SSP_50315-Rev_C.docx

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

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This request for proposal solicits offers for a human space flight technical integration contract. NASA/JSC plans to issue the solicitation seeking integration services to support human space flight programs. The anticipated small business set-aside procurement has a NAICS code of 541715 and size standard of 1,250 employees. Offers are due around December 11, 2019. Questions must be submitted in writing, while the solicitation and amendments will be available on a specified website. Offerors should monitor the site and are responsible for downloading relevant documents.

SSP 50315-Rev C

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Water Recovery System Rack #1 to Node 3 Interface Control Document

International Space Station Program

October 20, 2010

REVISION C

Type 1 NASA Approved

National Aeronautics and Space Administration International Space Station Program Johnson Space Center Houston, TX Contract # PIC-NNJ09GA18B DRD # PIC-SI-01 European Space Agency

REVISION AND HISTORY PAGE

REV.

DESCRIPTION

PUB. DATE

-
Initial Release per SSCN 002329, EFF. 12-16-99
02-02-00
A
Revision A release per SSCD 005876 EFF. 08-23-01

Incorporates the following IRNs, EFF 05/18/01: IRN 50315-01 (PIRN 50315-NA-0002C), IRN 50315-02 (PIRN 50315-NA-0006), IRN 50315-03 (PIRN 50315-NA-0008), IRN 50315-04 (PIRN 50315-NA-0012A), IRN 50315-05 (PIRN 50315-NA-0014) 03-11-02

IRN 50315-0006 (PIRN 50315-NA-0004A) per SSCN 006789 EFF. 05-23-02 - CCBD ND3-00-0014 modifies page 3-18 in accordance with IRN 50315-06, EFF 5/23/02 06-29-05

IRN 50315-0007 (PIRN 50315-NA-0001B) per SSCN 006789 EFF. 05-23-02 - CCBD ND3-00-0014 modifies page 3-4 in accordance with IRN 50315-07, EFF 5/23/02 06-29-05

IRN 50315-0008 (PIRN 50315-NA-0003E) per SSCN 006789 EFF. 05-23-02 - CCBD ND3-00-0014 modifies pages 3-5, 3-6, 3-14, 3-38, B-1, B-2, B-3, & C-5 in accordance with IRN 50315-08, EFF 5/23/02

06-29-05

IRN 50315-0009 (PIRN 50315-NA-0015B) per SSCN 006789 EFF. 05-23-02 - CCBD ND3-00-0014 modifies pages 3-10, 3-12, & 3-35 in accordance with IRN 50315-09, EFF 5/23/02 06-29-05

B
Revision B (Reference per SSCD 009617, EFF. 02/02/06)

Incorporates the following IRNs 50315-06 (PIRN 50315-NA-0004A), 50315-07 (PIRN 50315-NA-0001B), 50315-08 (PIRN 50315-NA-0003E), 50315-09 (PIRN 50315-NA-0015B), 50315-10 (PIRN 50315-NA-0009B), 50315-11 (PIRN 50315-NA-0010B), 50315-12 (PIRN 50315-NA-0016A), 50315-13 (PIRN 50315-NA-0017A), 50315-14 (PIRN 50315-NA-0007B), 50315-15 (PIRN 50315-NA-0005A), 50315-16 (PIRN 50315-NA-0018), 50315-17 (PIRN 50315-NA-0019A) 06-12-06

C
Revision C (Reference SSCD 012697, Eff 04/12/11)
05/04/11

Revision C incorporates the following approved PIRNs:

PIRN SSCN

50315-ES-0001 012697

50315-NA-0020 012697

50315-NA-0021 008007

50315-NA-0022 012697

50315-NA-0024A 012697

PREFACE

The contents of this document are intended to be consistent with the tasks and products to be prepared by Program participants. The Water Recovery System Rack #1 to Node 3 Interface Control Document, shall be implemented on all new ISS contractual and internal activities and shall be included in any existing contracts through contract changes. This document is under the control of the Vehicle Control Board as designated by the Space Station Control Board, and any changes or revisions will be approved by the Vehicle Control Board Chairperson.

/s/ Kevin Window4/12/11
SignatureDate

Kevin Window Vehicle Office Manager ISS Program Office

INTERNATIONAL SPACE STATION PROGRAM

Water Recovery System Rack #1 to Node 3

CONCURRENCE

Created by:
Gregg D. Singer

OM/ARES

(PRINT NAME)

ORG

/s/ Gregg D. Singer

3/28/11

(SIGNATURE)

DATE

Prepared by:
Sharon E. Hock

OM/ARES

(PRINT NAME)

ORG

/s/ Sharon E. Hock

3/28/11

(SIGNATURE)

DATE

Approved by:
Tyson E. Richmond

OM/NASA

(PRINT NAME)

ORG

/s/ Tyson E.. Richmond

4-6-11

(SIGNATURE)

DATE

DQA:
Victoria C. Rodriguez

OM/ARES

(PRINT NAME)

ORG

/s/ Victoria C. Rodriguez

3/28/2011

(SIGNATURE)

DATE

INTERNATIONAL SPACE STATION PROGRAM

Water Recovery System Rack #1 to Node 3

LIST OF CHANGES

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

Board Name
Entry Date
Change
Paragraph(s))
February 2000
Initial Release
All
March 2002
Revision A
All
June 2005
IRN 0006
3.2.1.5.1.1
June 2005
IRN 0007
3.2.1.3
June 2005
IRN 0008
3.2.1.4.5.3

3.2.1.4.5.4 3.2.1.4.5.5 3.2.2.4.5.5 Appendix B Appendix C Figures 3.2.1.3-1 3.2.1.3-2

June 2005
IRN 0009
3.2.1.4.4.1

3.2.1.4.4.5 3.2.1.4.4.6 3.2.1.4.4.7 3.2.2.4.4.1 3.2.2.4.4.4 3.2.2.4.4.5 Table 3.2.1.4-2

