SSP_42004_Part_2-Update_to_Cover.pdf

PDF 2 MB Posted Oct 31, 2019

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

About this file

Written by GovTribe AI · Dec 28, 2023

This notice announces a solicitation for the Human Space Flight Technical Integration Contract (HSFTIC). NASA/JSC will issue a request for proposal for technical integration services to support human space flight programs. The procurement is a total small business set-aside with a NAICS code of 541715 and size standard of 1,250 employees. The RFP is expected to release on November 1, 2019 with a proposal due date of December 11, 2019. The solicitation and any amendments will be available on the Johnson Space Center procurement website and Federal Business Opportunities portal. Prospective offerors must notify the agency of their intent to submit a proposal and are responsible for monitoring the websites for solicitation materials. All technical questions must be submitted in writing.

From the source

SSP 42004 Part 2-Update to Cover

View the file

Other files for this federal contract opportunity

Other files attached to Human Space Flight Technical Integration Contract (HSFTIC), newest first.
File	Type	Posted
HSFTIC J-17 placeholder (FRFP).docx	DOCX document	Dec 4, 2019
HSFTIC Interested Parties List - Rev. 1.pdf	PDF	Nov 19, 2019
MD_1015_RA_FINAL.docx	DOCX document	Oct 31, 2019
SSP41142P1_RF_CD_012044_.pdf	PDF	Oct 31, 2019
42097P1_AE_RF_012968.pdf	PDF	Oct 31, 2019
SSP41017p1rG.pdf	PDF	Oct 31, 2019
SSP41143Pt1RevC.PDF	PDF	Oct 31, 2019
6.0.zip	ZIP file	Oct 31, 2019
N_PR_9501_002E_.pdf	PDF	Oct 31, 2019
SSP_50316-Rev_C.docx	DOCX document	Oct 31, 2019
SSP_57011_Rev_E.docx	DOCX document	Oct 31, 2019
Applicable_5.zip	ZIP file	Oct 31, 2019
ISS_Program_Flight_Rate.pptx	PPTX presentation	Oct 31, 2019
MD_1040_FINAL_PSF_US_Charter.docx	DOCX document	Oct 31, 2019
SSP_50578-RevC.docx	DOCX document	Oct 31, 2019
42097P2RE_AE_RE_012967.pdf	PDF	Oct 31, 2019
DSG-PLAN-004_Gateway_Configuration_and_Data_Management_Plan_Baseline.pdf	PDF	Oct 31, 2019
SSP_50826.doc	DOC document	Oct 31, 2019
SSP-50615_Baseline.doc	DOC document	Oct 31, 2019
Subsystem_&_Mission_Functions_to_Modules.xlsx	XLSX spreadsheet	Oct 31, 2019
Gateway_generic_org_chart.pptx	PPTX presentation	Oct 31, 2019
SSP_50038.DOC	DOC document	Oct 31, 2019
SSP_50190-RevF.docx	DOCX document	Oct 31, 2019
SSP-50715_RevA.docx	DOCX document	Oct 31, 2019
SSP_50273_Rev_J.docx	DOCX document	Oct 31, 2019
50281.DOC	DOC document	Oct 31, 2019
SSP_50469-RevD-Retired.docx	DOCX document	Oct 31, 2019
Initial_Baseline_DSG-CONOP-001_06_2019.docx	DOCX document	Oct 31, 2019
POH_Vol_2_2-2-18.pdf	PDF	Oct 31, 2019
SSP_50200-01-ANXZ-RevB_SPIP_OZ.docx	DOCX document	Oct 31, 2019
SSP_50744-Rev_A.docx	DOCX document	Oct 31, 2019
ssp42097_p2_rd.pdf	PDF	Oct 31, 2019
SSP_52055_Revision_D.doc	DOC document	Oct 31, 2019
Work_Load_Indicators_Matrix_FRFP.xlsx	XLSX spreadsheet	Oct 31, 2019
SSP_41140_P2_RD_111010.pdf	PDF	Oct 31, 2019
SSP_42007-Rev_L-SSCD_15992.docx	DOCX document	Oct 31, 2019
SSP_50420-HTV3-Baseline.docx	DOCX document	Oct 31, 2019
Signed_Approved_Charter_31Aug08_IRT_Charter.doc	DOC document	Oct 31, 2019
SSP_41147,_Part_1_Rev_C.pdf	PDF	Oct 31, 2019
SSP_42121-Part_1-RevC.docx	DOCX document	Oct 31, 2019
SSP_50754-RevA-DCN001-EAR99.docx	DOCX document	Oct 31, 2019
SSP_50839-RevB-DCN001-Collated_Master.pdf	PDF	Oct 31, 2019
SSP41148.pdf	PDF	Oct 31, 2019
PALSTORE.PROD.O0073170.G0000001.IL	TXT text file	Oct 31, 2019
SSP_30575-RevF.docx	DOCX document	Oct 31, 2019
SSP_41165-RevN.docx	DOCX document	Oct 31, 2019
SSP_50005_Rev_G.pdf	PDF	Oct 31, 2019
SSP_50309_Part_2.pdf	PDF	Oct 31, 2019
DRFP_Industry_Questions_and_Answers.pdf	PDF	Sep 24, 2019
Draft_HSFTIC_Request_for_Proposal.pdf	PDF	Aug 16, 2019

Show all 50

Human Space Flight Technical Integration Contract (HSFTIC) has more files on GovTribe.

On GovTribe

Work with this file on GovTribe

Download the original file
Contacts named in this file
Similar government files
Ask GovTribe AI about this file

Try for free Login

Text version

The file's text, extracted by GovTribe without its formatting.

SSP 42004, Part 2, Revision C

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

Revision C

February 15, 2002

This document is currently under review to retire. Unique and/or required data is being reviewed to be documented in the Part 1 version. After completion of the review a CR will be written to update Part 1 and retire Part 2. Estimated Completion Date: December 2013.

Please contact the Points of Contact: JSC/Cheryln Tignor, Michael D. Wright and CSA/Mathieu Prieur.

National Aeronautics and Space Administration International Space Station Program Johnson Space Center Houston, Texas Contract No. NNJ12GA46C

SSP 42004, Part 2, Revision C 15 February 2002 ii

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 000729, EFF. 09–08–98) 03–09–99

Note: Revision A was developed in a special meeting in February 1997 with International Partners per IFM 1MSS17013–03. This document was reviewed line by line and issues worked out and agreed to. Any PIRNs outstanding were withdrawn and coordinated as part of the meeting.

B Revision B (Reference per SSCD 002801, EFF. 02–07–00) 06–15–00

Incorporates the following PIRNs associated with the appropriate SSCNs.

PIRN 42004-NA–2005 IRN 0001 SSCN 000843

PIRN 42004-NA–2006 IRN 0001 SSCN 000843

PIRN 42004-NA–2007A IRN 0001 SSCN 000843

PIRN 42004-NA–2008 IRN 0001 SSCN 000843

PIRN 42004-NA–2009A IRN 0001 SSCN 000843

PIRN 42004-NA–2010A IRN 0001 SSCN 000843

PIRN 42004-NA–2011 IRN 0001 SSCN 000843

PIRN 42004-NA–2013 IRN N/A SSCN 002801

Revision B accounts for impacts identified in the following SSCNs: 000653, 000845, 000773, 001004, 000832, 000671, 000877, 000894, 000915, 000844, 001029, 001051, 001052, 001026, 000823, 000673, 000585, 000588, and 000554.

Revision B also closes IRN 0346 for SSCN 000346 as the PIRN 42004–NA–2001A was withdrawn.

C Revision C ( Reference per SSCD 006769, EFF. 05/14/02) 03–14–03

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

PIRN IRN SSCN

42004–NA–2002 IRN N/A 000600

42004-NA–2003 IRN N/A 006769

42004-NA–2012B IRN N/A 000737

42004-NA–2015B IRN N/A 006769

N/A 0004 002133 N/A 0005 002134 N/A 0006 002191 N/A 0007 002130

Revision C closes the following SSCNs as they were withdrawn or overcome by events:

000567, 000583, 000591, 000889, 001481, 001594

NOTE: IRN 0003 has been retired without use.

ERU: /s/ M. Hehn 03–14–03 iii

PREFACE

SSP 42004, Mobile Servicing System to User (Generic) Interface Control Document, Part 2, shall be implemented on all new Program contractural and internal activity and shall be included in any existing contracts through contract changes. This document is under the control of the Space Station Control Board (SSCB) with the concurrence of the respective International Partners, any changes or revisions will be approved by the SSCB and the respective International Partners.

