SSP41017p2rJ.pdf

SSP 41017, Part 2

Rack to Mini Pressurized Logistics Module Interface Control Document (ICD) Part 2

Revision J

February 04, 2005

National Aeronautics and Space Administration International Space Station Program Johnson Space Center Houston, Texas Contract No. NAS15−10000 esa european space agency

International Space Station Program

Japan Aerospace Exploration Agency

SSP 41017, Part 2 February 4, 2005 Revision J i

REVISION AND HISTORY PAGE

REV. DESCRIPTION PUB.

DATE

− BASELINE ISSUE (REFERENCE SSCBD BB003562 EFF. 07−01−93)

Incorporating the following IRN:

IRN 0001 (REFERENCE SSCBD BB003562 EFF. 07−01−93)

A REVISION A (REFERENCE SSCBD BB003562A EFF. 09−29−93) 09−93

Incorporating the following IRNs:

IRN 0002 (REFERENCE SSCBD BB003562A EFF. 09−29−93)

IRN 0003 (REFERENCE SSCBD BB003562A EFF. 09−29−93)

DRAFT REVISION B DRAFT 07−95

B REVISION B 06−12−96

Incorporating the following PIRNs:

41017−AS−0002B, 41017−AS−0004F, 41017−AS−0006C,

41017−AS−0007A, 41017−NA−0004, 41017−NA−0005B, 41017−NA−0006

C REVISION C (REFERENCE SSCBD 000403, EFF. 10/04/96) 04−17−98

Incorporating the following PIRNs:

41017−AS−0011B, 41017−ES−0004, 41017−NA−2001, 41017−NA−2002,

41017−NA−2003, 41017−NA−2005, 41017−NA−2006, 41017−NA−2007A,

41017−NA−2008B, 41017−NA−2012, 41017−ND−0004A,

41017−NA−2010A, 41017−ND−0002B

D REVISION D (REFERENCE SSCD 000610, EFF. 01/08/98) 08−14−98

41017−ES−0010, 41017−ES−0011A, 41017−NA−2013A,

41017−NA−2014A

E REVISION E (REFERENCE SSCBD 000989, EFF. 02/13/98) 09−18−98

41017−NA−2016A, 41017−NA−2017

ii

REVISION AND HISTORY PAGE − Continued

REV. DESCRIPTION PUB.

DATE

For information: The PIRNs rolled into Revision B by previously released IRNs or as part of Revision B are noted below with their associated SSCNs.

PIRN 41017-AS−0002B IRN N/A SSCN 000293

PIRN 41017-AS−0004F IRN N/A SSCN 000293

PIRN 41017-AS−0006C IRN N/A SSCN 000293

PIRN 41017-AS−0007A IRN N/A SSCN 000293

PIRN 41017-NA−0004 IRN N/A SSCN 000293

PIRN 41017-NA−0005B IRN N/A SSCN 000293

PIRN 41017-NA−0006 IRN N/A SSCN 000293

For information: The PIRNs rolled into Revision C by previously released IRNs or as part of Revision C are noted below with their associated SSCNs.

PIRN 41017-AS−0011B IRN N/A SSCN 000403

PIRN 41017-ES−0004 IRN N/A SSCN 000403

PIRN 41017-NA−2001 IRN N/A SSCN 000403

PIRN 41017-NA−2002 IRN N/A SSCN 000403

PIRN 41017-NA−2003 IRN N/A SSCN 000403

PIRN 41017-NA−2005 IRN N/A SSCN 000403

PIRN 41017-NA−2006 IRN N/A SSCN 000403

PIRN 41017-NA−2007A IRN N/A SSCN 000403

PIRN 41017-NA−2008B IRN N/A SSCN 000403

PIRN 41017-NA−2012 IRN N/A SSCN 000403

PIRN 41017-ND−0004A IRN N/A SSCN 000403

PIRN 41017-NA−2010A IRN N/A SSCN 000403

PIRN 41017-ND−0002B IRN N/A SSCN 000403

For information: The PIRNs rolled into Revision D by previously released IRNs or as part of Revision D are noted below with their associated SSCNs.

PIRN 41017-ES−0010 IRN N/A SSCN 000610

PIRN 41017-ES−0011A IRN N/A SSCN 000610

PIRN 41017-NA−2013A IRN N/A SSCN 000610

PIRN 41017-NA−2014A IRN N/A SSCN 000610

For information: The PIRNs rolled into Revision E by previously released IRNs or as part of Revision E are noted below with their associated SSCNs.

PIRN 41017-NA−2016A IRN N/A SSCN 000989

PIRN 41017-NA−2017 IRN N/A SSCN 000989

iii

REVISION AND HISTORY PAGE − Continued

REV. DESCRIPTION PUB.

DATE

F Revision F (Reference per SSCD 001810, EFF. 02−21−00) 05−22−00

Incorporates the following PIRNs associated with the appropriate SSCNs.

PIRN 41017-NA−2020B IRN N/A SSCN 001810

PIRN 41017-NA−2021A IRN N/A SSCN 001810

PIRN 41017-NA−2022 IRN N/A SSCN 001810

PIRN 41017-ND−0007 IRN N/A SSCN 001810

Revision F accounts for impacts identified in the following SSCNs: 000653, 000845, 000591, 000583, 000773, 001004, 000832, 000440, 000671, 000877, 000894, 000915, 000844, 001029, 001051, 001052, 001026, 000470, 000823, 000673, 000585, 000588, 000600, 000567, 001481, and 000554.

Revision F also closes IRN 0346 for SSCN 000346 as the PIRN 41017−NA−2011 was withdrawn.

G Revision G (Reference SSCD 003760, EFF. 11−14−01) 04−15−02

Incorporates the following PIRNs associated with the appropriate SSCNs.

PIRN 41017−ND−0009 IRN N/A SSCN 003760

PIRN 41017−NA−2023A IRN N/A SSCN 001937

PIRN 41017−NA−2031A IRN 0015 SSCN 003141

PIRN 41017−ND−0006C IRN 0017 SSCN 001866

Revision G also closes PIRN 41017−NA−2024B for SSCN 001959 as it was withdrawn.

H Revision H (Reference SSCD 005508, EFF. 05/18/01) 05−06−02

Incorporates the following PIRNs associated with the appropriate SSCNs.

PIRN 41017−NA−2027A IRN N/A SSCN 005508

PIRN 41017−NA−2034A IRN N/A SSCN 005508

PIRN 41017−NA−2029F IRN 0018 SSCN 001446

J Revision J (Reference SSCN 008198 EFF. 11−08−05) 11−29−05

Incorporates the following PIRNs associated with the appropriate SSCNs.

PIRN 41017−NA−2036 IRN N/A SSCN 008198

PIRN 41017−NA−2037E IRN N/A SSCN 008198

PIRN 41017−NA−2038 IRN N/A SSCN 008198

PIRN 41017−NA−2039 IRN N/A SSCN 008198

PIRN 41017−NA−2040C IRN N/A SSCN 008198

PIRN 41017−NA−2041A IRN N/A SSCN 008198

PIRN 41017−ND−0011C IRN N/A SSCN 008198

Revision J also closes the action from the following SSCN as the impact previously defined has been overcome by events:

PIRN N/A IRN 0013 SSCN 001704

iv

REVISION AND HISTORY PAGE − Continued

REV. DESCRIPTION PUB.

DATE

Revision J also closes the action form the following SSCN as it has been determined to be of no impact:

PIRN N/A IRN 0019 SSCN 003286

ERU: /s/Beth Mason 11−29−05 v

PREFACE

The contents of this document are intended to be consistent with tasks and products to be prepared by Program participants. The Rack to Mini Pressurized Logistics Module Interface Control Document Part 2 shall be implemented on all new ISS contractual and internal activities and shall be included in any existing contracts through contract changes. This document is under the control of the Interface Control Working Group (ICWG), and any changes or revisions will be approved by the ICWG Chairman.

vi

INTERNATIONAL SPACE STATION PROGRAM

RACK TO MINI PRESSURIZED LOGISTICS MODULE

INTERFACE CONTROL DOCUMENT, PART 2

FEBRUARY 4, 2005

CONCURRENCE

Warren England Boeing

PREPARED BY: PRINT NAME ORGN

/s/ Warren England 4/13/05

SIGNATURE DATE

CHECKED BY: Quentin Henry Boeing

SIGNATURE DATE

/s/ Quentin L. Henry 4/13/05

SIGNATURE DATE

DQA BY: Merry McClain Boeing

PRINT NAME ORGN

/s/ Merry McClain 4/13/05

SIGNATURE DATE

APPROVED BY

NASA ICWG CHAIR: Chau Hong NASA/OM

PRINT NAME ORGN

/s/ Chau Hong 6/5/2005

SIGNATURE DATE

vii

INTERNATIONAL SPACE STATION PROGRAM

RACK TO MINI PRESSURIZED LOGISTICS MODULE

INTERFACE CONTROL DOCUMENT

FEBRUARY 4, 2005

NASA/JAXA/ESA/ASI APPROVAL

Print Name

See Directive

NASA Program Manager Date

Print Name

See Directive

JAXA Program Manager Date

Print Name

See Directive

ESA Program Manager Date

Print Name

See Directive

ASI Program Manager Date viii

SPACE STATION PROGRAM OFFICE

RACK TO MINI PRESSURIZED LOGISTICS MODULES

INTERFACE CONTROL DOCUMENT

LIST OF CHANGES

(SHEET 1 OF 8)

FEBRUARY 4, 2005

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

SSCBD ENTRY DATE CHANGE PARAGRAPH(S)

March Telecons Cover Page Revision Page

Signature Page(s)

PARAGRAPH(S)