June 2006
Revision B
All
January 2011
Revision C
All

Table of Contents

1.Introduction1-1
1.1Purpose1-1
1.2scope1-1
1.3precedence1-1
1.4delegation of authority1-1
1.5responsibility and change authority1-1
2.DOCUMENTS2-1
2.1APPLICABLE documents2-1
3.Interfaces3-1
3.1GENERAL3-1
3.1.1INTERFACE DESCRIPTION3-1
3.1.1.1Water Recovery SYSTEM Rack #1 Description3-2
3.1.1.2Node 3 DESCRIPTION3-2
3.1.2INTERFACE RESPONSIBILITIES3-2
3.1.2.1RESPONSIBILITY FOR Water Recovery System3-2
3.1.2.2RESPONSIBILITY FOR Node 33-2
3.1.2.3RESPONSIBILITY FOR interconnect cabling/tubing/connectors3-2
3.1.3COORDINATE SYSTEMS3-2
3.1.4engineering units, tolerances and conversions3-2
3.1.4.1engineering units and tolerances3-2
3.1.4.1.1Tolerances3-3
3.2INTERFACE REQUIREMENTS3-3
3.2.1WATER RECOVERY SYSTEM RACK #1 REQUIREMENTS3-3
3.2.1.1ENVELOPE REQUIREMENTS3-3
3.2.1.2MASS PROPERTIES3-3
3.2.1.2.1MASS3-3
3.2.1.2.2CENTER OF MASS3-3
3.2.1.3STRUCTURAL/MECHANICAL ATTACHMENT3-3
3.2.1.3.1Rack Interface Panel3-3
3.2.1.3.1.1Accessibility3-3
3.2.1.4FLuid Interfaces3-6
3.2.1.4.1Fire Suppressant3-6
3.2.1.4.2RECEIVE COOLANT3-6
3.2.1.4.2.1WRS Rack #1 heat transport capability3-6
3.2.1.4.2.1.1WRS Rack #1 moderate temperature loop HEAT LOAD3-6
3.2.1.4.2.2receive Coolant characteristics3-6
3.2.1.4.2.2.1receive coolant specification3-6
3.2.1.4.2.2.2receive coolant temperature3-6
3.2.1.4.2.2.3RECEIVE COOLANT PRESSURE3-6
3.2.1.4.2.2.4RECEIVE coolant Flow rate3-6
3.2.1.4.2.2.5Receive Coolant Interface Control3-6
3.2.1.4.2.2.6RECEIVE coolant quantity3-6
3.2.1.4.2.2.7RECEIVE coolant leakage rate3-7
3.2.1.4.2.3Receive Coolant connector3-7
3.2.1.4.3RETURN COOLANT3-8
3.2.1.4.3.1Return COOLANT CHARACTERISTICS3-8
3.2.1.4.3.1.1Return COOLANT SPECIFICATIONS3-8
3.2.1.4.3.1.2Return COOLANT TEMPERATURE3-8
3.2.1.4.3.1.3RETURN coolant pressure drop3-8
3.2.1.4.3.2RETURN coolant cONNECTOR3-8
3.2.1.4.4SUPPLY potable water3-8
3.2.1.4.4.1SUPPLY potable water Temperature3-8
3.2.1.4.4.2SUPPLY potable water Pressure3-8
3.2.1.4.4.2.1SUPPLY potable water maximum design Pressure3-8
3.2.1.4.4.3SUPPLY potable water Flow rate3-8
3.2.1.4.4.4SUPPLY potable water Interface control3-8
3.2.1.4.4.5Supply Potable Water Quality3-8
3.2.1.4.4.6supply potable water connector3-9
3.2.1.4.4.7Supply potable water manual container connector3-9
3.2.1.4.4.8Supply potable water sample port3-9
3.2.1.4.5WPA Process Water3-9
3.2.1.4.5.1WPA Process Water Temperature3-9
3.2.1.4.5.2WPA Process Water Pressure3-9
3.2.1.4.5.2.1WPA Process Water maximum design Pressure3-10
3.2.1.4.5.2.2WPA Process Water Maximum Pressure Drop3-10
3.2.1.4.5.3WPA Process Water Flow rate3-10
3.2.1.4.5.4WPA Process Water Interface control3-10
3.2.1.4.5.5WPA process water connectors3-11
3.2.1.4.6Supply Vent gas to Cabin Atmosphere3-11
3.2.1.4.6.1Supply Vent gas to Cabin Atmosphere Temperature3-11
3.2.1.4.6.2Supply Vent gas to Cabin Atmosphere Pressure3-11
3.2.1.4.6.3Supply Vent gas to Cabin Atmosphere Flow rate3-11
3.2.1.4.6.4Supply Vent cabin gas to Cabin Atmosphere Interface control3-11
3.2.1.4.6.5Supply Vent gas connector3-11
3.2.1.4.6.6Supply vent gas humidity3-11
3.2.1.4.7Receive OXYGEN3-17
3.2.1.4.7.1Receive OXYGEN Temperature3-17
3.2.1.4.7.2Receive OXYGEN Pressure3-17
3.2.1.4.7.2.1Receive OXYGEN maximum design Pressure3-17
3.2.1.4.7.3Receive OXYGEN Flow rate3-17
3.2.1.4.7.4Receive OXYGEN Interface control3-17
3.2.1.4.7.5Receive OXYGEN connector3-17
3.2.1.5ELECTRICAL INTERFACES3-17
3.2.1.5.1RECEIVE POWER3-17
3.2.1.5.1.1POWER QUALITY3-19
3.2.1.5.1.2steady-state current3-19
3.2.1.5.2Supply Electrical Power3-19
3.2.1.5.2.1Power Connectors3-27
3.2.1.6Command and Data Handling (C&DH) INTERFACES3-27
3.2.1.6.1mil-std-1553B interface3-30
3.2.1.6.1.1respond to input amplitude3-33
3.2.1.6.1.21553B bus signal characteristics3-33
3.2.1.6.1.2.11553B bus coupling3-33
3.2.1.6.1.3terminal operations3-33
3.2.1.6.1.41553B bus interface functions3-33
3.2.1.6.2C&DH Connectors3-33
3.2.1.6.3DELETED3-33
3.2.1.6.4Time distribution3-33
3.2.1.7SOFTWARE INTERFACES3-34
3.2.1.8environments3-34
3.2.1.8.1WRS Rack #1 Bonding Interface3-34
3.2.1.8.2STRUCTURAL LOADS3-34
3.2.1.8.2.1Acceleration3-34
3.2.1.8.3vibroacoustics3-34
3.2.1.8.4cabin air3-34
3.2.1.8.4.1cabin air CHARACTERISTICS3-34
3.2.1.8.4.1.1cabin air temperature3-34
3.2.1.8.4.1.1.1Receive cabin air temperature3-34
3.2.1.8.4.1.1.2Supply cabin air temperature3-34
3.2.1.8.4.1.2cabin air pressure3-34
3.2.1.8.4.1.2.1receive cabin air pressure3-34
3.2.1.8.4.1.2.2supply cabin air pressure3-35
3.2.1.8.4.1.3cabin air humidity3-35
3.2.1.8.4.1.3.1receive cabin air humidity3-35
3.2.1.8.4.1.3.2supply cabin air humidity3-35
3.2.1.8.4.1.4REPRESSURIZATION/DEPRESSURIZATION3-35
3.2.1.8.4.1.5cabin air OXYGEN concentration3-35
3.2.1.8.4.1.5.1Receive cabin air oxygen concentration3-35
3.2.1.8.4.1.5.2Supply cabin air oxygen concentration3-35
3.2.1.8.4.1.6Cabin air exchange flowrate3-35
3.2.1.8.4.1.7Cabin air exchange velocity3-35
3.2.1.8.4.2Wrs Rack #1 air heat load3-35
3.2.2NODE 3 INTERFACE REQUIREMENTS3-36
3.2.2.1ENVELOPE REQUIREMENTS3-36
3.2.2.2MASS PROPERTIES3-36
3.2.2.2.1MASS3-36
3.2.2.2.2CENTER OF MASS3-36
3.2.2.3STRUCTURAL/MECHANICAL ATTACHMENT3-36
3.2.2.3.1Rack Interface Panel3-36
3.2.2.3.1.1Accessibility3-36
3.2.2.4FLUID INTERFACES3-36
3.2.2.4.1Fire suppressant3-36
3.2.2.4.2SUPPLY COOLANT3-36
3.2.2.4.2.1Node 3 HEAT TRANSPORT CAPABILITY3-36
3.2.2.4.2.1.1Wrs rack #1 moderate temperature loop heat load3-36
3.2.2.4.2.2supply Coolant characteristics3-37
3.2.2.4.2.2.1supply coolant specification3-37
3.2.2.4.2.2.2supply coolant temperature3-37
3.2.2.4.2.2.3supply coolant pressure3-37
3.2.2.4.2.2.4RECEIVE coolant Flow rate3-37
3.2.2.4.2.2.5SUPPLY coolant rate/ PRESSURE DROP3-37
3.2.2.4.2.2.6SUPPLY coolant quantity3-37
3.2.2.4.2.2.7SUPPLY coolant leakage rate3-37
3.2.2.4.2.3Supply Coolant Connector3-37
3.2.2.4.3receive RETURN COOLANT3-37
3.2.2.4.3.1Receive RETURN COOLANT CHARACTERISTICS3-37
3.2.2.4.3.1.1receive RETURN COOLANT SPECIFICATIONS3-37
3.2.2.4.3.1.2receive RETURN COOLANT TEMPERATURE3-37
3.2.2.4.3.2Receive Return Coolant Connector3-37
3.2.2.4.4receive POtable water3-38
3.2.2.4.4.1receive POtable water Temperature3-38
3.2.2.4.4.2receive POtable water Pressure3-38
3.2.2.4.4.2.1receive POtable water maximum design Pressure3-38
3.2.2.4.4.3receive POtable water Flow rate3-38
3.2.2.4.4.4Receive Potable Water Connector3-38
3.2.2.4.4.5Receive potable water manual transfer container connector3-38
3.2.2.4.4.6Receive potable water quality3-38
3.2.2.4.5WPA Process Water3-39
3.2.2.4.5.1WPA Process Water Temperature3-39
3.2.2.4.5.2WPA Process Water Pressure3-39
3.2.2.4.5.2.1WPA Process Water maximum design Pressure3-39
3.2.2.4.5.2.2WPA Process Water Maximum Pressure Drop3-40
3.2.2.4.5.3WPA Process Water Flow rate3-40
3.2.2.4.5.4WPA Process Water Interface control3-40
3.2.2.4.5.5WPA process water connectors3-40
3.2.2.4.6receive vent gas to cabin atmosphere3-40
3.2.2.4.6.1receive vent gas to cabin atmosphere Temperature3-41
3.2.2.4.6.2receive vent gas to cabin atmosphere Pressure3-41
3.2.2.4.6.3receive vent gas to cabin atmosphere Flow rate3-41
3.2.2.4.6.4Receive Vent Gas Connector3-41
3.2.2.4.6.5Receive vent gas humidity3-41
3.2.2.4.7supply OXYGEN3-41
3.2.2.4.7.1supply OXYGEN Temperature3-41
3.2.2.4.7.2supply OXYGEN Pressure3-41
3.2.2.4.7.2.1supply OXYGEN maximum design Pressure3-41
3.2.2.4.7.3supply OXYGEN Flow rate3-41
3.2.2.4.7.4Supply Cabin Oxygen Connector3-42
3.2.2.5ELECTRICAL INTERFACES3-42
3.2.2.5.1Transfer Electrical Power3-42
3.2.2.5.1.1Power Connectors3-42
3.2.2.5.1.2Transfer electrical power/data line length3-42
3.2.2.6C&DH INTERFACES3-42
3.2.2.6.1mil-std-1553 interfaces3-43
3.2.2.6.1.11553B BUS format/standard3-43
3.2.2.6.1.21553B bus signal characteristics3-43
3.2.2.6.1.2.11553B bus coupling3-43
3.2.2.6.1.3terminal operations3-43
3.2.2.6.1.41553B bus interface functions3-43
3.2.2.6.2C&DH Connectors3-43
3.2.2.6.3DELETED3-44
3.2.2.6.4TIME DISTRIBUTION3-44
3.2.2.7SOFTWARE INTERFACES3-44
3.2.2.8environments3-44
3.2.2.8.1Bonding Interface3-44
3.2.2.8.2STRUCTURAL LOADS3-44
3.2.2.8.2.1Acceleration3-44
3.2.2.8.3vibroacoustics3-44
3.2.2.8.4cabin air3-44
3.2.2.8.4.1cabin air characteristics3-44
3.2.2.8.4.1.1cabin air temperature3-44
3.2.2.8.4.1.1.1Supply cabin air temperature3-44
3.2.2.8.4.1.1.2Receive cabin air temperature3-44
3.2.2.8.4.1.2cabin air pressure3-45
3.2.2.8.4.1.2.1Supply cabin air pressure3-45
3.2.2.8.4.1.2.2Receive cabin air pressure3-45
3.2.2.8.4.1.3cabin air humidity3-45
3.2.2.8.4.1.3.1Supply cabin air humidity3-45
3.2.2.8.4.1.3.2Receive cabin air humidity3-45
3.2.2.8.4.1.4repressurization/depressurization3-45
3.2.2.8.4.1.5cabin air OXYGEN concentration3-45
3.2.2.8.4.1.5.1Supply cabin air oxygen concentration3-45
3.2.2.8.4.1.5.2Receive cabin air oxygen concentration3-45
3.2.2.8.4.1.6Cabin air exchange flowrate3-45
3.2.2.8.4.1.7Cabin air exchange velocity3-45
3.2.2.8.4.2Wrs rack #1 air heat load3-45

