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This notice announces a forthcoming request for proposal for a human space flight technical integration contract. NASA/Johnson Space Center plans to issue the RFP on or about November 1, 2019, with proposals due on or about December 11, 2019. The contract is a total small business set-aside under NAICS code 541715 with a size standard of 1,250 employees. The contractor will provide technical integration services for human space flight. Interested parties should monitor the listed websites for the RFP and amendments. All technical questions must be submitted in writing.
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SSP 41004
National Aeronautics and Space Administration International Space Station Program Johnson Space Center Houston, Texas Contract No. NAS15−10000
International Space Station Program esa european space agency
Common Berthing Mechanism to Pressurized Elements Interface Control Document Part 2
Revision J October 25, 2005
SSP 41004, Part 2, Revision J October 25, 2005 ii
REVISION AND HISTORY PAGE
REV. DESCRIPTION PUB.
DATE
− BASELINE ISSUE (REFERENCE SSCBD BB003287 EFF. 02−25−92) 02−92
IRNs 0001 − 0035 (REFERENCE SSCBD BB003287A EFF. 04−03−92) 04−92
IRN 0036 (REFERENCE SSCBD BB003287B EFF. 07−16−92) 07−92
A REVISION A (REFERENCE IRN 0037, SSCBD BB003287B EFF. 07−16−92) 07−92
IRN 0038 (REFERENCE SSCBD BB003287C EFF. 11−13−92) 12−92
IRNs 0040 − 0046 (REFERENCE SSCBD BB003287C EFF. 11−13−92) 12−92
IRN 0048 (REFERENCE SSCBD BB003287C EFF. 11−13−92) 12−92
IRN 0049 (REFERENCE SSCBD BB003287D EFF. 12−18−92) 01−93
B REVISION B (REFERENCE IRN 0050, SSCBD BB003287D EFF. 12−18−92) 01−93
C REVISION C (ECP BHE0001) 04−95
D REVISION D (REFERENCE SSCD 000293 EFF. 05−10−96) 06−12−96
Note: This is the first release of Part 2. As of this release Part 1 and Part 2 will be tracked separately.
INCORPORATING AGREED PIRNS AS FOLLOWS:
PIRN 41004−NA−0016a, PIRN 41004−NA−0017a, PIRN 41004−NA−0018a, PIRN 41004−NA−0019, PIRN 41004−NA−0020, PIRN 41004−NA−2001, 41004−NA−2002a, 41004−NA−2003, 41004−NA−2005a, 41004−NA−2006, 41004−NA−2007, 41004−NA−2008, 41004−NA−2010
E REVISION E (REFERENCE SSCD 000429, EFF. 11−08−96) 08−12−97
Correction to Revision D − PIRNS 41004−NA−0015, 41004−NA−0021a were added in Rev D. These PIRNs in Rev D, were just omitted from the Rev/History page.
INCORPORATING THE FOLLOWING PIRNS:
PIRNs 41004−ES−0002A, 41004−ES−0003A, 41004−ES−0004, 41004−NA−2004,41004−2011D, 41004−NA−2012B, 41004−NA−2013A, 41004−NA−2014C, 41004−NA−2015A, 41004−NA−2016A, 41004−NA−2017, 41004−NA−2018, 41004−NA−2019, 41004−NA−2020A, 41004−NA−2022, 41004−NA−2023, 41004−NA−2024, 41004−NA−2025, 41004−NA−2026A, 41004−NA−2027A, 41004−NA−2028C, 41004−NA−2032B, 41004−ND−0001B, 41004−ND−0002A iii
REVISION AND HISTORY PAGE − CONTINUED
REV. DESCRIPTION PUB.
DATE
IRN 0606 per SSCD 000606R1, EFF. 04−14−98 (Release to File) 03−19−99
F REVISION F per SSCD 000838R1, EFF. 04−14−98. 03−19−99
INCORPORATING THE FOLLOWING PIRNS:
41004−ES−0006B, 41004−ES−0007B, 41004−NA−2029F, 41004−NA−2030G,
41004−NA−2035A, 41004−NA−2037A, 41004−NA−2038B, 41004−NA−2039B,
41004−NA−2040B
G REVISION G per SSCD 001165, EFF. 06−16−99 07−08−99
INCORPORATING THE FOLLOWING PIRNS:
41004−AS−0009A, 41004−AS−0011C, 41004−AS−0015A, 41004−AS−0020A,
41004−ES−0011A, 41004−NA−2041, 41004−NA−2042B, 41004−NA−2043B,
41004−NA−2044, 41004−ND−0007A, 41004−ND−0009A
H REVISION H released per SSCD 006955, EFF. 03−24−03 05−03−04
Incorporating the following PIRNs:
41004−AS−0010F
41004−AS−0016D
41004−AS−0019D
41004−AS−2001
41004−AS−2002A
41004−AS−2003E
41004−AS−2004C
41004−ES−0009A
41004−ES−0015
41004−NA−2046
41004−NA−2050A
41004−NA−2051B
41004−NA−2052A
41004−NA−2053A
41004−NA−2054
41004−NA−2056
iv
REV. DESCRIPTION PUB.
DATE
41004−NA−2057A
41004−NA−2058A
41004−NA−2059
41004−ND−0005B
41004−ND−0008A
41004−ND−0010B
Revision H also incorporates the following PIRNs with associated SSCNs:
41004−NA−2045B SSCN 001465
41004−NA−2047B SSCN 001594
41004−NA−2048A SSCN 001481
41004−NA−2049A SSCN 001555
Revision H closes the following SSCNs as they were overcome by events:
000554, 000583, 000585, 000588, 000591, 000673, 000773, 000823, 000832, 000844, 000845, 000877, 000889, 000894, and 000915
NOTE: Due to past history of this document, IRN 0003 (SSCN 001920) has been retired without use.
J REVISION J released per SSCD 009719, EFF. 06−07−06 01−10−07
Incorporate the following approved PIRNs which were created by the applicable Changes listed below:
PIRN 41004−AS−2005C IRN N/A SSCN 009719
PIRN 41004−ES−0014A IRN N/A SSCN 009719
PIRN 41004−NA−2060A IRN 0005 SSCN 006135
PIRN 41004−ND−0012B IRN N/A SSCN 009719
Revision J closes the following SSCNs as they were overcome by events:
PIRN N/A IRN N/A SSCN 000780
PIRN N/A IRN 0002 SSCN 001740
ERU: /s/ J. Rivas 01−10−07 v
PREFACE
SSP 41004, Part 2 Common Berthing Mechanism to Pressurized Elements Interface Control Document shall be implemented on all new Program contractual and internal activity and shall be included in any existing contracts through contract changes. This document is under the control of the Interface Control Working Group (ICWG), as described in SSP 30459, ISS Interface Control Plan.
vi
INTERNATIONAL SPACE STATION PROGRAM
COMMON BERTHING MECHANISM TO PRESSURIZED ELEMENTS
INTERFACE CONTROL DOCUMENT
LIST OF CHANGES
(SHEET 1 OF 1)
OCTOBER 25, 2005
All changes to paragraphs, tables, and figures in this document are shown below:
SSCBD ENTRY DATE CHANGE PARAGRAPH(S)
009719 10/05 AS−2005C Table 3.3.2.1.4−1
009719 10/05 ES−0014A Table 3.3.2.1.4−1
006135 10/05 NA−2060A Para. 2.2, 3.1.4, App. A
009719 10/05 ND−0012B Figs. 3.1.4.2−3, 3.3.2.1−7, 3.3.2.1−10, 3.3.2.1−11, 3.3.8−5, 3.3.10−1, Table 3.3.2.1.4−1 vii
NASA/JAXA/ESA/ASI APPROVAL
INTERNATIONAL SPACE STATION PROGRAM
COMMON BERTHING MECHANISM TO PRESSURIZED ELEMENTS
INTERFACE CONTROL DOCUMENT
PART 2
OCTOBER 25, 2005
Date
Print Name
NASA Program Manager JAXA Program Manager
Print Name
Date
Randy H. Brinkley Kazuo Suzuki
Date
Print Name
ESA Program Manager ASI Program Manager
Print Name
Date
Giovanni RumAlan Thirkettle
/s/Alan Thirkettle
26 Mar’96 27 Mar 1996
/s/Giovanni Rum
/s/D. R. Cooke for Randy H. Brinkley /s/Yasushi Horikawa for Kazuo Suzuki
31 May 199610 May 1996 viii
CONCURRENCE
INTERNATIONAL SPACE STATION PROGRAM
COMMON BERTHING MECHANISM TO PRESSURIZED ELEMENTS
INTERFACE CONTROL DOCUMENT
PART 2
OCTOBER 25, 2005
NASA ICWG Chairman __________ Representative for Concurrence Frank Monahan DATE
ASI ICWG Chairman __________ Representative for Concurrence Andrea Lorenzoni DATE
Boeing ICWG Chairman __________ Representative for Concurrence Howard Griffin DATE
JAXA ICWG Chairman __________ Representative for Concurrence Kuniaki Shiraki DATE
ESA ICWG Chairman __________ Representative for Concurrence Alessio Festa DATE
DASA ICWG Chairman __________ Representative for Concurrence Hans−Jorg Pospieszcyk DATE
Alenia ICWG Chairman __________ Representative for Concurrence Alessandro Bellomo DATE
