SSP_50309_Part_2.pdf

PDF 271 KB Posted Oct 31, 2019

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

About this file

Written by GovTribe AI · Dec 28, 2023

This is a summary of a federal contract solicitation for a Human Space Flight Technical Integration Contract. NASA/JSC is seeking proposals for technical integration services to support human space flight programs. The total small business set-aside solicitation is expected to be released on November 1st, with proposals due December 11th. The NAICS code is 541715 with a size standard of 1,250 employees. All responsible sources may submit an offer which will be considered by the agency. Interested parties should monitor the listed websites for the solicitation and any amendments. Questions must be submitted in writing prior to the response date.

From the source

SSP 50309 Part 2

View the file

Other files for this federal contract opportunity

Other files attached to Human Space Flight Technical Integration Contract (HSFTIC), newest first.
File	Type	Posted
FRFP Industry Questions and Responses 120419.pdf	PDF	Dec 4, 2019
HSFTIC L Instructions 11.22.19 FRFP-2.docx	DOCX document	Nov 22, 2019
Attachment L-7 Cost Estimating Wookbook 11.21.19 FRFP-2.xlsx	XLSX spreadsheet	Nov 22, 2019
SF30 - RFP - Amendment 2.pdf	PDF	Nov 22, 2019
Attachment L-6 EPM Workbook 11.21.19 FRFP-2.xlsx	XLSX spreadsheet	Nov 22, 2019
Attachment L-6 EPM Workbook MOD FRFP-1.xlsx	XLSX spreadsheet	Nov 20, 2019
80JSC019R0023 HSFTIC RFP with MOD FRFP-1.docx	DOCX document	Nov 20, 2019
HSFTIC Pre-Proposal Conference - Posting.pdf	PDF	Nov 19, 2019
Attachment_L-7_Cost_Estimating_Workbook.xlsx	XLSX spreadsheet	Nov 1, 2019
80JSC019R0023_Request_for_Proposal.pdf	PDF	Nov 1, 2019
APA_Style_Website_Ref.pptx	PPTX presentation	Oct 31, 2019
SSP_50821.doc	DOC document	Oct 31, 2019
CR_16052_ATTA_SSP_54353_54354_Baseline.docx	DOCX document	Oct 31, 2019
MD_106_RB_FINAL.docx	DOCX document	Oct 31, 2019
MD_1036_RA_FINAL_PIP_Charter.docx	DOCX document	Oct 31, 2019
SSP_50869-Rev_A.docx	DOCX document	Oct 31, 2019
SSP-57003_Rev_L.docx	DOCX document	Oct 31, 2019
MD_1054_PSCB_Charter.pdf	PDF	Oct 31, 2019
SSP_30234-RevH.docx	DOCX document	Oct 31, 2019
SSP_42007-Part_1-RevK.pdf	PDF	Oct 31, 2019
SSP_50318_RevJ.docx	DOCX document	Oct 31, 2019
SSP_41162BA.pdf	PDF	Oct 31, 2019
SSP41148_IRN.pdf	PDF	Oct 31, 2019
BASEPLATE-Mobile_Back-1.png	PNG image	Oct 31, 2019
SSP_50908-Baseline.docx	DOCX document	Oct 31, 2019
CCT-REQ-1130_Rev_F.docx	DOCX document	Oct 31, 2019
50104a.pdf	PDF	Oct 31, 2019
SSP-50136_RevA.doc	DOC document	Oct 31, 2019
SSP_50420-HTV1-Baseline.docx	DOCX document	Oct 31, 2019
Applicable_1.zip	ZIP file	Oct 31, 2019
OrionProgramOrg.pdf	PDF	Oct 31, 2019
SSP_42004_Part_2-Update_to_Cover.pdf	PDF	Oct 31, 2019
SSP_50333-RevH.docx	DOCX document	Oct 31, 2019
SSP_50406_Rev_B_.doc	DOC document	Oct 31, 2019
MD_1034_RA_FINAL_2__RICB_Charter.docx	DOCX document	Oct 31, 2019
SSP_42004_Part_1_Revision_L.docx	DOCX document	Oct 31, 2019
SSP_50128-C3.doc	DOC document	Oct 31, 2019
GRA_for_Gateway.xlsx	XLSX spreadsheet	Oct 31, 2019
SSP_41140_P1_RF_final.pdf	PDF	Oct 31, 2019
SSP_50182.RTF	RTF text file	Oct 31, 2019
41004P1_H-1.pdf	PDF	Oct 31, 2019
SSP_50627-RevA.docx	DOCX document	Oct 31, 2019
SSP-50264.doc	DOC document	Oct 31, 2019
19AA0613D_MAPI_Abstract_Blue_Book_Rev_EE.pdf	PDF	Oct 31, 2019
SSP_42000-RevU.docx	DOCX document	Oct 31, 2019
SSP50251P2.pdf	PDF	Oct 31, 2019
Applicable_2.zip	ZIP file	Oct 31, 2019
SSP_57000_Revision_S.docx	DOCX document	Oct 31, 2019
DRAFT_HSFTIC_Cover_Letter.pdf	PDF	Aug 16, 2019
Draft_HSFTIC_Request_for_Proposal.pdf	PDF	Aug 16, 2019

