42124_P1_RC.pdf
PDF 109 KB Posted
- Attached to
- Human Space Flight Technical Integration Contract (HSFTIC) Federal contract opportunity
- Solicitation number
- 80JSC019R0023
About this file
This solicitation is for a Human Space Flight Technical Integration Contract (HSFTIC). NASA/JSC will issue a Request for Proposal for technical integration services to support human space flight programs. The procurement is a total small business set-aside with a NAICS code of 541715 and size standard of 1,250 employees. The anticipated RFP release date is November 1, 2019 with a proposal due date of December 11, 2019. The solicitation and any amendments will be available on NASA's procurement website and Federal Business Opportunities site. Prospective offerors must notify the agency of their intent to submit a proposal. All technical questions must be submitted in writing. The Center Ombudsman information is provided.
42124 P1 RC
View the file
Other files for this federal contract opportunity
Show all 50
Human Space Flight Technical Integration Contract (HSFTIC) has more files on GovTribe.
On GovTribe
Work with this file on GovTribe
- Download the original file
- Contacts named in this file
- Similar government files
- Ask GovTribe AI about this file
Text version
SSP 42124, Part 1, Revision C
SPACE STATION PROGRAM
INTEGRATED TRUSS SEGMENT S0
TO NODE 2 INTERFACE CONTROL
DOCUMENT PART 1
Revision C November 17, 2005
Type 4 Approved by NASA
International Space Station Program
National Aeronautics and Space Administration International Space Station Program Johnson Space Center Houston, Texas Contract No. NAS15−10000
SSP 42124, Part 1, Revision C November 17, 2005 ii
REVISION AND HISTORY PAGE
REV. DESCRIPTION PUB.
DATE
− Initial Release in accordance with DR VE−06 12−08−94
Change 1, IRN 0145 (REFRENCE SSCD 000145 EFF. 10−31−95) 06−14−96
Change 2, IRN 0002 (REFRENCE SSCD 000102 EFF. 11−04−94) 10−30−96
Change 3, IRN 0008 per CCR 000111 06−19−97
Change 4, IRN 0001 per CCR 000263 06−19−97
A Revision A released per SSCN 001252 (Release to File) 02−04−99
This revision incorporates the following PIRNs/IRNs associated with the appropriate SSCNs:
PIRN 42124−0006 IRN 0145 SSCN 000145
PIRN 42124−0001 IRN 0001 SSCN 000263
PIRN 42124−0002 IRN 0001 SSCN 000263
PIRN 42124−0004 IRN 0001 SSCN 000263
PIRN 42124−0007D IRN 0002 SSCN 000102
PIRN 42124−0009 IRN 0002 SSCN 000102
PIRN 42124−0008A IRN 0008 SSCN 000111
PIRN 42124−0011A N/A SSCN 001252
PIRN 42124−0012A N/A SSCN 000311
PIRN 42124−0013A N/A SSCN 000249
PIRN 42124−0014 N/A SSCN 000561
B Revision B released per SSCD 001208, EFF. 04−02−98 02−04−99
Incorporate the following approved PIRNs:
42124−AS−0004B, 42124−NA−0002A, 42124−NA−0003B, 42124−NA−0004B,
42124−NA−0006
C Revision C released per SSCD 009745, EFF. 03−30−06 07−14−06
This revision incorporates the following approved PIRNs/IRNs associated with the appropriate SSCNs:
PIRN 42124−AS−0008 IRN N/A SSCN 009745
PIRN 42124−NA−0001 IRN N/A SSCN 009745
PIRN 42124−NA−0007 IRN N/A SSCN 000737
PIRN 42124−NA−0008AIRN N/A SSCN 002559
PIRN 42124−NA−0009 IRN N/A SSCN 002559
PIRN 42124−NA−0010CIRN N/A SSCN 009745
PIRN N/A IRN 0004 SSCN 001262
PIRN N/A IRN 0003 SSCN 001662
PIRN N/A IRN 0006 SSCN 001711
PIRN N/A IRN 0009 SSCN 001920
PIRN N/A IRN 0007 SSCN 001929
PIRN N/A IRN 0014 SSCN 001938
PIRN N/A IRN 0010 SSCN 002107
PIRN N/A IRN 0017 SSCN 002189
iii
REVISION AND HISTORY PAGE
REV. DESCRIPTION PUB.
DATE
PIRN N/A IRN 0013 SSCN 002199
PIRN N/A IRN 0011 SSCN 002345
PIRN N/A IRN 0012 SSCN 002485
PIRN N/A IRN 0022 SSCN 002588
PIRN N/A IRN 0016 SSCN 003213
PIRN N/A IRN 0023 SSCN 003282
PIRN N/A IRN 0018 SSCN 003690
PIRN N/A IRN 0019 SSCN 003746
PIRN N/A IRN 0021 SSCN 003827
PIRN N/A IRN 0020 SSCN 004676
ERU: /s/ J. Rivas 07−14−06 iv v
PREFACE
The contents of this doucment are intended to be consistent with the tasks and products to be prepared by Program participants. The Itegrated Truss Segment (ITS) S0 to Node 2 Interface Control Document (ICD) shall be implemented on all new International Space Station (ISS) contractual and internal activities and shall be included in any existing contracts through contract changes. This document is under the control of the Space Station Control Board and any changes or revisions will be approved by the Program Manager (or statement to indicate the delegated authority, i.e. Space Staion Analysis and Integration team (SSAIT), Vehicle Analysis and Integration Team (VAIT)).
vi vii
INTERNATIONAL SPACE STATION PROGRAM
INTERNATIONAL SPACE STATION PROGRAM
INTEGRATED TRUSS SEGMENT S0 TO NODE 2
November 17, 2005
CONCURRENCE
Warren England AG−92−J3ES
PREPARED BY: PRINT NAME ORGN
/s/ Warren England 07/06/06
SIGNATURE DATE
CHECKED BY (BOEING): Quentin Henry AG−92−J3ES
PRINT NAME ORGN
/s/ Quentin L. Henry 07/06/06
SIGNATURE DATE
APPROVED BY (NASA): Chau Hong NASA/OM
PRINT NAME ORGN
/s/ Chau Hong 07/6/06
SIGNATURE DATE
DQA: Merry McClain AG−92−J3ES
PRINT NAME ORGN
/s/ Merry McClain 7/7/06
SIGNATURE DATE
viii
Node 2 Project Concurrence
ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁ
Alenia ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ
/s/ Walter Cugno ÁÁÁ
ÁÁÁ
ÁÁÁÁÁ
ÁÁÁÁÁ
11/21/97
ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ
Walter Cugno ÁÁÁ
ÁÁÁ
ÁÁÁÁÁ
ÁÁÁÁÁ
Date
ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁ
ÁÁÁ
ÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁ
ÁÁÁ
ÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁ
ÁÁÁ
ÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁASI
ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ/s/ Andrea Lorenzoni
ÁÁÁ
ÁÁÁ
ÁÁÁÁÁ
ÁÁÁÁÁ1/7/98ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁAndrea Lorenzoni
ÁÁÁ
ÁÁÁ
ÁÁÁÁÁ
ÁÁÁÁÁDateÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁ
ÁÁÁ
ÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁ
ÁÁÁ
ÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁ
ÁÁÁ
ÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁ
ÁÁÁ
ÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁ
NASA−MSFC ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ
/s/ Robert Crumbley ÁÁÁ
ÁÁÁ
ÁÁÁÁÁ
ÁÁÁÁÁ
11/21/97
ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ
Robert Crumbley ÁÁÁ
ÁÁÁ
ÁÁÁÁÁ
ÁÁÁÁÁ
Date ix
INTERNATIONAL SPACE STATION PROGRAM
INTERNATIONAL SPACE STATION PROGRAM
INTEGRATED TRUSS SEGMENT S0 TO NODE 2
LIST OF CHANGES
November 17, 2005
All changes to paragraphs, tables, and figures in this document are shown below:
ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁ
APPROVAL
AUTHORITY NO.