(S) Document has been signed by representative
/s/F. J. Monahan
/s/H. S. Griffin
3/26/96
3/26/96
3/25/96/s/Kuniaki Shiraki
/s/Hans−Jorg Pospieszczyk
26/March/96/s/Alessio Festa
/s/Alessandro Bellomo 25.03.96
25.3.96
/s/F. J. Monahan
03 −26’96/s/Andrea Lorenzoni ix
PRODUCT GROUP
CONCURRENCE
INTERNATIONAL SPACE STATION ALPHA PROGRAM
COMMON BERTHING MECHANISM TO PRESSURIZED ELEMENTS
INTERFACE CONTROL DOCUMENT
PART 2
OCTOBER 25, 2005
Product Group − 1 ICWG __________ Representative for Concurrence DATE
Product Group − 2 ICWG __________ Representative for Concurrence DATE
Product Group − 3 ICWG __________ Representative for Concurrence DATE
(S) Document has been signed by representative
/s/Ralph Thompson 3/25/96
/s/L. T. Archibald 3/25/96
L. T. Archibald
NA
x
INTERNATIONAL SPACE STATION PROGRAM
COMMON BERTHING MECHANISM TO PRESSURIZED ELEMENTS
INTERFACE CONTROL DOCUMENT
PART 2
OCTOBER 25, 2005
CONCURRENCE
Warren England BHOU
PREPARED BY: PRINT NAME ORGN
/s/ Warren England 4/10/06
SIGNATURE DATE
CHECKED BY: Quentin Henry BHOU
PRINT NAME ORGN
/s/ Quentin L. Henry 4/11/06
SIGNATURE DATE
APPROVED BY (NASA): Chau Hong OB/NASA
PRINT NAME ORGN
/s/ Chau Hong 4/4/06
SIGNATURE DATE
DQA: Merry McClain BHOU
PRINT NAME ORGN
/s/ Merry McClain 4/12/06
SIGNATURE DATE
xi
INTERNATIONAL SPACE STATION PROGRAM
COMMON BERTHING MECHANISM TO PRESSURIZED ELEMENTS
INTERFACE CONTROL DOCUMENT
PART 2
APRIL 30, 2002
NODE 2 PROJECT CONCURRENCE
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SSP 41004, Part 2 Revision J
TABLE OF CONTENTS
October 25, 2005 xii
PARAGRAPH PAGE
1.0 INTRODUCTION 1 − 1
1.1 PURPOSE 1 − 1
1.2 SCOPE 1 − 1
1.3 PRECEDENCE 1 − 1
1.4 DELEGATION OF AUTHORITY 1 − 1
2.0 DOCUMENTS 2 −1
2.1 APPLICABLE DOCUMENTS 2 −1
2.2 REFERENCE DOCUMENTS 2 −8
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 ENVELOPE INTERFACES 3 − 3
3.1.4.1 CBM HARDWARE ENVELOPES 3 − 23
3.1.4.2 CBM IVA SEAL SYSTEM HARDWARE ENVELOPE 3 − 46
3.1.4.3 ACTIVE CBM WIRE HARNESS ENVELOPE 3 − 46
3.1.4.4 NODE 2/3 ACBM RADIAL PORT DEPLOYABLE M/D PETAL HARDWARE
ENVELOPE 3 − 55
3.1.5 MASS PROPERTIES 3 − 55
3.1.5.1 CENTER OF MASS 3 − 55
3.1.5.2 MOMENTS OF INERTIA 3 − 55
3.1.5.3 MASS LIMITATIONS 3 − 55
3.1.6 ENGINEERING UNITS AND TOLERANCES 3 − 57
3.1.6.1 TOLERANCE 3 − 57
3.1.6.2 CONVERSIONS 3 − 57
3.2 STRUCTURAL INTERFACES 3 − 57
3.2.1 GENERAL 3 − 57
3.2.1.1 ACTIVE CBM−TO−MODULE INTERFACE DEFLECTION LIMITATIONS 3 − 57
3.2.1.1.1 RADIAL DEFORMATIONS 3 − 57
3.2.1.1.2 DIFFERENTIAL DISPLACEMENT ALONG THE XCBM AXIS 3 − 59
3.2.1.1.3 TANGENTIAL ROTATIONS 3 − 59
3.2.1.2 DELETED 3 − 59
3.2.1.3 PASSIVE CBM−TO−MODULE INTERFACE DEFLECTION LIMITATIONS 3 − 64
3.2.1.3.1 RADIAL DEFORMATIONS 3 − 64
3.2.1.3.2 DIFFERENTIAL DISPLACEMENT ALONG THE XCBM AXIS 3 − 66
3.2.1.3.3 TANGENTIAL ROTATIONS 3 − 66
SSP 41004, Part 2 Revision J October 25, 2005 xiii
TABLE OF CONTENTS
PARAGRAPH PAGE
3.2.2 STRUCTURAL MATHEMATICAL MODELS 3 − 66
3.3 MECHANICAL INTERFACES 3 − 66
3.3.1 GENERAL 3 − 66
3.3.2 ATTACHMENT MECHANISMS 3 − 66
3.3.2.1 COMMON BERTHING MECHANISM−TO−MODULE ATTACHMENT 3 − 66
3.3.2.1.1 ALIGNMENT AND INDEXING 3 − 78
3.3.2.1.2 MODULE CRITICAL DIMENSIONS 3 − 78
3.3.2.1.3 CBM−TO−MODULE IVA SEAL ATTACHMENT 3 − 78
3.3.2.1.4 CBM−TO−MODULE CLOCKING 3 − 78
3.3.2.1.5 MATCH DRILLED HOLES 3 − 78
3.3.3 THERMAL INTERFACES 3 − 89
3.3.3.1 CONDUCTIVE INTERFACES 3 − 89
3.3.3.1.1 INTERFACE DESCRIPTION 3 − 89
3.3.3.2 THERMAL MATHEMATICAL MODELS 3 − 89
3.3.4 ACTIVE CBM−TO−MODULE MOTOR CONTROLLER INTERFACES 3 − 89
3.3.4.1 ACTIVE CBM UNIQUE EPS BULKHEAD CONNECTORS 3 − 89
3.3.4.2 MOTOR CONTROLLER CABLE INTERFACE 3 − 89
3.3.4.3 MOTOR CONTROLLER MOUNTING PROVISIONS (ACTIVE CBM ONLY) 3 − 89
3.3.4.3.1 MOTOR CONTROLLER ATTACHMENT 3 − 89
3.3.5 LEAK CHECK INTERFACES 3 − 99
3.3.5.1 LEAK CHECK PORT DESIGN 3 − 99
3.3.5.2 ATMOSPHERIC CONTAINMENT 3 − 99
3.3.6 ACTIVE CBM−TO−MODULE BULKHEAD FEEDTHRU INTERFACES 3 − 99
3.3.7 GROUND HANDLING INTERFACES 3 − 99
3.3.7.1 HANDLING AND LIFT POINT LOCATIONS 3 − 99
3.3.8 VESTIBULE CLOSEOUT PANEL INTERFACES 3 − 107
3.3.9 M/D CENTER DISK BRACKET INTERFACE DETAILS 3 − 115
3.3.9.1 AXIAL ACBM HATCH BEAM HOLES 3 − 115
3.3.10 PASSIVE THERMAL EQUIPMENT ATTACHMENT PROVISIONS 3 − 115
3.3.10.1 AVAILABLE HOLE LOCATIONS FOR SHIELDING ON ACBM/PCBM RINGS 3 − 115
3.3.11 ACBM WIRE HARNESS ATTACHMENT LOCATIONS 3 − 117
3.3.12 NODE 2 RADIAL PORT M/OD SHIELD/ACBM INTERFACES 3 − 118
3.3.13 PCBM INTERFACES FOR CUPOLA HANDRAIL BRACKETS 3 − 118
3.3.13.1 CUPOLA HANDRAIL INDUCED LOADS 3 − 118
3.4 ENVIRONMENTAL INTERFACES 3 − 165
xiv
TABLE OF CONTENTS
PARAGRAPH PAGE
3.4.1 ACBM ENVIRONMENTAL INTERFACES 3 − 165
3.4.2 PCBM ENVIRONMENTAL INTERFACES 3 − 165
3.5 SYSTEM INTERFACES (ACTIVE COMMON BERTHING MECHANISM ONLY) 3 − 165. . .
3.5.1 GENERAL 3 − 165
3.5.2 CONNECTORS 3 − 165
3.5.2.1 POWER DISTRIBUTION 3 − 165
3.5.2.1.1 DELETED 3 − 165
3.5.2.1.2 POWER QUALITY 3 − 165
3.5.2.2 DELETED 3 − 165
3.5.2.3 ELECTRICAL BONDING 3 − 165
3.5.2.4 CABLE CHARACTERISTICS 3 − 166
3.5.3 MODULE BULKHEAD UTILITY PENETRATION 3 − 166
3.5.3.1 CONNECTORS 3 − 166
3.5.4 EXTRAVEHICULAR ACTIVITY SYSTEM 3 − 166
3.6 SOFTWARE INTERFACES (NASA ONLY) 3 − 166
APPENDIX PAGE
A ABBREVIATIONS AND ACRONYMS A − 1
B INDEX OF TBDS/TBRS/TBCS B − 1
C ISSUE LIST FOR SSP 41004 C − 1
xv
TABLE OF CONTENTS
TABLES
TABLE PAGE
3.1.6.1−1 LINEAR TOLERANCES 3 − 57
3.3.2.1.3−1 PASSIVE CBM IVA SEAL ANGULAR ATTACHMENT LOCATIONS 3 − 82
3.3.2.1.3−2 ACTIVE CBM IVA SEAL ANGULAR ATTACHMENT LOCATIONS 3 − 84
3.3.2.1.4−1 CBM INSTALLATION CLOCKING (SHEET 2 OF 3) 3 − 86
3.3.4.1−1 EPS BULKHEAD CONNECTOR FOR ACTIVE CBM CONTROL (POWER) 3 − 90
3.3.4.1−2 EPS BULKHEAD CONNECTOR FOR ACTIVE CBM CONTROL
(REDUNDANT POWER) 3 − 91
3.3.4.2−1 C&DH BULKHEAD CONNECTOR FOR ACTIVE CBM CONTROL
(1553 NETWORK A) 3 − 92
3.3.4.2−2 C&DH BULKHEAD CONNECTOR FOR ACTIVE CBM CONTROL
(1553 NETWORK B) 3 − 93
xvi
TABLE OF CONTENTS
FIGURES
FIGURE PAGE
3.1.3−1 COMMON BERTHING MECHANISM COORDINATE SYSTEM 3 − 2
3.1.4−1 STATIC ENVELOPE OF PASSIVE CBM (SIDE VIEW) 3 − 4
3.1.4−2 STATIC ENVELOPE OF PASSIVE COMMON BERTHING MECHANISM
(END VIEW) 3 − 5
3.1.4−3 STATIC ENVELOPE OF ACTIVE CBM ON AXIAL PORT WITHOUT
THERMAL/DEBRIS COVER (SIDE VIEW) 3 − 6
3.1.4−4 STATIC ENVELOPE OF ACTIVE COMMON BERTHING MECHANISM ON AXIAL
PORT WITHOUT THERMAL/DEBRIS COVER (END VIEW) 3 − 7
3.1.4−5 STATIC ENVELOPE OF ACTIVE CBM ON AXIAL PORT WITH
METEOROID / DEBRIS SKIRT (SIDE VIEW) 3 − 8
3.1.4−5.1 ANGULAR POSITION OF THERMAL DEBRIS / SKIRT ATTACH POINTS 3 − 9
3.1.4−5.2 AXIAL AND RADIAL POSITION OF THERMAL / DEBRIS SKIRT ATTACH
POINTS 3 − 10
3.1.4−6 STATIC ENVELOPE OF ACTIVE CBM ON RESOURCE NODE RADIAL PORT WITHOUT
THERMAL/DEBRIS COVER 3 − 11
3.1.4−7 STATIC ENVELOPE OF ACTIVE CBM ON RESOURCE NODE RADIAL PORT WITH
THERMAL/DEBRIS COVERS CLOSED 3 − 12
3.1.4−7.1 STATIC AND DYNAMIC ENVELOPE OF ACTIVE CBM ON RESOURCE NODE RADIAL
PORT WITH THERMAL/DEBRIS COVERS OPEN AND SKIRTS 3 − 13
3.1.4−7.2 STATIC AND DYNAMIC ENVELOPE OF ACTIVE CBM ON RESOURCE NODE RADIAL
PORT WITH THERMAL/DEBRIS COVERS OPEN AND SKIRTS (SECTION B−B) 3 − 14.