Show all 50

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

On GovTribe

Work with this file on GovTribe

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

Try for free Login

Text version

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

SSP 50309, Part 2

National Aeronautics and Space Administration International Space Station Alpha Program Johnson Space Center Houston, Texas Contract No. NAS15–10000 (DR VE06)

International Space Station Program

May 19, 1999

”TYPE 3 DOCUMENT – FOR INFORMATION,

SURVEILLANCE, REVIEW OR MANAGEMENT

CONTROL”.

Node Element 3 to Habitation Module Element Interface Control Document, Part 2

SSP 50309, Part 2 May 19, 1999 ii

REVISION AND HISTORY PAGE

REV. DESCRIPTION PUB.

DATE

– Baseline Issue reference SSCBD 002807, Effective 10/13/1999 09/21/01

The following IRN number has been cancelled. This IRN was never created and will never be released. The IRN has been cancelled due to the incorporation of it into the basic (baseline) revision of this document.

IRN 0001 SSCN 002820 (Administrative Cancellation)

ERU: /s/ M. Hehn 09/21/01 iii

PREFACE

The Node 3 to Habitation Module Interface Control Document (ICD) defines the physical, functional, and environmental interfaces between the Node 3 and the Habitation modules for the on–orbit interfaces.

The contents of this document are intended to be consistent with the task and products to be prepared by the International Space Station (ISS) Program Partners as defined in SSP 41000, International Space Station System Specification. This ICD shall be implemented on all new ISS Program activities and shall be included in any existing contracts through contract changes. This document is under the control of the Interface Control Working Group (ICWG) as described in

SSP 30459.