appendix list

A ABBREVIATIONS AND ACRONYMS A - 1

List of figures

3.1.1.1-1 Water Recovery System Rack #1 to Node 3 Functional Interface Diagram3-1
3.2.1.3-1 WRS Rack #1/Node 3 Rack Interface Plane3-4
3.2.1.3-2 WRS Rack #1 Specific Panel Connector Locations3-5
3.2.1.4-1 WPA Interfaces with Rack faceplate3-12
3.2.1.42 Cabin air inlet (detail a of figure 3.2.1.4-1)3-13
3.2.1.43 Cabin air outlet (detail e of figure 3.2.1.4-1)3-14
3.2.1.44 oxygen vent fitting (detail C of figure 3.2.1.4-1)3-15
3.2.1.45 Wrs rack #1 sample port (detail F of figure 3.2.1.4-1)3-16

list of tables

3.1.4.1-1 Linear Tolerances3-3
3.2.1.4-2 fluid interface connectors3-9
3.2.1.5-1 Maximum Rack Power input from WRS Rack #23-17
3.2.1.5-2 J2 Power Connector Description and Pin Assignments3-18
3.2.1.5-3 Maximum Allowable Steady-State Current (116-126 Vdc)3-19
3.2.1.5-4 J6 Power Connector Description and Pin Assignments3-20
3.2.1.5-5 J7 Power Connector Description and Pin Assignments3-21
3.2.1.5-6 J8 Power Connector Description and Pin Assignments3-22
3.2.1.6-1 J3 Hardwire Data Connector Description and Pin Assignments3-28
3.2.1.6-2 J4 1553B A Data Connector Description and Pin Assignments3-31
3.2.1.6-3 J5 1553B B Data Connector Description and Pin Assignments3-32

SSP 50315C

SSP 50315C October 20, 2010 ii

Introduction Purpose The purpose of this document is to define the physical, functional, and environmental interface between the Water Recovery System (WRS) Rack # 1 and the Node 3.

scope The scope of this document is limited to the interfaces between the WRS Rack #1 and the Node 3. This document also includes limited information on the electrical interfaces between WRS Racks #1 and #2.

precedence In the event of conflict between SSP 41000, ISS System Specification, and the contents of this Interface Control Document (ICD), the requirements of SSP 41000 shall take precedence.

delegation of authority NASA may delegate the responsibility for preparation and maintenance of this ICD.

responsibility and change authority This document is prepared and maintained in accordance with SSP 30459, NASA Space Station Interface Control Plan.

1- 3-45

DOCUMENTS

APPLICABLE documents The following documents of the exact issue shown form a part of this document to the extent specified herein.

ASTM E380Standard Practice for Use of the International System of
Units (SI) (the Modernized Metric System)
(Reference 3.1.4.1.1)
MIL-STD-1553BDigital Time Division Command/Response Multiplex Data
Rev. BBus
Notice 2(Reference 3.2.1.6.1, 3.2.1.6.1.1, 3.2.1.6.1.2,
8-Sept-19863.2.1.6.1.2.1, 3.2.1.6.1.3, 3.2.1.6.1.4, 3.2.2.6.1, 3.2.2.6.1.1, 3.2.2.6.1.2, 3.2.2.6.1.2.1, 3.2.2.6.1.3, 3.2.2.6.1.4)
SSP 41002International Standard Payload Rack to NASA/ESA/JAXA Modules ICD
(Reference 3.1.1.1)
SSP 30261:002Space Station Multiplexer/ Demultiplexer Standard ICD
(Reference 3.2.1.6, 3.2.2.6)
SSP 30459NASA Space Station Interface Control Plan
(Reference 1.5)
SSP 30482Electrical Power Specifications and Standards, Volume 1: EPS Electrical Performance Specifications
(Reference 3.2.1.5.1.1)
SSP 30573Fluid Procurement and Use Control Specification
(Reference 3.2.1.4.2.2.1, 3.2.1.4.3.1.1, 3.2.2.4.2.2.1, 3.2.2.4.3.1.1)
SSP 41017Rack to Mini Pressurized Logistics Module Interface
Part 1Control Document
(Reference 3.2.1.1, 3.2.1.2.1, 3.2.1.3, 3.2.1.8.1, 3.2.1.8.2, 3.2.1.8.2.1, 3.2.1.8.3, 3.2.1.8.4.1.4, 3.2.2.1, 3.2.2.2.1, 3.2.2.3, 3.2.2.8.2, 3.2.2.8.3, 3.2.2.8.4.1.4, Figure 3.2.1.3-1)
SSP 41017Rack to Mini Pressurized Logistics Module Interface
Part 2Control Document
(Reference 3.1.3, 3.2.1.3, 3.2.1.8.1, 3.2.1.8.4.1.4, 3.2.2.3, 3.2.2.8.1, 3.2.2.8.4.1.4, Figure 3.2.1.3-1)
SSP 41000ISS System Specification
(Reference 1.3)
SSP 50005International Space Station Flight Crew Standard
(Reference 3.2.1.3.1.1, 3.2.2.3.1.1)
SSP 50318Prime Item Development Specification for the Node 3
(Reference 3.2.1.4.4.5, 3.2.2.4.4.6)
SSP 50405-07Software Interface Control Document Hub Control Zone (HCZ) Multiplexer/Demultiplexer (MDM) to International Space Station (ISS) Book 7 Water Processor Assembly (WPA) Interface
(Reference 3.2.1.7, 3.2.2.7)
683-16348Coupling, Quick Disconnect, Fluid, Self-Sealing, Internal Source Control Drawing
(Reference Table 3.2.1.4-2)

2- Interfaces

GENERAL

INTERFACE DESCRIPTION

The interfaces specified herein are applicable to the WRS Rack #1 and the Node 3. The Node 3 will provide power, data, thermal coolant, oxygen, environmental, cabin atmosphere, and the structural/mechanical interfaces at the rack location. The WRS Rack #1 will provide return thermal coolant, data, cabin atmosphere, vent cabin gas, potable water, and process water, environmental and structural/mechanical interfaces at the rack location. A functional interface diagram is shown in Figure 3.1.1.1-1 Water Recovery System Rack #1 to Node 3 Functional Interface Diagram.

The Node 3 to WRS Rack #1 interface plane is defined at the Rack Interface Panel (RIP) and rack structural/mechanical attach points. Note: The only exception to the interface plane description is the vent cabin gas to the cabin and atmosphere exchange between the Node 3 and WRS Rack #1. In these cases the interface plane is not relevant.

Figure 3.1.1.1-1 Water Recovery System Rack #1 to Node 3 Functional Interface Diagram

Water Recovery SYSTEM Rack #1 Description The WRS Rack #1 consists of an Environmental Control Life Support System (ECLSS) Equipment Rack, components of the Water Processor Assembly (WPA), Rack Interface Panel (RIP), Rack Power Switch (RPS), Area Smoke Detector (ASD), Avionics Air Assembly (AAA), and rack secondary structure. The WRS Rack #1 is fully compatible with the International Standard Payload Rack attachment mechanisms and envelopes.