3.1.4−7.3 STATIC AND DYNAMIC ENVELOPE OF ACTIVE CBM ON RESOURCE NODE RADIAL
PORT WITH THERMAL/DEBRIS COVERS OPEN AND SKIRTS (SECTION B−B) 3 − 15.
3.1.4−8 STATIC ENVELOPE OF ACTIVE CBM ON JAPANESE EXPERIMENT MODULE RADIAL
PORT WITHOUT THERMAL/DEBRIS COVER (SIDE VIEW) 3 − 16
3.1.4−9 STATIC ENVELOPE OF ACTIVE CBM ON JAPANESE EXPERIMENT MODULE RADIAL
PORT WITH THERMAL/DEBRIS COVER 3 − 17
3.1.4−10 MODULE−TO−MODULE UTILITY JUMPER ENVELOPE ACTIVE AND PASSIVE
CBM−TO−MODULE INTERFACE 3 − 18
3.1.4−11 MODULE−TO−MODULE UTILITY JUMPER ENVELOPE (SECTION A−A) 3 − 19
3.1.4−12 MODULE−TO−MODULE UTILITY JUMPER ENVELOPE (SECTION B−B) 3 − 20
3.1.4−13 STATIC ENVELOPE OF ACTIVE CBM ASI NODES MODULE RADIAL PORTS WITHOUT
THERMAL/DEBRIS COVER 3 − 21
3.1.4−14 STATIC ENVELOPE OF ACTIVE CBM ON RESOURCE NODE RADIAL PORT WITH
THERMAL/DEBRIS COVERS CLOSED 3 − 22
xvii
TABLE OF CONTENTS
FIGURE PAGE
3.1.4.1−1 ACTIVE CBM CLEARANCE ENVELOPE FOR PASSIVE CBM ALIGNMENT GUIDES 3 − 24. .
3.1.4.1−2 ACTIVE CBM CLEARANCE ENVELOPE FOR PASSIVE CBM ALIGNMENT GUIDES (VIEW
A−A) 3 − 25
3.1.4.1−3 ACTIVE CBM CAPTURE LATCH CLEARANCE ENVELOPE 3 − 26
3.1.4.1−4 ACTIVE CBM CAPTURE LATCH CLEARANCE ENVELOPE (VIEW A−A) 3 − 27
3.1.4.1−5 ACTIVE CBM CAPTURE LATCH CLEARANCE ENVELOPE (VIEW B−B) 3 − 28
3.1.4.1−6 MOTOR CONTROLLER CLEARANCE ENVELOPE 3 − 29
3.1.4.1−7 TYPICAL MOTOR CONTROLLER AXIAL HATCH BEAM CLEARANCE ENVELOPE
(VIEW A−A) 3 − 30
3.1.4.1−8 POWERED BOLT CENTERLINE LOCATIONS 3 − 31
3.1.4.1−9 POWERED BOLT MOTOR CLEARANCE ENVELOPE 3 − 32
3.1.4.1−10 POWER BOLT MOTOR CLEARANCE ENVELOPE (VIEW A−A) 3 − 33
3.1.4.1−11 ACTIVE CBM READY-TO-LATCH CLEARANCE ENVELOPE 3 − 34
3.1.4.1−12 READY-TO-LATCH CLEARANCE ENVELOPE (VIEW A−A) 3 − 35
3.1.4.1−13 READY-TO-LATCH CLEARANCE ENVELOPE (VIEW B−B) 3 − 36
3.1.4.1−14 PASSIVE CBM CLEARANCE ENVELOPE FOR ACTIVE CBM ALIGNMENT
GUIDES 3 − 37
3.1.4.1−15 PASSIVE CBM CLEARANCE ENVELOPE FOR ACTIVE CBMALIGNMENT GUIDES
(VIEW A−A) 3 − 38
3.1.4.1−16 ACTIVE CBM CAPTURE LATCH AND FITTING CLEARANCE ENVELOPE FOR
PASSIVE CBM 3 − 39
3.1.4.1−17 PASSIVE CBM CAPTURE LATCH AND FITTING CLEARANCE ENVELOPE
(VIEW A−A) 3 − 40
3.1.4.1−18 PASSIVE CBM CAPTURE LATCH AND FITTING CLEARANCE ENVELOPE
(VIEW B−B) 3 − 41
3.1.4.1−19 MOTOR CONTROLLER AND M/D CENTER COVER PASSIVE CBM HARDWARE
CLEARANCE ENVELOPE 3 − 42
3.1.4.1−20 MOTOR CONTROLLER AND M/D CENTER COVER PCBM HARDWARE CLEARANCE
(VIEW D −D) 3 − 43
3.1.4.1−21 PASSIVE CBM CLEARANCE ENVELOPE FOR POWERED BOLT NUT 3 − 44
3.1.4.1−22 PCBM CLEARANCE ENVELOPE FOR POWERED BOLT NUT
(VIEW E −E) 3 − 45
3.1.4.2−1 STAY OUT ZONES FOR CBM-TO-CBM IVA SEALS IN PLACE 3 − 47
3.1.4.2−2 STAY OUT ZONES FOR CBM-TO-CBM IVA SEALS IN PLACE
(VIEWS A−A AND B−B) 3 − 48
xviii
TABLE OF CONTENTS
FIGURE PAGE
3.1.4.2−3 STAY OUT ZONES FOR CBM−TO−PE IVA SEALS 3 − 49
3.1.4.2−4 GUSSET INTRUSIONS INTO CBM−TO−PE IVA SEAL STAYOUT 3 − 50
3.1.4.2−5 LEAK CHECK PORT INTRUSIONS INTO CBM−TO−PE IVA SEAL STAYOUT 3 − 51
3.1.4.2−6 POWERED BOLT INTRUSIONS INTO ACBM−TO−PE IVA SEAL STAYOUT 3 − 52
3.1.4.2−7 CAPTURE LATCH INTRUSION INTO IVA SEAL STAYOUT ZONE 3 − 53
3.1.4.3−1 ACTIVE CBM WIRE HARNESS ENVELOPE 3 − 54
3.1.4.4−1 DEPLOYABLE COVER MODELS 3 − 55
3.1.5.1−1 COMMON BERTHING MECHANISM CENTER OF MASS AND MOMENTS OF
INERTIA 3 − 56
3.2.1.1.1−1 ACTIVE CBM−TO−MODULE INTERFACE RADIAL DISPLACEMENTS 3 − 58
3.2.1.1.2−1 DIFFERENTIAL DISPLACEMENT ALONG THE XCBM AXIS 3 − 60
3.2.1.1.3−1 DEFINITION OF BULKHEAD DEFLECTION PARAMETERS −
UNDEFORMED STATE 3 − 61
3.2.1.1.3−2 DEFINITION OF BULKHEAD DEFLECTION PARAMETERS −
DEFORMED STATE (MMAX) 3 − 62
3.2.1.1.3−3 DEFINITION OF BULKHEAD DEFLECTION PARAMETERS −DEFORMED STAT
(MMIN) 3 − 63
3.2.1.3.1−1 PASSIVE CBM−TO−MODULE INTERFACE RADIAL DISPLACEMENTS 3 − 65
3.3.2.1−1 PASSIVE CBM−TO−MODULE ATTACHMENT BOLT CIRCLES AND INDEXING
PIN LOCATIONS 3 − 67
3.3.2.1−2 ACTIVE CBM−TO−MODULE ATTACHMENT BOLT CIRCLES AND INDEXING
PIN LOCATIONS 3 − 68
3.3.2.1−3 ACTIVE CBM−TO−MODULE ATTACHMENT BOLT CIRCLES AND INDEXING
PIN LOCATIONS (VIEW A) 3 − 69
3.3.2.1−4 MODULE−TO−PASSIVE CBM ATTACHMENT BOLT CIRCLES AND HOLE
LOCATIONS 3 − 70
3.3.2.1−5 MODULE−TO−ACTIVE CBM ATTACHMENT BOLT CIRCLES HOLE LOCATIONS 3 − 71.
3.3.2.1−6 MODULE−TO−ACTIVE CBM ATTACHMENT BOLT CIRCLES AND INDEXING HOLE
LOCATIONS (VIEW B) 3 − 72
3.3.2.1−7 ATTACHMENT FASTENERS CONFIGURATION 3 − 73
3.3.2.1−8 PASSIVE CBM FLANGE DETAIL AND SEAL CONFIGURATION 3 − 74
3.3.2.1−9 ACTIVE CBM FLANGE DETAIL AND SEAL CONFIGURATION 3 − 75
3.3.2.1−10 MODULE FLANGE DETAIL AT THE CBM−TO−MODULE INTERFACE 3 − 76
3.3.2.1−11 MODULE FLANGE DETAIL AT THE CBM−TO−MODULE INTERFACE (VIEW H) 3 − 77. .