ÁÁÁÁÁ
ÁÁÁÁÁ
ÁÁÁÁÁ
ENTRY
DATE
ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁ
CHANGE ÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁ
PARAGRAPH(S), TABLE(S)
AND FIGURE(S)
ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁ
SSCN 009745
SSCN 009745
SSCN 000737
ÁÁÁÁÁ
ÁÁÁÁÁ
ÁÁÁÁÁ
ÁÁÁÁÁ
ÁÁÁÁÁ
ÁÁÁÁÁ
ÁÁÁÁÁ
ÁÁÁÁÁ
ÁÁÁÁÁ
ÁÁÁÁÁ
ÁÁÁÁÁ
17 Nov 05 17 Nov 05 17 Nov 05
ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁ
42124−AS−0008
42124−NA−0001
42124−NA−0007
ÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁ
Para 3.2.1.4.4, 3.2.2.4.4 Front Matter Para 3.2.1.3.1, 3.2.2.3.1 Table 3.2.1.3.1.1−1 Figure 3.2.1.3−1
ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁ
SSCN 002559 ÁÁÁÁÁ
ÁÁÁÁÁ
17 Nov 05ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁ
42124−NA−0008A ÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁ
Table 3.2.1.3.1.1−1
ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁ
SSCN 002559 ÁÁÁÁÁ
ÁÁÁÁÁ
17 Nov 05ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁ
42124−NA−0009 ÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁ
Table 3.2.1.3.1.2−1
ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁ
SSCN 009745 ÁÁÁÁÁ
ÁÁÁÁÁ
ÁÁÁÁÁ
17 Nov 05ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁ
42124−NA−0010C ÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁ
Table 3.2.1.2.2.1.1−1 Table 3.2.2.2.2.1.1−1
ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁ
ÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁ
ÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁ
x
TABLE OF CONTENTS
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 - 3
3.0 INTERFACES 3 − 1
3.1 GENERAL 3 − 1
3.1.1 INTERFACE DESCRIPTION 3 − 1
3.1.1.1 ITS S0 DESCRIPTION 3 − 1
3.1.1.2 NODE DESCRIPTION 3 − 1
3.1.1.3 INTERFACE PLANE DESCRIPTION 3 − 1
3.1.1.4 COORDINATE SYSTEMS 3 − 1
3.1.1.5 ENGINEERING UNITS 3 − 2
3.1.1.6 TOLERANCE 3 − 2
3.1.1.7 ITS S0 INTERFACE FUNCTIONS 3 − 2
3.1.1.8 NODE 2 INTERFACE FUNCTIONS 3 − 2
3.1.2 INTERFACE RESPONSIBILITIES 3 − 2
3.1.2.1 RESPONSIBILITY FOR ITS S0 3 − 2
3.1.2.2 RESPONSIBILITY FOR NODE 2 3 − 3
3.1.2.3 RESPONSIBILITY FOR UTILITY CONNECTORS 3 − 3
3.2 INTERFACE REQUIREMENTS 3 − 3
3.2.1 ITS S0 INTERFACE REQUIREMENTS 3 − 3
3.2.1.1 INTERCONNECTING UTILITY HARDWARE 3 − 3
3.2.1.1.1 ACCESSIBILITY 3 − 3
3.2.1.1.2 ELECTRICAL CONNECTORS 3 − 3
3.2.1.1.3 UTILITY CABLE SPECIFICATIONS 3 − 3
3.2.1.1.3.1 VIDEO CABLE SPECIFICATIONS 3 − 3
3.2.1.1.3.2 HEAT EXCHANGER INSTRUMENTATION CABLES 3 − 3
3.2.1.1.3.3 ELECTRICAL POWER CABLE SPECIFICATIONS 3 − 4
3.2.1.1.4 GROUNDING 3 − 4
3.2.1.1.5 SHIELD TERMINATION OF ELECTRICAL CABLES 3 − 4
3.2.1.1.6 FLUID CONNECTORS 3 − 4
3.2.1.1.7 REDUNDANT UTILITY INTERFACES 3 − 4
3.2.1.2 ELECTRONIC INTERFACES 3 − 4
3.2.1.2.1 VIDEO SIGNALS 3 − 4
xi
TABLE OF CONTENTS − CONTINUED
PARAGRAPH PAGE
3.2.1.2.1.1 OPTICAL PULSE FREQUENCY MODULATION (PFM) NATIONAL TELEVISION
STANDARDS COMMITTEE (NTSC) VIDEO SIGNAL CHARACTERISTICS 3 − 4
3.2.1.2.1.1.1 OPTICAL PFM NTSC VIDEO SIGNAL RECEIVE POWER LEVELS 3 − 4
3.2.1.2.1.2 DELETED 3 − 5
3.2.1.2.1.3 DELETED 3 − 5
3.2.1.2.1.4 DELETED 3 − 5
3.2.1.2.2 SYNC AND CONTROL SIGNALS 3 − 5
3.2.1.2.2.1 OPTICAL PFM NTSC SYNC AND CONTROL SIGNAL CHARACTERISTICS 3 − 5
3.2.1.2.2.1.1 OPTICAL PFM NTSC SYNC AND CONTROL SIGNAL TRANSMIT
POWER LEVELS 3 − 5
3.2.1.2.2.2 DELETED 3 − 6
3.2.1.2.2.3 DELETED 3 − 6
3.2.1.2.2.4 DELETED 3 − 6
3.2.1.2.3 INSTRUMENTATION AND CONTROLS 3 − 6
3.2.1.2.3.1 HEAT EXCHANGER ORBITAL REPLACEABLE UNITS 3 − 6
3.2.1.2.3.1.1 HX ORU CONTROL SIGNALS 3 − 6
3.2.1.2.3.1.1.1 NODE 2 HX ORU’S 3 − 6
3.2.1.2.3.1.1.2 JEM HX ORU’S 3 − 6
3.2.1.2.3.1.1.3 APM HX ORU’S 3 − 7
3.2.1.2.3.1.2 HX ORU INSTRUMENTATION/SENSOR SIGNALS 3 − 7
3.2.1.2.3.1.2.1 HX ORU VALVE POSITION SENSORS 3 − 7
3.2.1.2.3.1.2.1.1 NODE 2 HX ORU’S 3 − 7
3.2.1.2.3.1.2.1.2 JEM HX ORU’S 3 − 7
3.2.1.2.3.1.2.1.3 APM HX ORU’S 3 − 8
3.2.1.2.3.1.2.2 HX ORU TEMPERATURE SENSORS 3 − 8
3.2.1.2.3.1.2.2.1 NODE 2 HX ORU’S 3 − 8
3.2.1.2.3.1.2.2.2 JEM HX ORU’S 3 − 8
3.2.1.2.3.1.2.2.3 APM HX ORU’S 3 − 9
3.2.1.3 ELECTRICAL INTERFACES 3 − 9
3.2.1.3.1 SUPPLY POWER 3 − 10
3.2.1.3.1.1 POWER QUALITY 3 − 10
3.2.1.3.1.2 FAULT PROTECTION 3 − 10
3.2.1.3.1.3 DELETED 3 − 11
3.2.1.3.1.4 DELETED 3 − 11
3.2.1.4 FLUID INTERFACES 3 − 11
3.2.1.4.1 SUPPLY COOLANT 3 − 11
3.2.1.4.2 RECEIVE COOLANT 3 − 12
3.2.1.4.3 DELTA PRESSURE 3 − 12
3.2.1.4.4 VOLUME ALLOCATION 3 − 12
xii
TABLE OF CONTENTS − CONTINUED
PARAGRAPH PAGE
3.2.1.5 STRUCTURAL INTERFACE 3 − 12
3.2.1.5.1 CREW INDUCED LOADS 3 − 12
3.2.1.5.1.1 DELETED 3 − 13
3.2.1.5.2 BONDING 3 − 13
3.2.1.5.3 DELETED 3 − 13
3.2.1.5.4 MATERIALS AND FINISHES 3 − 13
3.2.1.5.5 DELETED 3 − 14
3.2.1.6 ENVIRONMENTS 3 − 14
3.2.1.6.1 ELECTROMAGNETIC COMPATIBILITY 3 − 14
3.2.1.6.2 ELECTROSTATIC DISCHARGE 3 − 14
3.2.1.6.3 CORONA 3 − 14
3.2.2 NODE 2 INTERFACE REQUIREMENTS 3 − 14
3.2.2.1 INTERCONNECTING UTILITY HARDWARE 3 − 14
3.2.2.1.1 ACCESSIBILITY 3 − 14
3.2.2.1.2 ELECTRICAL CONNECTORS 3 − 14
3.2.2.1.3 UTILITY CABLE SPECIFICATIONS 3 − 14
3.2.2.1.3.1 VIDEO CABLE SPECIFICATIONS 3 − 14
3.2.2.1.3.2 HEAT EXCHANGER INSTRUMENTATION CABLES 3 − 15
3.2.2.1.3.3 ELECTRICAL POWER CABLE SPECIFICATIONS 3 − 15
3.2.2.1.4 GROUNDING 3 − 15