/s/ Denny A. Kross 5–2–96

Program Manager, Date International Space Station Alpha iv

NASA/CSA

INTERNATIONAL SPACE STATION PROGRAM

MOBILE SERVICING SYSTEM TO USER (GENERIC)

INTERFACE CONTROL DOCUMENT PART 2

15 FEBRUARY 2002

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 6 March 96 v

INTERNATIONAL SPACE STATION PROGRAM

MOBILE SERVICING SYSTEM TO USER (GENERIC)

INTERFACE CONTROL DOCUMENT PART 2

FEBRUARY 15, 2002

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

Freddie G. Young OM5/Muniz

Freddie Garrison Young

Gregg Singer

Quentin L. Henry

Michael Engle

OM5/Muniz

OM5/NASA

Boeing

/s/Freddie Garrison Young 7/31/02

7/31/02/s/Quentin L. Henry

/s/Gregg Singer 4/26/02

/s/Michael Engle 8/2/02

/s/Freddie G. Young 7/31/02 vi

CONCURRENCE

INTERNATIONAL SPACE STATION PROGRAM

MOBILE SERVICING SYSTEM TO USER (GENERIC)

INTERFACE CONTROL DOCUMENT PART 2

Product Group–1 ICWG

Product Group–3 ICWG

SIGNATURE

PRINT NAME

DATE

SIGNATURE

PRINT NAME

DATE

Representative for Concurrence

SPAR

SIGNATURE

PRINT NAME

DATE

Product Group–2 ICWG

SIGNATURE

PRINT NAME

DATE

Representative for Concurrence

L. T. Archibald

/s/ L. T. Archibald 2/28/96

N/A

Ralph Thompson

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

P. Chadwick

/s/ P. Chadwick 4/3/96 vii

INTERNATIONAL SPACE STATION PROGRAM

MOBILE SERVICING SYSTEM TO USER (GENERIC)

INTERFACE CONTROL DOCUMENT PART 2

LIST OF CHANGES

FEBRUARY 15, 2002

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

SSCBD ENTRY DATE CHANGE PARAGRAPH(S)

006769 02–02 NA–2003 2.2

006769 02–02 NA–2015B B3.1.1, B3.1.3, T:B3.1.3–1 (add), T:B3.1.3–2 (add),B3.1.4(add), B3.2, B3.2.1(add), B3.2.1.1(add), B3.2.1.1.1(add), B3.2.1.2(add), B3.2.1.3(add), B3.2.1.4(add), B3.2.2(add), B3.2.2.1(add), B3.2.2.1.1(add), B3.2.2.1.2(add), B3.2.2.1.3(add), B3.2.2.1.4(add), B3.4.2, B3.5, F:B3.2–1(deleted), F:B3.2–2(deleted), F:B3.2–3(deleted), F:B3.2.1–1, (2 pages) (add), F:B3.2.2.1–1 (3 pages) (add), F:B3.4–1, F:B3.4.2–1(add), T:3.4.2–1

000600 02–02 NA–2002 2.1

000737 02–02 NA–2012B Figure A3.4–4

NA–2005 Section H

NA–2006 Section K

NA–2007A Section C

NA–2008 Section D

NA–2009A Section L

NA–2010A Section G

NA–2011 Section J

NA–2013 A3.2–1

NA–2013 Issue Sheet

42004–02–TC–01

viii

TABLE OF CONTENTS

PARAGRAPH PAGE

1.0 INTRODUCTION 1–1

1.1 PURPOSE AND SCOPE 1–1

1.2 PRECEDENCE 1–1

1.3 RESPONSIBILITY AND CHANGE 1–1

2.0 DOCUMENTS 2–1

2.1 APPLICABLE DOCUMENTS 2–1

2.2 REFERENCE DOCUMENTS 2–1

SECTION A3 PDGF TO USER INTERFACES A3–1

A3.0 INTERFACE DEFINITION A3–1

A3.1 GENERAL A3–1

A3.1.1 INTERFACE DESCRIPTION A3–1

A3.1.2 ENGINEERING UNITS AND TOLERANCES A3–1

A3.2 STRUCTURAL/MECHANICAL INTERFACES A3–1

A3.3 ENVIRONMENTS A3–1

A3.4 ELECTRICAL INTERFACES A3–1

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

A3.4.2 PDGF POWER CONNECTORS AND PIN ASSIGNMENTS A3–2

A3.4.3 PDGF DATA AND PFM VIDEO INTERFACES A3–2

A3.4.3.1 PDGF DATA AND VIDEO CONNECTORS AND PIN ASSIGNMENTS A3–3

A3.4.4 VIDEO PROVISIONS FOR USERS A3–3

A3.5 THERMAL INTERFACES A3–3

A3.6 SOFTWARE INTERFACES A3–3

A3.7 PDGF TARGET A3–3

SECTION B3 MCAS TO USER INTERFACE B3–1

B3.0 INTERFACE DEFINITION B3–1

B3.1 GENERAL B3–1

B3.1.1 INTERFACE DESCRIPTION B3–1

B3.1.2 DELETED B3–1

B3.1.3 ENGINEERING UNITS AND TOLERANCES B3–1

B3.1.4 GENERAL NOTES B3–2

B3.2 STRUCTURAL/MECHANICAL INTERFACES B3–2

B3.2.1 MCAS ACTIVE HALF INTERFACES B3–2

B3.2.1.1 MCAS GUIDE VANE INTERFACE B3–2

B3.2.1.1.1 MCAS GUIDE VANE READY TO LATCH INDICATORS B3–2

B3.2.1.2 MCAS CAPTURE LATCH ASSEMBLY INTERFACE B3–3

B3.2.1.3 MCAS UMA ACTIVE HALF INTERFACE B3–3

B3.2.1.4 EBCS TARGET INTERFACES B3–3

B3.2.2 USER INTERFACES B3–3

TABLE OF CONTENTS

PARAGRAPH PAGE

B3.2.2.1 MCAS PASSIVE HALF INTERFACES B3–3

B3.2.2.1.1 USER GUIDE PIN ASSEMBLY INTERFACE B3–4

B3.2.2.1.2 USER CAPTURE LATCH ASSEMBLY INTERFACE B3–4

B3.2.2.1.3 USER UMA PASSIVE HALF INTERFACE B3–4

B3.2.2.1.4 EBCS CAMERA SYSTEM INTERFACE B3–4

B3.3 DELETED B3–4

B3.4 ELECTRICAL INTERFACES B3–4

B3.4.1 POWER, RETURN AND GROUNDING INTERFACES B3–4

B3.4.2 POWER CONNECTORS AND PIN ASSIGNMENTS B3–5

B3.4.3 DATA INTERFACES B3–5

B3.4.3.1 DATA CONNECTORS AND PIN ASSIGNMENTS B3–5

B3.5 ENVIRONMENTS B3–5

B3.6 SOFTWARE INTERFACES B3–5

SECTION C3 SDGF TO USER INTERFACES 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 SDGF INTERFACES C3–1

C3.2.1.1 MODIFIED TRUNCATED CONE TARGET INTERFACES C3–1

C3.2.1.2 ENVIRONMENTS C3–2

C3.2.2 USER INTERFACES C3–2

C3.2.2.1 ELECTRICAL INTERFACE C3–2

C3.2.2.2 POWER, RETURN AND GROUNDING INTERFACE C3–2

C3.2.2.3 POWER CONNECTOR AND PIN ASSIGNMENTS C3–2

C3.2.2.4 USER VIDEO INTERFACE C3–2

C3.2.2.5 USER DATA INTERFACE C3–2

C3.2.2.6 DATA AND VIDEO CONNECTORS AND PIN ASSIGNMENTS C3–2

C3.2.2.7 ENVIRONMENTS C3–2

SECTION D3 MICRO CONICAL FITTING TO USER INTERFACES D3–1

D3.0 INTERFACE DEFINITION D3–1

D3.1 GENERAL D3–1

D3.1.1 INTERFACE DESCRIPTION D3–1

D3.1.2 INTERFACE RESPONSIBILITIES D3–1

D3.1.3 ENGINEERING UNITS AND TOLERANCES D3–1

D3.2 STRUCTURAL/MECHANICAL INTERFACES D3–1

TABLE OF CONTENTS

PARAGRAPH PAGE

D3.2.1 MICRO CONICAL FITTING INTERFACES D3–1

D3.3 ENVIRONMENTS D3–1

D3.4 SOFTWARE INTERFACES D3–1

SECTION E3 RESERVED E3–1

SECTION F3 RESERVED F3–1

SECTION G3 SOCKET DRIVE EXTENSION TOOL TO USER INTERFACES 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 SOCKET DRIVE EXTENSION TOOL INTERFACES G3–1