3.1.1 3.1.4

3.1.4.2 3.2

3.2.2 3.3

3.3.1−1 Ref 3.4.2.3

3.4.2.3.1 3.4.2.3.2

March Telecons 3.4.2.1.4 3.4.2.14

3.4.2.14.1 3.4.2.14.2 3.4.2.14.3

Add Issue Sheets

FIGURE(S)

3.1.1−1 3.1.4.1−1 3.1.4.2−1 3.1.4.2−2 3.3.1−1 3.3.1−2 3.3.1−1 ix

SPACE STATION PROGRAM OFFICE

RACK TO MINI PRESSURIZED LOGISTICS MODULES

INTERFACE CONTROL DOCUMENT

FEBRUARY 4, 2005

LIST OF CHANGES

(SHEET 2 OF 8)

SSCBD ENTRY DATE CHANGE TABLE(S)

3.1.1−2 3.4.2.3.1−1 3.4.2.3.2−1

SSCD 000293 3−22−96 AS−0002B PARAGRAPH(S)

1.0 1.1 1.2 1.3 1.4 2.0

AS−0004F FIGURE(S)

3.1..3−1 3.1.3−2 3.1.3−3 3.3.4−1

AS−0006C PARAGRAPH(S)

3.1.1 3.2

AS−0006C FIGURE(S)

3.1.1−2 3.3.1−3

AS−0007A PARAGRAPH(S)

3.1.1

NA−0004 FIGURE(S)

3.3.2−5 x

SPACE STATION PROGRAM OFFICE

RACK TO MINI PRESSURIZED LOGISTICS MODULES

INTERFACE CONTROL DOCUMENT

FEBRUARY 4, 2005

LIST OF CHANGES

(SHEET 3 OF 8)

SSCBD ENTRY DATE CHANGE FIGURE(S)

NA−0005B 3.3.5−1

NA−0006 PARAGRAPH(S

3.2.1

3.2.1.1

TABLE(S)

3.2.1−1 3.2.1−2

NA−0006 FIGURE(S)

3.2.1.1−1

SSCD 000403 10/4/96 AS−0011B 3.2.1.4.4

ES−0004 PARAGRAPH(S)

4.0

NA−2001 FIGURE(S)

3.3.4−2

NA−2002 FIGURE(S)

3.3.2−3 3.3.3−1

NA−2003 FIGURE(S)

3.3.2−3

NA−2005 FIGURE(S)

3.3.1−5

NA−2006 FIGURE(S)

3.1.3−3

NA−2007A FIGURE(S)

3.3.4−3

NA−2008B PARAGRAPH(S)

2.0 xi

SPACE STATION PROGRAM OFFICE

RACK TO MINI PRESSURIZED LOGISTICS MODULES

INTERFACE CONTROL DOCUMENT

FEBRUARY 4, 2005

LIST OF CHANGES

(SHEET 4 OF 8)

SSCBD ENTRY DATE CHANGE PARAGRAPH(S)

NA−2012 Closed Issues

ND−0004A FIGURE(S)

3.3.1−4

NA−2010A FIGURE(S)

3.3.1−6 3.3.2−6

ND−0002B FIGURE(S)

3.3.1−6 3.3.2−7

SSCD 000610 5−30−97 ES−0010 FIGURE(S)

3.3.1−1

ES−0011A FIGURE(S)

3.3.1−3

NA−2013 FIGURE(S)

3.1.1−1

NA−2014A PARAGRAPH(S)

3.1.6.2

SSCD 000989 NA−2016A PARAGRAPH(S)

2.0 2.1

NA−2017 PARAGRAPH(S)

Concurrence Sheet xii

SPACE STATION PROGRAM OFFICE

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INTERFACE CONTROL DOCUMENT

FEBRUARY 4, 2005

LIST OF CHANGES

(SHEET 5 OF 8)

SSCBD ENTRY DATE CHANGE PARAGRAPH(S)

SSCD 001810 NA−2020B 3.3.2.1

3.3.2.2 3.3.2.3 3.3.2.4

FIGURE(S)

3.3.2.3−1 3.3.2.3−2 3.3.2.3−3 3.3.2.3−4 3.3.2.3−5 3.3.2.3−6 3.3.2.3−7 3.3.2.3−8

TABLE(S)

3.3.2.3−1

NA−2021A PARAGRAPH(S)

3.3.4

3.3.4.1

FIGURE(S)

3.3.4−4

NA−2022 PARAGRAPH(S)

3.3.2.5

FIGURE(S)

3.3.2.5−1 xiii

SPACE STATION PROGRAM OFFICE

RACK TO MINI PRESSURIZED LOGISTICS MODULES

INTERFACE CONTROL DOCUMENT

FEBRUARY 4, 2005

LIST OF CHANGES

(SHEET 6 OF 8)

SSCBD ENTRY DATE CHANGE PARAGRAPH(S)

ND−0007 3.3.2

FIGURE(S)

3.3.2−8

SSCD 003760 ND−0009 FIGURE(S)

3.3.2.3−1 3.3.2.3−4

SSCD 001937 NA−−2023A PARAGRAPH(S)

3.3.4.1

SSCD 001866 ND−0006C FIGURE(S)

3.3.2−5

TABLE(S)

3.3.2.3−1

SSCD 003141 NA−2031A FIGURE(S)

3.3.3−1

SSCD 005508 NA−2027A FIGURE(S)

3.1.1−1

NA−2034A TABLE(S)

3.3.2.3−1

SSCD 001446 NA−2029F PARAGRAPH(S)

3.3.2

FIGURE(S)

3.3.3−9 (Page 1 of 2) Add 3.3.3−9 (Page 2 of 2) Add xiv

SPACE STATION PROGRAM OFFICE

RACK TO MINI PRESSURIZED LOGISTICS MODULES

INTERFACE CONTROL DOCUMENT

FEBRUARY 4, 2005

LIST OF CHANGES

(SHEET 7 OF 8)

SSCBD ENTRY DATE CHANGE PARAGRAPH(S)

008198 NA−2036 3.3.2.6, 3.3.2.7, 3.3.4.2(Adds)

008198 NA−2037E PARAGRAPH(S)

3.3.4, 3.3.4.1

FIGURE(S)

3.3.4−1, 3.3.4−4, 3.3.4−5 (ADD)

008198 NA−2038 PARAGRAPH(S)

3.3.1

FIGURE(S)

3.3.1−6.1, 3.3.1−6.2 (ADD)

008198 NA−2039 FIGURE(S)

3.3.4−4

008198 ND−0011C PARAGRAPH(S)

3.3.2.4

FIGURE(S)

3.3.2.3−5 (DELETED),

3.3.2.3−6 (DELETED)

008198 NA−2040C PARAGRAPH(S)

3.3.2.3

FIGURE(S)

3.3.2.3−1, 3.3.2.3−2, 3.3.2.3−3, 3.3.2.3−4

TABLE

3.3.2.3−1

008198 NA−2041A Cover xv

SPACE STATION PROGRAM OFFICE

RACK TO MINI PRESSURIZED LOGISTICS MODULES

INTERFACE CONTROL DOCUMENT

FEBRUARY 4, 2005

LIST OF CHANGES

(SHEET 8 OF 8)

SSCBD ENTRY DATE CHANGE PARAGRAPH(S)

NA−2041A Concurrence(s)

008198 NA−2041A PARAGRAPH(S)

1.0, 2.1, 2.2, 2.3 (add), 3.3.2, 3.3.4, 3.3.4.1, 3.5.7.1

NA−2041A FIGURE(S)

3.1.3−3, 3.3.1−4, 3.3.1−5, 3.3.1−6, 3.3.2−6, 3.3.2−8, 3.3.2.3−3, 3.3.2.3−4, 3.3.2.3−7, 3.3.2.3−8, 3.3.3−1, 3.3.4−5