3.2.2.1.5 SHIELD TERMINATION OF ELECTRICAL CABLES 3 − 15
3.2.2.1.6 FLUID CONNECTORS 3 − 15
3.2.2.1.7 REDUNDANT UTILITY INTERFACES 3 − 15
3.2.2.2 ELECTRONIC INTERFACES 3 − 15
3.2.2.2.1 VIDEO SIGNALS 3 − 15
3.2.2.2.1.1 OPTICAL PFM NTSC VIDEO SIGNAL CHARACTERISTICS 3 − 15
3.2.2.2.1.1.1 OPTICAL PFM NTSC VIDEO SIGNAL TRANSMIT POWER LEVELS 3 − 15
3.2.2.2.1.2 DELETED 3 − 16
3.2.2.2.1.3 DELETED 3 − 16
3.2.2.2.1.4 DELETED 3 − 16
3.2.2.2.2 SYNC AND CONTROL SIGNALS 3 − 16
3.2.2.2.2.1 OPTICAL PFM NTSC SYNC AND CONTROL SIGNAL CHARACTERISTICS 3 − 16
3.2.2.2.2.1.1 OPTICAL PFM NTSC SYNC AND CONTROL SIGNAL RECEIVE POWER LEVELS 3 − 16.
3.2.2.2.2.2 DELETED 3 − 17
3.2.2.2.2.3 DELETED 3 − 17
3.2.2.2.2.4 DELETED 3 − 17
3.2.2.2.3 INSTRUMENTATION AND CONTROLS 3 − 17
3.2.2.2.3.1 HEAT EXCHANGER ORBITAL REPLACEABLE UNIT 3 − 17
xiii
TABLE OF CONTENTS − CONTINUED
PARAGRAPH PAGE
3.2.2.2.3.1.1 HX ORU CONTROL SIGNALS 3 − 17
3.2.2.2.3.1.1.1 NODE 2 HX ORU’S 3 − 17
3.2.2.2.3.1.1.2 JEM HX ORU’S 3 − 17
3.2.2.2.3.1.1.3 APM HX ORU’S 3 − 17
3.2.2.2.3.1.2 HX ORU INSTRUMENTATION/SENSOR SIGNALS 3 − 18
3.2.2.2.3.1.2.1 HX ORU VALVE POSITION SENSORS 3 − 18
3.2.2.2.3.1.2.1.1 NODE 2 HX ORU’S 3 − 18
3.2.2.2.3.1.2.1.2 JEM HX ORU’S 3 − 18
3.2.2.2.3.1.2.1.3 APM HX ORU’S 3 − 18
3.2.2.2.3.1.2.2 HX ORU TEMPERATURE SENSORS 3 − 19
3.2.2.2.3.1.2.2.1 NODE 2 HX ORU’S 3 − 19
3.2.2.2.3.1.2.2.2 JEM HX ORU’S 3 − 19
3.2.2.2.3.1.2.2.3 APM HX ORU’S 3 − 19
3.2.2.3 ELECTRICAL INTERFACES 3 − 19
3.2.2.3.1 RECEIVE POWER 3 − 19
3.2.2.3.1.1 POWER QUALITY 3 − 19
3.2.2.3.1.2 DELETED 3 − 19
3.2.2.3.1.3 DELETED 3 − 19
3.2.2.3.1.4 DELETED 3 − 19
3.2.2.4 FLUID INTERFACES 3 − 19
3.2.2.4.1 RECEIVE COOLANT 3 − 19
3.2.2.4.2 RETURN COOLANT 3 − 20
3.2.2.4.3 DELTA PRESSURE 3 − 20
3.2.2.4.4 VOLUME ALLOCATION 3 − 20
3.2.2.5 STRUCTURAL INTERFACE 3 − 20
3.2.2.5.1 CREW INDUCED LOADS 3 − 20
3.2.2.5.1.1 DELETED 3 − 20
3.2.2.5.2 BONDING 3 − 20
3.2.2.5.3 DELETED 3 − 20
3.2.2.5.4 MATERIALS AND FINISHES 3 − 20
3.2.2.5.5 DELETED 3 − 21
3.2.2.6 ENVIRONMENTS 3 − 21
3.2.2.6.1 ELECTROMAGNETIC COMPATIBILITY 3 − 21
3.2.2.6.2 ELECTROSTATIC DISCHARGE 3 − 21
3.2.2.6.3 CORONA 3 − 21
xiv
TABLE OF CONTENTS − CONTINUED
TABLES
TABLE PAGE
3.1.1.6−1 LINEAR TOLERANCES 3 − 2
3.2.1.1.6−1 FLUID CONNECTOR SPECIFICATION 3 − 4
3.2.1.2.1.1.1−1 OPTICAL PFM NTSC VIDEO SIGNAL RECEIVE POWER 3 − 5
3.2.1.2.2.1.1−1 OPTICAL PFM NTSC SYNC AND CONTROL SIGNAL TRANSMIT POWER 3 − 5
3.2.1.3.1.1−1 ELECTRICAL INTERFACE PARAMETERS 3 − 10
3.2.1.3.1.2−1 ELECTRICAL INTERFACE FAULT CURRENT PARAMETERS 3 − 11
3.2.1.4.1−1 SUPPLY AMMONIA CHARACTERISTICS 3 − 12
3.2.1.4.2−1 RETURN AMMONIA CHARACTERISTICS 3 − 12
3.2.1.5.1−1 CREW INDUCED CONNECTOR LOADS 3 − 13
3.2.2.2.1.1.1−1 OPTICAL PFM NTSC VIDEO SIGNAL TRANSMIT POWER 3 − 16
3.2.2.2.2.1.1−1 OPTICAL PFM NTSC SYNC AND CONTROL SIGNAL RECEIVE POWER 3 − 16
FIGURES
FIGURE PAGE
3.1.1−1 ITS S0 TO NODE 2 FUNCTIONAL INTERFACE DIAGRAM 3 − 1
3.2.1.3−1 ITS S0 TO NODE 2 ELECTRICAL INTERFACES 3 − 9
APPENDICIES
APPRENDIX PAGE
A ABBREVIATIONS AND ACRONYMS A - 1
B ISSUES B - 1
1 - 1
1.0 INTRODUCTION
1.1 PURPOSE
The purpose of this document is to provide definition of physical and functional interface requirements between ITS S0 and Node 2.
1.2 SCOPE
The scope of this document is limited to the interfaces between ITS S0 and Node 2.
1.3 PRECEDENCE
In the event of conflict between SSP 41162, United States On−Orbit Segment (USOS) Specification, and the contents of this ICD, the requirements of the USOS specification shall take precedence. In the event of conflict between the contents of this ICD and any related Prime Item Development Specification (PIDS), the contents of this ICD take precedence.
1.4 DELEGATION OF AUTHORITY
This document is prepared and maintained in accordance with SSP 30459, International Space Station Interface Control Plan.
2 - 1
2.0 DOCUMENTS
2.1 APPLICABLE DOCUMENTS
The following documents form a part of this document to the extent specified herein. In the event of conflict between documents referenced here and the contents of section 3, the order of precedence shall be as stated in paragraph 1.2 of this document.
DOCUMENT NO. TITLE
SSP 30219 Space Station Reference Coordinate Systems Rev E 4 Sept 98 Reference 3.1.1.4
SSP 30233 Space Station Requirements for Materials and Processes Rev E 27 Jan 1995 Reference 3.2.1.5.4, 3.2.2.5.4
SSP 30240 Space Station Grounding Requirements Revision C, DCNs 002, 003, 005, SSCN 3282
22 Dec 98 Reference 3.2.1.1.4, 3.2.2.1.4
SSP 30242 Space Station Cable/Wire Design and Control Requirements for Rev C, DCN 004, Electromagnetic Compatibility
SSCN 3282
3 Jun 1994 References 3.2.1.1.3, 3.2.1.1.5, 3.2.2.1.3, 3.2.2.1.5
SSP 30243 Space Station Requirements for Electromagnetic Compatibility Rev E,DCNs 003, 004, 005, 006, 007, 4 June 98 References 3.2.1.6.1, 3.2.1.6.2, 3.2.1.6.3, 3.2.2.6.1, 3.2.2.6.2, 3.2.2.6.3
SSP 30245 Space Station Electrical Bonding Requirements Rev D, DCNs 004, 005, 006, 007, 008, 009, 010, 011, 013, SSCN 2345
4 June 98 References 3.2.1.5.2, 3.2.2.5.2
2 - 2
SSP 30426 Space Station External Contamination Control Requirements Rev D, 001 21 Jan 1994 References 3.2.1.5.4, 3.2.2.5.4
SSP 30459 Space Station Interface Control Plan.