3.3.2.1.1−1 MODULE−TO−CBM INDEXING HOLE LOCATIONS 3 − 79
xix
TABLE OF CONTENTS
FIGURE PAGE
3.3.2.1.2−1 MODULE CRITICAL DIMENSIONS 3 − 80
3.3.2.1.3−1 PASSIVE CBM IVA SEAL ATTACHMENT 3 − 81
3.3.2.1.3−2 ACTIVE CBM IVA SEAL ATTACHMENT 3 − 83
3.3.2.1.4−1 NODE 1 CBM CLOCKING 3 − 85
3.3.2.1.4−2 NODE 2 CBM CLOCKING 3 − 86
3.3.2.1.4−3 NODE 3 CBM CLOCKING 3 − 86
3.3.2.1.4−4 CUPOLA PCBM CLOCKING 3 − 87
3.3.2.1.5−1 NODE 2 AND NODE 3 RADIAL PORT MATCH DRILLED HOLE LOCATION 3 − 88
3.3.4.3−1 MOTOR CONTROLLER MOUNTING AREAS 3 − 94
3.3.4.3−2 MOTOR CONTROLLER MOUNTING AREAS (VIEW A−A) 3 − 95
3.3.4.3.1−1 MOTOR CONTROLLER−TO−MODULE MOUNTING DETAILS 3 − 96
3.3.4.3.1−2 MOTOR CONTROLLER−TO−MODULE MOUNTING DETAILS
(RADIAL PORTS) (VIEW A) 3 − 97
3.3.4.3.1−3 MOTOR CONTROLLER−TO−MODULE MOUNTING DETAILS (SECTION A−A) 3 − 98. . .
3.3.5.1−1 CBM LEAK CHECK PORT LOCATION 3 − 100
3.3.5.1−2 CBM LEAK CHECK PORT DETAIL 3 − 101
3.3.5.1−3 PCBM LEAK CHECK PORT DETAIL 3 − 102
3.3.6−1 CBM FEEDTHRU LOCATIONS (ACTIVE CBM ONLY) 3 − 103
3.3.6−2 CBM FEEDTHRU LOCATIONS (JEM−PM ACTIVE CBM ONLY) 3 − 104
3.3.7.1−1 HANDLING AND LIFT POINT LOCATIONS FOR ACBM AND PCBM STRUCTURAL
RINGS 3 − 105
3.3.7.1−2 TYPICAL HANDLING/LIFT POINT HOLE 3 − 106
3.3.8−1 CLOSEOUT PANEL TO NODE 1 RADIAL BULKHEAD INTERFACE 3 − 108
3.3.8−2 CLOSEOUT PANEL TO NODE 1, LAB AND AIRLOCK AXIAL BULKHEAD
INTERFACE 3 − 109
3.3.8−3 CLOSEOUT PANEL TO APM, MPLM, NODE 2 AND NODE 3 PCBM AXIAL BULKHEAD
INTERFACE 3 − 110
3.3.8−4 CLOSEOUT PANEL TO PMA INTERFACE 3 − 111
3.3.8−5 CLOSEOUT PANEL TO JEM PM, JEM ELM PS AND HTV AXIAL BULKHEAD
INTERFACE 3 − 112
3.3.8−6 CLOSEOUT PANEL TO NODE 2 & 3 RADIAL BULKHEAD INTERFACE 3 − 113
3.3.8−7 CLOSEOUT PANEL TO NODE 2 AND NODE 3 ACBM AXIAL BULKHEAD
INTERFACE 3 − 114
3.3.9−1 RADIAL PORT M/D CENTER DISK BRACKET HOLE DETAILS
(NODE RADIAL PORTS ONLY) 3 − 116
xx
TABLE OF CONTENTS
FIGURE PAGE
3.3.9.1−1 AXIAL ACBM GROUND STRAP HOLE DETAILS 3 − 117
3.3.10−1 PASSIVE CBM EXTERNAL ATTACHMENT PROVISIONS 3 − 119
3.3.10−2 ALIGNMENT SOCKET DETAILS (SHEET 1 OF 2) 3 − 120
3.3.10−2 ALIGNMENT SOCKET DETAILS (SHEET 2 OF 2) 3 − 121
3.3.10−3 THERMAL STANDOFF DETAILS 3 − 122
3.3.10−3.1 FOLLOWER STAY OUT ZONE 3 − 123
3.3.10−3.2 CONTAMINATION COVER STAY OUT ZONE 3 − 124
3.3.10−4 ACTIVE CBM EXTERNAL ATTACHMENT PROVISIONS 3 − 125
3.3.10−5 ALIGNMENT PIN DETAILS 3 − 126
3.3.10−6 STRIKE PLATE DETAILS 3 − 127
3.3.10−6 .1 BUMPER STAY OUT ZONE 3 − 128
3.3.10−7 PASSIVE CBM SKIRT ATTACH POINTS (SHEET 1 OF 9) 3 − 129
3.3.10−7 PASSIVE CBM SKIRT ATTACH POINTS (SHEET 2 OF 9) 3 − 130
3.3.10−7 PASSIVE CBM SKIRT ATTACH POINTS (SHEET 3 OF 9) 3 − 131
3.3.10−7 PASSIVE CBM SKIRT ATTACH POINTS (SHEET 4 OF 9) 3 − 132
3.3.10−7 PASSIVE CBM SKIRT ATTACH POINTS (SHEET 5 OF 9) 3 − 133
3.3.10−7 PASSIVE CBM SKIRT ATTACH POINTS (SHEET 6 OF 9) 3 − 134
3.3.10−7 PASSIVE CBM SKIRT ATTACH POINTS (SHEET 7 OF 9) 3 − 135
3.3.10−7 PASSIVE CBM SKIRT ATTACH POINTS (SHEET 8 OF 9) 3 − 136
3.3.10−7 PASSIVE CBM SKIRT ATTACH POINTS (SHEET 9 OF 9) 3 − 137
3.3.10−8 PCBM SKIRT SUPPORT DETAILS (SHEET 1 OF 8) 3 − 138
3.3.10−8 PCBM SKIRT SUPPORT DETAILS (SHEET 2 OF 8) 3 − 139
3.3.10−8 PCBM SKIRT SUPPORT DETAILS (SHEET 3 OF 8) 3 − 140
3.3.10−8 PCBM SKIRT SUPPORT DETAILS (SHEET 4 OF 8) 3 − 141
3.3.10−8 PCBM SKIRT SUPPORT DETAILS (SHEET 5 OF 8) 3 − 142
3.3.10−8 PCBM SKIRT SUPPORT DETAILS (SHEET 6 OF 8) 3 − 143
3.3.10−8 PCBM SKIRT SUPPORT DETAILS (SHEET 7 OF 8) 3 − 144
3.3.10−8 PCBM SKIRT SUPPORT DETAILS (SHEET 8 OF 8) 3 − 145
3.3.10−9 PCBM PASSIVE THERMAL ATTACH LOCATIONS−INTERNAL 3 − 146
3.3.10−10 PCBM PASSIVE THERMAL AND GROUNDING AVAILABLE HOLE ATTACH
LOCATIONS−INTERNAL (SECTION A−A OF RING GUSSETS) (PAGE 1 OF 2) 3 − 147. .
3.3.10−10 PCBM PASSIVE THERMAL AND GROUNDING AVAILABLE HOLE ATTACH
LOCATIONS−INTERNAL (SECTION A−A OF RING GUSSETS) (PAGE 2 OF 2) 3 − 148. .
3.3.10−11 PCBM GUSSET DETAILS − INTERNAL 3 − 149
3.3.10−12 PCBM AVAILABLE ATTACHMENT AREA − INTERNAL FACE 3 − 150
xxi
TABLE OF CONTENTS
FIGURE PAGE
3.3.10−13 TYPICAL PCBM ENVELOPES FOR MLI INSTALLATION 3 − 151
3.3.10.1−1 CLOSE−OUT ATTACHMENT HOLE LOCATIONS FOR ACTIVE AND PASSIVE CBM
STRUCTURAL RINGS 3 − 152
3.3.10.1−2 TYPICAL CLOSE−OUT ATTACHMENT HOLE CONFIGURATION 3 − 153
3.3.11−1 DEVIATION FROM DRAWING 683−13418, SHEET FOR NODE 2 AND 3 3 − 154
3.3.11−2 (1/3) DEVIATION FROM DRAWING 683−13418, SHEET 2 JEM PM
RADIAL PORT 3 − 155
3.3.11−2 (2/3) DEVIATION FROM DRAWING 683−13418, SHEET 2 JEM PM
RADIAL PORT 3 − 156
3.3.11−2 (3/3) DEVIATION FROM DRAWING 683−13418, SHEET 2 JEM PM
RADIAL PORT 3 − 157
3.3.12−1 M/OD BRACKET LOCATIONS 3 − 158
3.3.12−2 M/OD BRACKET DETAIL 3 − 159
3.3.13−1 PCBM TO CUPOLA SECONDARY STRUCTURE INTERFACES 3 − 160
3.3.13−2 PCBM TO CUPOLA SECONDARY STRUCTURE INTERFACES, BRACKET GEOMETRY
AND FASTENER ORIENTATION 3 − 161
3.3.13−3 PCBM TO CUPOLA SECONDARY STRUCTURE INTERFACES, BRACKET GEOMETRY
AND FASTENER ORIENTATION 3 − 162
3.3.13−4 PCBM TO CUPOLA SECONDARY STRUCTURE INTERFACES, BRACKET GEOMETRY
AND FASTENER ORIENTATION 3 − 163
3.3.13−5 PCBM TO CUPOLA SECONDARY STRUCTURE INTERFACES, BRACKET GEOMETRY
AND FASTENER ORIENTATION 3 − 164
3.5.2.1−1 ACBM POWER DISTRIBUTION 3 − 167
1 − 1
1.0 INTRODUCTION
The Space Station Common Berthing Mechanism (CBM) will be used on the Agenzia Spaziale Italiana (ASI) pressurized element, European Space Agency (ESA) pressurized element, the Japanese Aerospace Exploration Agency of Japan (JAXA) pressurized elements, and the National Aeronautics and Space Administration (NASA) pressurized elements, all of which are hereinafter referred to simply as PEs.