G3.3 ENVIRONMENTS G3–1

G3.4 SOFTWARE INTERFACES G3–1

SECTION H3 MODIFIED MICRO FIXTURE TO USER INTERFACES H3–1

H3.0 INTERFACE DEFINITION 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

H3.2.1 MODIFIED MICRO FIXTURE INTERFACES H3–1

H3.2.2 MODIFIED DEXTROUS HANDLING TARGET INTERFACES H3–1

H3.3 ENVIRONMENTS H3–1

H3.4 SOFTWARE INTERFACES H3–1

SECTION I3 FRGF TO USER INTERFACES I3–1

I3.0 INTERFACE DEFINITION I3–1

SECTION J3 ROBOT OFFSET SOCKET TOOL TO MODIFIED MICRO FIXTURE

INTERFACES J3–1

J3.0 INTERFACE DEFINITION J3–1

J3.1 GENERAL J3–1

J3.1.1 INTERFACE DESCRIPTION J3–1

J3.1.2 INTERFACE RESPONSIBILITIES J3–1

J3.1.3 ENGINEERING UNITS AND TOLERANCES J3–1

J3.2 STRUCTURAL/MECHANICAL INTERFACES J3–1

J3.2.1 OST TO MODIFIED MICRO FIXTURE INTERFACES J3–1

J3.3 ENVIRONMENTS J3–1

TABLE OF CONTENTS

PARAGRAPH PAGE

J3.4 SOFTWARE INTERFACES J3–1

SECTION K3 MODIFIED MICRO CONICAL FITTING TO USER INTERFACES K3–1

K3.0 INTERFACE DEFINITION K3–1

K3.1 GENERAL K3–1

K3.1.1 INTERFACE DESCRIPTION K3–1

K3.1.2 INTERFACE RESPONSIBILITIES K3–1

K3.1.3 ENGINEERING UNITS AND TOLERANCES K3–1

K3.2 STRUCTURAL/MECHANICAL INTERFACES K3–1

K3.2.1 MODIFIED MICRO CONICAL FITTING INTERFACES K3–1

K3.3 ENVIRONMENTS K3–1

K3.4 SOFTWARE INTERFACES K3–1

SECTION L3 OTCM TO SDGF INTERFACES L3–1

L3.0 INTERFACE DEFINITION L3–1

L3.1 GENERAL L3–1

L3.1.1 INTERFACE DESCRIPTION L3–1

L3.1.2 INTERFACE RESPONSIBILITIES L3–1

L3.1.3 ENGINEERING UNITS AND TOLERANCES L3–1

L3.2 STRUCTURAL/MECHANICAL INTERFACES L3–1

L3.2.1 OTCM INTERFACES L3–1

L3.2.1.1 OTCM ELECTRICAL INTERFACE L3–1

L3.2.1.2 OTCM POWER, RETURN AND GROUNDING INTERFACE L3–2

L3.2.1.3 OTCM POWER CONNECTOR AND PIN ASSIGNMENTS L3–2

L3.2.1.4 OTCM VIDEO INTERFACE L3–2

L3.2.1.4.1 OTCM CAMERA INTERFACE L3–2

L3.2.1.4.2 OTCM LIGHTS INTERFACE L3–2

L3.2.1.4.3 OTCM VIDEO CONNECTORS AND PIN ASSIGNMENTS L3–2

L3.2.1.5 OTCM DATA INTERFACE L3–2

L3.2.1.6 OTCM DATA CONNECTORS AND PIN ASSIGNMENTS L3–2

L3.2.1.7 ENVIRONMENTS L3–2

L3.2.2 SDGF INTERFACES L3–3

L3.2.2.1 ENVIRONMENTS L3–3

APPENDIX

APPENDIX PAGE

A ABBREVIATIONS AND ACRONYMS A–1

B ISSUE SHEETS B–1

C TBD/TBS LIST C–1

xii

TABLE OF CONTENTS

FIGURES

FIGURES PAGE

A3.2–1 PDGF INTERFACES TO USERS A3–4

A3.2–2 PDGF INTERFACE TO USERS A3–5

A3.2–3 PDGF INTERFACE TO USERS A3–6

A3.4–1 PDGF TO USER (VIA SSRMS) ELECTRICAL INTERFACE AND CURRENT

PROTECTION DIAGRAM A3–7

A3.4–2 PDGF TO USER (VIA POA) ELECTRICAL INTERFACE AND CURRENT

PROTECTION DIAGRAM A3–8

A3.4–3 PDGF TO USER (VIA SPDM) ELECTRICAL INTERFACE AND CURRENT

PROTECTION DIAGRAM A3–9

A3.4–4 JEM–PM TO PDGF KEEP–ALIVE ELECTRICAL SYSTEM DIAGRAM A3–10

A3.4–5 APM TO PDGF KEEP–ALIVE ELECTRICAL SYSTEM DIAGRAM A3–11

B3.2–1 DELETED B3–6

B3.2–2 DELETED B3–6

B3.2–3 DELETED B3–6

B3.2.1–1 MCAS TO USER MECHANICAL INTERFACE (1 OF 2) B3–7

B3.2.1–1 MCAS TO USER MECHANICAL INTERFACE (2 OF 2) B3–8

B3.2.2.1–1 USER PASSIVE HALF INTERFACES (1 OF 3) B3–9

B3.2.2.1–1 USER PASSIVE HALF INTERFACES (2 OF 3) B3–10

B3.2.2.1–1 USER PASSIVE HALF INTERFACES (3 OF 3) B3–11

B3.4–1 MCAS TO USER ELECTRICAL INTERFACE AND CURRENT

PROTECTION DIAGRAM B3–12

B3.4.2–1 UMA INSERT PINOUT DESIGNATIONS B3–13

C3.2.1–1 H FIXTURE C3–3

C3.2.1–2 MICRO FIXTURE C3–4

C3.2.1–3 DHT C3–5

C3.2.1–4 UTILITY CONNECTOR C3–6

C3.2.1.1–1 MODIFIED TRUNCATED CONE TARGET C3–7

D3.2.1–1 MODIFIED TRUNCATED CONE TARGET D3–2

D3.2.1–2 MICRO CONICAL FITTING, 3/4 INCH HOLE MCS D3–3

D3.2.1–3 MICRO CONICAL FITTING, FLANGED MCS D3–4

D3.2.1–4 MICRO CONICAL FITTING, FLANGED MCS D3–5

D3.2.1–5 MICRO CONICAL FITTING, STEPPED BORE MCS D3–6

G3.2.1–1 MODIFIED TRUNCATED CONE TARGET G3–2

G3.2.1–2 SOCKET EXTENSION TOOL TO USER (SHEET 1 OF 2) G3–3

G3.2.1–3 SOCKET EXTENSION TOOL TO USER (SHEET 2 OF 2) G3–4

H3.2.1–1 HANDLE MICRO–SQUARE, ORU BOX ASSY OF ( 1 OF 3) H3–2

xiii

TABLE OF CONTENTS

FIGURES CONTINUED

FIGURES PAGE

H3.2.1–1 HANDLE MICRO–SQUARE, ORU BOX ASSY OF ( 2 OF 3) H3–3

H3.2.1–1 HANDLE MICRO–SQUARE, ORU BOX ASSY OF ( 3 OF 3) H3–4

H3.2.1–2 MICRO HANDLE FQDC PFCS ASSY OF H3–5

H3.2.1–3 FIXTURE ROBOT INTERFACE (SHEET 1) H3–6

H3.2.1–4 FIXTURE ROBOT INTERFACE (SHEET 2) H3–7

H3.2.1–5 FIXTURE ROBOT INTERFACE (SHEET 3) H3–8

H3.2.1–6 FIXTURE ROBOT INTERFACE (SHEET 4) H3–9

H3.2.1–7 FIXTURE ROBOT INTERFACE (SHEET 5) H3–10

H3.2.2–1 STATUS INDICATOR FRONT ASSY (SHEET 1 OF OF 2) H3–11

H3.2.2–1 STATUS INDICATOR FRONT ASSY (SHEET 2 OF OF 2) H3–12

H3.2.2–2 STATUS INDICATOR REAR ASSY (SHEET 1 OF OF 2) H3–13

H3.2.2–2 STATUS INDICATOR REAR ASSY (SHEET 2 OF OF 2) H3–14

H3.2.2–3 HOUSING STATUS INDICATOR FQDC ASSY (SHEET 1 OF OF 4) H3–15

H3.2.2–3 HOUSING STATUS INDICATOR FQDC ASSY (SHEET 2 OF OF 4) H3–16

H3.2.2–3 HOUSING STATUS INDICATOR FQDC ASSY (SHEET 3 OF OF 4) H3–17

H3.2.2–3 HOUSING STATUS INDICATOR FQDC ASSY (SHEET 4 OF OF 4) H3–18

H3.2.2–4 HOUSING STATUS INDICATOR FRONT ASSY (SHEET 1 OF OF 4) H3–19

H3.2.2–4 HOUSING STATUS INDICATOR FRONT ASSY (SHEET 2 OF OF 4) H3–20

H3.2.2–4 HOUSING STATUS INDICATOR FRONT ASSY (SHEET 3 OF OF 4) H3–21

H3.2.2–4 HOUSING STATUS INDICATOR FRONT ASSY (SHEET 4 OF OF 4) H3–22

H3.2.2–5 HOUSING STATUS INDICATOR REAR ASSY (SHEET 1 OF OF 4) H3–23

H3.2.2–5 HOUSING STATUS INDICATOR REAR ASSY (SHEET 2 OF OF 4) H3–24

H3.2.2–5 HOUSING STATUS INDICATOR REAR ASSY (SHEET 3 OF OF 4) H3–25

H3.2.2–5 HOUSING STATUS INDICATOR REAR ASSY (SHEET 4 OF OF 4) H3–26

H3.2.2–6 TARGET TELEROBOTIC – ECU ASSEMBLY OF H3–27

H3.2.2–7 TOP TARGET H3–28

H3.2.2–8 BASE TARGET H3–29

H3.2.2–9 FQDC INDICATOR PFCS – ASSY H3–30

H3.2.2–10 HOUSING TARGET H3–31

H3.2.2–11 HOUSING TARGET CONTINUED H3–32

H3.2.2–12 TARGET FACE H3–33

H3.2.2–13 PLATE PATTERN UPPER STATUS INDICATOR H3–34