Node 3 DESCRIPTION The Node 3 is a pressurized element used to supplement and in some cases replace the Habitation Modules functions for crew accommodations. The Node 3 will contain the ECLSS, Fecal Control System, and Avionics Racks.

INTERFACE RESPONSIBILITIES

RESPONSIBILITY FOR Water Recovery System Unless otherwise noted herein, Marshall Space Flight Center, under agreement with the ISS Program Office, has the responsibility for designing the WRS Rack #1 to the interface requirements herein.

RESPONSIBILITY FOR Node 3 Unless otherwise noted herein, Agenzia Spaziale Italiana (ASI) has the responsibility for designing the Node 3 to the interface requirements herein.

RESPONSIBILITY FOR interconnect cabling/tubing/connectors The Node 3 is responsible for providing interconnecting cabling/tubing/connectors to the rack utility interface panel. The WRS Rack #1 is responsible for providing rack utility interface panel connectors.

COORDINATE SYSTEMS

The coordinate system applicable to the Node 3 to WRS Rack #1 interface is as defined in SSP 41017, Part 2, paragraph 3.1.3.

engineering units, tolerances and conversions engineering units and tolerances Dimensions in this document are shown in the English (inch, pound, second) system of units followed by the equivalent SI (metric) value in parenthesis. Measurements may be verified in either system of units.

Tolerances Linear tolerances on English dimensions are as indicated in Table 3.1.4.1-1 Linear Tolerances. Linear tolerances on metric dimensions are derived from English measurements and tolerances as defined in ASTM E380, Standard Practice for Use of the International System of Units (SI) (The Modernized Metric System), section 4.5. Angular tolerances are ±0.1° on all angles unless otherwise stated.

Table 3.1.4.11 Linear Tolerances

English dimension
Implied tolerance (inches)
x.xx
+/- 0.030
x.xxx
+/- 0.010

INTERFACE REQUIREMENTS

WATER RECOVERY SYSTEM RACK #1 REQUIREMENTS

ENVELOPE REQUIREMENTS

The WRS Rack #1 shall comply with the envelopes defined in SSP 41017, Part 1, paragraph 3.2.1.1.1, except for the presence of the Rack Interface Panel specified in 3.2.1.3.1.

MASS PROPERTIES

MASS

The WRS Rack #1 shall comply with the mass requirements defined in SSP 41017, Part 1, paragraph 3.2.1.2.

CENTER OF MASS

Deleted.

STRUCTURAL/MECHANICAL ATTACHMENT

The structural/mechanical interface description shall be as defined in SSP 41017, Part 1, paragraph 3.2.1.3.

The WRS RACK #1 structural/mechanical interface is as defined in SSP 41017, Part 2, paragraphs 3.2 and 3.3.

Rack Interface Panel The WRS Rack #1 shall incorporate provisions for a rack interface panel for connection of utilities between WRS Rack #1 and Node 3. The interface plane is at the rack interface panel located on the WRS Rack #1 systems rack as shown in Figure 3.2.1.3-1 WRS Rack #1/Node 3 Rack Interface Plane. Figure 3.2.1.3-2 WRS Rack #1 Specific Panel Connector Locations, defines the rack interface panel layout.

Accessibility The WRS Rack #1 to Node 3 utility shall comply with the accessibility requirements of SSP 50005.

Figure 3.2.1.3-1 WRS Rack #1/Node 3 Rack Interface Plane

Notes:

· View is from front of Rack Interface Panel

· Dimensions indicate center point of connector with respect to the center of the panel

· All connector master keyways are in the 12:00 o’clock position

Notes:

· View is from front of Rack Interface Panel

· Dimensions indicate center point of connector with respect to the center of the panel

· All connector master keyways are in the 12:00 o’clock position

Figure 3.2.1.3-2 WRS Rack #1 Specific Panel Connector Locations

FLuid Interfaces Fire Suppressant The WRS Rack #1 shall receive fire suppressant via injection into the front panel of the rack at the location defined in Figure 3.2.1.4-1.

RECEIVE COOLANT

The WRS Rack #1 shall receive single-phase, moderate temperature loop water coolant from the Node 3 for active heat acquisition and transport.

WRS Rack #1 heat transport capability WRS Rack #1 moderate temperature loop HEAT LOAD The heat load rejected to the moderate temperature loop by the WRS Rack #1 shall not exceed 1066 watts during Process Mode and 551 watts during Standby Mode.

receive Coolant characteristics receive coolant specification The WRS Rack #1 shall receive coolant with the requirements of SSP 30573, Fluid Procurement and Use Control Specification.

receive coolant temperature The WRS Rack #1 shall receive moderate temperature coolant at 61 to 65 deg Fahrenheit (16 to 18.3 deg Celsius).

RECEIVE COOLANT PRESSURE

The WRS Rack #1 shall receive moderate temperature coolant at an operating pressure of 18 to 100 psia (124 to 690 kPa).

RECEIVE coolant Flow rate The WRS Rack #1 shall receive moderate temperature loop coolant at a minimum flow rate of 290 lb./hr.

Receive Coolant Interface Control Instrumentation and control of the moderate temperature cooling loop shall be located within the WRS Rack #1.

RECEIVE coolant quantity The WRS Rack #1 shall contain no more than 8.8 lbs. (4 kg) of water in its internal cooling loop for the moderate temperature loop.

RECEIVE coolant leakage rate The WRS Rack #1 maximum coolant leakage rate, for coolant received at the maximum pressure specified in paragraph 3.2.1.4.2.2.3, shall be 9E-3 scc/hr for the moderate temperature loop.

Receive Coolant connector The WRS Rack #1 shall receive coolant at the Rack Interface Panel via a “MT Water Supply” connector as defined in Table 3.2.1.4-2 Fluid Interface Connectors.

Table 3.2.1.4-2 Fluid Interface Connectors

Connection:
Category (1)
Keying (2)
QD Body Size
Rack Side Vendor Part Number (2)
Node 3 Side Vendor Part Number (2)
O2
9
F(180°)
3/8 in
2003-XX04X-G09F
2000-XX06X-G09F
Potable Water Return (4)
7
D(135°)
1/2 in
2003-XX12X-P07D
2000-XX08X-P07D
Potable Water Manual Container (4)
7
D(135°)
1/2 in
2003-XX12X-P07D
2000-XX08X-P07D (3)
Process Water Line A
7
F(195°)
1/2 in
2003-XX04X-W07F
2000-XX08X-W07F
Process Water Line B
7
G(225°)
1/2 in
2003-XX04X-W07G
2000-XX08X-W07G
Process Water Line C
7
H(255°)
1/2 in
2003-XX04X-W07H
2000-XX08X-W07H
Process Water Line D
7
I(285°)
1/2 in
2003-XX04X-W07I
2000-XX08X-W07I
MT Water Supply
6
B(75°)
1/2 in
2003-XX08X-T06B
2000-XX12X-T06B
MT Water Return
6
C(105°)
1/2 in
2003-XX08X-T06C
2000-XX12X-T06C

(1) Categories as defined in Boeing drawing 683-16348.

(2) Vendor part numbers and keying as defined by Symetrics drawing 200.

(3) Interface is Marshall Space Flight Center (MSFC) responsibility.

(4) Potable Water Return and Potable Water Manual Container connectors are functionally identical.

RETURN COOLANT

The WRS Rack #1 shall return moderate temperature coolant to the Node 3.

Return COOLANT CHARACTERISTICS Return COOLANT SPECIFICATIONS The return water coolant shall comply with the requirements of SSP 30573.

Return COOLANT TEMPERATURE The WRS Rack #1 shall return moderate temperature coolant at 61° to 120°F.

RETURN coolant pressure drop The WRS Rack #1 shall have a moderate temperature coolant pressure drop of 6.58 + 0.1 psid , at a flow rate of 300 lb/hr.

RETURN coolant cONNECTOR The WRS Rack #1 shall return coolant at the Rack Interface Panel via a “MT Water Return” connector as defined in Table 3.2.1.4-2 Fluid Interface Connectors.

SUPPLY potable water The WRS Rack #1 shall supply potable (product) water to the Node 3.

SUPPLY potable water Temperature The WRS Rack #1 shall supply potable water to the Node 3 at a temperature range of 65 to 90 deg Fahrenheit (18.3 to 32.2 deg Celsius).

SUPPLY potable water Pressure The WRS Rack #1 shall supply potable water to the Node 3 at a pressure range of 15 to 30 psig (104 to 207 kPa) (TBR).

SUPPLY potable water maximum design Pressure The WRS Rack #1 shall design to a maximum potable water pressure of 35 psig.

SUPPLY potable water Flow rate The WRS Rack #1 shall supply potable water to the Node 3 at a flow rate of 0 to 500 lb./hr.

SUPPLY potable water Interface control Instrumentation and controls of the potable water interface shall be located within the WRS Rack #1.

Supply Potable Water Quality The quality of the potable water supplied to the Node 3 by WRS Rack #1 shall be in accordance with SSP 50318 Table VI. Water Quality Requirements.

supply potable water connector The WRS Rack #1 shall supply potable water at the Rack Interface Panel via a “Potable Water Return” connector as defined in Table 3.2.1.4-2 Fluid Interface Connectors.