There are two types of CBMs used on the Space Station. These are referred to as the Active CBM (ACBM) and the Passive CBM (PCBM). ‘CBM’ will be used to refer to either the ACBM or the PCBM interchangeably.
1.1 PURPOSE
This document defines the physical and functional interfaces between the CBM with its local controllers and the PEs. The CBM is used as a means of structural attachment and pressurized crew transfer between PEs. The physical and functional interfaces required for the PCBM are applicable to NASA, ASI, ESA, and JAXA. The physical and functional interfaces required for the ACBM are applicable to NASA and JAXA. Interface requirements between the Active or Passive CBM and the PEs are identified in SSP 41004, Part 1.
1.2 SCOPE
The scope of this document is limited to interfaces between the CBM and the PE with the exception of defining the associated volume for inter−module jumpers.
1.3 PRECEDENCE
In the event of conflict between SSP 41162, Segment Specification for the U.S. On−orbit Segment and the contents of this Interface Control Document (ICD), the requirements of SSP 41162 shall take precedence.
1.4 DELEGATION OF AUTHORITY
This document is prepared and maintained in accordance with SSP 30459, NASA Space Station Interface Control Plan.
2 −1
2.0 DOCUMENTS
The following documents of the exact issue shown form a part of this document to the extent specified herein.
2.1 APPLICABLE DOCUMENTS
DOCUMENT NO. TITLE
1F48000−1.−−.04.NADIR.modelNode 1 Exterior − Nadir
Rev Basic
July 29, 1998
Reference Table 3.1.4.4−1
1F98912−1.−−.03.model Node 1 Exterior − Nadir
Rev Basic
July 29, 1998
Reference Table 3.1.4.4−1
683−11610−1.−−.04.model Node 1 Structural Assembly − Nadir
Rev Basic
July 29, 1998
Reference Table 3.1.4.4−1
683−11617−15.−−.01.model Node 1 Support Structure − Nadir
Rev D
July 29, 1998
Reference Table 3.1.4.4−1
683−11617−3.−−.01.model Node 1 Support Structure − Nadir
Rev D
July 29, 1998
Reference Table 3.1.4.4−1
683−11690−1.−−.04.model Node 1 Secondary Structure − Nadir
Rev A
July 29, 1998
Reference Table 3.1.4.4−1
2 −2
DOCUMENT NO. TITLE
683−11690−1.−−.06.model Node 1 Secondary Structure − Nadir
Rev A
July 29, 1998
Reference Table 3.1.4.4−1
683−11691−3.−−.01.model Node 1 Debris Shielding − Nadir
Rev C
July 29, 1998
Reference Table 3.1.4.4−1
683−13400−4.−A.01.model Node 1 CBM − Nadir
Rev A
July 29, 1998
Reference Table 3.1.4.4−1
683−14572−1.−−.03.model Node 1 CBM Deployable Cover − Nadir
Rev A
July 29, 1998
Reference Table 3.1.4.4−1
683−14576−1.−−.03.model Node 1 CBM Center Cover − Nadir
Rev B
July 29, 1998
Reference Table 3.1.4.4−1
683−23543−1.−−.03.model Node 1 CBM Closeout Shielding − Nadir
Rev A
July 29, 1998
Reference Table 3.1.4.4−1
683−27927 Bracket Assembly−Meteroid Debris Cover
Rev B
Notice 2
10 Nov 97
Reference Paragraph 3.3.12
2 −3
DOCUMENT NO. TITLE
683−55110−6.−−.01.model Node 1 Feedthroughs − Nadir
Rev D
July 29, 1998
Reference Table 3.1.4.4−1
AMS 5525F Steel Sheet, Strip, and Plate, Corrosion and Heat Resistant 15
1989 Cr − 25.5 − Ni − 1.2 Mo − 2.1 Ti − 0.006B − 0.30 V 1800 Degrees F (980 Degrees C) Solution Heat Treated
Reference Figure 3.3.2.1−7
AMS 5737L Steel Bars, Wire, Forging, and Tubing, Corrosion and Heat
1989 Resistant 15 Cr − 25.5 Ni − 1.2 Mo − 21 Ti − 0.006B −
0.30 V Consumable Electrode Melted 1650 Degrees F
(899 Degrees C) Solution and Precipitation Heat Treated
Reference Figures 3.3.2.1−7, 3.3.4.3.1−2
ASTM E380 Standard Practice for Use of the International System
Rev A of Units (SI) (The Modernized Metric System)
1 Jan 93
Reference Paragraphs 3.1.6.1, 3.1.6.2
CLT−TN−AI−040 Reduced CBM and Hatch Interface Thermal Mathematical Model for APM Analysis
Reference Paragraph 3.3.3.2
CLS−TN−AI−0049 CBM and Hatch Static Mathematical Model Description
Reference Paragraph 3.2.2
D 683−13418 Insert Installation Berthing Mechanism
Rev G
Feb 99
Reference Paragraph 3.3.11
D 683−85132 CBM Structural Mathematical Model Description
Reference Paragraph 3.2.2
2 −4
DOCUMENT NO. TITLE
D 683−85133 CBM Thermal Mathematical Model Description
Reference Paragraph 3.3.3.2
FED−STD−H28 Screw Thread Standards for Federal Services, Change Notice 3
3 Dec 90
Reference Figure 3.3.4.3.1−2
MIL−L−8937 Lubricant, Solid Film, Heat Cured, Corrosion Inhibiting, NATO Code No. S−1738 (Superceded by MIL−L−46010)
Reference Figure 3.3.2.1−7
MIL−L−46010 Lubricant, Solid Film, Heat Cured, Corrosion Inhibiting
Rev B, Amend 2
9/5/90
Reference Figure 3.3.4.3.1−2, 3.3.5.1−2, 3.3.5.1−3
MIL−S−8879 Screw Threads, Controlled Radius Root with Increased Minor
Rev C, Amend 1 Diameter, General Specification
9/2/92
Reference Figure 3.3.2.1−7, 3.3.5.1−2, 3.3.7.1−2, 3.3.5.1−3, 3.3.10.1−2
MIL−STD−865 Selective (Brush Plating), Electrodeposition
Rev C
11/1/88
Reference Figure 3.3.4.3.1−1
MIL−STD−1246 Product Cleanliness levels and Contamination Control Program
Rev Latest
Reference Paragraph 3.2.1
MS 33537 Insert, Screw Thread, Helical Coil, Inch Series, Coarse and
Rev E Fine Thread, Standard Assembly Dimensions
6/11/91
Reference Figure 3.3.2.1−4, 3.3.2.1−6, 3.3.2.1.3−1, 3.3.2.1.3−2
2 −5
DOCUMENT NO. TITLE
MS 51835 Inserts and Studs, Locked In−Key Locked, Hole Dimensions
Rev A for Assembly
11/25/70
Reference Figure 3.3.4.3.1−2, 3.3.9.1−1
MSFC−STD−486 Threaded Fasteners, Torque Limits for, Standard
Rev B
Reference Figure 3.3.2.1−7
QQ−P−35C Passivation Treatments for Corrosion Resistant Steel
Rev C
10/28/88
Reference Figure 3.3.2.1−7, 3.3.4.3.1−2
SSP 30459 International Space Station Interface Control Plan
Rev F
3/23/94
Reference Preface, Paragraph 1.4
SSP 41004 Common Berthing Mechanism to Pressurized Elements
Rev D Interface Control Document (ICD), Part 1
27 Mar 97
Rev F (Node 1, PMA 1 and
PMA 2 only)
3/27/98
IRN 41004−1465,
1594, 1481, 1555
Reference Paragraph 1.1, Figure 3.1.4−8, Paragraph 3.1.5.1, 3.1.5.3, 3.3.5.2, 3.4.1, 3.4.2, 3.5.2.1.2
SSP 41140 Node Element 1 to U.S. Habitation Element ICD, Part 2
Reference Figure 3.3.6−1
SSP 41015 Common Hatch Pressurized Element ICD
Reference Paragraph 3.1.4
2 −6
SSP 41142 NASA Space Station Node Elements to Cupola Element, Part 2
Reference Figure 3.3.6−1
SSP 41143 NASA Space Station Node Element 2 to U.S. Laboratory Element ICD, Part 2
Reference Figure 3.3.6−1
SSP 41145 NASA Space Station Node Element 1 to Airlock Element ICD, Part 2
Reference Figure 3.3.6−1
SSP 41151 Space Station Manned Base to Japanese Experiment
Rev A Module IRD
10/17/95
Reference Paragraph 3.6
SSP 41175 Space Station Management and Control to International Space Station, General Software ICD
Reference Paragraph 3.6
SSP 41178−27 Software Interface Control Document Part 1 Internal
Basic Multiplexer/Demultiplexer to International Space Station Book
June 10, 1996 27, Common Berthing Mechanism Interface
Reference Paragraph 3.6
SSP 42000 United States On-Orbit to Japanese Experiment Module ICD
Rev K
6/13/96
Reference Paragraph 3.5.3, 3.5.4
SSP 42001 Space Station Manned Base to Columbus to Attached
Rev K Pressurized Module ICD
July 1997
Reference Figure 3.3.6−1, Paragraph 3.5.4
2 −7
DOCUMENT NO. TITLE
SSP 42007 U.S. On-Orbit Segment to Italian Mini-Pressurized Logistics
Rev D Module ICD, Part 2
Rev F (Node 1, PMA 1 and
PMA 2 only)
13 Feb 98
IRNs 42007−0311, 0253, 0600, 0719 and 1465
Reference Figure 3.3.6−1
SSP 42097 Pressurized Mating Adapter to U.S. Pressurized Elements ICD
Reference Figure 3.3.6−1
SSP 44030 Z1 to Node 1 ICD, Part 2
Reference Figure 3.3.6−1
SSP 50144−4 Prime Contractor Software Interface Control Document, Part 1, Rev A Primary Node Control Software to International Space Station
30 May 97 Book 4, Common Berthing Mechanism Interface. (Node 1)
Rev A (Node 1, PMA 1 and
PMA 2 only)
30 May 97
IRN 50144−4−0004
Reference Paragraph 3.6
SSQ 21635 Connectors and Accessories, Electrical, Circular, Miniature, Rev B IVA/EVA Compatible, Space Quality, General Specification
7/16/93
Rev H (Node 1, PMA 1 and
PMA 2 only)
1 Aug 97
DCN 001, 011, 012, 013 and
014, 015
Reference Table 3.3.4.1−1, 3.3.4.1−2, 3.3.4.2−1, 3.3.4.2−2
2 −8
2.2 REFERENCE DOCUMENTS
DOCUMENT NO. TITLE
SSP 41162 U. S. On−Orbit Segment Specification
Reference Paragraph 1.3
AMS 5844 Iron−Nickel Alloy bars, forgings and rings
Reference Figure 3.3.2.1−7
AMS 5732 Steel, Corrosion and Heat Resistant, bars, wire, forgings, tubing, and rings
Reference Figure 3.3.2.1−7
MIL−A−8625 Anodic Coatings for Aluminum and Aluminum Alloys
Reference Figures 3.3.2.1−8, −9, 3.3.10−2, 3.3.10−3, 3.3.10−3.1, 3.3.10−3.2, 3.3.10−5, 3.3.10−6, 3.3.10−10, 3.3.10−11, 3.3.10−12
MIL−C−5541 Chemical Conversion Coatings on Aluminum and Aluminum Alloys
Reference Figures 3.3.2.1−8, 3.3.2.1−9, 3.3.2.1−10, 3.3.2.1−11, 3.3.7.1−2, 3.3.10−10
3 − 1
3.0 INTERFACE
3.1 GENERAL
Two types of CBMs are used on the International Space Station: Active CBMs and Passive CBMs.