H3.2.2–14 PLATE PATTERN LOWER STATUS INDICATOR H3–35

J3.2.1–1 SOCKET 7/16 INCHES ROBOTIC OFFSET TOOL J3–2

K3.2.1–1 GRAPPLE MICRO CONICAL – RPCM K3–2

K3.2.1–2 GRAPPLE MICRO CONCICAL – RPCM K3–3

xiv

TABLE OF CONTENTS

FIGURES CONTINUED

FIGURES PAGE

K3.2.1–3 VISUAL TARGET ASSEMBLY – RPCM K3–4

K3.2.1–4 VISUAL TARGET ASSEMBLY – RPCM K3–5

K3.2.1–5 DRIVE SCREW – RPCM K3–6

K3.2.1–6 DRIVE SCREW – RPCM K3–7

L3.2.1–1 OTCM STRUCTURAL/MECHANICAL INTERFACES (SHEET 1 OF 2) L3–4

L3.2.1–2 OTCM STRUCTURAL/MECHANICAL INTERFACES (SHEET 2 OF 2) L3–5

L3.2.1.1–1 OTCM ELECTRICAL INTERFACES L3–6

L3.2.1.4.1–1 OTCM CAMERA AND LIGHTS INTERFACES L3–7

L3.2.1.4.1–2 OTCM CAMERA AND LIGHTS INTERFACE L3–8

L3.2.1.4.1–3 OTCM CAMERA AND LIGHTS INTERFACE L3–9

L3.2.1–5 H FIXTURE – FIXTURE KIT ASSEMBLY L3–10

L3.2.1–6 MICRO FIXTURE KIT L3–11

L3.2.2–1 MICRO HANDLE FQDC PFCS – ASSY OF L3–12

L3.2.2–2 ROBOT FIXTURE INTERFACE L3–13

L3.2.2–3 ROBOT FIXTURE INTERFACE L3–14

L3.2.2–4 ORU BOX MICRO – SQUARE HANDLE – ASSY OF L3–15

L3.2.2–7 ASSY OF ROBOTIC OFFSET TOOL TOP HOUSING (1 OF 2) L3–16

L3.2.2–7 ASSY OF ROBOTIC OFFSET TOOL TOP HOUSING ( 2 OF 2) L3–17

TABLE OF CONTENTS

TABLES

TABLES PAGE

A3.4.2–1 PDGF POWER FROM SSRMS (PRIME) CHARACTERISTICS,

CONNECTORS, AND PIN ASSIGNMENTS (J7) A3–12

A3.4.2–2 PDGF POWER FROM SSRMS (REDUNDANT) CHARACTERISTICS,

CONNECTORS, AND PIN ASSIGNMENTS (J8) A3–13

A3.4.2–3 PDGF POWER FROM POA (PRIME) CHARACTERISTICS, CONNECTORS,

AND PIN ASSIGNMENTS (J7) A3–14

A3.4.2–4 PDGF POWER FROM POA (REDUNDANT) CHARACTERISTICS,

CONNECTORS, AND PIN ASSIGNMENTS (J8) A3–15

A3.4.3.1–1 PDGF DATA AND VIDEO FROM SSRMS (PRIME) CONNECTORS AND PIN

ASSIGNMENTS (J5) A3–16

A3.4.3.1–2 PDGF DATA AND VIDEO FROM SSRMS (REDUNDANT) CONNECTORS

AND PIN ASSIGNMENTS (J6) A3–17

A3.4.3.1–3 PDGF DATA AND VIDEO FROM POA (PRIME) CONNECTORS AND PIN

ASSIGNMENTS (J5) A3–18

A3.4.3.1–4 PDGF DATA AND VIDEO FROM POA (REDUNDANT) CONNECTORS AND

PIN ASSIGNMENTS (J6) A3–19

A3.4.4–1 VIDEO PROVISIONS FOR USERS A3–20

A3.4.4–2 DELETED A3–21

B3.1.3–1 LINEAR TOLERANCES B3–1

B3.1.3–2 ANGULAR TOLERANCES B3–1

B3.4.2–1 MCAS TO USER PRIME AND REDUNDANT POWER AND DATA

CHARACTERISTICS, CONNECTORS, AND PIN ASSIGNMENTS B3–14

1–1

1.0 INTRODUCTION

1.1 PURPOSE AND SCOPE

This Interface Control Document (ICD) Part 2 defines and controls the physical and functional interfaces between the Canadian Mobile Servicing System (MSS) and Users. For purposes of this ICD, the term “user” shall be defined as any payload, pallet, or Orbit–Replaceable Unit (ORU) that interfaces with the Space Station Remote Manipulator System (SSRMS) Latching End Effector (LEE), the Special Purpose Dexterous Manipulator (SPDM) LEE, the Payload/ORU Accommodation (POA), the Mobile Base System (MBS) Common Attach System (CAS), or the SPDM manipulators.

1.2 PRECEDENCE

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

1.3 RESPONSIBILITY AND CHANGE

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

2–1

2.0 DOCUMENTS

2.1 APPLICABLE DOCUMENTS

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

DOCUMENT NO. TITLE

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

Rev C EPS Electrical Performance Specifications 7 July 1997

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

Rev A, DCN–001, Consumer Constraints

DCN–002, 003, 004, 005, 006,

TBD (2191), TBD (2130)

1 Jan 1994

DOD–STD–100 Military Standard Engineering Drawing Practices

SP–M–601 Configuration Item Specification for the Umbilical Mechanism Assembly CI No. 222067

Revision A 14 December 1999

SSQ 21635 Electrical Connector Specifications

MDR–BCS–R–6024 Berthing Cues System Interface Definition Document

NSTS–21000–IDD–ISS Shuttle Orbiter/International Space Station Interface Definition Document

SSP 42003, Part 2 Space Station Manned Base to Mobile Servicing System Interface Control Document, Part 2

SSP 42004, Part 1 Mobile Servicing System (MSS) to User (Generic) Interface Control Document, Part 1

2.2 REFERENCE DOCUMENTS

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

DOCUMENT NO. TITLE

SSP 41000 International Space Station System Specification Reference 1.2

SSP 30459 International Space Station Interface Control Plan Reference 1.3

A3–1

SECTION A3 PDGF TO USER INTERFACES

A3.0 INTERFACE DEFINITION

A3.1 GENERAL

A3.1.1 INTERFACE DESCRIPTION

The physical interface (mechanical, structural, thermal and environmental) plane is defined at the Power and Data Grapple Fixture (PDGF) mounting ring surface to the User. The utility interface plane (power, data and video) is defined between the PDGF harness and the User connectors at the User end of the harness.

A3.1.2 ENGINEERING UNITS AND TOLERANCES

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

A3.2 STRUCTURAL/MECHANICAL INTERFACES

The PDGF attaches to the User via eight fasteners. The bolt hole pattern and related mechanical installation details are defined in Figures A3.2–1 through A3.2–3.

A3.3 ENVIRONMENTS

The PDGF to User electromagnetic, grounding and bonding interface implementation will be as defined in Figures A3.2–1 through A3.2–3.

A3.4 ELECTRICAL INTERFACES

The SSRMS Tip LEE will provide power, data and Pulse Frequency Modulation (PFM) sync and control, and PFM video interfaces to the User via the User PDGF as defined in Figure A3.4–1.

A3–2

The MBS POA will provide power, data and PFM sync and control, and PFM video interfaces to the User via the User PDGF as defined in Figure A3.4–2.

The SPDM LEE will provide power interfaces to the User via the User PDGF as defined in Figure A3.4–3 (TBD#1).

The SSRMS will provide Keep–Alive power to the JEM–PM via the PDGF as defined in Figure A3.4–4.