008198 NA−2041A Appendix A

008198 NA−2041A Appendix B

TABLE OF CONTENTS

PARAGRAPH PAGE

xvi

1.0 INTRODUCTION 1 − 1

1.1 PURPOSE AND SCOPE 1 − 1

1.2 PRECEDENCE 1 − 1

1.3 DELEGATION OF AUTHORITY 1 − 1

2.0 DOCUMENTS 2 − 1

2.1 APPLICABLE DOCUMENTS 2 − 1

2.2 REFERENCE DOCUMENTS 2 − 1

2.3 REFERENCE DRAWINGS 2 − 2

3.0 INTERFACE 3 − 1

3.1 GENERAL 3 − 1

3.1.1 INTERFACE DESCRIPTION 3 − 1

3.1.2 INTERFACE RESPONSIBILITIES 3 − 1

3.1.3 COORDINATE SYSTEMS 3 − 1

3.1.4 DELETED 3 − 1

3.1.5 MASS PROPERTIES 3 − 6

3.1.5.1 MASS 3 − 6

3.1.6 ENGINEERING UNITS AND TOLERANCES 3 − 6

3.1.6.1 ENGINEERING UNITS 3 − 6

3.1.6.2 TOLERANCES AND CONVERSIONS 3 − 6

3.2 STRUCTURAL INTERFACES 3 − 6

3.2.1 INTERFACE LOADS 3 − 6

3.3 MECHANICAL INTERFACES 3 − 6

3.3.1 LOWER REAR ATTACHMENT INTERFACES 3 − 7

3.3.2 UPPER ATTACHMENT INTERFACES 3 − 15

3.3.2.1 ON−ORBIT UPPER ATTACHMENT INTERFACES 3 −25

3.3.2.2 ARIS ON−ORBIT INTERFACES 3 −25

3.3.2.3 ON ORBIT KNEEBRACE REPLACEMENT (MODULE) 3 −26

3.3.2.4 ON ORBIT KNEEBRACE REPLACEMENT (RACK) 3 −26

3.3.2.5 ARIS RACK COMPATIBILITY 3 −26

3.3.2.6 PaRIS ON–ORBIT INTERFACES 3 −26

3.3.2.7 PaRIS RACK COMPATIBILITY 3 −26

3.3.3 GROUND HANDLING ATTACHMENT INTERFACES 3 − 36

3.3.4 PIVOT ATTACHMENT INTERFACES 3 − 39

3.3.4.1 ARIS COMPATIBLE PIVOT INTERFACES 3 − 39

3.3.4.2 PaRIS COMPATIBLE PIVOT INTERFACES 3 − 39

3.3.5 RESTRAINTS AND MOBILITY AIDS HARDWARE INTERFACE 3 − 44

3.4 ENVIRONMENTAL INTERFACES 3 − 44

3.4.1 NATURAL ENVIRONMENT 3 − 44

3.4.1.1 NEUTRAL ATMOSPHERE ENVIRONMENT 3 − 44

3.4.1.2 METEOROIDS AND ORBITAL DEBRIS ENVIRONMENT 3 − 44

3.4.1.3 MAGNETIC FIELD ENVIRONMENT 3 − 44

3.4.1.4 GRAVITATIONAL FIELD ENVIRONMENT 3 − 44

3.4.1.5 THERMAL ENVIRONMENT 3 − 44

3.4.1.6 PHYSICAL CONSTANTS 3 − 44

3.4.2 INDUCED ENVIRONMENT 3 − 44

xvii

3.4.2.1 ELECTROMAGNETIC ENVIRONMENT 3 − 46

3.4.2.2 ELECTROSTATIC ENVIRONMENT 3 − 46

3.4.2.3 DELETED 3 − 46

3.4.2.4 ACOUSTICS ENVIRONMENT 3 − 46

3.4.2.5 THERMAL ENVIRONMENT 3 − 46

3.4.2.6 REDUCED ATMOSPHERE ENVIRONMENT 3 − 46

3.4.2.7 CONTAMINATION ENVIRONMENT 3 − 46

3.4.2.7.1 INTERNAL CONTAMINATION ENVIRONMENT 3 − 47

3.4.2.7.2 EXTERNAL CONTAMINATION ENVIRONMENT 3 − 47

3.4.2.8 PLASMA ENVIRONMENT 3 − 47

3.4.2.9 IONIZING RADIATION ENVIRONMENT 3 − 47

3.4.2.10 MICROGRAVITY ENVIRONMENT 3 − 47

3.4.2.11 ENVIRONMENTAL CONTROL AND LIFE SUPPORT SYSTEM EFFECTS

ENVIRONMENT 3 − 47

3.4.2.11.1 DEPRESSURIZATION/REPRESSURIZATION ENVIRONMENT 3 − 47

3.4.2.11.2 LEAKAGE ENVIRONMENT 3 − 47

3.4.2.12 MAN SYSTEMS ENVIRONMENT 3 − 47

3.4.2.13 ON−ORBIT CREW−INDUCED LOADING 3 − 47

3.5 SYSTEM INTERFACES 3 − 48

3.5.1 ELECTRICAL POWER SYSTEM 3 − 48

3.5.2 DATA MANAGEMENT SYSTEM 3 − 48

3.5.3 THERMAL CONTROL SYSTEM 3 − 48

3.5.4 COMMUNICATIONS AND TRACKING SYSTEM 3 − 48

3.5.5 GUIDANCE, NAVIGATION, AND CONTROL SYSTEM 3 − 48

3.5.6 EXTRAVEHICULAR ACTIVITY SYSTEM 3 − 48

3.5.7 ENVIRONMENTAL CONTROL AND LIFE SUPPORT SYSTEM 3 − 48

3.5.7.1 FIRE SUPPRESSION 3 − 48

3.5.8 MAN SYSTEMS 3 − 48

3.5.8.1 RESTRAINT AND MOBILITY HARDWARE INTERFACE 3 − 48

3.5.9 FLUID MANAGEMENT SYSTEMS 3 − 48

3.6 SOFTWARE INTERFACES 3 − 48

APPENDIX

A ABBREVIATIONS AND ACRONYMS A − 1

B INDEX OF TBDs AND TBRs B − 1 xviii

TABLES

3.1.6.2−1 LINEAR TOLERANCES 3 − 6

3.3.2.3−1 KBAR COMPATIBLE ON−ORBIT RACK LOCATIONS 3 −34

3.3.2.3−1 KBAR COMPATIBLE ON−ORBIT RACK LOCATIONS (CONT’D) 3 −35

APPENDIX B INDEX OF TBDS AND TBRS B − 1

xix

FIGURES

3.1.1−1 MPLM LAUNCH, LANDING AND ON−ORBIT ATTACH POINT

COORDINATES ON THE MODULE SIDE (1−G CONDITION) 3 − 2

3.1.3−1 RACK COORDINATE SYSTEM 3 − 3

3.1.3−2 TYPICAL MPLM ISPR LOCATION COORDINATE SYSTEM 3 − 4

3.1.3−3 RELATIVE LOCATION OF RACK DATUM POINT TO POINT A, (MODULE

DATUM POINT) AT LAUNCH/LANDING AND ON−ORBIT CONFIGURATION

(REFERENCE ONLY) 3 − 5

3.3.1−1 RACK LOWER REAR ATTACHMENT ASSEMBLY − ENGAGED POSITION

(REFERENCE ONLY) 3 − 7

3.3.1−2 RACK LOWER REAR ATTACHMENT ASSEMBLY − DISENGAGED POSITION

(REFERENCE ONLY) 3 − 8

3.3.1−3 RACK LOWER REAR ATTACHMENT FITTINGS (REAR VIEW) 3 − 9

3.3.1−4 RACK LOWER REAR ATTACHMENT FITTING 3 − 10

3.3.1−5 LOWER REAR LONGERON FITTING 3 − 11

3.3.1−6.1 RACK LOWER REAR ATTACHMENT MECHANISM LOCKING PIN 3 − 12

3.3.1−6.2 RACK LOWER REAR ATTACHMENT MECHANISM LOCKING PIN,

RESUPPLY STOWAGE PLATFORM IN MPLM ONLY 3 − 13

3.3.1−7 LOWER REAR LONGERON FITTING SPHERICAL BEARING 3 − 14

3.3.1−8 RACK LOWER ATTACHMENT BEARING/BUSHING INTERFACE 3 − 15

3.3.2−1 RACK UPPER ATTACHMENT ASSEMBLY ENGAGED POSITION

(REFERENCE ONLY) 3 − 16

3.3.2−2 RACK UPPER ATTACHMENT ASSEMBLY DISENGAGED

POSITION (REFERENCE ONLY) 3 − 17

3.3.2−3 UPPER ATTACHMENT MECHANISM/UPPER GROUND SUPPORT

EQUIPMENT ATTACHMENT POINTS (FRONT VIEW) 3 − 18

3.3.2−4 RACK UPPER ATTACHMENT/UPPER GROUND SUPPORT EQUIPMENT

FITTING (SIDE/REAR VIEW) 3 − 19

3.3.2−5 UPPER ATTACHMENT KNEEBRACE 3 − 20

3.3.2−6 RACK UPPER ATTACHMENT MECHANISM LOCKING PIN 3 − 21

3.3.2−7 UPPER ATTACHMENT KNEEBRACE SPHERICAL BEARING 3 − 22

3.3.2−8 DETAILED INFORMATION FOR UPPER ATTACHMENT LEVER KNOB IN

IHI ISPR 3 − 23

3.3.2−9 KNEEBRACE TO MPLM INTERFACE (TOP VIEW) PAGE 1 OF 2 3 − 24

3.3.2−9 KNEEBRACE TO MPLM INTERFACE (TOP VIEW) PAGE 2 OF 2 3 − 25

3.3.2.3−1 U. S. KNEEBRACE BOLT ACTION REPLACEMENT INTERFACE FOR

BOEING RACK STRUCTURES 3 − 27

3.3.2.3−2 KNEEBRACE BOLT ACTION REPLACEMENT INTERFACE FOR BOEING

RACK STRUCTURES 3 − 28

3.3.2.3−3 KNEEBRACE BOLT ACTION REPLACEMENT INTERFACE FOR MHI/IHI

RACK STRUCTURES 3 − 29

3.3.2.3−4 KNEEBRACE BOLT ACTION REPLACEMENT INTERFACE FOR MHI/IHI

RACK STRUCTURES 3 − 30

3.3.2.3−5 DELETED 3 − 31

3.3.2.3−6 DELETED 3 − 31

3.3.2.3−7 RACK TO MODULE INTERFACE (CAPTURE MECHANISM) 3 − 32

3.3.2.3−8 KBAR PIN LOCATION FOR ESA/JAXA/NASA 3 − 33

3.3.2.5−1 MPLM RACK LOCATION NOMENCLATURE 3 − 36

3.3.3−1 RACK LOWER GROUND SUPPORT EQUIPMENT ATTACHMENT

(FRONT VIEW) 3 − 37

xx

3.3.3−2 RACK LOWER GROUND SUPPORT EQUIPMENT ATTACHMENT

(SIDE VIEW) 3 − 38

3.3.3−3 TYPICAL GROUND SUPPORT EQUIPMENT BOSS 3 − 38

3.3.4−1 PIVOT SLOT MECHANISM ENVELOPE IN RACK LATERAL FRAME 3 − 40

3.3.4−2 PIVOT SLOT (SIDE VIEW) 3 − 41

3.3.4−3 PIVOT PIN DETAIL 3 − 41

3.3.4−4 NASA ARIS PIVOT PIN DETAIL (NOT APPLICABLE TO MPLM) 3 − 42

3.3.4−5 MHI/IHI ARIS PIVOT PIN DETAIL (NOT APPLICABLE TO MPLM) 3 − 43

3.3.5−1 RESTRAINTS AND MOBILITY AIDS HARDWARE INTERFACE 3 − 45

3.3.5−2 RESTRAINTS AND MOBILITY AIDS HARDWARE INTERFACE

SCHEMATIC 3 − 46

1 − 1

1.0 INTRODUCTION

International standard payload racks are defined as racks which are interchangeable between National Aeronautics and Space Administration (NASA), European Space Agency (ESA), and Japan Aerospace Exploration Agency (JAXA) laboratories, regardless of the provider or site of initial installation within International Space Station.