3.1.1 INTERFACE DESCRIPTION
The CBM−to−Pressurized Element (PE) interface consists of the bolted flange and CBM utilities. The on−orbit module−to−module utility jumper envelope is also included in this ICD.
3.1.2 INTERFACE RESPONSIBILITIES
Providers of the CBM and modules ensure conformation to the interface defined in this document.
3.1.3 COORDINATE SYSTEMS
The CBM coordinate system is shown in Figure 3.1.3−1, Common Berthing Mechanism Coordinate System.
3 − 2
FIGURE 3.1.3−1 COMMON BERTHING MECHANISM COORDINATE SYSTEM
COMMON BERTHING
MECHANISM
Module
BERTHING
MECHANISM
+XCBM
+ZCBM
A
A
+ZCBM
RCBM
VIEW A−A
LOOKING INBOARD AT MODULE
CL
+YCBM
NOTE 1) RCBM defines radial coordinate system.
NOTE 2) This is a local coordinate system for the CBM and relates only to the drawings referenced or contained in this document.
θCBM
Ref (0, 0, 0)
Ref (0, 0, 0)
3 − 3
3.1.4 ENVELOPE INTERFACES
The Passive CBM static envelope is shown in Figure 3.1.4−1, Static Envelope of Passive CBM (Side View), and Figure 3.1.4−2, Static Envelope of Passive CBM (End View). The Active CBM static envelope on an axial port without thermal/debris cover is shown in Figure 3.1.4−3, Static Envelope of Active CBM on Axial Port Without Thermal/Debris Cover (Side View), and Figure 3.1.4−4, Static Envelope of Active CBM on Axial Port Without Thermal/Debris Cover (End View). The Active CBM static envelope on an axial port with thermal/debris cover is shown in Figure 3.1.4−5, Static Envelope of Active CBM on Axial Port With Thermal/Debris Cover (Side View). Figure 3.1.4−5.1 and Figure 3.1.4−5.2 show the node 2 forward and the node 3 nadir end cone secondary structure interface with the thermal/debris skirt. The Active CBM static envelope on a resource node radial port without thermal/debris cover is shown in Figure 3.1.4−6, Static Envelope of Active CBM on Resource Node Radial Port Without Thermal/Debris Cover. The Active CBM static envelope on a resource node radial port with thermal/debris covers closed is shown in Figure 3.1.4−7, Static Envelope of Active CBM on Resource Node Radial Port With Thermal/Debris Covers Closed. The Active CBM static and dynamic envelope on a node radial port with thermal/debris covers opened and skirts are shown in Figures 3.1.4−7.1, 3.1.4−7.2, and 3.1.4−7.3, Static and Dynamic Envelopes of Active CBM on Resource Node with Thermal/Debris Covers Open and Skirts, Section A−A, and Section B−B.
The Active CBM static envelope on a JEM radial port without thermal/debris cover is shown in Figure 3.1.4−8, Static Envelope of Active CBM on Japanese Experiment Module Radial Port Without Thermal/Debris Cover. The Active CBM static envelope on a JEM radial port with thermal/debris cover is shown in Figure 3.1.4−9, Static Envelope of Active CBM on Japanese Experiment Module Radial Port With Thermal/Debris Cover, Module−to−Module Utility Jumper Envelope Active and Passive CBM−to−Module Interface, Figure 3.1.4−10, and Module−to−Module Utility Jumper Envelope, (Section A−A), and Figure 3.1.4−11, Module−to−Module Utility Jumper Envelope, (Section B−B), Figure 3.1.4−12. CBM hardware (alignment guides, ready−to−latches, capture latch assemblies, and motor controllers) can be removed and stored after berthing if the hardware is identified to interfere with jumper installation.
For CBMs using the Centerline Berthing Camera System (CBCS), see SSP 41015, Part 2, paragraph 3.1.4.5 for stay out envelope necessary for camera viewing purposes. For applicability of which CBMs this applies to, see SSP 41015 Part 1 paragraph 3.2.1.1.2.3.
3 − 4
Module
∅ 82.0 (2083)
PASSIVE CBM
ENVELOPE
+XCBM
16.15 (410.2)
NOTE: 1) Envelope includes 5 inches (127) of space for alignment guides.
2) See Figures 3.1.4−10, 3.1.4−11, and 3.1.4−12 for the allowable penetrations into this envelope for utility jumpers/hardware.
3) See Figure 3.3.2.1.2−1 for CBM envelope from XCBM = 0 to module feed thru plane.
4) Envelope includes PCBM Skirt for PEs (not applicable to PMAs).
XCBM = 0
∅ 86.30 (2192)
See Note 4
FIGURE 3.1.4−1 STATIC ENVELOPE OF PASSIVE CBM (SIDE VIEW)
3 − 5
∅ 86.30 (2192)
PASSIVE CBM
ENVELOPE
+Z CBM
+Y CBM
1: See Figures 3.1.4−10 and 3.1.4−11 for the allowable penetrations into this envelope for utility jumpers in the berthed condition.
2: Envelope includes PCBM skirt for Pressurized Elements.
NOTES
FIGURE 3.1.4−2 STATIC ENVELOPE OF PASSIVE COMMON BERTHING MECHANISM
(END VIEW)
3 − 6
FIGURE 3.1.4−3 STATIC ENVELOPE OF ACTIVE CBM ON AXIAL PORT
WITHOUT THERMAL/DEBRIS COVER (SIDE VIEW)
Module
ACTIVE CBM
ENVELOPE
WITHOUT THERMAL
DEBRIS COVER
+XCBM
∅ 82.0 (2083)
10.15 (257.8)
NOTE: 1) Envelope includes 5 inches (127) of space for alignment guides.
2) See Figures 3.1.4−10 and 3.1.4−11 for the allowable penetrations into this envelope for utility jumpers/hardware.
3) See Figure 3.3.2.1.2−1 for CBM envelope from XCBM = 0 to module feed thru plane.
XCBM = 0
3 − 7
82.0 (2083)
ACTIVE CBM
ENVELOPE
WITHOUT THERMAL
DEBRIS COVER
+Z CBM
+Y CBM
FIGURE 3.1.4−4 STATIC ENVELOPE OF ACTIVE COMMON BERTHING MECHANISM ON
AXIAL PORT WITHOUT THERMAL/DEBRIS COVER (END VIEW)
NOTE: See Figures 3.1.4−10 and 3.1.4−11 for the allowable penetrations into this envelope for utility jumpers in the berthed condition.
3 − 8
Module
ACTIVE CBM ENVELOPE
WITH THERMAL DEBRIS SKIRT
+XCBM
∅ 86.7 (2202)
∅ 94.26 (2394.2)
17.62
(447.5)
8.7 (221)
1) Deleted
2) See Figures 3.1.4−10, 3.1.4−11, and 3.1.4−12 for the allowable penetrations into this envelope for utility jumpers/hardware.
3) See Figure 3.3.2.1.2−1 for the CBM envelope from XCBM = 0 to module feed thru plane.
FEEDTHRU
INTERFACE PLANE
(PRESSURE BULKHEAD)
XCBM = 0
58°
NOTE:
∅ 101.60 (2580.6)
0.23
5.2
(132.1) + .00
−.03 5.8
+ 0.0
− 0.76
FIGURE 3.1.4−5 STATIC ENVELOPE OF ACTIVE CBM ON AXIAL PORT
WITH METEOROID/DEBRIS SKIRT (SIDE VIEW)
3 − 9
FIGURE 3.1.4−5.1 ANGULAR POSITION OF THERMAL DEBRIS / SKIRT ATTACH POINTS
3 − 10
Section B−B
0.27 +0.30 (7.62)
−0.00 (0.00) (Note 4)
(Note 1)
R
.3
8+ 0.
00.25 − 0.261 (Note 3)
Note 1: Local thickness in attachment area.
Note 2: Anchor Nut in this side. (MS 210 60L4) Note 3: Minimum distance between hole center and end cone secondary structure edge shall be twice the hole diameter.
Note 4: Distance between hole center and Xcbm= 0 reference plane.
FIGURE 3.1.4−5.2 AXIAL AND RADIAL POSITION OF THERMAL / DEBRIS SKIRT ATTACH
POINTS
3 − 11
FIGURE 3.1.4−6 STATIC ENVELOPE OF ACTIVE CBM ON RESOURCE NODE
RADIAL PORT WITHOUT THERMAL/DEBRIS COVER
1) Envelope includes 5 inches (127) of space for alignment guides.