The SSRMS will provide Keep–Alive power to the APM via the PDGF as defined in Figure A3.4–5.

A3.4.1 POWER, RETURN AND GROUNDING INTERFACES

The SSRMS LEE and MBS POA will provide power, return and grounding interfaces to the User via the PDGF as shown in Figures A3.4–1 and A3.4–2.

The PDGF external harness design for a User will be unique for each application. An example of a PDGF external harness design is shown in SSP 42003, Part 2, Section D.

A3.4.2 PDGF POWER CONNECTORS AND PIN ASSIGNMENTS

The PDGF power connectors and pin assignments for the User (power via the SSRMS Tip LEE) will be as defined in Tables A3.4.2.–1 through A3.4.2.–2.

The PDGF power connectors and pin assignments for the User ( power via the MBS POA) will be as defined in Tables A3.4.2.–3 through A3.4.2.–4.

The PDGF power connectors and pin assignments for the User ( power via the SPDM LEE) will be as defined in Tables A3.4.2.–5 through A3.4.2.–6 (TBD#2).

A3.4.3 PDGF DATA AND PFM VIDEO INTERFACES

The C & DH subsystem will support data interfaces between the User and the SSRMS LEE.

The C & DH subsystem will support data interfaces between the User and the MBS POA.

PFM sync and control and PFM video will be carried by copper lines between the User PDGF and the SSRMS LEE, and User PDGF and the MBS POA.

A3–3

A3.4.3.1 PDGF DATA AND VIDEO CONNECTORS AND PIN ASSIGNMENTS

The PDGF data and PFM video connectors and pin assignments for the User (via the SSRMS Tip LEE) will be as defined in Tables A3.4.3.1–1 through A3.4.3.1–2.

The PDGF data and PFM video connectors and pin assignments for the User ( via the MBS POA) will be as defined in Tables A3.4.3.1–3 through A3.4.3.1–4.

A3.4.4 VIDEO PROVISIONS FOR USERS

During SSRMS or MBS POA operations, the MSS will provide video capability as defined in Table A3.4.4–1.

A3.5 THERMAL INTERFACES

The PDGF to User thermal interface implementation will be as defined in Figures A3.2–1 through A3.2–3.

A3.6 SOFTWARE INTERFACES

There are no software interfaces between the User PDGF and the SSRMS LEE or MBS POA.

A3.7 PDGF TARGET

The PDGF grapple target will have features as defined in Figures A3.2–1 through A3.2–3.

A3–4

(Reference SPAR drawing 51618–0012, sheet 1 of 3)

USER STRUCTURE SHALL PROVIDE FOR CLASS ’H’ AND ’R’ ELECTRICAL

BONDING AS PER SSP 30245. CLASS ’R’ BOND IS TO BE ACHIEVED

THROUGH DIRECT PRE LOADED CONTACT BETWEEN �H� CONTACT

PADS AND USER MOUNTING SURFACE. CLASS ’H’ BOND IS ACHIEVED

THROUGH THE CONNECTOR (SEE PIN–OUT).

FIGURE A3.2–1 PDGF INTERFACES TO USERS

A3–5

(Reference SPAR drawing 51618–0012, sheet 2 of 3)

FIGURE A3.2–2 PDGF INTERFACE TO USERS

A3–6

(Reference SPAR drawing 51618–0012, sheet 3 of 3)

FIGURE A3.2–3 PDGF INTERFACE TO USERS

A3–7

User Provided Connectors

ÉÉ

12ga

PDGF/User Interface Plane Provided Connectors

SSRMS LEE/User PDGF Interface Plane

Payload Power A1 Return A1

SSBA

12ga Payload Power A2

Return A2

Ground

ÉÉ

É É É É É É

ÉÉ

É É É É É É

Internal PDGF Wiring and Connectors

User Determined

PDGF

Harness Length

É É É É É É

SSRMS

É É É É É É

User Bus A

Data Bus A

12ga Payload Power B1 Return B1

12ga

Payload Power B2 Return B2

Ground

ÉÉ

1 TSP 22ga

ÉÉ

É É É É É É

ÉÉ

É É É É É É

É É É É É É É É É É É É

User Bus B

Data Bus B

MSS Local Bus B (LB1 B)

1 TSP 22ga

MSS Local Bus A (LB1 A)

1 TSP

Bus Coupler

RPC

25A

Return

RPC

25A

12ga

To User Loads

PFM Video 1 PFM Video 2 RD316

PFM Sync and Control 1 RD316

PFM Video 3

PFM Sync and Control 2 RD316

RD316

12ga 12ga

12ga

12ga 12ga

12ga

1 TSP 22ga

RD316

12ga 12ga

12ga

12ga 12ga

12ga

1 TSP 22ga

SSBA

SSBASSBA

PDGF User Interface Plane

RD316

FIGURE A3.4–1 PDGF TO USER (VIA SSRMS) ELECTRICAL INTERFACE AND CURRENT

PROTECTION DIAGRAM

A3–8

MBS

12ga

POA/User PDGF Interface Plane

Payload Power A1 Return A1

SSBA

12ga Payload Power A2 Return A2

Ground

Ï Ï Ï Ï Ï Ï

ÏÏ

Internal PDGF Wiring and Connectors

Ï Ï Ï Ï Ï Ï Ï

POA

Ï Ï Ï Ï Ï Ï Ï

User Bus A

Data Bus A

12ga Payload Power B1

Return B1

12ga Payload Power B2

Return B2

Ground

Ï Ï Ï Ï Ï Ï

1 TSP 22ga

Ï Ï Ï Ï Ï Ï Ï

ÏÏ

Ï Ï Ï Ï Ï Ï Ï Ï Ï Ï Ï Ï Ï

User Bus B

Data Bus B

SSBAMSS Local Bus B (LB1 B)

1 TSP 22ga

MSS Local Bus A (LB1 A)

1 TSP

RPC

25A

Return

RPC

25A

12ga

To User Loads

PFM Video 1 PFM Video 2 RD316 PFM Sync and Control 1 RD316

PFM Video 3

PFM Sync and Control 2 RD316

RD316

12ga 12ga

12ga

12ga 12ga

12ga

1 TSP 22ga

1 TSP 22ga 1 TSP 22ga

1 TSP 22ga

RD316

12ga 12ga

12ga

12ga 12ga

12ga

1 TSP 22ga

User Provided Connectors

ÉÉ

PDGF/User Interface Plane Provided Connectors

Bus Coupler

User Determined

PDGF

Harness Length

PDGF User Interface Plane

RD316

FIGURE A3.4–2 PDGF TO USER (VIA POA) ELECTRICAL INTERFACE AND CURRENT

A3–9

TBD #1

FIGURE A3.4–3 PDGF TO USER (VIA SPDM) ELECTRICAL INTERFACE AND CURRENT

A3–10

ÓÓÓÓÓÓÓÓ

Ñ Ñ Ñ Ñ Ñ Ñ Ñ

ÓÓ

Ñ Ñ Ñ Ñ Ñ Ñ Ñ

ÓÓ

ÑÑÑÑ

12ga

NASDA

Harnesses and

Connectors

JEM to PDGF Interface Plane

NASDA

Connector

Panel

PDGF Harnesses and

Connectors

JEM

Heaters

JEM

Heaters

ÓÓÓÓ

ÓÓÓÓ ÓÓNASDA Connectors

PDGF Connectors

Resources From

SSRMS

ÑÑÑ

J E M

P D G F

8ga

Notes:

1) The JEM PDGF Harness and Connectors provide only Prime and Redundant User Power Feeds (PDGFPL1 and PDGFPL2).

2) Total keep–alive power characteristics are as defined in SSP 41151, Paragraph 3.3.2.1.2.

Resources From

SSRMS

1 1

PDGFPL1

PDGFPL2

FIGURE A3.4–4 JEM–PM TO PDGF KEEP–ALIVE ELECTRICAL SYSTEM DIAGRAM

A3–11

ÓÓÓÓÓÓÓÓÓ

ÓÓ

Ñ Ñ Ñ Ñ Ñ Ñ Ñ

ÓÓ

Ñ Ñ Ñ Ñ Ñ Ñ Ñ

ÓÓ

ÑÑÑÑÑ

ÑÑÑÑ

12ga

12ga 2

12ga

ESA

Harnesses and

Connectors

APM to PDGF Interface Plane ESA Connector Panel

PDGF Harnesses and

Connectors

APM

Heaters

APM

Heaters

ÓÓÓÓ

ÓÓÓÓÓ

ÓÓÓÓÓ ÓÓESA Connectors

PDGF Connectors

Resources From

SSRMS

ÑÑÑ

A P M

P D G F

8ga

ÑÑÑ

Ó Ó Ó Ó Ó

Ñ Ñ Ñ Ñ Ñ Ñ Ñ Ñ Ñ Ñ Ñ Ñ

ÓÓ

Ó Ó Ó Ó Ó Ó

ÓÓ

1 TSP

ÑÑÑÑ

BC BC

Heater Control

Unit

Heater Control

Unit Note 1) The MSS LB termination is shown for reference only.