1.1 PURPOSE AND SCOPE

This Interface Control Document (ICD) defines the ground handling, launch and landing, and on−orbit physical, functional, and environmental interfaces between the Mini Pressurized Logistics Module (MPLM) and racks that conform to interfaces of the International Standard Payload Rack (ISPR). The scope of this document is limited to the structural/mechanical interfaces between the MPLM and the ISPR and between the GSE and the ISPR. The interfaces defined in this document apply to the MPLM and to all Space Station racks transported to/from orbit by the MPLM.

1.2 PRECEDENCE

In the event of conflict between SSP 41000, Space Station System Spec., and the contents of this ICD, only the requirements of SSP 41000 applicable to each International Partner and to the National Aeronautics and Space Administration (NASA) for MPLM shall take precedence.

1.3 DELEGATION OF AUTHORITY

This document is prepared and maintained in accordance with SSP 30459, International Space Station Interface Control Plan. The Prime Contractor shall delegate the responsibility for preparation and maintenance of this ICD.

2 − 1

2.0 DOCUMENTS

The documents in this paragraph are applicable to the extent specified herein.

2.1 APPLICABLE DOCUMENTS

The following documents of the date and issue shown include specifications, models, standards, guidelines, handbooks, and other special publications. “Current Issue” is shown in parentheses in place of the specific date and issue when the document is under Level II Space Station Control Board control. The status of documents identified by “Current Issue” may be determined from the International Space Station Baseline Activity Index and Status Report.

DOCUMENT NO. TITLE

SSP 41002 International Standard Payload Rack to NASA/ESA/NASDA Rev. K , July 31, 2001 Modules Interface Control Document

References Paragraphs 3.5.7.1

ASTM E380 Standard Practice For Use of The International System of Rev. A, 1993 Units (SI) (The Modernized Metric System)

Reference Paragraph 3.1.6.2

SSP 41017, Part 1 Rack to Mini Pressurized Logistics Module Interface Control Rev. G, Feb. 4, 2005 Document, Part 1

References Paragraphs 3.2, 3.2.1, 3.3

2.2 REFERENCE DOCUMENTS

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

DOCUMENT NO. TITLE

SSP 30459 International Space Station Interface Control Plan Rev. G, Nov. 8, 1995

Reference Paragraph 1.3

SSP 41000 Space Station System Specification Reference Paragraph 1.2

COL−RQ−ESA−013 Columbus Human Factors Engineering Requirements Reference Paragraph 3.4.2.13

SSP 50005 International Space Station Flight Crew Integration Standard Reference Paragraph 3.4.2.13

2 − 2

SSP 50251 ARIS to Pressurized Element Interface Control Document Latest Issue

Reference Paragraph 3.3.2.2, 3.3.2.6

2.3 REFERENCE DRAWINGS

The following drawings are referenced in this ICD for context and user convenience:

683−61711 Pivot Bracket Assembly Reference Paragraph 3.3.2.3

683−62201 KBAR Assembly Reference Paragraph 3.3.2.3

683−20100 JEM Pivot Fitting Assembly Reference Figure 3.3.4−5

3 − 1

3.0 INTERFACE

3.1 GENERAL

3.1.1 INTERFACE DESCRIPTION

The rack−to−MPLM interfaces consist of the launch and landing structural/mechanical attach points A, B, C, and D, the on−orbit structural/mechanical attachment points I and J for on−orbit tilting and the restraint and mobility aid interfaces. The rack−to−Ground Support Equipment (GSE) interfaces consist of the ground handling structural/ mechanical attach points E, F, G, and H. See Figure 3.1.1−1, MPLM Launch, Landing and On−Orbit Attach point coordinates on the Module Side for the Launch Landing and On−Orbit Point Locations on the Module Side of the interface, (1−g condition).

3.1.2 INTERFACE RESPONSIBILITIES

NASA ensures that the MPLM interface to racks conforms to the interface definition contained within this document.

3.1.3 COORDINATE SYSTEMS

The rack coordinate system is defined in Figure 3.1.3−1, Rack Coordinate System. The typical MPLM ISPR location coordinate system is defined in Figure 3.1.3−2, Typical MPLM ISPR Location Coordinate System. The relative location of the Rack Coordinate System to the Typical MPLM ISPR Location Coordinate System, for Launch/Landing/On−Orbit configuration, is defined in Figure 3.1.3−3, Relative Location of Rack Datum Point to Point A (Module Datum Point) at Launch/Landing and On−Orbit Configuration (Reference Only).

3.1.4 DELETED

3 − 2

POINT A

RACK TO MPLM ATTACHMENT POINT COORDINATES (1)

COORDINATE

W.R.T. MODULE

REFERENCE

LAUNCH & LANDING

ATTACH POINTS

A B C (2) D (2) I J

XM 0

(0)

39.30 ± .01 (998.22±

0.25)

− .09 (− 2.3)

39.39 (1000.5)

− 1.11 + 0 − .05

(−28.19 +0 − 1.27)

40.41 +.05 −0

(1026.41 + 1.27 − 0)

YM 0

(0)

0 ± .01 (0 ± 0.25)

− 23.98 (− 609.1)

− 23.98 (− 609.1)

−24.368 ±.050 (−618.95 ± 1.27)

−24.368 ±.050 (−618.95 ±1.27)

ZM 0

(0)

0 ± .01 (0 ± 0.25)

76.59 (1945.4) to 77.64

(1972.1)

76.59 (1945.4) to 77.64

(1972.1)

2.12 ±.05 (53.85 ± 1.27)

2.12 ±.05 (53.85 ± 1.27)

(1) Coordinates include only manufacturing tolerances (1−g condition)

(2) These positions can be kept at their nominal values by means of braces length adjustments

FIGURE 3.1.1−1 MPLM LAUNCH, LANDING AND ON−ORBIT ATTACH POINT

COORDINATES ON THE MODULE SIDE (1−G CONDITION)

3 − 3

Y Rack X

Rack

Z Rack

FIGURE 3.1.3−1 RACK COORDINATE SYSTEM

RACK DATUM POINT ORIGIN (0,0,0)

Z Rack

Y Rack

RACK DATUM POINT

BUSHING CENTERLINE

A

VIEW FROM A

Z Rack

X Rack

Note: The physical reference is the Rack Datum Point at the interface of the center line bushing attachment to the rear side of the lower module bearing behind point A.

3 − 4

YM

Í

ÍÍ

ÉÉÉÉÉÉÉÉÉ

ÉÉÉÉÉÉÉÉÉ

ÉÉÉÉÉÉÉÉÉ

ÉÉÉÉÉÉÉÉÉ

ÉÉÉÉÉÉÉÉÉ

ÉÉÉÉÉÉÉÉÉ

ÉÉÉ

ÉÉÉÉ

Í Í

Í Í

Í Í

ÍÍÍÍ

ÍÍÍÍ

XM

ÍÍÍÍ

ÍÍÍÍ

ZM

Module Attachment Bracket

Origin (0,0,0)

Point A

FIGURE 3.1.3−2 TYPICAL MPLM ISPR LOCATION COORDINATE SYSTEM

3 − 5

RACK DATUM POINT

YR/YM

ÍÍÍ

ÍÍÍZR

ÉÉÉÉ

ÉÉÉÉ

ÉÉÉÉ

ÉÉÉÉ

ÉÉÉÉ

ÍÍÍ

ÉÉÉÉÉÉÉ

ÉÉÉÉÉÉÉ

ÉÉÉÉÉÉÉ

ÉÉÉÉÉÉÉ

ÉÉÉÉÉÉÉ

ÉÉ

ÉÉÉÉ

0.5 (12.7)

POINT A (MODULE DATUM POINT)

ÍÍ

ÍÍ

Í Í

ÍÍ

ÉÉÉ

ÉÉÉ

ÉÉÉ

Applicable: • Launch/Landing/Ground when rack lower rear attachment is engaged

• On−orbit/Ground immediately before or after rack lower rear attachment disengagement/engagement.

(Not compatible with rack tilting or removal)

Applicable: • On−orbit nominal configuration. (Compatible with tilting)

• On−ground compatible with rack ground installation/removal

POINT A − NOMINAL LAUNCH/LANDING CONFIGURATION

ÍÍÍ

ÍÍÍ

ZM

YR/YM

ÍÍÍZR

0.632 (16.053)

ÍÍÍ

ÍÍÍZM

RACK DATUM POINT

POINT A (MODULE DATUM POINT)

POINT A − NOMINAL ON−ORBIT CONFIGURATION

ÉÉÉÉ

ÉÉÉÉ

ÉÉÉÉ

ÉÉÉÉ

ÉÉÉÉ

ÍÍ

ÉÉÉÉÉÉ

ÉÉÉÉÉÉ

ÉÉÉÉÉÉ

ÉÉÉÉÉÉ

ÉÉÉÉÉÉ

ÉÉ

ÉÉ

ÉÉ

ÉÉÉ

Í Í

Í Í

ÍÍ

FIGURE 3.1.3−3 RELATIVE LOCATION OF RACK DATUM POINT TO POINT A,

(MODULE DATUM POINT) AT LAUNCH/LANDING AND ON−ORBIT CONFIGURATION

(REFERENCE ONLY)

3 − 6

3.1.5 MASS PROPERTIES

3.1.5.1 MASS

MPLM interface hardware accommodates racks with a maximum mass of 1773 lbs (804.2 kg) for all operational phases.