/s/Tommy Holloway 2/15/07

Tommy Holloway Date

NASA Program Manager

International Space Station iv

NASA/ASI

INTERNATIONAL SPACE STATION PROGRAM

NODE 3 TO HABITATION MODULE INTERFACE CONTROL DOCUMENT

MAY 19, 1999

CONCURRENCE

NASA ICWG Chairman Ralph A. Grau

Print Name

/s/Ralph A. Grau 02/06/01

Signature Date

ASI ICWG Chairman Maria Cristina Falvella

Print Name

/s/Maria Cristina Falvella 12/20/00

Signature Date

Alenia ICWG Chairman Alessandro Bellomo

Print Name

/s/A. Ballomo 7/13/99

Signature Date

Boeing Houston Peter Wells

Print Name

/s/Peter Wells 7/7/99

Signature Date

Boeing Huntington Beach N/A

Print Name

N/A N/A

Signature Date

DQA Freddie G. Young

Print Name

/S/Freddie G. Young 02/06/01

Signature Date v

INTERNATIONAL SPACE STATION PROGRAM

NODE 3 TO HABITATION MODULE INTERFACE CONTROL DOCUMENT

MAY 19, 1999

CONCURRENCE

NASA/ASI

ÁÁÁÁÁÁÁÁÁ

Alenia ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

/s/Walter Cugno ÁÁÁ

ÁÁÁ

ÁÁÁÁ

7/14/99

ÁÁÁÁÁÁÁÁÁ

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Walter Cugno ÁÁÁ

ÁÁÁ

ÁÁÁÁ

Date

ÁÁÁÁÁÁÁÁÁ

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁ

ÁÁÁÁ

ÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁÁÁÁÁÁÁ

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁ

ÁÁÁÁ

ÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁÁÁÁÁÁÁ

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁ

ÁÁÁÁ

ÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁÁÁÁÁÁÁ

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁ

ÁÁÁÁ

ÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁÁÁÁÁÁÁ

ASI ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

/s/Andrea Lorenzoni ÁÁÁ

ÁÁÁ

ÁÁÁÁ

12/20/00

ÁÁÁÁÁÁÁÁÁ

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Andrea Lorenzoni ÁÁÁ

ÁÁÁ

ÁÁÁÁ

Date

ÁÁÁÁÁÁÁÁÁ

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁ

ÁÁÁÁ

ÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁÁÁÁÁÁÁ

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁ

ÁÁÁÁ

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁÁÁÁÁÁÁ

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁ

ÁÁÁÁ

ÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁÁÁÁÁÁÁNASA–MSFC

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ/s/Robert Crumbley

ÁÁÁ

ÁÁÁÁ

ÁÁÁÁ7/15/99ÁÁÁÁÁÁÁÁÁ

ÁÁÁÁÁÁÁÁÁ

ÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁÁ

Robert Crumbley

ÁÁÁ

ÁÁÁÁ

Date vi

INTERNATIONAL SPACE STATION PROGRAM

NODE 3 TO HABITATION MODULE

INTERFACE CONTROL DOCUMENT

MAY 19, 1999

LIST OF CHANGES

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

SSCBD ENTRY DATE PARAGRAPH TITLE

TABLE(S)

FIGURE(S)