Rev. F March 23, 1994 Reference 1.4
SSP 30558 Fracture Control Requirements for Space Station Rev B 30 Jun 94 References 3.2.1.5.3, 3.2.2.5.3
SSP 50002 International Space Station Video Standard Rev A, DCN 002 20 Oct 2000 References 3.2.1.2.1.1, 3.2.1.2.2.1, 3.2.2.2.1.1, 3.2.2.2.2.1
SSP 50005 International Space Station Flight Crew Integration Rev B, DCN 008 Standard (NASA−STD−3000/T) 10 Aug 1994 References 3.2.1.1.1, 3.2.2.1.1
SSQ 21635 Connectors and Accessories, Electrical, Circular, IVA/EVA/Robot Rev K Compatible, Space Station Quality, General 29 Oct 02 References 3.2.1.1.2, 3.2.2.1.2
SSQ 21652 Wire, Electric, Silicone Insulated, Nickel Coated Copper, Rev F Space Quality, General Specification 15 Jan 00 References 3.2.1.1.3.3, 3.2.2.1.3.3
SSQ 21654 Cable, Single Fiber, Multi−Mode, Space Quality, General Rev C Specification 03 May 99 References 3.2.1.1.3.1. 3.2.2.1.3.1
SSQ 21656 General Specification for Wire and Cable, Electrical, Rev D Fluoropolymer Insulated Nickel Coated Copper or Copper Alloy 15 Jan 00 References 3.2.1.1.3.2, 3.2.1.1.3.3, 3.2.2.1.3.2, 3.2.2.1.3.3
1F45540 Coupling, Quick Disconnect, Male, Type 1, Ammonia, External Reference 3.2.1.1.6, 3.2.2.1.6
1F45541 Coupling, Quick Disconnect, Female, Type 1, Ammonia, External Reference 3.2.1.1.6, 3.2.2.1.6
2 - 3
2.2 REFERENCE DOCUMENTS
The following documents are referenced in this ICD for context and user convenience.
DOCUMENT NO. TITLE
SSP 41162 United States On−Orbit Segment Specification Reference 1.3
SSP 30263:002 Remote Power Control Module (RPCM) Standard Interface Control Document
Reference Table 3.2.1.3.1.1−1
SSP 30258:001 Space Station Program External Active Thermal Control Heat Exchanger to Pressurized Elements Interface Control Document
Reference Paragraph 3.2.2.4.3
3 − 1
3.0 INTERFACES
3.1 GENERAL
3.1.1 INTERFACE DESCRIPTION
The ITS S0 to Node 2 functional interface is shown in Figure 3.1.1−1.
PRIMARY AND SECONDARY POWER
AMMONIA
VIDEO
VIDEO SYNCHRONIZATION
AND CONTROL
HEAT EXCHANGER MONITOR
AND CONTROL
FIGURE 3.1.1−1 ITS S0 TO NODE 2 FUNCTIONAL INTERFACE DIAGRAM
3.1.1.1 ITS S0 DESCRIPTION
ITS S0 is the center truss segment of the Space Station, providing attachment of the truss to the Module pattern by means of the Module to Truss Structure (MTS).
3.1.1.2 NODE DESCRIPTION
Node 2 is an element serving primarily as a berthing location for other pressurized elements.
Node 2 contains equipment for primary−to−secondary power conversion and plumbing and cable runs to other elements. Node 2 is located forward of the United States Laboratory (US Lab) between the Columbus Attached Pressurized Module (APM) and the Japanese Experi-ment Module (JEM).
3.1.1.3 INTERFACE PLANE DESCRIPTION
The interface between ITS S0 and Node 2 is at the utility connector halves from ITS S0 to the utility connector halves from Node 2.
3.1.1.4 COORDINATE SYSTEMS
The ITS S0 coordinate system and the Node 2 coordinate system are as shown in SSP 30219, Space Station Reference Coordinate System.
3 − 2
3.1.1.5 ENGINEERING UNITS
Unless otherwise noted herein, all dimensions are in the English system of inch pound (IP) units.
3.1.1.6 TOLERANCE
Linear tolerance on English dimensions are as indicated in Table 3.1.1.6−1, unless otherwise stated. Angular tolerances are +/− 0.5 deg on all angles, unless otherwise stated.
TABLE 3.1.1.6−1 LINEAR TOLERANCES
ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁEnglish Dimension
ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁImplied Tolerances (Inches)ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ
X.XX
ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ
+/− 0.030
ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ
X.XXX ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ
+/− 0.010
3.1.1.7 ITS S0 INTERFACE FUNCTIONS
ITS S0 provides the following functions at the interface to Node 2:
a. Utility Connections
b. Supply Primary Power
c. Supply Power and Data Grapple Fixutre (PDGF) Secondary Power
d. Video Synchronization and Control
e. Supply Heat Exchanger Instrumentation Signals
f. Receive Heat Exchanger Instrumentation Signals
g. Supply and Receive Ammonia Coolant
3.1.1.8 NODE 2 INTERFACE FUNCTIONS
Node 2 provides the following functions at the interface to the ITS S0:
a. Utility Connections
b. Receive Primary Power
c. Receive PDGF Secondary Power
d. Video
e. Supply Heat Exchanger Instrumentation Signals
f. Receive Heat Exchanger Instrumentation Signals
g. Receive and Return Ammonia Coolant
3.1.2 INTERFACE RESPONSIBILITIES
3.1.2.1 RESPONSIBILITY FOR ITS S0
McDonnell Douglas Aerospace (MDA), Inboard Truss Segment Integrated Product Team (IPT), provides ITS S0.
3 − 3
3.1.2.2 RESPONSIBILITY FOR NODE 2
Agenzia Spaziale Italiana (ASI) provides Node 2.
3.1.2.3 RESPONSIBILITY FOR UTILITY CONNECTORS
National Aeronautical Space Administration (NASA) is responsible for the utility connectors at the ITS S0/Node 2 interface.
3.2 INTERFACE REQUIREMENTS
3.2.1 ITS S0 INTERFACE REQUIREMENTS
3.2.1.1 INTERCONNECTING UTILITY HARDWARE
ITS S0 shall incorporate provisions for the mechanical connection of ammonia coolant, power, instrumentation, and video utilities to Node 2 during on−orbit assembly. Utility interfaces shall contain physical provisions to preclude incorrect installation of utility lines and shall not be lockwired or staked.
3.2.1.1.1 ACCESSIBILITY
Fluid and avionic connectors shall comply with SSP 50005, International Space Station Flight Crew Standard, paragraphs 14.3, 14.4, and 14.6.4.3 requirements for accessibility by Extra−Ve-hicular Activity (EVA) suited crew members.
3.2.1.1.2 ELECTRICAL CONNECTORS
The characteristics for electrical connectors shall be in accordance with SSQ 21635, General Specifications for Connectors and Accessories, Electrical, Circular, Miniature, IVA/EVA/Robot Compatible, Space Quality.
3.2.1.1.3 UTILITY CABLE SPECIFICATIONS
Cable and wire design shall be in accordance with SSP 30242, Space Station Cable/Wire De-sign and Control Requirements for Electromagnetic Compatibility.
3.2.1.1.3.1 VIDEO CABLE SPECIFICATIONS
The video interconnect cables shall comply with the requirements of SSQ 21654, General Specification for Cable, Single Fiber, Multi−Mode, Space Quality.
3.2.1.1.3.2 HEAT EXCHANGER INSTRUMENTATION CABLES
Heat exchanger instrumentation utility cables shall conform to SSQ 21656, General Specifica-tion for Wire and Cable, Electrical, Fluoropolymer Insulated Nickel Coated Copper or Copper Alloy.
3 − 4
3.2.1.1.3.3 ELECTRICAL POWER CABLE SPECIFICATIONS
Power cables shall conform to SSQ 21652, General Specification For Wire, Electric, Silicone Insulated, Nickel Coated Copper, Space Quality or to SSQ 21656, General Specification for Wire and Cable, Electric, Fluoropolymer−insulated, Nickel Coated Copper or Copper Alloy.
3.2.1.1.4 GROUNDING
Grounding between ITS S0 and Node 2 shall be in accordance with SSP 30240, Space Station Grounding Requirements.
3.2.1.1.5 SHIELD TERMINATION OF ELECTRICAL CABLES
All shields shall be terminated to structure or chassis at ITS S0. Shield termination shall be in accordance with SSP 30242.
3.2.1.1.6 FLUID CONNECTORS
Fluid connectors at the interface shall comply with specifications shown in Table 3.2.1.1.6−1, Fluid Connector Specification.
TABLE 3.2.1.1.6−1 FLUID CONNECTOR SPECIFICATIONÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁ
APPLICATION
ÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁ
SPECIFICATION
ÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁ
REMARKS
ÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁ
Quick Disconnect, EVA Compatible, Ammonia, External
ÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁ
1F45540/1F45541 ÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁ
3.2.1.1.7 REDUNDANT UTILITY INTERFACES
ITS S0 shall provide redundant utility interfaces for power distribution and heat exchanger in-strumentation. Alternate or redundant functional paths shall be separated or protected at the interface such that a credible event, which causes the loss of one functional path, will not result in the loss of the alternate or redundant functional path(s).
3.2.1.2 ELECTRONIC INTERFACES
3.2.1.2.1 VIDEO SIGNALS
The ITS S0 shall receive the National Television Standards committee (NTSC) video signals described in the following subparagraphs from Node 2.
3.2.1.2.1.1 OPTICAL PULSE FREQUENCY MODULATION (PFM) NATIONAL TELEVISION
STANDARDS COMMITTEE (NTSC) VIDEO SIGNAL CHARACTERISTICS
The optical PFM NTSC video signal characteristics shall be in accordance with SSP 50002, paragraphs 3.2.1.5.4. and 3.2.1.5.5.