Resources From

SSRMS

FIGURE A3.4–5 APM TO PDGF KEEP–ALIVE ELECTRICAL SYSTEM DIAGRAM

A3–12

TABLE A3.4.2–1 PDGF POWER FROM SSRMS (PRIME) CHARACTERISTICS,

CONNECTORS, AND PIN ASSIGNMENTS (J7)

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

POWER SPECIFICATIONS

ÁÁÁÁÁ

Contact

ÁÁÁÁÁ

Signal Function

ÁÁÁÁ

Peak 2

Power

(kW)

ÁÁÁÁÁ

Minimum Voltage

(VDC)

ÁÁÁÁÁ

Maximum Current 3

[A]

ÁÁÁÁ

EMC

Class

ÁÁÁÁÁ

Power 1

Quality Type

ÁÁÁÁÁÁ

Wire Gauge

(ga)

ÁÁÁÁÁ

Ground

Payload Power Bus 1

Return 1

Payload Power Bus 2

Return 2

ÁÁÁÁ

1.8

ÁÁÁÁÁ

108.5

ÁÁÁÁÁ

ÁÁÁÁ

ÁÁÁÁÁ

N/A

ÁÁÁÁÁÁ

Notes:

1) Power quality characteristics at this interface shall meet the interface “C” power quality requirements in SSP 30482 except for minimum voltage.

2) Table reflects design to peak power requirements and the associated minimum voltage at the LEE/PDGF interface plane.

3) Nominal rating of CRPCM output port, as defined in SSP 42004, Section A, Part 1.

4) Connector specifications are as per SSQ 21635.

5) For connector part numbers, refer to Figure A3.2–3.

A3–13

TABLE A3.4.2–2 PDGF POWER FROM SSRMS (REDUNDANT) CHARACTERISTICS,

CONNECTORS, AND PIN ASSIGNMENTS (J8)

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

POWER SPECIFICATIONS

ÁÁÁÁÁ

Contact

ÁÁÁÁÁ

Signal Function

ÁÁÁÁ

Peak 2

Power

(kW)

ÁÁÁÁÁ

Minimum Voltage

(VDC)

ÁÁÁÁÁ

Maximum Current 3

[A]

ÁÁÁÁ

EMC

Class

ÁÁÁÁÁ

Power 1 Quality Type

ÁÁÁÁÁÁ

Wire Gauge

(ga)

ÁÁÁÁÁ

Ground

Payload Power Bus 1

Return 1

Payload Power Bus 2

Return 2

ÁÁÁÁ

1.8

ÁÁÁÁÁ

108.5

ÁÁÁÁÁ

ÁÁÁÁ

ÁÁÁÁÁ

N/A

ÁÁÁÁÁÁ

Notes:

1) Power quality characteristics at this interface shall meet the interface ”C” power quality requirements in SSP 30482, except for minimum voltage.

2) Table reflects design to peak power requirements and the associated minimum voltage at the LEE/PDGF interface plane.

3) Nominal rating of CRPCM output port, as defined in SSP 42004, Section A, Part 1.

A3–14

TABLE A3.4.2–3 PDGF POWER FROM POA (PRIME) CHARACTERISTICS, CONNECTORS,

AND PIN ASSIGNMENTS (J7)

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

POWER SPECIFICATIONS

ÁÁÁÁÁ

Contact

ÁÁÁÁÁ

Signal Function

ÁÁÁÁ

Peak Power 2

(kW)

ÁÁÁÁÁ

Minimum Voltage

(VDC)

ÁÁÁÁÁ

Maximum Current 3

[A]

ÁÁÁÁ

EMC

Class

ÁÁÁÁÁÁ

Power 1

Quality Type

ÁÁÁÁÁ

Wire Gauge

(ga)

ÁÁÁÁÁ

Ground

Payload Power Bus 1

Return 1

Payload Power Bus 2

Return 2

ÁÁÁÁ

1.8

ÁÁÁÁÁ

ÁÁÁÁ

ÁÁÁÁÁÁ

N/A

ÁÁÁÁÁ

Notes:

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

2) Table reflects design to peak power requirements and the associated minimum voltage at the POA/PDGF interface plane.

3) Nominal rating of CRPCM output port, as defined in SSP 42004, Section A, Part 1.

4)Connector specifications are as per SSQ 21635.

A3–15

TABLE A3.4.2–4 PDGF POWER FROM POA (REDUNDANT) CHARACTERISTICS,

CONNECTORS, AND PIN ASSIGNMENTS (J8)

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁPOWER SPECIFICATIONSÁÁÁÁÁ

ÁÁÁÁÁ

Contact

ÁÁÁÁÁ

Signal Function

ÁÁÁÁ

Peak 2

Power

(kW)

ÁÁÁÁÁ

Minimum Voltage

(VDC)

ÁÁÁÁÁÁ

Maximum Current 3

[A]

ÁÁÁÁÁ

EMC

Class

ÁÁÁÁ

Power 1

Quality Type

ÁÁÁÁÁ

Wire Gauge

(ga)

ÁÁÁÁÁ

Ground

Payload Power Bus 1

Return 1

Payload Power Bus 2

Return 2

ÁÁÁÁ

1.8

ÁÁÁÁÁ

ÁÁÁÁÁÁ

ÁÁÁÁÁ

ÁÁÁÁ

N/A

ÁÁÁÁÁ

Notes:

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

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

3) Nominal rating of CRPCM output port, as defined in SSP 42004, Section A, Part 1.

A3–16

TABLE A3.4.3.1–1 PDGF DATA AND VIDEO FROM SSRMS (PRIME) CONNECTORS AND

PIN ASSIGNMENTS (J5)

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

CONNECTOR SPECIFICATIONS

ÁÁÁÁÁ

Contact

ÁÁÁÁÁÁÁÁ

Signal Function

ÁÁÁÁÁ

EMC

Type

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Remarks

ÁÁÁÁÁ

ÁÁÁÁÁÁÁÁ

MSS LB1 A Hi

MSS LB1 A Lo

Video Channel 1

Video Channel 2

Sync and Control 1

ÁÁÁÁÁ

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Notes:

1) Specific local bus that supports payloads depends on location of SSRMS.

2) Connector specifications are as per SSQ 21635.

A3–17

TABLE A3.4.3.1–2 PDGF DATA AND VIDEO FROM SSRMS (REDUNDANT) CONNECTORS

AND PIN ASSIGNMENTS (J6)

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

CONNECTOR SPECIFICATIONS

ÁÁÁÁÁ

Contact

ÁÁÁÁÁÁÁÁ

Signal Function ÁÁÁÁÁ

ÁÁÁÁÁ

EMC

Type

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Remarks

ÁÁÁÁÁ

ÁÁÁÁÁÁÁÁ

MSS LB1 B Hi

MSS LB1 B Lo

Video Channel 3

Sync and Control 2

ÁÁÁÁÁ

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Notes:

1) Specific local bus that supports payloads depends on location of SSRMS.

2) Connector specifications are as per SSQ 21635.

A3–18

TABLE A3.4.3.1–3 PDGF DATA AND VIDEO FROM POA (PRIME) CONNECTORS AND PIN

ASSIGNMENTS (J5)

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

CONNECTOR SPECIFICATIONS

ÁÁÁÁÁ

Contact

ÁÁÁÁÁÁÁÁ

Signal Function ÁÁÁÁÁ

ÁÁÁÁÁ

EMC

Type

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Remarks

ÁÁÁÁÁ

ÁÁÁÁÁÁÁÁ

MSS LB1 A Hi

MSS LB1 A Lo

Video Channel 1

Video Channel 2

Sync and Control 1

ÁÁÁÁÁ

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Notes:

1) Connector specifications are as per SSQ 21635.

A3–19

TABLE A3.4.3.1–4 PDGF DATA AND VIDEO FROM POA (REDUNDANT) CONNECTORS

AND PIN ASSIGNMENTS (J6)

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

CONNECTOR SPECIFICATIONS

ÁÁÁÁÁ

Contact

ÁÁÁÁÁÁÁÁ

Signal Function

ÁÁÁÁÁ

EMC

Type

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Remarks

ÁÁÁÁÁ

ÁÁÁÁÁÁÁÁ

MSS LB1 B Hi

MSS LB1 B Lo

Video Channel 3

Sync and Control 2

ÁÁÁÁÁ

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Notes:

1) Connector specifications are as per SSQ 21635.

