PAGE 1 OF 2)

D3–23 2–21–97

15 TABLE D3.4.2.2–3 DETAILED ELECTRICAL DESCRIPTIONOF HAB PDGF CONNECTOR J402 (BACKUP DRIVE POWER)

D3–25 2–21–97

16 TABLE D3.4.4.1–1 DETAILED ELECTRICAL DESCRIPTIONOF LAB PDGF CONNECTOR J403 (1553 & VIDEO)(PAGE 1OF 2)

D3–26 2–21–97


D3–28 2–21–97


D3–30 2–21–97


D3–32 2–21–97

20 TABLE D3.4.4.2–1 DETAILED ELECTRICAL DESCRIPTIONOF HAB PDGF CONNECTOR J403 (1553 & VIDEO)(PAGE 1OF 2)

D3–34 2–21–97


B – 2

21 TABLE D3.4.4.2–2 DETAILED ELECTRICAL DESCRIPTIONOF HAB PDGF CONNECTOR J404 (1553 & VIDEO)(PAGE 1OF 2)

D3–36 2–21–97

22 TABLE F3.4.2.1–1 DETAILED ELECTRICAL DESCRIPTIONOF FSEGF TO USL CONNECTOR J300 (PRIME POW-ER)(PAGE 1 OF 2)

F3–15 2–21–97

23 TABLE F3.4.2.1–2 DETAILED ELECTRICAL DESCRIPTIONOF FSEGF TO USL CONNECTOR J301 (REDUNDANT POW-ER)(PAGE 1 OF 2)

F3–17 2–21–97

24 TABLE F3.4.4–1 DETAILED ELECTRICAL DESCRIPTION OFFSEGF TO USL CONNECTOR J303 (1553 & VIDEO)(PAGE 1OF 2)

F3–19 2–21–97


F3–21 2–21–97


F3–23 2–21–97

TBD E3.2–1 PHYSICAL ORIENTATION OF THE PWP IN THE WIFON THE MBS

F3–23 2–21–97

TBD TABLE D3.4.2.3–1 RECEPTACLE INSTALLATION DRAWINGNUMBER AND WIRE HARNESS DRAWING NUMBER

D3–23


D3–24


D3–36


D3–37


D3–38

TBD FIGURE H3.2–1 VSC MODULE MOUNTING BRACKET H3–4

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