3.2.1.2.1.1.1 OPTICAL PFM NTSC VIDEO SIGNAL RECEIVE POWER LEVELS
The ITS S0 shall meet all transmission quality requirements with minimum average optical PFM NTSC video signal input power, at ambient temperature, provided by Table 3.2.1.2.1.1.1−1 at each signal interface.
3 − 5
TABLE 3.2.1.2.1.1.1−1 OPTICAL PFM NTSC VIDEO SIGNAL RECEIVE POWER
ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ
Source to Destination ÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁ
ITS S0 Input
ÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁ
Video Source
ÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁ
Destination
ÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁ
Optical Power (dBm)
ÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁ
Ext Port 11 ÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁ
VSW 1 ÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁ
−20.4
ÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁPDGF Node 2 −1
ÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁVSW 1
ÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁ−20.1ÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁ
PDGF Node 2 −2
ÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁ
VSW 2
ÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁ
−20.1
ÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁ
PDGF Node 2 −3 ÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁ
VSW 3 ÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁ
−20.1
3.2.1.2.1.2 DELETED
3.2.1.2.1.3 DELETED
3.2.1.2.1.4 DELETED
3.2.1.2.2 SYNC AND CONTROL SIGNALS
ITS S0 shall transmit the signals described in the following subparagraphs to Node 2.
3.2.1.2.2.1 OPTICAL PFM NTSC SYNC AND CONTROL SIGNAL CHARACTERISTICS
The optical PFM NTSC sync and control signal characteristics shall be in accordance with SSP 50002, paragraphs 3.2.1.5.4. and 3.2.1.5.5.
3.2.1.2.2.1.1 OPTICAL PFM NTSC SYNC AND CONTROL SIGNAL TRANSMIT POWER
LEVELS
The minimum average optical PFM NTSC sync and control signal transmit power, measured at ambient temperature, transmitted by ITS S0 shall meet Table 3.2.1.2.2.1.1−1 at each signal interface.
TABLE 3.2.1.2.2.1.1−1 OPTICAL PFM NTSC SYNC AND CONTROL SIGNAL TRANSMIT
POWER
ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ
Source to Destination ÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁ
ITS S0 Output
ÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁVideo Source
ÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁDestination
ÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁOptical Power (dBm)ÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁ
VSW 1
ÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁ
Ext Port 11
ÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁ
−18.7
ÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁ
VSW 2 ÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁ
PDGF NODE 2 −1 ÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁ
−19.0
ÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁVSW 3
ÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁPDGF NODE 2 −2
ÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁ−19.0
3 − 6
3.2.1.2.2.2 DELETED
3.2.1.2.2.3 DELETED
3.2.1.2.2.4 DELETED
3.2.1.2.3 INSTRUMENTATION AND CONTROLS
3.2.1.2.3.1 HEAT EXCHANGER ORBITAL REPLACEABLE UNITS
The ITS S0 to Node 2 interface shall provide for the instrumentation and control of six (6) Heat Exchanger (Hx) Orbital Replacement Units (ORUs) as defined in the following paragraphs.
3.2.1.2.3.1.1 HX ORU CONTROL SIGNALS
All Hx ORU Control Signals are conditioned secondary power. The maximum voltage level associated with these signals shall be 126 Volts Direct Current (DC). Short circuit current protection shall be provided by ITS S0 for each control signal. The short circuit current for each control signal shall not exceed 3.0 Amps DC.
Loop A Hx ORU’s and Loop B Hx ORU’s are redundant utility interfaces. Routing and sepa-ration of associated wiring shall meet the requirements of paragraph 3.2.1.1.7.
3.2.1.2.3.1.1.1 NODE 2 Hx ORUs
ITS S0 shall provide four signals to Node 2 to command valves that control Node 2 Loop A Hx ORU. These include (1) Command the Bypass Valve to NORMAL Flow, (2) Command the Bypass Valve to BYPASS Flow, (3) Command the Isolation/Relief Valve to OPEN, and (4) Command the Isolation/Relief Valve to CLOSE.
ITS S0 shall provide four signals to Node 2 to command valves that control Node 2 Loop B Hx ORU. These include (1) Command the Bypass Valve to NORMAL Flow, (2) Command the Bypass Valve to BYPASS Flow, (3) Command the Isolation/Relief Valve to OPEN, and (4) Command the Isolation/Relief Valve to CLOSE.
3.2.1.2.3.1.1.2 JEM Hx ORUs
ITS S0 shall provide four signals to Node 2 to command valves that control JEM Loop A Hx ORU. These include (1) Command the Bypass Valve to NORMAL Flow, (2) Command the Bypass Valve to BYPASS Flow, (3) Command the Isolation/Relief Valve to OPEN, and (4) Command the Isolation/Relief Valve to CLOSE.
ITS S0 shall provide four signals to Node 2 to command valves that control JEM Loop B Hx ORU. These include (1) Command the Bypass Valve to NORMAL Flow, (2) Command the Bypass Valve to BYPASS Flow, (3) Command the Isolation/Relief Valve to OPEN, and (4) Command the Isolation/Relief Valve to CLOSE.
3 − 7
3.2.1.2.3.1.1.3 APM Hx ORUs
ITS S0 shall provide four signals to Node 2 to command valves that control APM Loop A Hx ORU. These include (1) Command the Bypass Valve to NORMAL Flow, (2) Command the Bypass Valve to BYPASS Flow, (3) Command the Isolation/Relief Valve to OPEN, and (4) Command the Isolation/Relief Valve to CLOSE.
ITS S0 shall provide four signals to Node 2 to command valves that control APM Loop B Hx ORU. These include (1) Command the Bypass Valve to NORMAL Flow, (2) Command the Bypass Valve to BYPASS Flow, (3) Command the Isolation/Relief Valve to OPEN, and (4) Command the Isolation/Relief Valve to CLOSE.
3.2.1.2.3.1.2 Hx ORU INSTRUMENTATION/SENSOR SIGNALS
3.2.1.2.3.1.2.1 Hx ORU VALVE POSITION SENSORS
ITS S0 shall provide to Node 2 the excitation voltages required for monitoring each Hx ORU limit switch as described below. The maximum excitation voltage provided by ITS S0 when switch contacts are OPEN shall be 29 Volts DC. ITS S0 shall limit the current to closed switch contacts to 0.2 milliamps (mA) maximum.
Loop A Hx ORU and Loop B Hx ORU are redundant utility interfaces. Routing and separation of associated wiring shall meet the requirements of paragraph 3.2.1.1.7.
3.2.1.2.3.1.2.1.1 NODE 2 Hx ORUs
ITS S0 shall receive four signals from Node 2 for monitoring Node 2 Loop A Hx ORU valve status. Closed contacts on limit switches located in the Node 2 Loop A Hx ORU indicate (1) the Bypass Valve is in full NORMAL Position, (2) the Bypass Valve is in full BYPASS posi-tion, (3) the Isolation/Relief Valve is in fully OPEN position, and (4) the Isolation/Relief Valve is in fully CLOSED position.
ITS S0 shall receive four signals from Node 2 for monitoring Node 2 Loop B Hx ORU valve status. Closed contacts on limit switches located in the Node 2 Loop B Hx ORU indicate (1) the Bypass Valve is in full NORMAL Position, (2) the Bypass Valve is in full BYPASS posi-tion, (3) the Isolation/Relief Valve is in fully OPEN position, and (4) the Isolation/Relief Valve is in fully CLOSED position.
3.2.1.2.3.1.2.1.2 JEM Hx ORUs
ITS S0 shall receive four signals from Node 2 for monitoring JEM Loop A Hx ORU valve sta-tus. Closed contacts on limit switches located in the JEM Loop A Hx ORU indicate (1) the By-pass Valve is in full NORMAL Position, (2) the Bypass Valve is in full BYPASS position, (3) the Isolation/Relief Valve is in fully OPEN position, and (4) the Isolation/Relief Valve is in ful-ly CLOSED position.
ITS S0 shall receive four signals from Node 2 for monitoring JEM Loop B Hx ORU valve sta-tus. Closed contacts on limit switches located in the JEM Loop B Hx ORU indicate (1) the By-pass Valve is in full NORMAL Position, (2) the Bypass Valve is in full BYPASS position, (3) the Isolation/Relief Valve is in fully OPEN position, and (4) the Isolation/Relief Valve is in ful-ly CLOSED position.
3 − 8
3.2.1.2.3.1.2.1.3 APM Hx ORUs
ITS S0 shall receive four signals from Node 2 for monitoring APM Loop A Hx ORU valve sta-tus. Closed contacts on limit switches located in the APM Loop A Hx ORU indicate (1) the By-pass Valve is in full NORMAL Position, (2) the Bypass Valve is in full BYPASS position, (3) the Isolation/Relief Valve is in fully OPEN position, and (4) the Isolation/Relief Valve is in ful-ly CLOSED position.