A3–20

TABLE A3.4.4–1 VIDEO PROVISIONS FOR USERS

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Link

ÁÁÁÁÁÁÁÁÁ

Communication Type

ÁÁÁÁÁÁÁÁÁÁ

# of Channels

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Payload at SSRMS LEE

ÁÁÁÁÁÁÁÁÁ

Video Sync Channels to Payload

Video Channels From Pay-load

ÁÁÁÁÁÁÁÁÁÁ

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Payload at MBS POA

ÁÁÁÁÁÁÁÁÁ

Video Sync Channels To Payload

Video Channels From Pay-load

ÁÁÁÁÁÁÁÁÁÁ

A3–21

TABLE A3.4.4–2 DELETED

B3–1

SECTION B3 MCAS TO USER INTERFACES

B3.0 INTERFACE DEFINITION

B3.1 GENERAL

B3.1.1 INTERFACE DESCRIPTION

The physical interface (mechanical, structural, thermal and environmental) plane is defined between the active half of the MBS Common Attach System (MCAS) and the passive half of the User. The utility interface plane (power and data) is defined between the MCAS Umbilical Mechanism Assembly (UMA) connector and User connector.

There are no video/High Rate Data Link interfaces between the MCAS and the User.

B3.1.2 DELETED

B3.1.3 ENGINEERING UNITS AND TOLERANCES

Unless otherwise noted herein, all dimensions in this document are shown in the English system of Inch Pound (IP) units. Implied tolerances on linear dimensions are defined in Table B3.1.3–1.

Angular Tolerances are shown in Table B3.1.3–2. Orthographic projections are constructed using the third angle projection system.

TABLE B3.1.3–1 LINEAR TOLERANCES

Dimensions Tolerances

.xx +/– .03

.xxx +/– .010

TABLE B3.1.3–2 ANGULAR TOLERANCES

Dimensions Tolerances

X degrees +/– 1 degrees

X degrees X minutes +/– 0 degrees 30 minutes

B3–2

B3.1.4 GENERAL NOTES

The following notes apply to all figures and drawings.

a) All critical tolerances and dimensions shown are in accordance with ANSI Y14.5M–1982, Dimensioning and Tolerancing.

b) All dimensions are in inches (unless otherwise specified).

c) Physical and mechanical interface design definition are in accordance with DOD–

STD–100, Military Standard Engineering Drawing Practices.

B3.2 STRUCTURAL/MECHANICAL INTERFACES

DELETED

B3.2.1 MCAS ACTIVE HALF INTERFACES

The MCAS provides the active half of the interface consisting of the following components:

a) Platform (1)

b) Guide Vane Assemblies (GVA) (3)

c) Capture Latch Assembly (CLA) (1) with Integrated Motor Controller Actuator (IMCA) (2)

d) Umbilical Mechanism Assembly (UMA) Active Half (1) with IMCA (2)

e) External Berthing Camera System (EBCS) Target

The interface and dimensional details of these components are shown in Figures B3.2.1–1, Sheets 1 and 2.

B3.2.1.1 MCAS GUIDE VANE INTERFACE

The MCAS active half provides three Guide Vane Assemblies capable of passive guidance during berthing of the user, and fine alignment while being drawn into final position by the CLA.

SP–M–603 controls the guide vane design. Figures B3.2.1–1, Sheets 1 and 2, show the locations of the guide vanes.

B3.2.1.1.1 MCAS GUIDE VANE READY TO LATCH INDICATORS

a) The MCAS GVAs include Ready to Latch Indicators for providing positive feedback to the

Intravehicular Activity (IVA) crew who are operating the Space Station Remote Manipulator

System (SSRMS).

b) The MCAS GVAs will initiate a signal to the IVA crew operating the SSRMS that a user is properly positioned within the CLA capture envelope prior to CLA activation.

B3–3

B3.2.1.2 MCAS CAPTURE LATCH ASSEMBLY INTERFACE

a) The MCAS active half includes one CLA. The CLA design is controlled by CIS SP–M–600.

b) The MCAS CLA interfaces with the user provided EVA releasable capture bar.

c) The MCAS CLA will be capable of pulling a user into proper position at the specified preload.

B3.2.1.3 MCAS UMA ACTIVE HALF INTERFACE

The MCAS active half includes one UMA active half. The UMA active half is controlled by Boeing specification CIS SP–M–601. The location of the UMA active half is shown in Figures B3.2.1–1, Sheets 1 and 2.

B3.2.1.4 EBCS TARGET INTERFACES

The MCAS Active Half provides mounting provisions for one EBCS Target per the Berthing Cues System (BCS) Interface Definition Document (IDD), MDR–BCS–R–6024, and shown in Figure B3.2.1–1, Sheets 1 and 2.

B3.2.2 USER INTERFACES

B3.2.2.1 MCAS PASSIVE HALF INTERFACES

Each MCAS Passive Half interface includes the following components:

a) Passive half interface structure (1)

b) Guide Pins (3)

c) EVA releasable CLA capture bar (1)

d) UMA passive half (1)

e) External Berthing Camera System (EBCS) Camera

The MCAS passive half to MCAS Active half interface consists of five surfaces including three guide pins which connect to the three guide vanes, an EVA releasable capture bar which connects to the CLA, and the UMA passive half which connects to the MCAS active UMA.

The interface and dimensional details of these components are shown in Figures B3.2.2.1–1, Sheets 1, 2, and 3.

B3–4

B3.2.2.1.1 USER GUIDE PIN ASSEMBLY INTERFACE

Each User provides three guide pins to interface with three MCAS guide vanes. The location of these guide pins is defined in Figures B3.2.2.1–1, Sheets 1 and 2.

B3.2.2.1.2 USER CAPTURE LATCH ASSEMBLY INTERFACE

The User provides one EVA releasable capture bar to interface with the MCAS active half CLA.

The User EVA releasable capture bar is located as defined in Figures B3.2.2.1–1, Sheets 1 and 2, and designed to withstand the MCAS CLA operation of pulling the User into proper position and preload.

B3.2.2.1.3 USER UMA PASSIVE HALF INTERFACE

The User provides one UMA passive half to interface with the MCAS active half UMA. The UMA passive half dimensions and mechanical interfaces are shown in Figures B3.2.2.1–1, Sheets 1, 2, and 3. The User passive half is located as defined in Figures B3.2.2.1–1, Sheets 1, 2, and 3. The User UMA passive half meets the design and operability requirements as specified in

CIS SP–M–601.

B3.2.2.1.4 EBCS CAMERA SYSTEM INTERFACE

The User provides mounting provisions for one EBCS Camera per the BCS IDD, MDR–BCS–R–6024, and shown in Figure B3.2.2.1–1, Sheet 1.

B3.3 DELETED

B3.4 ELECTRICAL INTERFACES

The MCAS to User power and data interfaces will be as defined in Figure B3.4–1.

B3.4.1 POWER, RETURN AND GROUNDING INTERFACES

The MCAS to User power, return and grounding interfaces will be as defined in Figure B3.4–1.

B3–5

B3.4.2 POWER CONNECTORS AND PIN ASSIGNMENTS

The power connectors and pin assignments between the MCAS and the User will be as defined in Table B3.4.2–1 and Figure B3.4.2–1.

B3.4.3 DATA INTERFACES

The C & DH subsystem will support data interfaces between the MCAS and the User as defined in Figure B3.4–1.

B3.4.3.1 DATA CONNECTORS AND PIN ASSIGNMENTS

The data connectors and pin assignments between the MCAS and the User will be as defined in Table B3.4.2–1.

B3.5 ENVIRONMENTS

The MCAS to User grounding interface implementation will be as defined in Figure B3.4–1 and bonding interface implementation will be as defined in Paragraphs B3.2.1.9.1.3 and B3.2.2.9.1.3 of Part 1.

B3.6 SOFTWARE INTERFACES

There are no software interfaces between the MCAS and the User.