Supply potable water manual container connector The WRS Rack #1 shall supply potable water, for manual transfer container and for accommodated payloads, at the Rack Interface Panel via a “Potable Water Manual Container” connector as defined in Table 3.2.1.4-2 Fluid Interface Connectors.

Supply potable water sample port The WRS Rack #1 shall supply potable water via a sample port at the Rack Front Panel as depicted in Figure 3.2.1.4-1 and via the physical interface as defined in Figure 3.2.1.4-5.

WPA Process Water

a. The WRS Rack #1 shall supply WPA process water to the WRS Rack #2 via Process Water Line A in Node 3.

b. The WRS Rack #1 shall supply WPA process water to the WRS Rack #2 via Process Water Line B in Node 3.

c. The WRS Rack #1 shall receive WPA process water from the WRS Rack #2 via Process Water Line C in Node 3.

d. The WRS Rack #1 shall receive WPA process water from the WRS Rack #2 via Process Water Line D in Node 3.

WPA Process Water Temperature

a. The WRS Rack #1 shall supply WPA process water to the WRS Rack #2 via the Node 3 at a temperature range of 63 to 113 deg Fahrenheit (17.2 to 45 deg Celsius).

b. The WRS Rack #1 shall receive WPA process water from the WRS Rack #2 via the Node 3 at a temperature range of 63 to 113 deg Fahrenheit (17.2 to 45 deg Celsius).

WPA Process Water Pressure

a. The WRS Rack #1 shall supply WPA process water to the WRS Rack #2 via Process Water Line A in the Node 3 at a pressure range of 0 to 88 psig.

b. The WRS Rack #1 shall supply WPA process water to the WRS Rack #2 via Process Water Line B in the Node 3 at a pressure range of 0 to 3 psig.

c. The WRS Rack #1 shall receive WPA process water from the WRS Rack #2 via Process Water Line C in the Node 3 at a pressure range of 0 to 108 psig.

d. The WRS Rack #1 shall receive WPA process water from the WRS Rack #2 via Process Water Line D in the Node 3 at a pressure range of 0 to 75 psig.

WPA Process Water maximum design Pressure

a. The WRS Rack #1 shall supply WPA process water to the WRS Rack #2 via Process Water Line A in the Node 3 at a maximum pressure of 125 psig.

b. The WRS Rack #1 shall supply WPA process water to the WRS Rack #2 via Process Water Line B in the Node 3 at a maximum pressure of 85 psig.

c. The WRS Rack #1 shall receive WPA process water from the WRS Rack #2 via Process Water Line C in the Node 3 at a maximum pressure of 125 psig.

d. The WRS Rack #1 shall receive WPA process water from the WRS Rack #2 via Process Water Line D in the Node 3 at a maximum pressure of 125 psig.

WPA Process Water Maximum Pressure Drop

a. The maximum pressure drop in Process Water Line A in the Node 3 shall be 0.25 psid at a flow rate of 19 lb./hr. This pressure drop is for the Node supplied quick disconnects and plumbing.

b. The maximum pressure drop in Process Water Line B in the Node 3 shall be 0.25 psid at a flow rate of 19 lb./hr. This pressure drop is for the Node supplied quick disconnects and plumbing.

c. The maximum pressure drop in Process Water Line C in the Node 3 shall be 0.25 psid at a flow rate of 19 lb./hr. This pressure drop is for the Node supplied quick disconnects and plumbing.

d. The maximum pressure drop in Process Water Line D in the Node 3 shall be 0.25 psid at a flow rate of 19 lb./hr. This pressure drop is for the Node supplied quick disconnects and plumbing.

WPA Process Water Flow rate

a. The WRS Rack #1 shall supply WPA process water to the WRS Rack #2 via Line A in the Node 3 at a flow rate up to 20 lb./hr.

b. The WRS Rack #1 shall supply WPA process water to the WRS Rack #2 via Line B in the Node 3 at a flow rate up to 20 lb./hr.

c. The WRS Rack #1 shall receive WPA process water from the WRS Rack #2 via Line C in the Node 3 at a flow rate up to 20 lb./hr.

d. The WRS Rack #1 shall receive WPA process water from the WRS Rack #2 via Line D in the Node 3 at a flow rate up to 20 lb./hr.

WPA Process Water Interface control Instrumentation and controls of the WPA process water interface shall be located within both the WRS Rack #1 and WRS Rack #2.

WPA process water connectors The WRS Rack #1 shall exchange process water at the Rack Interface Panel via connectors “Process Water Line A”, “Process Water Line B”, “Process Water Line C” and “Process Water Line D” as defined in Table 3.2.1.4-2 Fluid Interface Connectors.

Supply Vent gas to Cabin Atmosphere The WRS Rack #1 shall supply the following vent gases to the Node 3 cabin atmosphere:

a. Waste Gas (O2, CO2, H2O vapor) contained within the rack to cabin dynamic air exchange

b. Oxygen Supply Vent gas to Cabin Atmosphere Temperature The WRS Rack #1 shall supply vent gases to the Node 3 at a temperature range of:

a. Waste Gas contained within the rack to cabin dynamic air exchange

b. Oxygen at 65 to 109 F (18.3 to 42.8 C) Supply Vent gas to Cabin Atmosphere Pressure The WRS Rack #1 shall supply vent gases to the Node 3 at a pressure of:

a. Waste Gas contained within the rack to cabin dynamic air exchange

b. Oxygen at 13.9 to 15.2 psia Supply Vent gas to Cabin Atmosphere Flow rate The WRS Rack #1 shall supply vent gases to the Node 3 at a flow rate of:

a. Waste Gas

i. Oxygen at 0 to 0.05 lb/hr

ii. Water vapor at 0 to 0.03 lb/hr

b. Oxygen at 0 to 0.2 lb./hr Supply Vent cabin gas to Cabin Atmosphere Interface control Instrumentation and controls of the vent cabin gas to cabin interface shall be located within the WRS Rack #1.

Supply Vent gas connector The rack shall vent gases and exchange cabin air through the rack front panel as depicted in Figure 3.2.1.4-1. Waste gas contained within the rack is exchanged with the cabin via dynamic air exchange as depicted in Figure 3.2.1.4-2 and Figure 3.2.1.4-3. Oxygen shall vent out the rack front panel through the fitting depicted in Figure 3.2.1.4-4.

Supply vent gas humidity The WRS Rack #1 shall supply waste gas to the Node 3 with a maximum dewpoint of 61 F (16.1 C).

Figure 3.2.1.4-1 WPA Interfaces with Rack faceplate

Figure 3.2.1.42 Cabin air inlet (detail a of figure 3.2.1.4-1)

Figure 3.2.1.43 Cabin air outlet (detail e of figure 3.2.1.4-1)

RACK DATUM –A-

B C

Figure 3.2.1.44 oxygen vent fitting (detail C of figure 3.2.1.4-1)

RACK DATUM –B-

B

Figure 3.2.1.45 Wrs rack #1 sample port (detail F of figure 3.2.1.4-1)

Receive OXYGEN The WRS Rack #1 shall receive oxygen from the Node 3.

Receive OXYGEN Temperature The WRS Rack #1 shall receive oxygen from the Node 3 at a temperature range of 60 to 113 deg Fahrenheit (17.2 to 45 deg Celsius).

Receive OXYGEN Pressure The WRS Rack #1 shall receive oxygen from the Node 3 at a pressure range of 90 to 135 psia. The nominal pressure range while the oxygen system is in use/flowing shall be 90 to 120 psia and while not in use/flowing is 110 to 135 psia.

Receive OXYGEN maximum design Pressure The WRS Rack #1 shall receive oxygen from the Node 3 at a maximum pressure of 200 psia.

Receive OXYGEN Flow rate The WRS Rack #1 shall receive oxygen from the Node 3 at a flow rate of 0.008 to 0.018 lb/hr.

Receive OXYGEN Interface control Instrumentation and controls of the cabin oxygen interface shall be located within the WRS Rack #1.

Receive OXYGEN connector The WRS Rack #1 shall receive oxygen at the Rack Interface Panel via an “Oxygen Supply” connector as defined in Table 3.2.1.4-2 Fluid Interface Connectors.

ELECTRICAL INTERFACES

RECEIVE POWER

The WRS Rack #1 shall receive power from the WRS Rack #2 via the Node 3.

a. The WRS Rack #1 electrical power requirements shall not exceed those presented in Table 3.2.1.5-1 Maximum Rack Power Input.

Table 3.2.1.51 Maximum Rack Power input from WRS Rack #2

WRS Rack #1

1779 Watts (startup)

The electrical power connector pin assignments are shown in Table 3.2.1.5-2 J2 Power Connector Description and Pin Assignments.