APPENDIX

vii

TABLE OF CONTENTS

PARAGRAPH PAGE

1.0 INTRODUCTION 1 - 1

1.1 PURPOSE AND SCOPE 1 - 1

1.2 PRECEDENCE 1 - 1

1.3 DELEGATION OF AUTHORITY 1 - 1

2.0 DOCUMENTS 2 - 1

2.1 APPLICABLE DOCUMENTS 2 - 1

2.2 REFERENCE DOCUMENTS 2 - 1

3.0 INTERFACE DEFINITION 3 - 1

3.1 GENERAL DESCRIPTION 3 - 1

3.1.1 INTERFACE DESCRIPTION 3 - 1

3.1.2 INTERFACE RESPONSIBILITIES 3 - 1

3.1.3 ENGINEERING UNITS AND TOLERANCES 3 - 3

3.1.3.1 ENGINEERING UNITS 3 - 3

3.1.3.2 CONVERSIONS AND TOLERANCES 3 - 3

3.1.3.3 TOLERANCE 3 - 3

3.2 INTERFACES 3 - 4

3.2.1 GENERAL 3 - 4

3.2.2 UTILITY PENETRATIONS 3 - 4

3.3 FLUID INTERFACES 3 - 4

3.4 ELECTRICAL INTERFACES 3 - 4

3.4.1 ELECTRICAL BONDING 3 - 5

3.4.2 SOFTWARE INTERFACES 3 - 5

FIGURES

3.1.1–1 ON–ORBIT MATED CONFIGURATION OF NODE 3 TO HAB 3 - 2

3.2.2–1 UTILITY PENETRATION LAYOUT OF NODE 3 PORT INTERNAL BULKHEAD

LOOKING TOWARD THE HAB 3 - 6

3.2.2–2 UTILITY PENETRATION LAYOUT OF HAB STARBOARD EXTERNAL

BULKHEAD LOOKING FROM THE NODE 3 - 7

3.2.2–3 PENETRATION DETAILS FOR FEEDTHROUGHS 3–10

3.2.2–3 PENETRATION DETAILS FOR FEEDTHROUGHS (CONTINUED) 3–11

3.3–1 NODE 3 TO HAB GENERIC FLUID UTILITY INTERFACE 3–12

3.3–2 INTERFACE DETAIL FOR IMV SUPPLY AND RETURN 3–13

3.3–3 THREADED FEEDTHROUGH ASSEMBLY INTERFACE DETAILS 3–14

3.3–4 SELF–SEALING FLUID QUICK DISCONNECT ASSEMBLY INTERFACE

DETAIL NODE 3 3–15

3.3–5 NON SELF–SEALING QUICK DISCONNECT FEEDTHROUGH ASSEMBLY

INTERFACE DETAIL 3–16

3.4–1 NODE 3 TO HAB GENERIC ELECTRICAL UTILITY INTERFACE 3–17

viii

PARAGRAPH PAGE

3.4–2 DETAILED ELECTRICAL DESCRIPTION OF NODE BULKHEAD J83 AND

HAB BULKHEAD J14 3–18

3.4–3 DETAILED ELECTRICAL DESCRIPTION OF NODE BULKHEAD J85 AND

HAB BULKHEAD J12 3–19

3.4–4 DETAILED ELECTRICAL DESCRIPTION OF NODE BULKHEAD J125 AND

HAB BULKHEAD J2 3–24

3.4–5 DETAILED ELECTRICAL DESCRIPTION OF NODE BULKHEAD J128 AND

HAB BULKHEAD J3 3–25

3.4–6 DETAILED ELECTRICAL DESCRIPTION OF NODE BULKHEAD J120 AND

HAB BULKHEAD J20 3–31

3.4–7 DETAILED ELECTRICAL DESCRIPTION OF NODE BULKHEAD J123 AND

HAB BULKHEAD J23 3–32

3.4–8 DETAILED ELECTRICAL DESCRIPTION OF NODE BULKHEAD J126 AND

HAB BULKHEAD J22 3–33

3.4–9 DETAILED ELECTRICAL DESCRIPTION OF NODE BULKHEAD J124 AND

HAB BULKHEAD J24 3–34

3.4.1–1 NODE 3 TO HAB ELECTRICAL BONDING 3–35

TABLES

3.1.2–1 NODE 3 TO HAB INTERFACE HARDWARE

(JUMPER ASSEMBLIES) RESPONSIBILITIES 3 - 3

3.1.3.3–1 LINEAR TOLERANCES 3 - 4

3.2.2–1 FLUID INTERFACE DETAIL DEFINITION 3 –8

3.2.2–2 ELECTRICAL INTERFACE DETAIL DEFINITION 3 –9

APPENDIX

A ABBREVIATIONS AND ACRONYMS A – 1

B ISSUE LIST FOR SSP 50309 B – 1

1 - 1

1.0 INTRODUCTION

1.1 PURPOSE AND SCOPE

The purpose of this document is to provide definition of the utility interface design between Node Element 3 (Node 3) and the Habitation Module Element (HAB).

The scope of this document is limited to the utility interfaces between Node 3 and the HAB.

1.2 PRECEDENCE

Not applicable.

1.3 DELEGATION OF AUTHORITY

The responsibility for assuring the definition, control, and implementation of the interfaces identified in this document is vested with the NASA ISS Program Office and the Italian Space Agency (ASI). This document shall be formally approved and controlled in accordance with the provisions of SSP 30459, ISS Interface Plan, and jointly signed by NASA and ASI. The NASA ISS Prime Contractor and the ASI Prime Contractor are participants in the development of this

ICD.

1 - 2

(This Page Intentionally Blank)

2 - 1

2.0 DOCUMENTS

2.1 APPLICABLE DOCUMENTS

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

SSP 30245 Space Station Electrical Bonding Requirements Revision D, (reference paragraphs ) DCNs 004, 005 4 June 1998

SSP 41004 Common Berthing Mechanism to Pressurized Elements Interface Control Document

SSP 41148 Active Common Berthing Mechanism (ACBM) to Passive Common Berthing Mechanism (PCBM) Interface Control Document

SSP 41175 Station Management and Control Computer to ISSA Interface Control Document

SSP 41176 Power Management and Control Computer to ISSA Interface Control Document

SSP 41178 Internal MDM Computer to ISSA Interface Control Document

SSP 42003 USOS to MSS Interface Control Document

2.2 REFERENCE DOCUMENTS

SSP 30459 International Space Station Interface Control Plan

2 - 2

3 - 1

3.0 INTERFACE DEFINITION

3.1 GENERAL DESCRIPTION

3.1.1 INTERFACE DESCRIPTION

The Node 3 to HAB mated on–orbit configuration is shown in Figure 3.1.1–1. The structural and mechanical interface is at the plane between the Active Common Berthing Mechanism (ACBM) connected to Node 3, and the Passive Common Berthing Mechanism (PCBM) connected to the HAB as documented in SSP 41148. The interface between the Node 3 and the HAB to the CBM is documented in SSP 41004. Utility interface planes exist at the bulkhead of each element and are documented herein. The utility interfaces between Node 3 and the HAB are interconnected using bulkhead connections.

3.1.2 INTERFACE RESPONSIBILITIES

Responsibilities for the element interfaces are:

ASI/Alenia:

• Development of Node 3 structural assembly

• Installation of fluid and electrical feedthroughs in the Node 3 bulkhead

• Vestibule outfitting

NASA:

• Development of HAB structural assembly

• Outfitting of HAB assembly

• Complete integration of HAB assembly

The quantities, development responsibility and manifesting responsibility is listed in Table 3.1.2–1.