3.1.6 ENGINEERING UNITS AND TOLERANCES

3.1.6.1 ENGINEERING UNITS

Dimensions shown in this document are in the English (inch, pound, second) system of units followed by the equivalent International System of Units (SI) value in parenthesis.

Measurements may be verified in either system of units.

3.1.6.2 TOLERANCES AND CONVERSIONS

Linear tolerance on English dimensions are as indicated in Table 3.1.6.2−1, Linear Tolerances.

For detailed description of conversions see ASTM E380, Standard Practice for Use of the International System of Units (SI) (The Modernized Metric System).

TABLE 3.1.6.2−1 LINEAR TOLERANCES

English Dimension Implied Tolerance (Inches)

X.XX +/− 0.03

X.XXX +/− 0.010

3.2 STRUCTURAL INTERFACES

The rack−to−MPLM/GSE structural interfaces consist of the load carrying capabilities associated with the launch, landing, ground handling, and on−orbit attach points as defined in SSP 41017, Rack to MPLM ICD, Part 1.

3.2.1 INTERFACE LOADS

Interface loads for launch and landing are the static and dynamic loads transmitted from the rack to the module through attach points A, B, C, and D. Interface loads for ground handling are the static and dynamic loads transmitted from the rack to the GSE through attach points E, F, G, and H. On−orbit interface loads are the static and dynamic loads transmitted from the rack to the module through the attachment points C, D, I, and J. The acceleration environment and the interface loads for launch, landing, on−orbit and ground handling are as specified in SSP 41017, Rack to MPLM ICD, Part 1.

3.3 MECHANICAL INTERFACES

The rack−to−MPLM/GSE mechanical interfaces consist of the launch, landing, on−orbit, and ground handling attach points as defined in SSP 41017, Rack to MPLM ICD, Part 1.

3 − 7

3.3.1 LOWER REAR ATTACHMENT INTERFACES

The rack−to−MPLM lower rear attachment interfaces are shown in the following Figures:

— 3.3.1−1, Rack Lower Rear Attachment Assembly − Engaged Position (Reference Only)

— 3.3.1−2, Rack Lower Rear Attachment Assembly − Disengaged Position (Reference Only)

— 3.3.1−3, Rack Lower Rear Attachment Fittings (Rear View)

— 3.3.1−4, Rack Lower Rear Attachment Fitting

— 3.3.1−5, Lower Rear Longeron Fitting

— 3.3.1−6.1, Rack Lower Rear Attachment Mechanism Locking Pin

— 3.3.1−6.2, Rack Lower Rear Attachment Mechanism Locking Pin, Resupply Stowage Platform in MPLM only

— 3.3.1−7, Lower Rear Longeron Fitting Spherical Bearing

— 3.3.1−8, Rack Lower Attachment Bearing/Bushing Interface.

The location of the rack datum is given in Figure 3.1.3−1 Rack Coordinate System.

1 Shaft with interface pin (integral part of rack)

2 Spherical bearing

3 Bushing

4 Rack rear fitting (integral part of rack)

5 Shell bracket (integral part of shell)

Point A,B

FIGURE 3.3.1−1 RACK LOWER REAR ATTACHMENT ASSEMBLY − ENGAGED

POSITION (REFERENCE ONLY)

3 − 8

1 Shaft with interface pin (integral part of rack)

2 Spherical bearing

3 Bushing

4 Rack rear fitting (integral part of rack)

5 Shell bracket (integral part of shell)

Point A,B

FIGURE 3.3.1−2 RACK LOWER REAR ATTACHMENT ASSEMBLY − DISENGAGED

3 − 9

Width of opening in rack to accommodate longeron fitting.

X

Z

1.165 minimum

(see Note 1)

39.329 (998.96)

(29.59 minimum)

1.165 minimum

(see Note 1) (29.59 minimum)

R

R

RACK

DATUM

NOTES: (1)

Dimension is from centerline of spherical bearing.

Sliding capability in B not shown for clarity

FIGURE 3.3.1−3 RACK LOWER REAR ATTACHMENT FITTINGS (REAR VIEW)

(2)

39.269 (997.43)

(see Note 2) (B)

3 − 10

1.195 (30.35)

1.185 (30.10)

CL BUSHING

.848 (21.54)

.838 (21.29)

1.480 minimum (37.59 mini-mum)

45° ± 1°x.29±.03

45° ± 1°x.13±.03

.13±.03

2PL

Rack Datum (Reference)

.488 minimum (12.40 minimum)

.760 maximum (19.30 maximum)

FIGURE 3.3.1−4 RACK LOWER REAR ATTACHMENT FITTING

(x 3.3 + 0.8)

(x 7.4 + 0.8)

(x 3.3 + 0.8)

NOTES: This dimension is applicable only to rack lower rear attachment fitting.

1. NASA Rack − Maximum static Envelope dimension as specified SSP41017 Part 1, Figure 3.2.1.1.2−1.

2. MHI/IHI Rack − 1.303 (33.10) maximum.

S ee

N O

T E

3 − 11

R 1.135 max. (28.83 max.) 2 PL of SPHERICAL

BEARINGS

CL

49.31o max49.31o max

FIGURE 3.3.1−5 LOWER REAR LONGERON FITTING

Reference Figure 3.3.1−7

3 − 12

Material: MP35N per AMS 5845 or INCONEL 718 per AMS 5662 (MHI/IHI only)

FIGURE 3.3.1−6.1 RACK LOWER REAR ATTACHMENT MECHANISM LOCKING PIN

1.63 min (41.4 min)

SPHERICAL

RADIUS

(Reference)

.7490 (19.025) .7485 (19.012)

Contact surface with spherical bearing

Lubricant: MIL-L-46010 Type 1 dry lube (Tiolube 460)

∅ .875 min

0.001 A

CL

2.005 max (50.93 max)

0 .01 A

A

PIN

3 Length of cylindrical surface

(0.025)

(0.8)

3 − 13

Material: MP35N per AMS 5845 or AMS 5844.

FIGURE 3.3.1−6.2 RACK LOWER REAR ATTACHMENT MECHANISM LOCKING PIN,

RESUPPLY STOWAGE PLATFORM IN MPLM ONLY

1.63 min (41.4 min)

Contact surface with spherical bearing.

Lubricant: MIL-L-46010 Type 1 dry lube (Tiolube 460)

∅ .875

.885

0.001 A

0 .01 A

3 Length of cylindrical surface.

See Detail ”A” o

.02 (.51) R undercut

.060 (1.52)

Detail A

.300 (to sharp)

.727 (18.47) Dia.7490

.7485 Dia

2.100

R .020 (.51)

R .13 (3.3) o o o

(.025)

(.25)

(53.34)

(7.62)

(19.025 19.012)

CL

A

PIN

3 − 14

Bearing housing

FIGURE 3.3.1−7 LOWER REAR LONGERON FITTING SPHERICAL BEARING

1.002 (25.451) 1.000 (25.400)

.7500 (19.050)

.7495 (19.037)

45° 2 PL

.015 (.38)

.005 (.13) X

.885 (22.48)

.865 (21.97)

2 PL

∅ CL

A .001 (.025)

A

(0.8)

3 − 15

FIGURE 3.3.1−8 RACK LOWER ATTACHMENT BEARING/BUSHING INTERFACE

Bushing

Bushing

A .001 (.025)

CL

ÉÉÉÉÉÉÉÉÉ

ÉÉ

ÉÉÉ

ÉÉÉÉÉÉÉÉÉÉÉ

ÉÉ

É

BEARING/BUSHING

INTERFACE PLANE

A

3.3.2 UPPER ATTACHMENT INTERFACES

The rack−to−MPLM upper attachment interfaces are shown in the following Figures:

— 3.3.2−1, Rack Upper Attachment Assembly Engaged Position (Reference Only)

— 3.3.2−2, Rack Upper Attachment Assembly Disengaged Position (Reference Only)

— 3.3.2−3, Upper Attachment Mechanism/Upper Ground Support Equipment Attachment Points (Front View)

— 3.3.2−4, Rack Upper Attachment/Upper Ground Support Equipment Fitting (Side/Rear View)

— 3.3.2−5, Upper Attachment Kneebrace

— 3.3.2−6, Rack Upper Attachment Mechanism Locking Pin

— 3.3.2−7, Upper Attachment Kneebrace Spherical Bearing.

— 3.3.2−8, Detailed Information for Upper Attachment Lever Knob in IHI ISPR.

— 3.3.2−9, Kneebrace to MPLM interface (Top View).

3 − 16

M P

LM

p ro vi de d

P oi nt C

, D

P oi nt G

, H

FIGURE 3.3.2−1 RACK UPPER ATTACHMENT ASSEMBLY ENGAGED POSITION

(REFERENCE ONLY)

3 − 17

M P

LM

p ro vi de d

P oi nt C

, D

P oi nt G

, H

FIGURE 3.3.2−2 RACK UPPER ATTACHMENT ASSEMBLY DISENGAGED

3 − 18

FIGURE 3.3.2−3 UPPER ATTACHMENT MECHANISM/UPPER GROUND

SUPPORT EQUIPMENT ATTACHMENT POINTS (FRONT VIEW)

O F

P

IN

O F

P

IN

.5

(1

3.