Table 3.2.1.52 J2 Power Connector Description and Pin Assignments CONNECTOR ID (J2 Receive Power)

Plug Part No. (NODE 3)
NATC06G21N11SN
Receptacle Part No. (WRS Rack #1)
NATC07T21N11PN
Insert Arrangement
21-11

J2 PIN FUNCTION TABLE

WRS RACK 1
NODE 3
Cont ID
Signal Function
EMC Class
AWG
Wire Type
AWG
Wire Type
Notes
A
NOT USED
B
NOT USED
C
NOT USED
D
120VDC_ 3.5A (ASD)
EO
20
TP
12
TP
SSQ 21656 or

MIL-DTL-27500

E
120VDC_3.5A RTN (ASD)
EO
20
TP
12
TP
SSQ 21656 or

MIL-DTL-27500

F
120VDC_3.5A (AAA)
EO
20
TP
12
TP
SSQ 21656 or

MIL-DTL-27500

G
120VDC_3.5A RTN (AAA)
EO
20
TP
12
TP
SSQ 21656 or

MIL-DTL-27500

H
120VDC_3.5A (WPA)
EO
16
TP
12
TP
SSQ 21656 or

MIL-DTL-27500

J
120VDC_3.5A RTN(WPA)
EO
16
TP
12
TP
SSQ 21656 or

MIL-DTL-27500

K
120VDC_12A (WPA)
EO
12
TP
12
TP
SSQ 21656 or

MIL-DTL-27500

L
120VDC_12A RTN (WPA)
EO
12
TP
12
TP
SSQ 21656 or

MIL-DTL-27500

POWER QUALITY

Power Quality is not defined at this interface. Power Quality at each of the loads within WRS Rack #1 is defined by SSP 30482, Electrical Power Specifications and Standards, Volume 1 for “Interface C”. Inrush current characteristics are defined in SSP 50314, Figure 3.2.2.5-1, “Inrush Current Characteristics”.

The maximum length of the cable that connects WRS Rack #2 connector J6 to WRS Rack #1 connector J2 shall be 18 feet (5.48 meters).

steady-state current The WRS Rack #1 steady state current requirements shall not exceed those listed in Table 3.2.1.5-3 Maximum Allowable Steady-State Current (116-126 Vdc).

Table 3.2.1.53 Maximum Allowable Steady-State Current (116-126 Vdc)

WRS Rack #1

11.15 Amps (continuous)

Supply Electrical Power The WRS Rack #1 shall supply power to select WRS Rack #2 Orbit Replacement Units (ORUs) via the Node 3 through RIP electrical lines J6, J7 and J8. The electrical power connector pin assignments and connectors are shown in the following tables:

Table 3.2.1.54 J6 Power Connector Description and Pin Assignments CONNECTOR ID (J6 Supply Power/ Exchange Data)

Plug Part No. (NODE 3)
NATC06G15N19PA
Receptacle Part No. (WRS Rack #1)
NATC07T15N19SA
Insert Arrangement
15-19

J6 PIN FUNCTION TABLE

WRS RACK 1
NODE 3
Cont ID
Signal Function
EMC Class
AWG
Wire Type
AWG
Wire Type
Notes
A
A210_PHASE1 B
EO
20
TST
20
TST
SSQ 21656 or

MIL-DTL-27500

B
NOT USED
C
A210_PHASE1 A
EO
20
TST
20
TST
SSQ 21656 or

MIL-DTL-27500

D
NOT USED
E
NOT USED
F
A210_HED1 A
ML
22
TS5C
22
TS5C
SSQ 21656 or

MIL-DTL-27500

G
A210_HED1 B
ML
22
TS5C
22
TS5C
SSQ 21656 or

MIL-DTL-27500

H
A210_HED1 C
ML
22
TS5C
22
TS5C
SSQ 21656 or

MIL-DTL-27500

J
NOT USED
K
NOT USED
L
A210_PHASE1 C
EO
20
TST
20
TST
SSQ 21656 or

MIL-DTL-27500

M
NOT USED
N
NOT USED
P
NOT USED
R
A210_MTR1 P15 VDC
HO
22
TS5C
22
TS5C
SSQ 21656 or

MIL-DTL-27500

S
NOT USED
T
NOT USED
U
A210_MTR1 15 RTN
HO
22
TS5C
22
TS5C
SSQ 21656 or

MIL-DTL-27500

V
NOT USED

Table 3.2.1.55 J7 Power Connector Description and Pin Assignments CONNECTOR ID (J7 Supply Power/ Exchange Data)

Plug Part No. (NODE 3)
NATC06G15N19PN
Receptacle Part No. (WRS Rack #1)
NATC07T15N19SN
Insert Arrangement
15-19

J7 PIN FUNCTION TABLE

WRS RACK 1
NODE 3
Cont ID
Signal Function
EMC Class
AWG
Wire Type
AWG
Wire Type
Notes
A
A210_PHASE2 B
EO
20
TST
20
TST
SSQ 21656 or

MIL-DTL-27500

B
NOT USED
C
A210_PHASE2 A
EO
20
TST
20
TST
SSQ 21656 or

MIL-DTL-27500

D
NOT USED
E
NOT USED
F
A210_HED2 A
ML
22
TS5C
22
TS5C
SSQ 21656 or

MIL-DTL-27500

G
A210_HED2 B
ML
22
TS5C
22
TS5C
SSQ 21656 or

MIL-DTL-27500

H
A210_HED2 C
ML
22
TS5C
22
TS5C
SSQ 21656 or

MIL-DTL-27500

J
NOT USED
K
NOT USED
L
A210_PHASE2 C
EO
20
TST
20
TST
SSQ 21656 or

MIL-DTL-27500

M
NOT USED
N
NOT USED
P
NOT USED
R
A210_MTR2 P15 VDC
HO
22
TS5C
22
TS5C
SSQ 21656 or

MIL-DTL-27500

S
NOT USED
T
NOT USED
U
A210_MTR2 15 RTN
HO
22
TS5C
22
TS5C
SSQ 21656 or

MIL-DTL-27500

V
NOT USED

Table 3.2.1.56 J8 Power Connector Description and Pin Assignments CONNECTOR ID (J8 Supply Power/ Exchange Data)

Plug Part No. (NODE 3)
NATC06G23N35PN
Receptacle Part No. (WRS Rack #1)
NATC07T23N35SN
Insert Arrangement
23-35

J8 PIN FUNCTION TABLE

WRS RACK 1
NODE 3
Cont ID
Signal Function
EMC Class
AWG
Wire Type
AWG
Wire Type
Notes
1
A210_HHLSW1 EXC
ML
22
TSP
22
TSP
SSQ 21656 or