2) See Figures 3.1.4−10 and 3.1.4−11 for the allowable penetrations into this envelope for utility jumpers/hardware.
3) See Figure 3.3.2.1.2−1 for CBM envelope from XCBM = 0 to module feed thru plane.
NOTE:
ÇÇ
ÇÇ
ÇÇ
ÇÇ
ÇÇ
ÇÇ
ÇÇ
ÇÇ
ÇÇÇÇÇÇÇÇÇÇÇÇÇÇ
ÇÇÇÇÇÇÇÇÇÇÇÇÇÇ
ÇÇÇÇÇÇÇÇÇÇÇÇÇÇ
ÇÇÇÇÇÇÇÇÇÇÇÇÇÇ
ÇÇ
ÇÇ
ÇÇ
Ç Ç
Ç Ç Ç
ÇÇ
ÇÇ
ÇÇ
10.15 (257.8)
83.5 (2121)
82.0 (2083)
Active CBM Envelope without Thermal/Debris Cover
64.0 (1626)
5.95 (151.1)
Module Static Envelope (Ref)
13.05 (331.5)
XCBM = 0
3.35 (85.1)
3.25 (82.6) REF
Feedthrough Interface Plane
REF
88.0 (2235) at Bumper Location∅
11.15 (283.2)
3 − 12
FIGURE 3.1.4−7 STATIC ENVELOPE OF ACTIVE CBM ON RESOURCE NODE
RADIAL PORT WITH THERMAL/DEBRIS COVERS CLOSED
ÉÉÉÉÉÉÉÉÉÉÉÉÉÉÉÉ
ÉÉÉÉÉÉÉÉÉÉÉÉÉÉÉÉ
ÉÉÉÉÉÉÉÉÉÉÉÉÉÉÉÉ
ÉÉÉÉÉÉÉÉÉÉÉÉÉÉÉÉ
13.05 (331.5)
83.25 (2114.5) OD
Active CBM Envelope with Thermal/Debris Cover Closed
83.5 (2121)
10.55 (268.0)
1) See Figure 3.3.2.1.2−1 for the CBM envelope from XCBM = 0 to module feedthrough plane.
2) Highest point (10.55) at the alignment guides only. Petal configuration detail not provided.
3) Deleted
XCBM = 0
3.35 (85.1)
3.25 (82.6) REF
Feedthrough Interface Plane
(See Note 1)
REF
NOTE:
Note 2 11.15
(283.2)
88.0 (2235) at Bumper Location∅
ÉÉ
ÉÉ
3 − 13
FIGURE 3.1.4−7.1 STATIC AND DYNAMIC ENVELOPE OF ACTIVE CBM ON RESOURCE
NODE RADIAL PORT WITH THERMAL/DEBRIS COVERS OPEN AND SKIRTS
(See Figure 3.1.4−7.2)
Module mated with Resource Node
(See Figure 3.1.4−7.3)
(305)
(1298)
(1542)
3 − 14
FIGURE 3.1.4−7.2 STATIC AND DYNAMIC ENVELOPE OF ACTIVE CBM ON
RESOURCE NODE RADIAL PORT WITH THERMAL/DEBRIS COVERS OPEN AND
SKIRTS (SECTION B−B)
Applicable during berthing operations only.
Module Center Line
Skirt terminates at module to CBM interface
Module mated with Resource Node Radial Port
Resource Node Radial Port
Berthing Stayout Zone
Module
(min) (259.1)
(1100)
(1090)
(986)
(30)
(2223) REF
(1242)
Skirt Max at center
REF
Rotated 90 CCW
− Stayout Zone
10.30 (max) (261.6)
3 − 15
FIGURE 3.1.4−7.3 STATIC AND DYNAMIC ENVELOPE OF ACTIVE CBM ON
RESOURCE NODE RADIAL PORT WITH THERMAL/DEBRIS COVERS OPEN AND
SKIRTS (SECTION B−B)
(1100)
(1090)
(986)
(2223) REF
(1298)
Module
Skirt terminates at module to CBM interface
Module mated with Resource Node Radial Port
Resource Node Radial Port
Berthing Stayout Zone
(347)
(1438)
(1542)
Module M/D shield
− Stayout Zone
REF
(min)
(259.1)
Center Line
10.30 (max) (261.6)
Applicable during berthing operations only.
3 − 16
11.15 (283.2)
ÉÉÉÉÉÉÉÉÉÉÉÉÉ
ÉÉÉÉÉÉÉÉÉÉÉÉÉ
ÉÉÉÉÉÉÉÉÉÉÉÉÉ
ÉÉÉÉÉÉÉÉÉÉÉÉÉ
ÉÉ
ÉÉ
ÉÉ
ÉÉ
ÉÉ ÉÉ
ÉÉ
ÉÉ
ÉÉ
ÉÉ10.15 (257.8)
82.5 (2095.5)
82.0 (2083)
Active CBM Envelope without Thermal/Debris Cover
64.0 (1626)
5.95 (151.1)
JEM Static Envelope (Ref)
17.9 (455.9)
XCBM = 0
3.35 (85.1)
3.25 (82.6) REF
Feedthrough Interface Plane
REF
88.0 (2235) at Bumper Location∅
FIGURE 3.1.4−8 STATIC ENVELOPE OF ACTIVE CBM ON JAPANESE
EXPERIMENT MODULE RADIAL PORT WITHOUT THERMAL/DEBRIS COVER
(SIDE VIEW)
1) Envelope includes 5 inches (127) of space for alignment guides.
2) See Figures 3.1.4−10, 3.1.4−11, and 3.1.4−12 for the allowable penetrations into this envelope for utility jumpers/hardware.
3) See Figure 3.3.2.1.2−1 for CBM envelope from XCBM = 0 to module feed thru plane.
4) For top view of JEM ACBM radial port, see Figure 3A.2.1.1.1−1 of SSP 41004, Part 1.
Note:
3 − 17
1) See Figure 3.3.2.1.2−1 for the CBM envelope from XCBM = 0 to module feed thru plane.
2) This figure does not contain the new thermal/debris cover. The new cover is still being designed and will have to be incorporated through the Preliminary Interface Revision Notice (PIRN) process.
3) Deleted
4) This figure does not contain the new bumper.
NOTE:
ÉÉÉÉÉÉÉÉÉÉÉÉÉÉÉ
ÉÉÉÉÉÉÉÉÉÉÉÉÉÉÉ
ÉÉÉÉÉÉÉÉÉÉÉÉÉÉÉ
ÉÉÉÉÉÉÉÉÉÉÉÉÉÉÉ
ÉÉ
ÉÉÉÉ ÉÉ
ÉÉ
ÉÉ
10.15 (257.8)
84.5 (2146)
82.0 (2083)
Active CBM Envelope With Thermal/Debris Cover
86.0 (2184)
15.40 (391.2)
FIGURE 3.1.4−9 STATIC ENVELOPE OF ACTIVE CBM ON JAPANESE EXPERIMENT
MODULE RADIAL PORT WITH THERMAL/DEBRIS COVER
84.5 (2146)
82.0 (2083)
86.0 (2184)
27°
XCBM = 0
3.35 (85.1)
3.25 (82.6) REF
Feed Thru Interface Plane
(See Note 1)
3 − 18
FIGURE 3.1.4−10 MODULE−TO−MODULE UTILITY JUMPER ENVELOPE ACTIVE AND
PASSIVE CBM−TO−MODULE INTERFACE
25o
MODULE BULKHEAD
MOTOR
ENVELOPE
= UTILITY JUMPER ENVELOPE
+YCBM
−ZCBM
AA
B
B
1) Feedthrough pattern shown on this figure is for reference only.
2) One quarter shown: Bilaterally symmetrical about YCBM and ZCBM axes.
3) Motor Controllers are removed from vestibules prior to jumper installation.
4) Closeout Panel attaching hardware and MLI envelope included in the utility jumper envelope.
5) Utility Jumper Envelope can be expanded to 40� post Berth.
MOTOR
ENVELOPE
Note:
11.25o
25�
See note 5)
3 − 19
FIGURE 3.1.4−11 MODULE−TO−MODULE UTILITY JUMPER ENVELOPE (SECTION A−A)
ÍÍÍ
ÍÍÍ
UTILITY JUMPER
ENVELOPE
= ÈÈÈ
ÈÈÈ
UTILITY JUMPER ENVELOPE,
MODULE/CBM STRUCTURE
MAY ENCROACH THIS AREA
ÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍ
ÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍ
ÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍ
ÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍ
ÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍ
ÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍ
ÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍ
ÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍ
ÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍ
ÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍ
ÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍ
ÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍ
ÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍ
ÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍ
ÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍ
ÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍ
ÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍ
ÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍ
ÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍ
ÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍ
ÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍ
ÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍ
ÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍ
ÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍ
ÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍ
Passive
CBM
Active
CBM
Module Bulkhead
Module Bulkhead
See Figure 3.1.4.2−1 IVA Seal
ÈÈÈÈÈ
ÈÈÈÈÈ
ÈÈÈÈÈ
ÈÈÈÈÈ
ÈÈÈÈ
ÈÈÈÈ
ÈÈÈÈ
ÈÈÈÈ
ÈÈÈÈÈ
ÈÈÈÈÈ
ÈÈÈÈÈ
ÈÈÈÈÈ
ÈÈÈÈ
ÈÈÈÈ
ÈÈÈÈ
ÈÈÈÈ
See Figure 3.3.2.1.2−1
See Figure 3.3.2.1.2−1
IMV Flange
IMV Flange
ÈÈÈÈ
ÈÈÈÈ
ÈÈÈÈ
ÈÈÈÈ
ÈÈÈÈ
ÈÈÈÈ
ÈÈÈÈ
ÈÈÈÈ
ÈÈÈÈ
ÈÈÈÈ
ÈÈÈÈ
ÈÈÈÈ
ÈÈÈÈ
ÈÈÈÈ
ÈÈÈÈ
R 35.45 (900.4) Ref
R 37.45 (951.2)
25.0 (635) Ref
R 37.45 (951.2)
Note: Closeout panel attaching hardware and MLI envelope included in utility jumper envelope.