ITS S0 shall receive four signals from Node 2 for monitoring APM Loop B Hx ORU valve sta-tus. Closed contacts on limit switches located in the APM Loop B Hx ORU indicate (1) the Bypass Valve is in full NORMAL Position, (2) the Bypass Valve is in full BYPASS position,
(3) the Isolation/Relief Valve is in fully OPEN position, and (4) the Isolation/Relief Valve is in fully CLOSED position.
3.2.1.2.3.1.2.2 HX ORU TEMPERATURE SENSORS
ITS S0 shall provide excitation for the six temperature measurements below. Each measure-ment is defined as low level analog 1.0 mA current loop configured for a standard resistance temperature device (RTD) sensor.
Sensors for Loop A Hx ORU and Loop B Hx ORU as defined below are redundant utility inter-faces. Routing and separation of wiring shall meet the requirements of 3.2.1.1.7.
3.2.1.2.3.1.2.2.1 NODE 2 HX ORUs
ITS S0 shall receive one signal from Node 2 for monitoring Node 2 Loop A Hx ORU ammo-nia outlet temperature.
ITS S0 shall receive one signal from Node 2 for monitoring Node 2 Loop B Hx ORU ammonia outlet temperature.
3.2.1.2.3.1.2.2.2 JEM HX ORUs
ITS S0 shall receive one signal from Node 2 for monitoring JEM Loop A Hx ORU ammonia outlet temperature.
ITS S0 shall receive one signal from Node 2 for monitoring JEM Loop B Hx ORU ammonia outlet temperature.
3 − 9
3.2.1.2.3.1.2.2.3 APM HX ORUs
ITS S0 shall receive one signal from Node 2 for monitoring APM Loop A Hx ORU ammonia outlet temperature.
ITS S0 shall receive one signal from Node 2 for monitoring APM Loop B Hx ORU ammonia outlet temperature.
3.2.1.3 ELECTRICAL INTERFACES
The ITS S0 to Node 2 electrical interfaces are shown in Figure 3.2.1.3−1.
APM 1B
APM 2A
APM 3A
APM 4B
JEM 1B
JEM 2B
JEM 3A
JEM 4A
CENT 1A
CENT 3B
PDGFSSRMS1NODE2
PDGFSSRMS2NODE2
PDGFPL1NODE2
PDGFPL2NODE2
FIGURE 3.2.1.3−1 ITS S0 TO NODE 2 ELECTRICAL INTERFACES
3 − 10
3.2.1.3.1 SUPPLY POWER
ITS S0 shall supply power to the Node 2 through the APM1B, APM2A, APM3A, APM4B, JEM1B, JEM2B, JEM3A, JEM4A, CENT1A, CENT3B, PDGFSSRMS1NODE2, PDGFSSRMS2NODE2, PDGFPL1NODE2 and PDGFPL2NODE2, power output circuits.
3.2.1.3.1.1 POWER QUALITY
The steady state voltage over the interface operating current range shall be within the envelope shown in Table 3.2.1.3.1.1−1.
TABLE 3.2.1.3.1.1−1 ELECTRICAL INTERFACE PARAMETERS
ÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁ
Circuit Name
ÁÁÁÁÁÁ
ÁÁÁÁÁÁ
ÁÁÁÁÁÁ
ÁÁÁÁÁÁ
ÁÁÁÁÁÁ
Interface Vrange
(volts)
ÁÁÁÁÁÁ
ÁÁÁÁÁÁ
ÁÁÁÁÁÁ
ÁÁÁÁÁÁ
ÁÁÁÁÁÁ
Operating Current (amps)
ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁ
Overcurrent Protection
ÁÁÁÁÁ
ÁÁÁÁÁ
ÁÁÁÁÁ
ÁÁÁÁÁ
ÁÁÁÁÁ
Min Steady
State Wire Rating
ÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁ
APM1B ÁÁÁÁÁÁ
ÁÁÁÁÁÁ
118.4 to 173ÁÁÁÁÁÁ
ÁÁÁÁÁÁ
0 to 65 ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁ
See Table 3.2.1.3.1.2−1ÁÁÁÁÁ
ÁÁÁÁÁ
78A
ÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁ
APM2A ÁÁÁÁÁÁ
ÁÁÁÁÁÁ
118.5 to 173ÁÁÁÁÁÁ
ÁÁÁÁÁÁ
0 to 65 ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁ
See Table 3.2.1.3.1.2−1ÁÁÁÁÁ
ÁÁÁÁÁ
78A
ÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁ
APM3A ÁÁÁÁÁÁ
ÁÁÁÁÁÁ
119 to 173 ÁÁÁÁÁÁ
ÁÁÁÁÁÁ
0 to 65 ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁ
See Table 3.2.1.3.1.2−1ÁÁÁÁÁ
ÁÁÁÁÁ
78A
ÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁ
APM4B ÁÁÁÁÁÁ
ÁÁÁÁÁÁ
118.5 to 173ÁÁÁÁÁÁ
ÁÁÁÁÁÁ
0 to 65 ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁ
See Table 3.2.1.3.1.2−1ÁÁÁÁÁ
ÁÁÁÁÁ
78A
ÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁ
JEM1B ÁÁÁÁÁÁ
ÁÁÁÁÁÁ
118.4 to 173ÁÁÁÁÁÁ
ÁÁÁÁÁÁ
0 to 65 ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁ
See Table 3.2.1.3.1.2−1ÁÁÁÁÁ
ÁÁÁÁÁ
78A
ÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁ
JEM2B ÁÁÁÁÁÁ
ÁÁÁÁÁÁ
117.5 to 173ÁÁÁÁÁÁ
ÁÁÁÁÁÁ
0 to 65 ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁ
See Table 3.2.1.3.1.2−1ÁÁÁÁÁ
ÁÁÁÁÁ
78A
ÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁ
JEM3A ÁÁÁÁÁÁ
ÁÁÁÁÁÁ
119 to 173 ÁÁÁÁÁÁ
ÁÁÁÁÁÁ
0 to 65 ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁ
See Table 3.2.1.3.1.2−1ÁÁÁÁÁ
ÁÁÁÁÁ
78A
ÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁ
JEM4A ÁÁÁÁÁÁ
ÁÁÁÁÁÁ
118.5 to 173ÁÁÁÁÁÁ
ÁÁÁÁÁÁ
0 to 65 ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁ
See Table 3.2.1.3.1.2−1ÁÁÁÁÁ
ÁÁÁÁÁ
78A
ÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁ
CENT1A
ÁÁÁÁÁÁ
ÁÁÁÁÁÁ
118.9 to 173
ÁÁÁÁÁÁ
ÁÁÁÁÁÁ
0 to 65
ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁ
See Table 3.2.1.3.1.2−1
ÁÁÁÁÁ
ÁÁÁÁÁ
78A
ÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁCENT3B
ÁÁÁÁÁÁ
ÁÁÁÁÁÁ119 to 173
ÁÁÁÁÁÁ
ÁÁÁÁÁÁ0 to 65
ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁSee Table 3.2.1.3.1.2−1
ÁÁÁÁÁ
ÁÁÁÁÁ78AÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁPDGFSSRMS1NODE2
ÁÁÁÁÁÁ
ÁÁÁÁÁÁ118 to 126
ÁÁÁÁÁÁ
ÁÁÁÁÁÁ0 to 17.7
ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁ1
ÁÁÁÁÁ
ÁÁÁÁÁ30AÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁ
PDGFSSRMS2NODE2
ÁÁÁÁÁÁ
ÁÁÁÁÁÁ
ÁÁÁÁÁÁ
118 to 126
ÁÁÁÁÁÁ
ÁÁÁÁÁÁ
ÁÁÁÁÁÁ
0 to 17.7
ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁ
ÁÁÁÁÁ
ÁÁÁÁÁ
30A
ÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁ
PDGFPL1NODE2 ÁÁÁÁÁÁ
ÁÁÁÁÁÁ
118 to 126 ÁÁÁÁÁÁ
ÁÁÁÁÁÁ
0 to 17.7 ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁ
1 ÁÁÁÁÁ
ÁÁÁÁÁ
30A
ÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁ
PDGFPL2NODE2 ÁÁÁÁÁÁ
ÁÁÁÁÁÁ
118 to 126 ÁÁÁÁÁÁ
ÁÁÁÁÁÁ
0 to 17.7 ÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁ
1 ÁÁÁÁÁ
ÁÁÁÁÁ
30A 1 Protection is equivalent with SSP 30263:002, Type II Remote Power Control Module (RPCM) Standard ICD.
3.2.1.3.1.2 FAULT PROTECTION
ITS S0 shall provide protection as shown in Table 3.2.1.3.1.2−1.