3 - 2

HAB

UTILITY I/F PLANE ACBM

PCBM

NADIR

STARBOARD

PORT

AFT

NODE 3

ZENITH

STARBOARD

FOR STRUCTURAL/MECHANICAL INTERFACE BETWEEN NODE 3/HAB REFER TO

SSP 41004 AND SSP 41148

NOTE:

STRUCTURAL

INTERFACE

FIGURE 3.1.1–1 ON–ORBIT MATED CONFIGURATION OF NODE 3 TO HAB

3 - 3

TABLE 3.1.2–1 NODE 3 TO HAB INTERFACE HARDWARE

(JUMPER ASSEMBLIES) RESPONSIBILITIES

Node 3 to HAB Interface

NASA

Supplied ASI/Alenia Supplied Quantity

Jumper Manifest

Responsibility

Interface Node 3 HAB

PRIMARY AVIONIC X 2 X

REDUNDANT AVIONIC X 3 X

INTERMODULE AIR

RETURN

X 1 X

INTERMODULE AIR SUPPLY X 1 X

WASTE WATER X 1 X

ATMOSPHERE MONITOR X 1 X

POTABLE WATER X 1 X

NITROGEN X 1 X

OXYGEN X 1 X

ELECTRICAL POWER X 2 X

LTL SUPPLY X 1 X

LTL RETURN X 1 X

MTL SUPPLY X 1 X

MTL RETURN X 1 X

NITROGEN RECHARGE X 1 X

OXYGEN RECHARGE X 1 X

3.1.3 ENGINEERING UNITS AND TOLERANCES

3.1.3.1 ENGINEERING UNITS

Dimensions shown in this document are in the English (inch, pound, second) system of units followed by the equivalent SI (metric) value in parentheses. Measurement may be verified in either system of units except that connector threads, tubes/ducts diameters will be verified in English standard convention of units.

3.1.3.2 CONVERSIONS AND TOLERANCES

For detailed descriptions of conversions and tolerances, reference ASTM E380, Standard Practice for Use of the International System of Units (SI) (The Modernized Metric System).

3.1.3.3 TOLERANCE

Linear tolerance on English dimensions are as indicated in Table 3.1.3.3–1, Linear Tolerances.

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

3 - 4

TABLE 3.1.3.3–1 LINEAR TOLERANCES

ENGLISH DIMENSION IMPLIED TOLERANCE

INCHES

X.XX ±0.03

X.XXX ±0.010

3.2 INTERFACES

3.2.1 GENERAL

Node 3 attaches to the HAB via a Common Berthing Mechanism (CBM). The CBM has two halves, one of which is attached to the pressure shell of each element in accordance with SSP 41004. Node 3 contains the Active CBM (ACBM), and the HAB contains the Passive CBM

(PCBM).

The bulkhead of each element provides for the routing of utilities around the clear passage envelope and within the CBM volume. This document provides the details related to the utility interfaces.

3.2.2 UTILITY PENETRATIONS

The general arrangements for the utility penetrations with the associated reference designations are shown in Figures 3.2.2–1 and 3.2.2–2. ”A” designations refer to fluid interfaces and ”J” designations refer to electrical interfaces. The centerline address and hole type for each utility interface is in accordance with Tables 3.2.2–1 and 3.2.2–2 for the Node and the HAB. The penetration hole details are shown in Figure 3.2.2–3.

3.3 FLUID INTERFACES

The fluid interface between the Node 3 and HAB consist of a series of flexible lines, within the vestibule, connected between the fluid feedthroughs in the element bulkheads. These interfaces provide for the transport of liquid and gaseous fluids between the elements. A generic interface connection is shown in Figure 3.3–1. The detailed definition of the fluid interfaces is shown in Table 3.2.2–1. Detailed definition of the intermodule air interfaces is shown in Figures 3.3–2, 3.3–3, 3.3–4, and 3.3–5.

3.4 ELECTRICAL INTERFACES

Electrical interfaces between Node 3 and the HAB consist of a series of electrical jumpers, within the vestibule, connected between the electrical feedthroughs in the element bulkheads.

These interfaces provide for the transport of electrical power and electrical signals for control and data between the elements. A generic interface connection is shown in Figure 3.4–1. The detailed definition of the electrical interfaces is shown in Table 3.2.2–2. Details of each interface with its jumper are contained in Figures 3.4–2 through 3.4–9.

3 - 5

3.4.1 ELECTRICAL BONDING

Electrical bonding between the Node 3 and the HAB is accomplished utilizing a combination of metal–to–metal contact at the CBM–to–Pressurized Element interface and redundant bond straps at the ACBM–to–PCBM interface. Figure 3.4.1–1 shows the location of these bond planes in accordance with SSP 41148 and SSP 41004. Class R bonds per SSP 30245 exist between the mated CBM halves as well as between the element to CBM interface.