MIL-DTL-27500

2
A210_HHLSW1 RTN
ML
22
TSP
22
TSP
SSQ 21656 or

MIL-DTL-27500

3
A211_VLV1 HI
EO
22
TSP
22
TSP
SSQ 21656 or

MIL-DTL-27500

4
A211_VLV1 RTN
EO
22
TSP
22
TSP
SSQ 21656 or

MIL-DTL-27500

5
NOT USED
6
NOT USED
7
A211_VLV3 HI
EO
22
TSP
22
TSP
SSQ 21656 or

MIL-DTL-27500

8
A211_VLV3 RTN
EO
22
TSP
22
TSP
SSQ 21656 or

MIL-DTL-27500

9
NOT USED
10
NOT USED
11
A210_SOL1 HI
EO
22
TSP
22
TSP
SSQ 21656 or

MIL-DTL-27500

12
A210_SOL1 RTN
EO
22
TSP
22
TSP
SSQ 21656 or

MIL-DTL-27500

13
A210_LLLSW1 EXC
ML
22
TSP
22
TSP
SSQ 21656 or

MIL-DTL-27500

14
A210_LLLSW1 RTN
ML
22
TSP
22
TSP
SSQ 21656 or

MIL-DTL-27500

15
A210_T2 HI
ML
22
TSP
22
TSP
SSQ 21656 or

MIL-DTL-27500

16
A210_T2 LO
ML
22
TSP
22
TSP
SSQ 21656 or

MIL-DTL-27500

17
NOT USED
18
NOT USED
19
A210_TSW2 HI
ML
22
TSP
22
TSP
SSQ 21656 or

MIL-DTL-27500

20
A210_TSW2 LO
ML
22
TSP
22
TSP
SSQ 21656 or

MIL-DTL-27500

21
A211_PIN3 A1
ML
22
TSP
22
TSP
SSQ 21656 or

MIL-DTL-27500

22
A211_PIN3 B1
ML
22
TSP
22
TSP
SSQ 21656 or

MIL-DTL-27500

23
A210_PIN3 A1
ML
22
TSP
22
TSP
SSQ 21656 or

MIL-DTL-27500

24
A210_PIN3 B1
ML
22
TSP
22
TSP
SSQ 21656 or

MIL-DTL-27500

25
A211_PIN1 A1
ML
22
TSP
22
TSP
SSQ 21656 or

MIL-DTL-27500

26
A211_PIN1 B1
ML
22
TSP
22
TSP
SSQ 21656 or

MIL-DTL-27500

27
NOT USED
28
NOT USED
29
NOT USED
30
A210_HHLSW1 HI
ML
22
TSP
22
TSP
SSQ 21656 or

MIL-DTL-27500

31
A210_HHLSW1 LO
ML
22
TSP
22
TSP
SSQ 21656 or

MIL-DTL-27500

32
A211_VLV2 HI
EO
22
TSP
22
TSP
SSQ 21656 or

MIL-DTL-27500

33
A211_VLV2 RTN
EO
22
TSP
22
TSP
SSQ 21656 or

MIL-DTL-27500

34
A210_VLV2 HI
EO
22
TSP
22
TSP
SSQ 21656 or

MIL-DTL-27500

35
A210_VLV2 RTN
EO
22
TSP
22
TSP
SSQ 21656 or

MIL-DTL-27500

36
A210_VLV3 HI
EO
22
TSP
22
TSP
SSQ 21656 or

MIL-DTL-27500

37
A210_VLV3 RTN
EO
22
TSP
22
TSP
SSQ 21656 or

MIL-DTL-27500

38
A210_LLLSW1 HI
ML
22
TSP
22
TSP
SSQ 21656 or

MIL-DTL-27500

39
A210_LLLSW1 LO
ML
22
TSP
22
TSP
SSQ 21656 or

MIL-DTL-27500

40
A210_T1 HI
ML
22
TSP
22
TSP
SSQ 21656 or

MIL-DTL-27500

41
A210_T1 LO
ML
22
TSP
22
TSP
SSQ 21656 or

MIL-DTL-27500

42
A210_PG1 HI
HO
22
TSP
22
TSP
SSQ 21656 or

MIL-DTL-27500

43
A210_PG1 LO
HO
22
TSP
22
TSP
SSQ 21656 or

MIL-DTL-27500

44
A210_PG2 HI
HO
22
TSP
22
TSP
SSQ 21656 or

MIL-DTL-27500

45
A210_PG2 LO
HO
22
TSP
22
TSP
SSQ 21656 or

MIL-DTL-27500

46
A210_PIN2 A1
ML
22
TSP
22
TSP
SSQ 21656 or

MIL-DTL-27500

47
A210_PIN2 B1
ML
22
TSP
22
TSP
SSQ 21656 or

MIL-DTL-27500

48
A211_PIN2 A1
ML
22
TSP
22
TSP
SSQ 21656 or

MIL-DTL-27500

49
A211_PIN2 B1
ML
22
TSP
22
TSP
SSQ 21656 or

MIL-DTL-27500

50
A212_PG1 HI
HO
22
TSP
22
TSP
SSQ 21656 or

MIL-DTL-27500

51
A212_PG1 LO
HO
22
TSP
22
TSP
SSQ 21656 or

MIL-DTL-27500

52
A210_HLSW1 EXC
ML
22
TSP
22
TSP
SSQ 21656 or

MIL-DTL-27500

53
A210_HLSW1 RTN
ML
22
TSP
22
TSP
SSQ 21656 or

MIL-DTL-27500

54
A210_HLSW1 HI
ML
22
TSP
22
TSP
SSQ 21656 or

MIL-DTL-27500

55
A210_HLSW1 LO
ML
22
TSP
22
TSP
SSQ 21656 or

MIL-DTL-27500

56
A210_LLSW1 EXC
ML
22
TSP
22
TSP
SSQ 21656 or

MIL-DTL-27500

57
A210_LLSW1 RTN
ML
22
TSP
22
TSP
SSQ 21656 or

MIL-DTL-27500

58
A210_LLSW1 HI
ML
22
TSP
22
TSP
SSQ 21656 or

MIL-DTL-27500

59
A210_LLSW1 LO
ML
22
TSP
22
TSP
SSQ 21656 or

MIL-DTL-27500

60
A211_QS1 EXC
HO
22
TS4C
22
TS4C
SSQ 21656 or

MIL-DTL-27500

61
A211_QS1 WPR
HO
22
TS4C
22
TS4C
SSQ 21656 or

MIL-DTL-27500

62
A211_QS1 REF
HO
22
TS4C
22
TS4C
SSQ 21656 or

MIL-DTL-27500

63
A211_QS1 RTN
HO
22
TS4C
22
TS4C
SSQ 21656 or

MIL-DTL-27500

64
A210_TSW1 HI
ML
22
TSP
22
TSP
SSQ 21656 or

MIL-DTL-27500

65
A210_TSW1 LO
ML
22
TSP
22
TSP
SSQ 21656 or

MIL-DTL-27500

66
A211_QS2 EXC
HO
22
TS4C
22
TS4C
SSQ 21656 or

MIL-DTL-27500

67
A211_QS2 WPR
HO
22
TS4C
22
TS4C
SSQ 21656 or

MIL-DTL-27500

68
A211_QS2 REF
HO
22
TS4C
22
TS4C
SSQ 21656 or

MIL-DTL-27500

69
A211_QS2 RTN
HO
22
TS4C
22
TS4C
SSQ 21656 or

MIL-DTL-27500

70
A211_LS1_P15 VDC
HO
22
TST
22
TST
SSQ 21656 or

MIL-DTL-27500

71
A211_LS1_15 RTN
HO
22
TST
22
TST
SSQ 21656 or

MIL-DTL-27500

72
A211_LS1_N15 VDC
HO
22
TST
22
TST
SSQ 21656 or

MIL-DTL-27500

73
A211_LS1 HI
HO
22
TSP
22
TSP
SSQ 21656 or

MIL-DTL-27500

74
A211_LS1 LO
HO
22
TSP
22
TSP
SSQ 21656 or

MIL-DTL-27500

75
A212_CS1 HI
HO
22
TSP
22
TSP
SSQ 21656 or

MIL-DTL-27500

76
A212_CS1 LO
HO
22
TSP
22
TSP
SSQ 21656 or

MIL-DTL-27500

77
A212_CS1_P15 VDC
HO
22
TST
22
TST
SSQ 21656 or

MIL-DTL-27500

78
A212_CS1_15 RTN
HO
22
TST
22
TST
SSQ 21656 or

MIL-DTL-27500

79
A212_CS1_N15 VDC
HO
22
TST
22
TST
SSQ 21656 or

MIL-DTL-27500

80
NOT USED
81
NOT USED
82
NOT USED
83
NOT USED
84
NOT USED
85
NOT USED
86
NOT USED
87
NOT USED
88
NOT USED
89
NOT USED
90
NOT USED
91
NOT USED
92
NOT USED
93
NOT USED
94
NOT USED
95
NOT USED
96
NOT USED
97
NOT USED
98
NOT USED
99
NOT USED
100
NOT USED

Power Connectors

a. The WRS Rack #1 shall receive power at the rack interface panel via a “J2 - “ connector as specified in SSQ 21635 and defined in Table 3.2.1.5-2 J2 Power Connector Description and Pin Assignments.

b. The WRS Rack #1 shall supply power and exchange data at the rack interface panel via connectors “J6”, “J7”, and “J8” as specified in SSQ 21635 and defined in Table 3.2.1.5-4 J6 Power Connector Description and Pin Assignments, Table 3.2.1.5-5 J7 Power Connector Description and Pin Assignments, and Table 3.2.1.5-6 J8 Power Connector Description and Pin Assignments.

Command and Data Handling (C&DH) INTERFACES The following non-1553B, WRS components shall exchange data with the Node 3 in accordance with SSP 30261:002:

a. Avionics Air Assembly

b. Maintenance Switch Assembly

c. Area Smoke Detector The interface is at the rack interface panel shown in Figure 3.2.1.3-1 WRS Rack #1/Node 3 Rack Interface Plane. The hardwire data connector pin assignments are shown in Table 3.2.1.6-1 J3 Hardwire Data Connector Description and Pin Assignments.

The WRS Rack #1 to Node 3, non-1553B hardwire cables shall be less than 60 feet in length.