6)

.3

.4

(1

1.

5)

C L C L

X

Z

.3

(1

0.

0)

U P

P E

R G

S E

AT

TA

C H

M E

N T

P O

IN

T

P

L

C L

D C

S E

E F

IG

. 3

.3 .3

R A

C K

D

AT

U M

.4

(1

2.

0)

.1

2.

.0

2.

.0

1.

4)

.0

1.

6)

.6

(1

1.

8)

.5

(1

5.

4)

.1

(1

9.

0)

.1

(1

7.

5)

C L

(9 .5

3) (1

2.

7)

U

N

JF

B

X .5

D

P

P L

O F

G S

E C L

S E

E F

IG

. 3

.3 .3

G H

O F

G S

E C L

3 − 19

X

.1

2.

.1

3.

1.

(3

1.

1.

(3 1.

.7

.0 3)

1.

(3

4.

.5

.2 1)

.5

.9 5)

.1

(4 .1

) 4 P

L .2

(7

.4

P

L1.

.2

U P

P E

R

S

ID

E V

IE

W

R E

A R

V

IE

W

1.

(3

4.

.9

(2 4.

6)

.1

(2 .5

.2

(5

.8

.6

.5 3)

G S

E B

O S

S

P L

C L

C L

P oi nt C

, D

.1

(4 .1

P oi nt

R ac k D at um

ÇÇÇÇÇÇÇÇÇÇÇÇ

ÇÇÇÇÇÇÇÇÇÇÇÇ

ÇÇÇÇÇÇÇÇÇÇÇÇ

ÇÇÇÇÇÇÇÇÇÇÇÇ

ÇÇÇÇÇÇÇÇÇÇÇÇ

ÇÇÇÇÇÇÇÇÇÇÇÇ

ÇÇÇÇÇÇÇÇÇÇÇÇ

ÇÇÇÇÇÇÇÇÇÇÇÇ

ÇÇÇÇÇÇÇÇÇÇÇÇ

ÇÇÇÇÇÇÇÇÇÇÇÇ

ÇÇÇÇÇÇÇÇÇÇÇÇ

ÇÇÇÇÇÇÇÇÇÇÇÇ

.5

(7

.7

.4

(7

.1

.2

6.

.2

6.

.5

(1 3.

2) .4

(1

2.

2)

.6

.4 2)

.6

.3 0)

.5

(6

.6

.4

(6

.0

R R

C L

(R ef er en ce o nl y)

G , H

C L

R

.4

(6

.2

.4

(6

.7

.1

(2 .5 or

FIGURE 3.3.2−4 RACK UPPER ATTACHMENT/UPPER

GROUND SUPPORT EQUIPMENT FITTING (SIDE/REAR VIEW)

S

P 41017, P art 2 F ebruary 4, 2005 R evision J

3 −

.522 (13.26)

.416 (10.57)

.500 (12.700)

45 x .085°

BEARING

HOUSING

SPHERICAL

BEARING

.396 (10.06)

.498 (12.649)

.442 (11.23) .678 (17.22) .658 (16.71)

1.346 (34.19)

1.326 (33.68)

.992 (25.20)

.972 (24.69)

1.504 (38.20)

1.484 (37.69)

1.10 (27.94)

1.04 (26.42)

.53 (13.46)

.47 (11.94)

.35 (8.89)

.29 (7.37)

.886 (22.50)

.866 (22.00)

TOP VIEW (1)

SIDE VIEW

.630 (16.00)

.610 (15.49)

FULL R

.48 (12.19)

.42 (10.67)

R

R

Note:

(1) Left upper attachment kneebrace shown.

+.010 −.000

(2.16 − 2.41)

Kneebrace Assembly Part Number 683−50249−4

For MPLM, use only

45 x .08(2) Minimum° 2 places in JEM

2 places inModules except JEM

FIGURE 3.3.2−5 UPPER ATTACHMENT KNEEBRACE

3 −21

∅ .3740 (9.500) .3735 (9.487)

.25 (6.4) SPHERICAL

RADIUS

(REF)

Material: MP35N per AMS 5845 or AMS 5844 (MHI/IHI only) Lubricant: MIL−L−46010 Type 1 dry lube (Tiolube 460)

FIGURE 3.3.2−6 RACK UPPER ATTACHMENT MECHANISM LOCKING PIN

3 −22

FIGURE 3.3.2−7 UPPER ATTACHMENT KNEEBRACE SPHERICAL BEARING

.476(12.09)

.466 (11.84)

X 45° or RADIUS 2

PL

.500 max (12.700 max) .015 (.38) .005 (.13)

Bearing housing

.3750 (9.525) .3745 (9.512)

Part #: KPWD−6

3 −23

FIGURE 3.3.2−8 DETAILED INFORMATION FOR UPPER ATTACHMENT LEVER KNOB IN

IHI ISPR

3 −24

Point D

Point C

24.661 (626.39)

24.641 (625.88)

19.85 (504.19)

19.82 (503.43)

1.60 (40.6), 2 plcs

43.44 (1103.4)

43.36 (1101.3)

38.60 (980.4)

38.57 (979.7) Reference

2 places

2 places 1), 2)

Notes:

1). MPLM adjusted dimension. Full kneebrace range is 24.401 (619.79) to 24.901 (632.49) and

24.519 (622.78) for on−orbit configuration.

2). Dimension controlled by Rack Integrator or by the crew on orbit.

39.48 (1002.8)

Reference

2), 1)

See Detail “A”

FIGURE 3.3.2−9 KNEEBRACE TO MPLM INTERFACE (TOP VIEW) PAGE 1 OF 2

3 −25

8�

11�

DETAIL “A”

1.62 (41.1)

1.38 (35.1)

.78 (19.8)

.72 (18.3) 2 X

1.14 (29.0)

1.12 (28.4)

.59 (15.0)

.53 (13.5)

1.28 (32.5)

1.22 (31.0)

1.41 (35.8) − 1.35 (34.3) FOR STRAIGHT STRUT

1.78 (45.2) − 1.72 (43.7) FOR DIAGONAL STRUT

FIGURE 3.3.2−9 KNEEBRACE TO MPLM INTERFACE (TOP VIEW) PAGE 2 OF 2

3.3.2.1 ON−ORBIT UPPER ATTACHMENT INTERFACES

The Rack−to−Module On−Orbit upper attachment mechanism designs comply with the interfaces (dimensions and tolerances) defined for kneebrace attachments and GSE attachments as shown in paragraph 3.3.2.

3.3.2.2 ARIS ON−ORBIT INTERFACES

ARIS On−Orbit interfaces are defined in SSP 50251 ARIS to Pressurized Element ICD, Part 2.

3 −26

3.3.2.3 ON ORBIT KNEEBRACE REPLACEMENT (MODULE)

The APM, CAM, JEM−PM, ELM−PS, U.S. Lab, and Node Modules will provide the ARIS Standoff Link and Capture Mechanism in accordance with part numbers 683−61711−3 and 683−62201−5 or equivalent, shown in Figures 3.3.2.3−1 through 3.3.2.3−8, at the locations listed in Table 3.3.2.3−1, KBAR Compatible On−orbit Rack Locations. The MPLM will not provide a KBAR interface.

3.3.2.4 ON ORBIT KNEEBRACE REPLACEMENT (RACK)

Rack to Module interfaces are defined in Figures 3.3.2.3−1, 3.3.2.3−2, 3.3.2.3−3, 3.3.2.3−4, 3.3.2.3−7 and 3.3.2.3−8 at the locations listed in Table 3.3.2.3−1.

3.3.2.5 ARIS RACK COMPATIBILITY

The MPLM accommodates ARIS in the launch configuration in the following positions: C2, C3, P3, F2, F3, and S3, reference Figure 3.3.2.5−1, MPLM Rack Location Nomenclature.

3.3.2.6 PARIS ON–ORBIT INTERFACES

Passive Rack Isolation System (PaRIS) On–Orbit interfaces are defined in SSP 50251 ARIS to Pressurized Element ICD, Part 2, Appendix B.

3.3.2.7 PARIS RACK COMPATIBILITY

The MPLM accommodates PaRIS in the launch configuration in any of the 6 ARIS positions noted in paragraph 3.3.2.5, ARIS Rack Compatibility.