3 − 11
TABLE 3.2.1.3.1.2−1 ELECTRICAL INTERFACE FAULT CURRENT PARAMETERS
ÁÁÁÁÁÁ
ÁÁÁÁÁÁ
ÁÁÁÁÁÁ
ÁÁÁÁÁÁ
Circuit Names
ÁÁÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁÁÁ
Source Limited Maximum Fault Current
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
Trip Current Threshold
Range (amps)
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
Trip Time/Max.
Fault Duration
(msec)
ÁÁÁÁÁÁ
ÁÁÁÁÁÁ
ÁÁÁÁÁÁ
ÁÁÁÁÁÁ
ÁÁÁÁÁÁ
ÁÁÁÁÁÁ
ÁÁÁÁÁÁ
ÁÁÁÁÁÁ
ÁÁÁÁÁÁ
APM1B
APM2A
APM3A
APM4B
JEM1B
JEM2B
JEM3A
JEM4A
ÁÁÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁÁÁ
No more than 4,000 amps peak surge to be limited to no more than 350 amps within 80 msec of fault onset
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
78.25 to 85.75
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
108 to 130
ÁÁÁÁÁÁ
ÁÁÁÁÁÁ
ÁÁÁÁÁÁ
CENT1A
CENT3B
ÁÁÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
3.2.1.3.1.3 DELETED
3.2.1.3.1.4 DELETED
3.2.1.4 FLUID INTERFACES
3.2.1.4.1 SUPPLY COOLANT
ITS S0 shall supply ammonia coolant to Node 2 for active heat acquisition and transport. Char-acteristics of the coolant shall be within the ranges shown in Table 3.2.1.4.1−1, Supply Ammo-nia Characteristics.
3 − 12
TABLE 3.2.1.4.1−1 SUPPLY AMMONIA CHARACTERISTICS
Loop Pressure Range(psia)
Operating Temperature Range * (°F)
Mass Flow Rate Range (lbm/hr)
Minimum Operating Mass
Flowrate (Lbm/Hr)***
A 0 − 500 34 − 40 0 − 4200 2830
B 0 − 500 34 − 40 0 − 5400 4100
* Non−operating temperature range is −100 degrees Fahrenheit to 120 degrees Fahrenheit no− flow conditions ** For Reference Only *** In the event of the loss of one ammonia loop, the other loop flow rate remains the same.
3.2.1.4.2 RECEIVE COOLANT
ITS S0 shall receive return ammonia coolant from Node 2 for heat transport. Characteristics of the coolant shall be within the ranges shown in Table 3.2.1.4.2−1, Return Ammonia Character-istics.
TABLE 3.2.1.4.2−1 RETURN AMMONIA CHARACTERISTICS
Loop Pressure Range (psia)
Operating Temperature Range *
(5F)
Mass Flowrate (Range) (lbm/hr)
Minimum Operating Mass
Flow Rate (lbm/hr)***
A 0 − 500 34 − 95 0 − 4200 2830
B 0 − 500 34 − 95 0 − 5400 4100
* Non−operating temperature range is −100 degrees Fahrenheit to 120 degrees Fahrenheit no− flow conditions ** For Reference Only.
*** In the event of the loss of one ammonia loop, the other loop flow rate remains the same.
3.2.1.4.3 DELTA PRESSURE
ITS S0 shall accommodate a pressure drop of 9.5 +/− 0.4 pounds per square inch differential (psid) at the flow rate of 2,830 lbm/hr across the Node 2 Loop A ammonia lines at the ITS S0 to Node 2 supply/return interface.
ITS S0 shall accommodate a pressure drop of 8.6 +/− 0.4 psid at the flow rate of 4,100 lbm/hr across the Node 2 Loop B ammonia lines at the ITS S0 to Node 2 supply/return interface.
3.2.1.4.4 VOLUME ALLOCATION
ITS S0 shall accomodate a minimum of 1.25 ft3 for loop A and 0.85 ft3 for loop B of ammonia coolant from Node 2.
3.2.1.5 STRUCTURAL INTERFACE
There are no structural considerations at this interface.
3 − 13
3.2.1.5.1 CREW INDUCED LOADS
The connector interfaces between the ITS S0 and Node 2 shall be designed to withstand the crew induced loads listed in Table 3.2.1.5.1−1.
3.2.1.5.1.1 DELETED
TABLE 3.2.1.5.1−1 CREW INDUCED CONNECTOR LOADS
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
DESCRIPTION
OF LOAD
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
LIMIT LOAD
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
TYPE OF
LOAD
ÁÁÁÁÁÁ
ÁÁÁÁÁÁ
ÁÁÁÁÁÁ
DIRECTION
OF LOAD
ÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁ
COMMENTS
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
Inadvertent kick/ bump
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
125 lbf
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
Quasi−static concentrated load over 0.5 inch diameter circular area
ÁÁÁÁÁÁ
ÁÁÁÁÁÁ
ÁÁÁÁÁÁ
ÁÁÁÁÁÁ
ÁÁÁÁÁÁ
ÁÁÁÁÁÁ
Any direction
ÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁ
Accidental impact applied to hardware near (within 24 in. ) of translation paths or work sites
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
EVA handling load
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
45 lbf (35 in−lbf for connector panels for mate/ demate of con-nector
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁ
Quasi−static concentrated load over 1.25 inch radius cir-cular area
ÁÁÁÁÁÁ
ÁÁÁÁÁÁ
ÁÁÁÁÁÁ
ÁÁÁÁÁÁ
ÁÁÁÁÁÁ
ÁÁÁÁÁÁ
ÁÁÁÁÁÁ
ÁÁÁÁÁÁ
ÁÁÁÁÁÁ
ÁÁÁÁÁÁ
ÁÁÁÁÁÁ
ÁÁÁÁÁÁ
ÁÁÁÁÁÁ
Any directionÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁ
This load can be ap-plied anytime to any hardware by the EVA crew member when in a foot re-straint. All hard-ware must be de-signed to this load as a minimum. This force would be ap-plied by the palm of the glove, tip of a boot or knee.
3.2.1.5.2 BONDING
The interfaces shall meet or exceed requirements for a Class R bond in accordance with SSP 30245, Space Station Electrical Bonding Requirements. The on−orbit bonding shall meet the requirements for a Class R Bond, which includes the Class H parameters, when permanently mated. During all other operations, the bond shall meet the requirements of a Class H Bond.
3.2.1.5.3 DELETED
3.2.1.5.4 MATERIALS AND FINISHES
Materials and finishes at the hardware interface shall be compatible with the environment and with interfacing hardware per the requirements of paragraph 4.5.4 of SSP 30233, Space Station Requirements for Materials and Processes. Materials located near sensitive hardware such as radiators and window cavities shall have lower outgassing rates per the requirements of para-graph 3.2.2.3 of SSP 30426, Space Station External Contamination Control Requirements.
3 − 14
3.2.1.5.5 DELETED
3.2.1.6 ENVIRONMENTS
3.2.1.6.1 ELECTROMAGNETIC COMPATIBILITY
The ITS S0 to Node 2 interface shall meet the requirements of SSP 30243, Space Station Sys-tems Requirements for Electromagnetic Compatibility.
3.2.1.6.2 ELECTROSTATIC DISCHARGE
The ITS S0 to Node 2 interface shall meet the requirements of SSP 30243.
3.2.1.6.3 CORONA
The ITS S0 to Node 2 interface shall meet the requirements of SSP 30243.
3.2.2 NODE 2 INTERFACE REQUIREMENTS
3.2.2.1 INTERCONNECTING UTILITY HARDWARE
Node 2 shall incorporate provisions for the mechanical connection of ammonia coolant, power, instrumentation, and video utilities to ITS S0 during on−orbit assembly. Utility interfaces shall contain physical provisions to preclude incorrect installation of utility lines and shall not be lockwired or staked.
3.2.2.1.1 ACCESSIBILITY
Fluid and avionic connectors shall comply with SSP 50005, paragraphs 14.3, 14.4, and 14.6.4.3, requirements for accessibility by EVA−suited crew members.
3.2.2.1.2 ELECTRICAL CONNECTORS
The characteristics for electrical connectors shall be in accordance with SSQ 21635, General Specifications for Connectors and Accessories, Electrical, Circular, Miniature, IVA/EVA/Robot Compatible, Space Quality.
3.2.2.1.3 UTILITY CABLE SPECIFICATIONS
Cable and wire design shall be in accordance with SSP 30242, Space Station Cable/Wire De-sign and Control Requirements for Electromagnetic Compatibility.
3.2.2.1.3.1 VIDEO CABLE SPECIFICATIONS
The video interconnect cables shall comply with the requirements of SSQ 21654, General Specification for Cable, Single Fiber, Multi−Mode, Space Quality.
3 − 15
3.2.2.1.3.2 HEAT EXCHANGER INSTRUMENTATION CABLES
Heat exchanger instrumentation utility cables shall conform to SSQ 21656.