Table 3.2.1.61 J3 Hardwire Data Connector Description and Pin Assignments CONNECTOR ID (J3 Hardwire Data)

Plug Part No. (NODE 3)
NATC06G15N35PB
Receptacle Part No. (WRS Rack #1)
NATC07T15N35SB
Insert Arrangement
15-35

J3 PIN FUNCTION TABLE

WRS Rack # 1
NODE 3
Cont ID
Signal Function
EMC Class
AWG
Wire Type
AWG
Wire Type
Notes
1
NOT USED
2
NOT USED
3
NOT USED
4
NOT USED
5
NOT USED
6
NOT USED
7
NOT USED
8
NOT USED
9
NOT USED
10
NOT USED
11
NOT USED
12
NOT USED
13
NOT USED
14
NOT USED
15
NOT USED
16
NOT USED
17
NOT USED
18
SMOKE DETECTOR SCATTER +
ML
22
TSP
22
TSP
SSQ21656 or MIL-DTL-27500
19
SMOKE DETECTOR SCATTER -
ML
22
TSP
22
TSP
SSQ21656 or MIL-DTL-27500
20
AAA ENABLE CMD +
HO
22

TP

22
TP
SSQ21656 or MIL-DTL-27500
21
AAA ENABLE CMD -
HO
22

TP

22
TP
SSQ21656 or MIL-DTL-27500
22
AAA FLOW TEMP1 MEAS +
HO
22
TSP
22
HO/TSP
SSQ21656 or MIL-DTL-27500
23
AAA FLOW TEMP1 MEAS -
HO
22
TSP
22
HO/TSP
SSQ21656 or MIL-DTL-27500
24
AAA FLOW TEMP2 MEAS +
HO
22
TSP
22
HO/TSP
SSQ21656 or MIL-DTL-27500
25
AAA FLOW TEMP2 MEAS -
HO
22
TSP
22
HO/TSP
SSQ21656 or MIL-DTL-27500
26
AAA SPEED CMD +
ML
22
TSP
22
TSP
SSQ21656 or MIL-DTL-27500
27
AAA SPEED CMD -
ML
22
TSP
22
TSP
SSQ21656 or MIL-DTL-27500
28
AAA SPEED FEEDBACK +
ML
22
TSP
22
TSP
SSQ21656 or MIL-DTL-27500
29
AAA SPEED FEEDBACK -
ML
22
TSP
22
TSP
SSQ21656 or MIL-DTL-27500
30
RPS LED ENABLE +
HO
22
TP
22
TP
SSQ21656 or MIL-DTL-27500
31
RPS LED ENABLE -
HO
22
TP
22
TP
SSQ21656 or MIL-DTL-27500
32
SMOKE DET OBSCURATION +
ML
22
TSP
22
TSP
SSQ21656 or MIL-DTL-27500
33
SMOKE DET OBSCURATION -
ML
22
TSP
22
TSP
SSQ21656 or MIL-DTL-27500
34
SMOKE DET BIT ENABLE +
HO
22
TSP
22
TP
SSQ21656 or MIL-DTL-27500
35
SMOKE DET BIT ENABLE -
HO
22
TSP
22
TP
SSQ21656 or MIL-DTL-27500
36
RPS SWITCH POS +
HO
22
TP
22
TP
SSQ21656 or MIL-DTL-27500
37
RPS SWITCH POS -
HO
22
TP
22
TP
SSQ21656 or MIL-DTL-27500

mil-std-1553B interface The following WRS Rack #1 to Node 3 data interface shall be provided:

a. Water Processor Firmware Controller interface on two separate, bi-directional stubs.

The 1553B data interfaces are at the rack interface panel shown in Figure 3.2.1.3-2 WRS Rack #1 Specific Panel Connector Locations. The 1553B data connector pin assignments are shown in Table 3.2.1.6-2 J4 1553B A Data Connector Description and Pin Assignments and in Table 3.2.1.6-3 J5 1553B B Data Connector Description and Pin Assignments.

Table 3.2.1.62 J4 1553B A Data Connector Description and Pin Assignments

CONNECTOR ID (J4 1553B A)

Plug Part No. (NODE 3)
NATC06G13N35PN
Receptacle Part No. (WRS Rack #1)
NATC07T13N35SN
Insert Arrangement
13-35

J4 PIN FUNCTION TABLE

WRS RACK 1
NODE 3
Cont ID
Signal Function
EMC Class
AWG
Wire Type
AWG
Wire Type
Notes
1
NOT USED
2
NOT USED
3
NOT USED
4
NOT USED
5
NOT USED
6
NOT USED
7
NOT USED
8
NOT USED
9
NOT USED
10
NOT USED
11
NOT USED
12
NOT USED
13
NOT USED
14
NOT USED
15
NOT USED
16
LB SYS-FLY-2 A HI
RF
22
TSP
22
TSP
WPA NOD3D5

SSQ21655

17
LB SYS-FLY-2 A LO
RF
22
TSP
22
TSP
WPA NOD3D5

SSQ21655

18
NOT USED
19
NOT USED
20
NOT USED
21
NOT USED
22
NOT USED

Table 3.2.1.63 J5 1553B B Data Connector Description and Pin Assignments

CONNECTOR ID (J5 1553B B)

Plug Part No. (NODE 3)
NATC06G13N35PA
Receptacle Part No. (WRS Rack #1)
NATC07T13N35SA
Insert Arrangement
13-35

J5 PIN FUNCTION TABLE

WRS RACK 1
NODE 3
Cont ID
Signal Function
EMC Class
AWG
Wire Type
AWG
Wire Type
Notes
1
NOT USED
2
NOT USED
3
NOT USED
4
NOT USED
5
NOT USED
6
NOT USED
7
NOT USED
8
NOT USED
9
NOT USED
10
NOT USED
11
NOT USED
12
NOT USED
13
NOT USED
14
NOT USED
15
NOT USED
16
LB SYS-FLY-2 B HI
RF
22
TSP
22
TSP
WPA NOD3D5

SSQ21655

17
LB SYS-FLY-2 B LO
RF
22
TSP
22
TSP
WPA NOD3D5

SSQ21655

18
NOT USED
19
NOT USED
20
NOT USED
21
NOT USED
22
NOT USED

respond to input amplitude When receiving addressed messages with MIL-STD-1553B defined waveforms at the Node 3 interface, the WRS Rack #1 shall provide response message in MIL-STD-1553B format.

1553B bus signal characteristics The WRS Rack #1 to Node 3 data interface signal characteristics shall be in accordance with MIL-STD-1553B.

1553B bus coupling

a. The WRS Rack #1 to Node 3 data interfaces shall be transformer coupled, on the Node 3 side of the Interface, in accordance with MIL-STD-1553B.

b. The WRS Rack #1 1553B bus stub length shall be less than 10.0 ft.

terminal operations The WRS Rack #1 components with software shall respond as a remote terminal to the Node 3 bus controller in accordance with MIL-STD-1553B.

1553B bus interface functions The WRS Rack #1 shall provide the MIL-STD-1553B interface capability defined in paragraph 3.2.1.7 herein.

C&DH Connectors

a. The WRS Rack #1 shall exchange non-1553B data at the rack interface panel via a “J3-Hardwire” connector as specified in SSQ 21635 defined in Table 3.2.1.6-1 J3 Hardwire Data Connector Description and Pin Assignments.

b. The WRS Rack #1 shall interface with the Node 3 1553B bus at the rack interface panel via a “J4-1553B A” connector and a “J5-1553B B” connector as specified in SSQ 21635 and defined in Table 3.2.1.6-2 J4 1553B A Data Connector Description and Pin Assignments and Table 3.2.1.6-3 J5 1553B B Data Connector Description and Pin Assignments.

DELETED

Time distribution Not applicable.

SOFTWARE INTERFACES

WRS Rack #1 software interfaces shall be as defined in:

a. SSP 50405-07, Software Interface Control Document Hub Control Zone (HCZ) Multiplexer/Demultiplexer (MDM) to International Space Station (ISS) Book 7 Water Processor Assembly (WPA) Interface environments WRS Rack #1 Bonding Interface The WRS Rack #1 shall provide a bonding receptacle in accordance with SSP 41017, part 1, paragraphs 3.2.1.3.4 and 3.2.2.3.5, and SSP 41017, part 2, paragraph 3.2.1.

STRUCTURAL LOADS

The WRS Rack #1 shall withstand structural loads as specified in SSP 41017, Part 1, paragraph 3.2.1.4.3, without loss of functionality as defined herein.

Acceleration The WRS Rack #1 shall withstand launch and landing accelerations as defined in SSP 41017, Part 1, paragraph 3.2.1.4.2, without loss of functionality as defined herein.

vibroacoustics The WRS Rack #1 shall withstand launch and landing vibroacoustics as defined in SSP 41017, Part 1, paragraph 3.2.1.4.1, without loss of functionality as defined herein.

cabin air The WRS Rack #1 shall have dynamic cabin air exchange with the Node 3 to facilitate the vent requirements of paragraph 3.2.1.4.6. Figure 3.2.1.4-2 and Figure 3.2.1.4-3 define the physical interfaces on the rack front panel through which air is exchanged between the rack and Node 3.

cabin air CHARACTERISTICS cabin air temperature Receive cabin air temperature The WRS Rack #1 shall receive cabin air from the Node 3 at a temperature range of 63 to 85°F (17.2 to 29.4C°).

Supply cabin air temperature The WRS Rack #1 shall supply cabin air to the Node 3 at a temperature range of 63 to 85°F (17.2 to 29.4C°).

cabin air pressure receive cabin air pressure The WRS Rack #1 shall receive cabin air from the Node 3 at a pressure between 13.9 to 15.2 psia.

supply cabin air pressure The WRS Rack #1 shall supply cabin air to the Node 3 at a pressure between 13.9 to 15.2 psia.

cabin air humidity receive cabin air humidity The WRS Rack #1 shall receive cabin air from the Node 3 with a dew…

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