3.4.2 SOFTWARE INTERFACES

The software interface between Node 3 and the HAB is defined in TBD.

3 - 6

A10

A12

A11

CBM 1553B LB–B

CBM 2/3 Power

J126

A13

J120

J128

J121

J85

Potable Water

Power

LTL

Return from

HAB

LTL

Supply from Node 3

Waste Water

ARS

MTL Return from HAB

MTL Supply from Node 3

N2 Supply

CBM 1/4 Power

CBM 1553B LB–A O2 Recharge

J122

J109 A16 J110

IMV to Node 3

FWD

AFT

1553B LB–A

Audio Bus B

1553B, LB–B

UHF (Coax)

J125

IMV to

HAB

N2 Recharge

A17

Audio Bus A/Video

J83

Z E N I T

OPS LAN

J124

N A D I R

O2 Supply

Hatch Opening

J123

HAB Power

FIGURE 3.2.2–1 UTILITY PENETRATION LAYOUT OF NODE 3 PORT INTERNAL

BULKHEAD LOOKING TOWARD THE HAB

3 - 7

A10

A12

A11

J22

A13

J20

J12

Potable Water

Power

LTL

Return from HAB

LTL

Supply from Node 3

O2 Recharge

Waste Water

ARS

MTL Return from HAB

MTL Supply from Node 3

N2 Supply

A17

IMV Supply

FWD

AFT

1553B LB–A

Audio Bus B1553B LB–B

UHF (Coax)

IMV to

HAB

N2 Recharge

A16

Audio Bus A/Video

J14 O2 Supply

Hatch Opening HAB Power

J23

OPS LAN

J24

Z E N I T H

N A D I R

FIGURE 3.2.2–2 UTILITY PENETRATION LAYOUT OF HAB STARBOARD EXTERNAL

BULKHEAD LOOKING FROM THE NODE

P 50309, P art 2 M ay 19, 1999

3–8

A1 A1 –30.57 12.77 –30.57 12.77 Potable Water TYPE 5 683–16348–303 NA 683–16347–151

A2 A2 30.57 12.77 30.57 12.77 Waste Water TYPE 5 683–16348–302 683–16347–149

A3 A3 –31.00 6.44 –31.00 6.44 LTL Return TYPE 1 683–16348–182 683–16348–168 683–16348–182

A4 A4 –32.12 0.00 –32.12 0.00 IMV to Node 3 See Fig. 3.3–2 See Fig. 3.3–2

A5 A5 –31.00 –6.44 –31.00 –6.44 LTL Supply TYPE 1 683–16348–181 683–16348–152 683–16348–181

A8 A8 31.68 –9.88 31.68 –9.88 Nitrogen Supply TYPE 3 683–16347–173 683–16347–173

A9 A9 TBD TBD TBD TBD Oxygen Supply TYPE 3 683–16347–185 683–16347–185

A10 A10 31.00 6.44 31.00 6.44 MTL Return TYPE 1 683–16348–182 683–16348–168 683–16348–182

A11 A11 32.12 0.00 32.12 0.00 IMV to HAB See Fig. 3.3–2 See Fig. 3.3–2

A12 A12 31.00 –6.44 31.00 –6.44 MTL Supply TYPE 1 683–16348–181 683–16348–152 683–16348–181

A13 A13 31.68 9.88 31.68 9.88 ARS TYPE 4 683–19485–003 683–19485–003

A14* A14 30.57 –12.77 30.57 –12.77 NA NA NA NA

A15* A15 –13.54 32.58 –13.54 32.58 NA NA NA NA

A16 A16 11.60 –30.66 11.60 –30.66 Oxygen Recharge TYPE 3 683–16347–214 683–16347–214

A17 A17 13.54 –32.58 13.54 –32.58 Nitrogen Recharge TYPE 3 683–16347–205 683–16347–205