B3–6

FIGURE B3.2–1 DELETED

FIGURE B3.2–2 DELETED

FIGURE B3.2–3 DELETED

B3–7

13.857

ORIGINMCASOCS

GUIDE VANE

WELL BOTTOM

CENTERLINE

GUIDE VANE

WELL BOTTOM

CENTERLINE

GUIDE VANE

ASSEMBLY # 1

GUIDE VANE

ASSEMBLY # 2

GUIDE VANE

ASSEMBLY # 3

CAPTURE LATCH

24.000

48.000 3X 4.00

34.139

1.560

41.570

CAPTIVE LATCH

BASE PLATE

19.700

CAPTIVE

LATCH

CLAWS

1.250

41.60

PLATFORM/UMA

SUPPORT BRACKET

INTERFACE

21.956

CAPTIVE

LATCH

BASE PLATE

5.025

3X 15.82

EBCS TARGET

W11

29.125

2X 1.560

37.52

16.80

UMBILICAL

(ACTIVE HALF)

FIGURE B3.2.1–1 MCAS TO USER MECHANICAL INTERFACE (1 OF 2)

B3–8

GUIDE VANE

ASSEMBLY # 2

CAPTURE LATCH ASSEMBLY

UMBILICAL

MECHANISM

ASSEMBLY

(ACTIVE HALF)

22.414

13.629

UMA TIE DOWN BOLT

ORIGIN

MCAS OCS

3.147

TARGET BRACKET

INTERFACE

XGVA WELL

3.397

BOTTOM

FIGURE B3.2.1–1 MCAS TO USER MECHANICAL INTERFACE (2 OF 2)

B3–9

–B –

–A –

.015

3 GUIDE PINS

3.534

30.432 (7.414)

8.50

23.14

MAX (9.360)

11.45MAX

35.45 MIN

(33.775)

30.550

23.450 30.550

.010 A

(1.450 )

–C –

.010 A B

41.000

46.900

49.00

MIN

(1.450 )

3.534

30.282

(7.714)

.028 B C

–E –

(1. 450 )

.020 E CS

.028 B C

31.14

MIN

A A

CLEARANCE

FOR LATCH

MECHANISM

9.8 INCH

DEEP (MIN)

FROM –A –

–D –

Guide Pin 1

ÏÏÏ

ÏÏÏÏ

POTENTIAL CONTACT

AREAS (TYP 3 PLACES) R .25 MIN

(CONTACT AREA)

16.0 MIN

5.414

Camera Mounting Plane

(5.750)

(2.897) 13.857(9.500)

EBCS Camera Attach Interface

Guide Pin 3

Guide Pin 2

10.960

FIGURE B3.2.2.1–1 USER PASSIVE HALF INTERFACES (1 OF 3)

B3–10

–A –

3.75MIN

R.725

.688

1.450

VIEW B –B

(GUIDE PIN DETAIL –TYPICAL 3 PLACES)

( –E– )

.004 A E

C D

FROM A TO B

.004 A E

FROM C TO D

ÎÎÎÎ

–A –

1.142 ±.005 1

1.505 1.495

.020 D SM

SECTION A–A

(CAPTURE BAR)

DIMENSION IS BASED ON SYSTEM PRELOAD REQUIREMENT B3.2.1.3.4.1 OF PART 1.

SEE FIGURE B3.2.1.1.1.1–1 OF PART 1 FOR THE ENTIRE PASSIVE HALF OPERATIONAL

3 SURFACE ROUGHNESS 63 MICROINCHES PER ANSI B46.1–1985.

4 APPLY MIL–L–46010, TYPE I LUBRICANT.

3 4

6 APPLIES TO HEIGHT OF GUIDE PIN ONLY.

ENVELOPE.

GUIDE PIN TO GVA INTERFACE. ELECTRICAL BOND PER REQUIREMENT

B3.2.2.9.1.3 OF PART 1.

MINIMUM PLATFORM HEIGHT IN THIS AREA IS 2.0 INCHES. PLATFORM DESIGN IS

DEPENDENT UPON SYSTEM PRELOAD REQUIREMENT B3.2.1.3.4.1 OF PART 1.

FIGURE B3.2.2.1–1 USER PASSIVE HALF INTERFACES (2 OF 3)

B3–11

(30.282) 7.714

1.126 1.126

.135

–A –

(3.534)

–D –

(30.432)

7.414

.976 .976

.135

–A –

(3.534) –D –

9.360

–F –

.361

2.00

MIN

.16X.16

CHAMFER

2PL

VIEW C

(UMAMOUNTING BRACKET)

.614

4X ∅ .078 THRU

∅ X 90° FS.15

.12

∅ .014 G M

∅ X R.02MAX .288

∅ .008 S

.535

.530

∅ .340

∅ .020 G S A F S

–G –

.014 A F2X2X30°±1°

2X.325 .040X.040

CHAMFER

–E –

33.775

8.36±.07

1.00 ±.07

8.65±.07 .55±.07

SECTION D–D

2.25MAX

VIEW E (4 PLCS)

SECTION F–F

.010 E

∅ .014 D S A F S

1.35”

UMAOperational KeepOut Zone

(4.650) UMA Active Centerline

FIGURE B3.2.2.1–1 USER PASSIVE HALF INTERFACES (3 OF 3)

B3–12

MBS MCAS/USER

INTERFACE PLANE

BUS COUPLER

MCAS/MBS

INTERFACE

W11

P6J4

1 TSP

MSS LOCAL BUS A

1 TSP

P/L

USER HARNESS

AND CONNECTORS

J3 P5

(LOOP BACK)

BIT 0

BIT 1

BIT 4

PARITY

BIT

USER

ADDRESS 21

8AWG

12AWG

J5 P7

GROUND

USER PASSIVE UMA CONNECTOR

RPC

12A

CRPCM (PRIME)

MCAS ACTIVE UMA CONNECTOR

POWER

RETURN

PRIME POWER

TO USER

LOADS

MCAS/MBS

INTERFACE

W12 P10J4

1 TSP

MSS LOCAL BUS B

1 TSP

P/L

8AWG

12AWG

J5 P8

GROUND

RPC

12A

CRPCM (REDUNDANT)

POWER

BIT 2

BIT 3

J1P19

REDUNDANT

POWER

TO USER

LOADS

RETURN

FIGURE B3.4–1 MCAS TO USER ELECTRICAL INTERFACE AND CURRENT

B3–13

FIGURE B3.4.2–1 UMA INSERT PINOUT DESIGNATIONS

B3–14

TABLE B3.4.2–1 MCAS TO USER PRIME AND REDUNDANT POWER AND DATA

CHARACTERISTICS, CONNECTORS AND PIN ASSIGNMENTS

CONNECTOR ID

MCAS Ref Des.: P19 Part Number: NUP1–005, W8072 1F72507

User Ref. Des.: J1 Part Number: NUR1–005, W8041 1F97487

POWER AND DATA SPECIFICATION

Contact

Signal Function Peak

Power (2) (W)

Minimum Voltage

(VDC)

Current (3)

[A]

EMC

Class

Power (1)

Quality

Type Wire Gauge (ga)

Remarks

1 MSS LB A HI NA NA NA RFH NA 22 NU–C–2022S

Contact

145 MSS LB B HI NA NA NA RFH NA 22 NU–C–2022S

Contact

2 MSS LB A LO NA NA NA RFL NA 22 NU–C–2022S

Contact

146 MSS LB B LO NA NA NA RFL NA 22 NU–C–2022S

Contact

50 User Power Bus 1 (4B Pwr)

1350 113 12 EO C 8 NU–C–8S

Contact

103 User Power Bus 2 (3A Pwr)

1350 113 12 EO C 8 NU–C–8S

Contact

51 Return 1 (4B Pwr)

1350 113 12 EO C 8 NU–C–8S

Contact

104 Return 2 (3A Pwr)

1350 113 12 EO C 8 NU–C–8S

Contact

66 Bus 1 GND (4B Pwr)

1350 113 12 EO NA 8 NU–C–8S

Contact

89 Bus 2 GND (3A Pwr)

1350 113 12 EO NA 8 NU–C–8S

Contact

135 ADD Bit 0 NA NA NA ML NA 22 NU–C–2022S Contact

148 ADD Bit 0 RTN NA NA NA ML NA 22 NU–C–2022S Contact

136 * ADD Bit 1 NA NA NA ML NA 22 ADD Bit 1 is shorted

NU–C–2022S

Contact

149 * ADD Bit 1 RTN NA NA NA ML NA 22 NU–C–2022S Contact

137 * ADD Bit 2 NA NA NA ML NA 22 NU–C–2022S Contact

150 * ADD Bit 2 RTN NA NA NA ML NA 22 NU–C–2022S Contact

138 * ADD Bit 3 NA NA NA ML NA 22 ADD Bit 3 is shorted

151 * ADD Bit 3 RTN NA NA NA ML NA 22 NU–C–2022S Contact

B3–15

139 * ADD Bit 4 NA NA NA ML NA 22 NU–C–2022S Contact

152 * ADD Bit 4 RTN NA NA NA ML NA 22 NU–C–2022S Contact

140 * ADD PARITY

BIT

NA NA NA ML NA 22 ADD PARITY

Bit is shorted

153 ADD RTN NA NA NA ML NA 22 NU–C–2022S

Contact

Notes:

* Address is set to 21 with Parity Bit 0

1) The Transient Voltage Limits & Time Duration are as defined in SSP 30482, except for minimum voltage.

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

3) Nominal rating of the MBS CRPCM output port.

4) Refer to SSQ 21637 for connector detailed specification.

C3–1

SECTION C3 SDGF TO USER INTERFACES

C3.0 INTERFACE DEFINITION

C3.1 GENERAL

C3.1.1…

This is the start of the file's text. The full file is on GovTribe.

File details come from the government source that posted it. Updated Dec 28, 2023.