3 −27

CAM, Nodes 1, 2, & 3

CAM, Nodes 1, 2, & 3

FIGURE 3.3.2.3−1 U. S. KNEEBRACE BOLT ACTION REPLACEMENT INTERFACE FOR

BOEING RACK STRUCTURES

3 −28

(REF)

(REF)

M&N

FIGURE 3.3.2.3−2 KNEEBRACE BOLT ACTION REPLACEMENT INTERFACE FOR

BOEING RACK STRUCTURES

3 −29

(REF)

(REF)

M&N

(REF)

FIGURE 3.3.2.3−3 KNEEBRACE BOLT ACTION REPLACEMENT INTERFACE FOR MHI/IHI

RACK STRUCTURES

3 −30

, CAM

, CAM

FIGURE 3.3.2.3−4 KNEEBRACE BOLT ACTION REPLACEMENT INTERFACE FOR

MHI/IHI RACK STRUCTURES

3 −31

FIGURE 3.3.2.3−5 DELETED

FIGURE 3.3.2.3−6 DELETED

3 −32

(REF)

(REF)

(REF)

(REF)

M&N

M&N .675 (17.15) .651 (16.54)

FIGURE 3.3.2.3−7 RACK TO MODULE INTERFACE (CAPTURE MECHANISM)

3 −33

(REF)

FIGURE 3.3.2.3−8 KBAR PIN LOCATION FOR BOEING/MHI/IHI

P 41017, P art 2 F ebruary 4, 2005 R evision J

3 −

TABLE 3.3.2.3−1 KBAR COMPATIBLE ON−ORBIT RACK LOCATIONS

MODULE LOCATIONS FOR ARIS STANDOFF LINK (SL), CAPTURE MECHANISM (CM) AND KBAR

USL1 S

L C M

K B A R

APM S

L

C M

K B A R

JEM S

L

C M

K B A R

CAM1 S

L

C M

K B A R

NODE 1 S

L

C M

K B A R

NODE 2 S

L

C M

K B A R

NODE 3 S

L

C M

K B A R

LAS1 X X X APM F1 X X X PM F1 X X X CAMS2 X X X NOD2S4 X X X NOD3F4 X X X

LAS2 X X X APM F2 X X X PM F2 X X X CAM S3 X X X NOD2S5 X X X NOD3F5 X X X

LAS3 X X X APM F3 X X X PM F3 X X X CAM S4 X X X

LAS4 X X X APM F4 X X X PM F4 X X X CAM S5 X X X NOD1S4 X X X

LAS5 X X X PM F5 X X X

LAS6 X PM F6 X X X

LAP1 X X X APM A1 X X X PM O1 X X X NOD2P4 X X X NOD3S4 X X X

LAP2 X X X APM A2 X X X PM O2 X X X CAM F3 X X X NOD2P5 X X X NOD3S5 X X X

LAP3 X X X APM A3 X X X PM O3 X X X CAM F4 X X X

LAP4 X X X APM A4 X X X PM O4 X X X CAM F5 X X X NOD1P4 X X X

LAP5 X X X PM O5 X X X

LAP6 X PM D1 X X X

LAD1 X X X APM O1 X X X PM D2 X X X CAM P2 X X X NOD2D4 X X X NOD3A4 X X X

LAD2 X X X APM O2 X X X PM D3 X X X CAM P3 X X X NOD2D5 X X X NOD3A5 X X X

LAD3 X X X APM O3 X X X PM D4 X X X CAM P4 X X X

LAD4 X X X APM O4 X X X PM D5 X X X CAM P5 X X X NOD1D4 X X X

LAD5 X X X PM D6 X X X

LAD6 X X X PM A1 X X X

LAO1 X X X APM D1 X PM A2 X X X CAM A2 X X X NOD2O4 X X X NOD3P4 X X X

LAO2 X X X APM D2 X PM A3 X X X CAM A3 X X X NOD2O5 X X X NOD3P5 X X X

LAO3 X X X APM D3 X PM A4 X X X CAM A4 X X X

LAO4 X X X APM D4 X PM A5 X X X CAM A5 X X X NOD1O4 X X X

LAO5 X X X PM A6 X X X

LAO6 X X X ELM−PS F1 X X X

ELM−PS F2 X X X

ELM−PS P1 X X X

ELM−PS P2 X X X

ELM−PS A1 X X X

ELM−PS A2 X X X

P 41017, P art 2 F ebruary 4, 2005 R evision J

3 −

TABLE 3.3.2.3−1 KBAR COMPATIBLE ON−ORBIT RACK LOCATIONS (CONT’D)

MODULE LOCATIONS FOR ARIS STANDOFF LINK (SL), CAPTURE MECHANISM (CM) AND KBAR

USL1 S

L C M

K B A R

APM S

L

C M

K B A R

JEM S

L

C M

K B A R

CAM1 S

L

C M

K B A R

NODE 1 S

L

C M

K B A R

NODE 2 S

L

C M

K B A R

NODE 3 S

L

C M

K B A R

ELM−PS S1 X X X

ELM−PS S2 X X X

F = Forward A = Aft O = Overhead D = Deck S = Starboard P = Port NOTE 1:USL and CAM will use the ARIS standoff link at all four corners of each RACK location (TOP and BOTTOM)

3 − 36

C1 C2 C3 C4

P1 P2 P3 P4

F1 F2 F3 F4

S1 S2 S3 S4

Ceiling

Port (MPLM, not ISS)

Floor

Starboard (MPLM)

FWD AFT

FIGURE 3.3.2.5−1 MPLM RACK LOCATION NOMENCLATURE

3.3.3 GROUND HANDLING ATTACHMENT INTERFACES

The rack−to−GSE attachment interfaces are shown in Figures 3.3.2−1 through 3.3.2−7, and in the following Figures:

— 3.3.3−1, Rack Lower Ground Support Equipment Attachment (Front View)

— 3.3.3−2, Rack Lower Ground Support Equipment Attachment (Side View)

— 3.3.3−3, Typical Ground Support Equipment Boss.

3 − 37

FIGURE 3.3.3−1 RACK LOWER GROUND SUPPORT EQUIPMENT ATTACHMENT

(FRONT VIEW)

39.43 (1001.5)

SEE FIG. 3.3.3−3

E

SEE FIG. 3.3.3−3

RACK

DATUM

39.37 (1000.0)

1.10 (27.9)

1.04 (26.4)

.060 (1.52)

.040 (1.02)

CL

F

(1)

(1) 39.27 (997.46) minimum for Resupply Stowage Rack only

.375 (9.53) − 24 UNJF 3B

x x .500 (12.7) DP 2 PL

3 − 38

POINT E, F

LOWER GSE

BOSS 2 PL

RACK

DATUM

28.53 (724.7)

28.47 (723.1)

27.49 (698.2)

27.43 (696.7) or

FIGURE 3.3.3−2 RACK LOWER GROUND SUPPORT EQUIPMENT ATTACHMENT

(SIDE VIEW)

.50 (12.7)

ÉÉÉÉÉÉÉÉÉÉÉÉ

ÉÉÉÉÉÉÉÉÉÉÉÉ

ÉÉÉÉÉÉÉÉÉÉÉÉ

ÉÉÉÉÉÉÉÉÉÉÉÉ

ÉÉÉÉÉÉÉÉÉÉÉÉ

ÉÉÉÉÉÉÉÉÉÉÉÉ

ÉÉÉÉÉÉÉÉÉÉÉÉ

ÉÉÉÉÉÉÉÉÉÉÉÉ

ÉÉÉÉÉÉÉÉÉÉÉÉ

ÉÉÉÉÉÉÉÉÉÉÉÉ

ÉÉÉÉÉÉÉÉÉÉÉÉ

ÉÉÉÉÉÉÉÉÉÉÉÉ

1.00 (25.4)

1.00 (25.4)

POINTS

E, F, G, H

.50 (12.7)

FIGURE 3.3.3−3 TYPICAL GROUND SUPPORT EQUIPMENT BOSS

3 − 39

3.3.4 PIVOT ATTACHMENT INTERFACES

The MPLM to rack pivot attachment interfaces are for transferring on−orbit loads associated with operations and for on−orbit placement of the rack relative to the rear and upper attachments.

The pivot attachment interfaces consist of two parts: (i) the capture slot at rack mechanism, which is part of the racks, (ii) the pivot pin which is mounted on the standoff and is removable and installable on−orbit. The pivot attachment interfaces do not support launch, ascent, reentry, landing, or ground handling loads.

The attachment interfaces are shown in the following Figures:

— 3.3.4−1, Pivot Slot Mechanism Envelope in Rack Lateral Frame

— 3.3.4−2, Pivot Slot (Side View)

— 3.3.4−3, Pivot Pin Detail

— 3.3.4−4, NASA ARIS Pivot Pin Detail (not applicable to MPLM)

— 3.3.4−5, MHI/IHI ARIS Pivot Pin Detail (not applicable to MPLM)

3.3.4.1 ARIS COMPATIBLE PIVOT INTERFACES

The ARIS Pivot Pin in Figure 3.3.4−4 will be used for NASA rack structures, and its equivalent will be used in the CAM and for ARIS/ISPR and ISPR locations in other modules. The ARIS Pivot Pin in figure 3.3.4−5 will be used for MHI/IHI rack structures.

3.3.4.2 PARIS COMPATIBLE PIVOT INTERFACES

The ARIS Pivot Pin in Figure 3.3.4–4 will be used in the USL, and its equivalent will be used in the CAM and for PaRIS/ISPR locations in other modules.

3 − 40

Note 1: Dimension from Rack datum point

38.74 to 40.40 (984.0 to 1026.1) Note 1

J −1.10 to 0.56 (−27.9 to 14.2) Note 1

I

ÇÇÇ

ÇÇÇ

ÇÇÇ

ÇÇÇ

ÇÇÇ

ÇÇÇ

ÇÇÇ

ÇÇÇ

ÇÇÇ

C L

ÇÇÇ

ÇÇÇ

ÇÇÇ

ÇÇÇ

ÇÇÇ

ÇÇÇ

ÇÇÇ

ÇÇÇ

37.623 (955.62) min. for Boeing

38.210 (970.6) min. for MHI

37.89 (962.4) min. for IHI

FIGURE 3.3.4−1 PIVOT SLOT MECHANISM ENVELOPE

IN RACK LATERAL FRAME

3 − 41

CAPTURE RANGE

Min 0.71 (18.03)

NOTES:

PIVOT POINT

I, J

2.15 (54.6)

2.09 (53.1)

25.03 (635.8)

24.97 (634.2)

RACK

DATUM

FIGURE 3.3.4−2 PIVOT SLOT (SIDE VIEW)

• Pivot point mechanism contains latching mechanism to fix the pivot attachment

Full RPIVOT SLOT Min 0.50 (12.70) Max 0.54 (13.72)

PIN

(TYPICAL)

BRACKET

(TYPICAL)