A18* A18 –11.60 30.66 –11.60 30.66 NA NA NA NA

HOLE

REFERENCE

NODE 3

HOLE LOCATION

HAB

HOLE LOCATION

FUNCTION

PENE–

TRATION

DETAILX Y X YNODE 3 HAB

FEEDTHROUGH/CONNECTOR PART NUMBER

NODE

FEEDTHROUGH

VESTIBULE

CONNECTOR

HAB

FEEDTHROUGH

* NOT SHOWN ON FIGURE 3.2.2–1

TABLE 3.2.2–1 FLUID INTERFACE DETAIL DEFINITION

P 50309, P art 2 M ay 19, 1999

3–9

J83 J14 TBD TBD TBD TBD Audio Bus A/Video TYPE 5 NATC77HF25N37PPE2 NATC06G25N37SE NATC77HF25N37PPE2

J104* J13 3.00 –30.66 3.00 –30.66 NA NA NA NA NA

J105* J11 0.00 –30.66 0.00 –30.66 NA NA NA NA NA

J85 J12 0.00 –34.30 0.00 –34.30 1553B, LB–A TYPE 5 NATC77H25N35PPC NATC06G25N35SC NATC77H25N35PPC

J107* J10 –3.00 –30.66 –3.00 –30.66 NA NA NA NA NA

J108* J22 –6.00 –30.66 –6.00 –30.66 NA NA NA NA NA

J109 –11.60 –30.66 CBM 1553B, LB–A TYPE 6 NATC77H13N35PPN** NA NA

J110 –13.54 –32.58 CBM 1/4 Power TYPE 6 NATC77H13NTBD98PPA** NA NA

J113* J9 –13.54 –32.58 –13.54 –32.58 NA NA NA NA NA

J114* J8 –11.60 –30.66 –11.60 –30.66 NA NA NA NA NA

J126 J22 –31.67 9.88 –31.67 9.88 Hab Power TYPE 6 NATC77H33N3PPN NATC06G33N3SN NATC77H33N3PPN

J125 J2 –6.00 30.66 –6.00 30.66 Audio Bus B TYPE 5 NATC77HF25N37PPN2 NATC06G25N37SN NATC77HF25N37PPN2

J117* J4 0.00 30.66 0.00 30.66 NA NA NA NA NA

J128 J3 0.00 34.30 0.00 34.30 1553B, LB–B TYPE 5 NATC77H25N35PPC NATC06G25N35SC NATC77H25N35PPC

J119* J5 3.00 30.66 3.00 30.66 NA NA NA NA NA

J120 J20 –3.00 30.66 –3.00 30.66 UHF (Coax) TYPE 5 NATC77H25N8PPA NATC06G25N8SA NATC77H25N8PPA

J121 11.60 30.66 CBM 1553B, LB–B TYPE 6 NATC77H13N35PPN** NA NA

J122 13.54 32.58 CBM 2/3 Power TYPE 6 NATC77H13N98PPA** NA NA

J123 J23 TBD TBD TBD TBD Hab Elec. Power TYPE 6 NATC77H33N3PPN NATC06G33N3SN NATC77H33N3PPN

J124 J24 TBD TBD TBD TBD OPS LAN TYPE 5 TBD TBD TBD

HOLE

REFERENCE

NODE 3

HOLE LOCATION

HAB

HOLE LOCATION

FUNCTION

PENE–

TRATION

DETAIL

TABLE 3.2.2–2 ELECTRICAL INTERFACE DETAIL DEFINITION

X Y X YNODE 3 HAB

FEEDTHROUGH/CONNECTOR PART NUMBER

NODE

FEEDTHROUGH

VESTIBULE

CONNECTOR

HAB

FEEDTHROUGH

* NOT SHOWN ON FIGURE 3.2.2–1

** DETAILED ELECTRICAL DESCRIPTION SHOWN IN SSP 41004, PART 2

*** DETAILED ELECTRICAL DESCRIPTION SHOWN IN SSP 42007

3–10

2.059 2.049

2X R .25

NOTE: FLATS ARE ORIENTED TOWARDS HATCH OPENING

1.509 1.499

2X R .25

1.410 1.390

2X R .25

∅ 2.119 2.109

1.460 1.440

HOLE DETAIL

FOR TYPE 1

HOLE

HOLE DETAIL

FOR TYPE 3

HOLE

HOLE DETAIL

FOR TYPE 4

HOLE

1.569 1.559

FIGURE 3.2.2–3 PENETRATION DETAILS FOR FEEDTHROUGHS

3–11

1.709 1.699

2X R .25

NOTE: FLATS ARE ORIENTED TOWARDS HATCH OPENING

.954

.949

2X R .25

1.769 1.759

1.037 1.030

HOLE DETAIL

FOR TYPE 5

HOLE

HOLE DETAIL

FOR TYPE 6

HOLE

FIGURE 3.2.2–3 PENETRATION DETAILS FOR FEEDTHROUGHS (CONTINUED)