3.2.2.1.3.3 ELECTRICAL POWER CABLE SPECIFICATIONS
Power cables shall conform to SSQ 21652 or SSQ 21656.
3.2.2.1.4 GROUNDING
Grounding between Node 2 and ITS S0 shall be in accordance with SSP 30240.
3.2.2.1.5 SHIELD TERMINATION OF ELECTRICAL CABLES
All shields shall be terminated to structure or chassis at Node 2. Shield termination shall be in accordance with SSP 30242.
3.2.2.1.6 FLUID CONNECTORS
Fluid connectors at the interface shall comply with specifications shown in Table 3.2.1.1.6−1.
3.2.2.1.7 REDUNDANT UTILITY INTERFACES
Node 2 shall provide redundant utility interfaces for power distribution and heat exchanger in-strumentation. Alternate or redundant functional paths shall be separated or protected at the interface such that a credible event, which causes the loss of one functional path, will not result in the loss of the alternate or redundant functional path(s).
3.2.2.2 ELECTRONIC INTERFACES
3.2.2.2.1 VIDEO SIGNALS
Node 2 shall transmit the signals described in the following subparagraphs to the ITS S0.
3.2.2.2.1.1 OPTICAL PFM NTSC VIDEO SIGNAL CHARACTERISTICS
The optical PFM NTSC video signal characteristics shall be in accordance with SSP 50002, paragraphs 3.2.1.5.4 and 3.2.1.5.5.
3.2.2.2.1.1.1 OPTICAL PFM NTSC VIDEO SIGNAL TRANSMIT POWER LEVELS
The minimum average optical PFM NTSC video signal transmit power, measured at ambient temperature, transmitted by Node 2 shall meet Table 3.2.2.2.1.1.1−1 at each signal interface.
3 − 16
TABLE 3.2.2.2.1.1.1−1 OPTICAL PFM NTSC VIDEO SIGNAL TRANSMIT POWER
ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ
Source to Destination ÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁ
Node 2 Output*
ÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁVideo Source
ÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁDestination
ÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁOptical Power (dBm)ÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁ
Ext Port 11
ÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁ
VSW 1
ÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁ
−18.8
ÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁ
PDGF NODE 2 −1 ÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁ
VSW 1 ÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁ
−18.4
ÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁPDGF NODE 2 −2
ÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁVSW 2
ÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁ−18.4ÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁ
PDGF NODE 2 −3
ÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁ
VSW 3
ÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁ
−18.4
* Measured at the Node 2 aft−end ring connector panel.
3.2.2.2.1.2 DELETED
3.2.2.2.1.3 DELETED
3.2.2.2.1.4 DELETED
3.2.2.2.2 SYNC AND CONTROL SIGNALS
Node 2 shall receive the signals described in the following subparagraphs from ITS S0.
3.2.2.2.2.1 OPTICAL PFM NTSC SYNC AND CONTROL SIGNAL CHARACTERISTICS
The optical PFM NTSC sync and control signal characteristics shall be in accordance with SSP 50002, paragraphs 3.2.1.5.4 and 3.2.1.5.5.
3.2.2.2.2.1.1 OPTICAL PFM NTSC SYNC AND CONTROL SIGNAL RECEIVE POWER
LEVELS
Node 2 shall meet all power level requirements with minimum average optical PFM NTSC sync and control signal input power, measured at ambient temperature, provided by Table 3.2.2.2.2.1.1−1 at each signal interface.
TABLE 3.2.2.2.2.1.1−1 OPTICAL PFM NTSC SYNC AND CONTROL SIGNAL RECEIVE
POWER
ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ
Source to Destination ÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁ
Node 2 Input *
ÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁ
Video Source
ÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁ
Destination
ÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁ
Optical Power (dBm)
ÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁ
VSW 1 ÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁ
Ext Port 11 ÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁ
−17.9
ÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁ
VSW 2 ÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁ
PDGF Node 2 −1 ÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁ
−20.7
ÁÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁÁVSW 3
ÁÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁÁPDGF Node 2 −2
ÁÁÁÁÁÁÁÁÁÁ
ÁÁÁÁÁÁÁÁÁÁ−20.7
* Measured at the Node 2 aft−end ring connector panel.
3 − 17
3.2.2.2.2.2 DELETED
3.2.2.2.2.3 DELETED
3.2.2.2.2.4 DELETED
3.2.2.2.3 INSTRUMENTATION AND CONTROLS
3.2.2.2.3.1 HEAT EXCHANGER ORBITAL REPLACEABLE UNIT
The Node 2 to ITS S0 interface shall provide for the instrumentation and control of six (6) Hx ORUs, which are defined as follows:
3.2.2.2.3.1.1 Hx ORU CONTROL SIGNALS
All Hx ORU Control Signals are conditioned secondary power. The maximum voltage level associated with each of these signals shall be 126 Volts DC. Short circuit current protection shall be provided by ITS S0 for each control signal. Short circuit current for each control sig-nal shall not exceed 3.0 Amps DC.
Loop A Hx ORUs and Loop B Hx ORUs are redundant utility interfaces. Routing and separa-tion of associated wiring shall meet the requirements of paragraph 3.2.2.1.7.
3.2.2.2.3.1.1.1 NODE 2 HxORUs
Node 2 shall receive four signals from ITS S0 to command valves that control Node 2 Loop A Hx ORU. These include (1) Command the Bypass Valve to NORMAL Flow, (2) Command the Bypass Valve to BYPASS Flow, (3) Command the Isolation/Relief Valve to OPEN, and (4) Command the Isolation/Relief Valve to CLOSE.
Node 2 shall receive four signals from ITS S0 to command valves that control Node 2 Loop B Hx ORU. These include (1) Command the Bypass Valve to NORMAL Flow, (2) Command the Bypass Valve to BYPASS Flow, (3) Command the Isolation/Relief Valve to OPEN, and (4) Command the Isolation/Relief Valve to CLOSE.
3.2.2.2.3.1.1.2 JEM Hx ORUs
Node 2 shall receive four signals from ITS S0 to command valves that control JEM Loop A Hx ORU. These include (1) Command the Bypass Valve to NORMAL Flow, (2) Command the Bypass Valve to BYPASS Flow, (3) Command the Isolation/Relief Valve to OPEN, and (4) Command the Isolation/Relief Valve to CLOSE.
Node 2 shall receive four signals from ITS S0 to command valves that control JEM Loop B Hx ORU. These include (1) Command the Bypass Valve to NORMAL Flow, (2) Command the Bypass Valve to BYPASS Flow, (3) Command the Isolation/Relief Valve to OPEN, and (4) Command the Isolation/Relief Valve to CLOSE.
3.2.2.2.3.1.1.3 APM Hx ORUs
Node 2 shall receive four signals from ITS S0 to command valves that control APM Loop A Hx ORU. These include (1) Command the Bypass Valve to NORMAL Flow, (2) Command the Bypass Valve to BYPASS Flow, (3) Command the Isolation/Relief Valve to OPEN, and (4) Command the Isolation/Relief Valve to CLOSE.
Node 2 shall receive four signals from ITS S0 to command valves that control APM Loop B Hx ORU. These include (1) Command the Bypass Valve to NORMAL Flow, (2) Command the Bypass Valve to BYPASS Flow, (3) Command the Isolation/Relief Valve to OPEN, and (4) Command the Isolation/Relief Valve to CLOSE.
3 − 18
3.2.2.2.3.1.2 Hx ORU INSTRUMENTATION/SENSOR SIGNALS
3.2.2.2.3.1.2.1 Hx ORU VALVE POSITION SENSORS
Node 2 shall receive from ITS S0 excitation voltage required for monitoring each Hx ORU limit switch as described below. The maximum excitation voltage provided by ITS S0 when switch contacts are OPEN shall be 29 Volts DC . ITS S0 shall limit the current to closed switch contacts to 0.2 mA maximum.
Loop A Hx ORU and Loop B Hx ORU are redundant utility interfaces. Routing and separation of associated wiring shall meet the requirements of paragraph 3.2.2.1.7.
3.2.2.2.3.1.2.1.1 NODE 2 Hx ORUs
Node 2 shall provide four signals to ITS S0 for monitoring Node 2 Loop A Hx ORU valve sta-tus. Closed contacts on limit switches located in Node 2 Loop A Hx ORU indicate (1) the By-pass Valve is in full NORMAL Position, (2) the Bypass Valve is in full BYPASS position, (3) the Isolation/Relief Valve is in fully OPEN position, and (4) the Isolation/Relief Valve is in ful-ly CLOSED position.
Node 2 shall provide four signals to ITS S0 for monitoring Node 2 Loop B Hx ORU valve sta-tus. Closed contacts on limit switches located in Node 2 Loop B Hx ORU indicate (1) the By-pass Valve is in full NORMAL Position, (2) the Bypass Valve is in full BYPASS position, (3) the Isolation/Relief Valve is in fully OPEN position, and…
This is the start of the file's text. The full file is on GovTribe.
File details come from the government source that posted it. Updated .