ÄÄÄ

ÄÄÄ

ÄÄÄ

ÄÄÄ

ÄÄÄÄ

ÄÄÄÄ

ÄÄÄÄ

ÄÄÄÄ

36.9 (937)

36.7 (932)

41.52 MINIMUM

.394 (10.01) .375 (9.52)∅

ÄÄÄÄ

ÄÄÄÄ

ÄÄÄÄ

ÄÄÄÄ

ÄÄÄ

ÄÄÄ

ÄÄÄ

ÄÄÄ

15° MIN

TYPICAL

15° MIN

TYPICAL

R .689 (17.5)

TYPICAL

FIGURE 3.3.4−3 PIVOT PIN DETAIL

3 − 42

41.19 (1046.2)

37.47 (951.7)

36.47 (926.3)

BRACKET

(TYPICAL)

PIN

(TYPICAL)

.375 (9.53)

Part Number 683−61711−31

Part Number 683−61711−32

FIGURE 3.3.4−4 NASA ARIS PIVOT PIN DETAIL

(NOT APPLICABLE TO MPLM)

3 − 43

Max. 41.320 (1049.52)

Max. 37.812 (960.4)

Min. 36.432 (925.38)

BRACKET

(TYPICAL)

PIN

(TYPICAL)

.375 (9.53)

Part Number 683−20100−1

Part Number 683−20100−2

FIGURE 3.3.4−5 MHI/IHI ARIS PIVOT PIN DETAIL

(NOT APPLICABLE TO MPLM)

3 − 44

3.3.5 RESTRAINTS AND MOBILITY AIDS HARDWARE INTERFACE

The restraints and mobility aids hardware interfaces with the modified seat tracks attached to the front face of the rack posts as shown in Figure 3.3.5−1, Restraints and Mobility Aids Hardware Interface. Figure 3.3.5−2, Restrains and Mobility Aids Hardware Interface Schematic, shows these interfaces schematically.

3.4 ENVIRONMENTAL INTERFACES

3.4.1 NATURAL ENVIRONMENT

The rack−to−MPLM/GSE interface design has no unique characteristics due to natural environment requirements.

3.4.1.1 NEUTRAL ATMOSPHERE ENVIRONMENT

Not Applicable.

3.4.1.2 METEOROIDS AND ORBITAL DEBRIS ENVIRONMENT

Not Applicable.

3.4.1.3 MAGNETIC FIELD ENVIRONMENT

Not Applicable.

3.4.1.4 GRAVITATIONAL FIELD ENVIRONMENT

Not Applicable.

3.4.1.5 THERMAL ENVIRONMENT

Not Applicable.

3.4.1.6 PHYSICAL CONSTANTS

Not Applicable.

3.4.2 INDUCED ENVIRONMENT

The rack−to−MPLM/GSE interfaces are capable of operation during and after exposure to any feasible combination of the following environments for launch, landing, and ground handling.

3 − 45

FIGURE 3.3.5−1 RESTRAINTS AND MOBILITY AIDS HARDWARE INTERFACE

.428 (11.38)

.820 (20.83)

.800 (20.32)

1.05 (26.7) .99 (25.1)

(1.5) R .06

.9

(1

1.

8)

A C

C U

M U

LA

T

E D

T O

LE

R

A N

C E

N O

T T

O E

X C

E E

D

.0

.5

1)

.070 (1.78)

.152 (3.86) .250 (6.35)

.049 (1.24)

.38 (9.7)

.780 (19.81) ∅ .790 (20.07)

1.03 (26.2) .97 (24.6)

.54 (13.7)

1.005 (25.53) .995 (25.27)

Typical for 80” rack. Length is dependent on rack size and available space. Minimum length of 40.54 (1029.7).

Centerline to centerline of tracks.

40.03 (1016.8)

39.97 (1015.2)

CL

3 Fastener will not protrude above the bottom of the seat track.

Track max

.0

(1

3.

4)

.48 (12.2)

.420 (10.67)

.17 (4.3)

.11 (2.8)

.316 (8.03)

.300 (7.62)

R .32 (8.1) R

.050 (1.27)

.230 (5.84)

.037 (.94)

.138 (3.51)

Full R

4 Maximum distance from GSE points E and F.

5 Maximum distance from GSE points G and H.

6 Front Face of Seat Track Is within static envelope.

17.15 (435.6)

14.40 (365.8)

3 − 46

Crewmembers

Equipment/ORUs

Restraints and Mobility Aids

Modified Seat Track

FIGURE 3.3.5−2 RESTRAINTS AND MOBILITY AIDS

HARDWARE INTERFACE SCHEMATIC

3.4.2.1 ELECTROMAGNETIC ENVIRONMENT

Not Applicable.

3.4.2.2 ELECTROSTATIC ENVIRONMENT

Not Applicable.

3.4.2.3 DELETED

3.4.2.4 ACOUSTICS ENVIRONMENT

Not Applicable.

3.4.2.5 THERMAL ENVIRONMENT

Not Applicable.

3.4.2.6 REDUCED ATMOSPHERE ENVIRONMENT

Not Applicable.

3.4.2.7 CONTAMINATION ENVIRONMENT

Not Applicable.

3 − 47

3.4.2.7.1 INTERNAL CONTAMINATION ENVIRONMENT

Not Applicable.

3.4.2.7.2 EXTERNAL CONTAMINATION ENVIRONMENT

Not Applicable.

3.4.2.8 PLASMA ENVIRONMENT

Not Applicable.

3.4.2.9 IONIZING RADIATION ENVIRONMENT

Not Applicable.

3.4.2.10 MICROGRAVITY ENVIRONMENT

Not Applicable.

3.4.2.11 ENVIRONMENTAL CONTROL AND LIFE SUPPORT SYSTEM EFFECTS

ENVIRONMENT

Not Applicable.

3.4.2.11.1 DEPRESSURIZATION/REPRESSURIZATION ENVIRONMENT

Not Applicable.

3.4.2.11.2 LEAKAGE ENVIRONMENT

Not Applicable.

3.4.2.12 MAN SYSTEMS ENVIRONMENT

Not Applicable.

3.4.2.13 ON−ORBIT CREW−INDUCED LOADING

Racks may be subjected to an inadvertent kick or push−off. Maximum crew−induced design limit loads are given in SSP 50005, International Space Station Flight Crew Integration Standard, or COL−RQ−ESA−013, Columbus Human Factors Engineering Requirements.

3 − 48

3.5 SYSTEM INTERFACES

Not Applicable.

3.5.1 ELECTRICAL POWER SYSTEM

Not Applicable.

3.5.2 DATA MANAGEMENT SYSTEM

Not Applicable.

3.5.3 THERMAL CONTROL SYSTEM

Not Applicable.

3.5.4 COMMUNICATIONS AND TRACKING SYSTEM

Not Applicable.

3.5.5 GUIDANCE, NAVIGATION, AND CONTROL SYSTEM

Not Applicable.

3.5.6 EXTRAVEHICULAR ACTIVITY SYSTEM

Not Applicable.

3.5.7 ENVIRONMENTAL CONTROL AND LIFE SUPPORT SYSTEM

The environmental control and life support system interface consists of manual fire suppression.

3.5.7.1 FIRE SUPPRESSION

The manual fire suppression interface is defined in SSP 41002, International Standard Payload Rack to NASA/ESA/JAXA Modules Interface Control Document.

3.5.8 MAN SYSTEMS

3.5.8.1 RESTRAINT AND MOBILITY HARDWARE INTERFACE

The restraint and mobility hardware interface is defined in section 3.3.5.

3.5.9 FLUID MANAGEMENT SYSTEMS

Not Applicable.

3.6 SOFTWARE INTERFACES

Not Applicable.

i

A.1 CONTROL AUTHORITY A − 1

A.2 ABBREVIATIONS AND ACRONYMS A − 1

A − 1

APPENDIX A ABBREVIATIONS AND ACRONYMS

A.1 CONTROL AUTHORITY

Appendix A is not subject to Level II SSCB change control. Responsibility for control of configuration management abbreviations and acronyms changes is delegated to the Level II SSCB Executive Secretary.

This appendix will be revised as required, and changes will be issued as replacement pages or by complete revision of the appendix as appropriate. All requested changes will be directed to the Level II SSCB Executive Secretary, SSFPO.

A.2 ABBREVIATIONS AND ACRONYMS

APM Attached Pressurized Module

ARIS Active Rack Isolation System

CAM Centrifuge Accomodation Module

ESA European Space Agency

FDS Fire Detection System g acceleration on earth’s surface due to earth gravity

GSE Ground Support Equipment

ICD Interface Control Document

ICWG Interface Control Working Group

IHI Ishikawajima−Harima Heavy Industries

ISO International Standards Organization

ISPR International Standard Payload Rack

JAXA Japan Aerospace Exploration Agency

JEM Japanese Experiment Module

JPDRD Joint Program Definition and Requirements Document

KBAR Kneebrace Bolt Action Replacement

Kg Kilograms lbs pounds max maximum

MHI Mitsubishi Heavy Industries min minimum

A − 2

MPLM Mini−Pressurized Logistics Module

NASA National Aeronautics and Space Administration

PaRIS Passive Rack Isolation System

PL places

PLM Pressurized Logistics Module

R radius

REF reference

SI International System of Units

SSFP Space Station Freedom Program

TBD To Be Determined

TBR To Be Resolved

USL United States Laboratory

US Lab United States Laboratory

B − 1

APPENDIX B INDEX OF TBD S AND TBRS

APPENDIX B − INDEX OF TBD S AND TBRS

TBD No. Page No. Paragraph No. Status

30 3−6 Paragraph 3.1.6.2 Closed

31 3−28 Figure 3.3.2.3−5 Closed

32 3−28 Figure 3.3.2.3−6 Closed