3 − 20
FIGURE 3.1.4−12 MODULE−TO−MODULE UTILITY JUMPER ENVELOPE
(SECTION B−B)
ÍÍÍÍ
ÍÍÍÍ
UTILITY JUMPER
ENVELOPE
See Note 2
= ÈÈÈÈ
ÈÈÈÈ
UTILITY JUMPER ENVELOPE,
MODULE/CBM STRUCTURE
MAY ENCROACH THIS AREA
Note 1: Envelope does not include motor connector and assorted cabling.
Note 2: Closeout panel attaching hardware and MLI envelope included in utility jumper envelope.
ÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍ
ÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍ
ÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍ
ÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍ
ÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍ
ÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍ
ÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍ
ÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍ
ÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍ
ÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍ
ÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍ
ÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍ
ÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍ
ÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍ
ÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍ
ÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍ
ÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍ
ÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍ
ÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍ
ÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍ
ÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍ
ÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍ
ÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍ
ÍÍÍÍÍÍÍÍÍÍÍÍÍÍÍ
ÈÈÈÈÈÈÈÈÈÈÈÈÈ
ÈÈÈÈÈÈÈÈÈÈÈÈÈ
ÈÈÈÈÈÈÈÈÈÈÈÈÈ
ÈÈÈÈÈÈÈÈÈÈÈÈÈ
Passive CBM
Active CBM
Module Bulkhead
Module Bulkhead
ÈÈÈÈÈÈÈÈÈÈÈÈÈ
ÈÈÈÈÈÈÈÈÈÈÈÈÈ
ÈÈÈÈÈÈÈÈÈÈÈÈÈ
ÈÈÈÈÈÈÈÈÈÈÈÈÈ
See Figure 3.1.4.2−1
IVA SEAL
See Figure 3.3.2.1.2−1
See Figure 3.3.2.1.2−1
Motor Envelope
ÈÈÈÈ
ÈÈÈÈ
ÈÈÈÈ
ÈÈÈÈ
ÈÈÈÈ
ÈÈÈÈ
ÈÈÈÈ
ÈÈÈÈ
ÈÈÈÈ
ÈÈÈÈ
ÈÈÈÈ
ÈÈÈÈ
ÈÈÈÈ
ÈÈÈÈ
R 37.45 (951.2)
R 35.45 (900.4) Ref
Hatch Opening
Ref
R 35.13 (892.3)See
Note 1
3 − 21
1) Envelope includes 5 inches (127) of space for alignment guides.
2) See Figures 3.1.4-10 and 3.1.4-11 for the allowable penetrations into this envelope for utility jumpers/hardware.
3) See Figure 3.3.2.1.2−1 for CBM envelope from XCBM = 0 to module feed thru plane.
NOTE:
ÇÇ
ÇÇ
ÇÇ
ÇÇ
ÇÇ
ÇÇ
ÇÇÇÇÇÇÇÇÇÇÇÇÇ
ÇÇÇÇÇÇÇÇÇÇÇÇÇ
ÇÇÇÇÇÇÇÇÇÇÇÇÇ
ÇÇ
ÇÇ
ÇÇ
ÇÇ
ÇÇ
ÇÇÇÇ
ÇÇ
84” (Node Static Envelope)
82.0 (2083)
Active CBM Envelope without Thermal/Debris Cover
64.0 (1626)
5.95 (151.1)
9.637 (244.78)
XCBM = 0
3.35 (85.1)
3.25 (82.6) REF
Feedthrough Interface Plane
REF
88.0 (2235) at Bumper Location∅
11.15 (283.2)
REF.
Node Static Envelope (Ref.) without M/D
(2133.6)
10.15 (257.8)
FIGURE 3.1.4−13 STATIC ENVELOPE OF ACTIVE CBM ASI NODES
MODULE RADIAL PORTS WITHOUT THERMAL/DEBRIS COVER
3 − 22
FIGURE 3.1.4−14 STATIC ENVELOPE OF ACTIVE CBM ON RESOURCE NODE
RADIAL PORT WITH THERMAL/DEBRIS COVERS CLOSED
ÉÉÉÉÉÉÉÉÉÉÉÉÉÉÉ
ÉÉÉÉÉÉÉÉÉÉÉÉÉÉÉ
ÉÉÉÉÉÉÉÉÉÉÉÉÉÉÉ
ÉÉÉÉÉÉÉÉÉÉÉÉÉÉÉ
83.25 (2114.5) OD
Active CBM Envelope with Thermal/Debris Cover Closed
83.5 (2121)
10.55 (268.0)
1) See Figure 3.3.2.1.2−1 for the CBM envelope from XCBM = 0 to module feedthrough plane.
2) Highest point (10.55) at the alignment guides only. Petal configuration detail not provided.
3) Deleted
XCBM = 0
3.35 (85.1)
3.25 (82.6) REF
Feedthrough Interface Plane
(See Note 1)
REF
NOTE:
Note 2 11.15
(283.2)
88.0 (2235) at Bumper Location∅
É É É
9.637 (244.78)
Node Static Envelope (Ref.)
without M/D
3 − 23
3.1.4.1 CBM HARDWARE ENVELOPES
Clearance envelopes for the alignment guides, capture latches, actuation system controller assembly (referred to as motor controller), powered bolt motors, and Ready-to-Latch are shown in Figure 3.1.4.1−1, Active CBM Clearance Envelope for Passive CBM Alignment Guides;
Figure 3.1.4.1−2, Active CBM Clearance Envelope for Passive CBM Alignment Guides (View A−A); Figure 3.1.4.1−3, Active CBM Capture Latch Clearance Envelope; Figure 3.1.4.1−4, Active CBM Capture Latch Clearance Envelope (View A−A); Figure 3.1.4.1−5, Active CBM Capture Latch Clearance Envelope (View B−B); Figure 3.1.4.1−6, Motor controller Clearance Envelope; Figure 3.1.4.1−7, Typical Motor Controller Axial Hatch Beam Clearance Envelope (View A−A); Figure 3.1.4.1−8, Powered Bolt Centerline Locations; Figure 3.1.4.1−9, Powered Bolt Motor Clearance Envelope; Figure 3.1.4.1−10, Powered Bolt Motor Clearance Envelope (View A−A); Figure 3.1.4.1−11, Active CBM Ready-to-Latch Clearance Envelope; Figure 3.1.4.1−12, Ready-to-Latch Clearance Envelope (View A−A); and Figure 3.1.4.1−13, Ready-to-Latch Clearance Envelope (View B−B); Figure 3.1.4.1−14, Passive CBM Clearance Envelope for Active CBM Alignment Guides; Figure 3.1.4.1−15, Passive CBM Clearance Envelope for Active CBM Alignment Guides (View A−A); Figure 3.1.4.1−16, Active CBM Capture Latch and Fitting Clearance Envelope for Passive CBM; Figure 3.1.4.1−17, Passive CBM Capture Latch and Fitting Clearance Envelope (View A−A); Figure 3.1.4.1−18, Passive CBM Capture Latch and Fitting Clearance Envelope (View B−B); Figure 3.1.4.1−19, Motor Controller and M/D Center Cover Passive CBM Hardware Clearance Envelope; Figure 3.1.4.1−20, Motor Controller and M/D Center Cover PCBM Hardware Clearance Envelope (View D−D); Figure 3.1.4.1−21, Passive CBM Clearance Envelope for Powered Bolt Nut; and Figure 3.1.4.1−22, PCBM Clearance Envelope for Powered Bolt Nut (View E−E).
3 − 24
25°
2 PL
11.25°
2 PL
15.5°
2PL
FIGURE 3.1.4.1−1 ACTIVE CBM CLEARANCE ENVELOPE FOR PASSIVE CBM
ALIGNMENT GUIDES
70.90 REF∅
= Stay Out Area θCBM =
(1800.9)
See Figure 3.1.4.1−2
R 30.5 (775)
45°, 135°, 225°, 315°
3 − 25
FIGURE 3.1.4.1−2 ACTIVE CBM CLEARANCE ENVELOPE FOR PASSIVE CBM
ALIGNMENT GUIDES (VIEW A−A)
Active CBM
= Stay Out Area
5.15 REF
(130.8)
= Stay Out Area
Ç Ç
ÇÇÇÇÇÇÇÇÇÇ
ÇÇÇÇÇÇÇÇÇÇ
ÇÇÇÇ
ÇÇÇÇ
ÇÇÇÇ
Ç Ç Ç Ç
ÇÇÇÇ
ÇÇÇÇ
ÇÇÇÇ
ÇÇÇÇ
Ç Ç
ÇÇ
ÇÇ
Ç Ç
R 30.5 (775)
REF
3 − 26
FIGURE 3.1.4.1−3 ACTIVE CBM CAPTURE LATCH CLEARANCE ENVELOPE
+ΖCBM
+YCBM
θCBM = 0°
44°
134°224°
314°
∅ = 77.296 REF
(1963.3)
∅ = 70.90 REF
(1800.9)
See Figure 3.1.4.1−4
A B
B
A
See Figure 3.1.4.1−5
= Stay Out Area
3 − 27
FIGURE 3.1.4.1−4 ACTIVE CBM CAPTURE LATCH CLEARANCE ENVELOPE
(VIEW A−A)
Active CBM
R 3.92 (99.6)
1.87 (47.5)
= Stay Out Area
RCBM = 35.05 (890.3)
XCBM
=5.15
(130.8)
REF
XCBM
0.00
REF
3 − 28
FIGURE 3.1.4.1−5 ACTIVE CBM CAPTURE LATCH CLEARANCE ENVELOPE (VIEW B−B)
θCBM = 44°, 134°, 224°, 314°
CAPTURE
LATCH
MOTOR CL
= Stay Out Area
XCBM
=5.15
(130.8)
REF
XCBM
0.00
REF
1.10 (27.9)
2.75 (69.9)
4.3 (109.2)
2.2 (55.9)
1.5 (38.1)
5.4 (129.6)
3.82 (97.03)
4.85 (123.2)
1.87 (47.5)
2.4 (61)
∅ .60 (15.2)
1.10 (27.9)
2.7 (68.6)
2.10 (53.3)
∅ 3.0 (76.2)
3 − 29
FIGURE 3.1.4.1−6 MOTOR CONTROLLER CLEARANCE ENVELOPE
FOR TYPICAL MOTOR
CONTROLLER ENVELOPE
10.0 (254)
10.0 (254)
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