3–12

ASI NASA

NODE 3 TO HAB FLUID

INTERFACE PLANE

HAB STBD

BULKHEAD

NODE 3 PORT

BULKHEAD

ÉÉ

ÉÉÉÉÉÉ

ÉÉÉÉ

ÉÉ

CONNECTOR CONNECTOR

FLUID FLEXIBLE

LINE

VESTIBULE

AREA

ÉÉ

ÉÉÉÉÉ

ÉÉÉ

ÉÉ

FEEDTHROUGH FEEDTHROUGH

FIGURE 3.3–1 NODE 3 TO HAB GENERIC FLUID UTILITY INTERFACE

3–13

VESTIBULE IMV

DUCT ASSEMBLY

P/N 683–15195–1

V BAND CLAMP

MS 27115–21R

3 Places

HAB Bulkhead

ASI/Alenia NASA

Node 3 Bulkhead

2X R.015

2X 30° ± 5°

2X .050

+.02 2X .50 –.00

+.02.95 –.00

5.45

+.02 –.00

4.50

2X 1.27

2X 20.0° +.5° –.0°

∅ 5.500

∅ 4.760 ± .005 ∅ 6.250 ± .005∅ 6.050

∅ 5.004+.002

04.760+.005

VIEW A

R.037 ± .005

+.00R.08 –.02.136

2X.03 ± .01 X 45°

REF

16 C

.002

1 The .136 (3.48) thickness is measured at the 6.050 (153.67) diameter.

NODE

INTERIOR

VESTIBULE SIDE

FIGURE 3.3–2 INTERFACE DETAIL FOR IMV SUPPLY AND RETURN

3–14

∅ M + .010

– .000

+ .000

– .010

2X R.25

Penetration Detail

NUTNUT

RETAINING

RING

FEED

THROUGH

FLANGE

SEALS

NODE 3

BULKHEAD

ASI NASA

PRESSURIZED

SIDE

VESTIBULE

AREA

WASHER

NUT

FLATS ARE ORIENTED

TOWARD HATCH

OPENING

FEEDTHROUGH MATE WITH NUT FLANGE

ASSEMBLY

PENETRATION DETAIL

Boeing P/N Boeing P/N M N

683–16347–173 683–16347–171 1.559 1.509

683–16347–185 683–16347–183 1.559 1.509

683–16347–73 683–16347–53 2.109 2.059

683–16347–74 683–16347–65 2.109 2.059

683–16347–214 683–16347–213 1.559 1.509

683–16347–205 683–16347–204 1.559 1.509

683–16347–149 683–16347–TBD TBD TBD

683–16347–151 683–16347–TBD TBD TBD

FIGURE 3.3–3 THREADED FEEDTHROUGH ASSEMBLY INTERFACE DETAILS

3–15

∅ M + .010

– .000

+ .000

– .010

Penetration DetailNUT

NUT

RETAINING

RING

FEEDTHROUGH

FLANGE

SEALS

NODE 3

BULKHEAD

ASI NASA

PRESSURIZED

SIDE

VESTIBULE

AREA

WASHER

NUT

QUICK

DISCONNECT

FEEDTHROUGH

NIPPLE ASSEMBLY

(MALE HALF)

KEYING

TAB

FLATS ARE ORIENTED

TOWARD HATCH

OPENING

2 X R.25

FEEDTHROUGH DETAILS

MALE HALF

MATES WITH FEMALE QD

FLANGE ASSEMBLY

MATES WITH NUT

FLANGE ASSEMBLY

PENETRATION

DETAIL

BOEING P/N BOEING P/N BOEING P/N M N

683–16348–181 683–16348–152 683–16347 2.109 2.059 683–16348–182 683–16348–168 683–16347 2.109 2.059

683–16348–302 683–16348–TBD TBD 1.759 1.709

683–16348–303 683–16348–TBD TBD 1.759 1.709

FIGURE 3.3–4 SELF–SEALING FLUID QUICK DISCONNECT ASSEMBLY INTERFACE

DETAIL NODE 3

3–16

NASAASI

Vestibule Area

Flexible Hose

Swivel nut mates with

MS33656–2

Fitting

Node 3 Bulkhead

683–19485–003

24.00

∅ 1.45 + .010 –.010

+ .010

– .010

1.40

2X R.25

Penetration Detail

Flats oriented toward Hatch opening

FIGURE 3.3–5 NON SELF–SEALING QUICK DISCONNECT FEEDTHROUGH ASSEMBLY

INTERFACE DETAIL

3–17

TBD

ÉÉÉÉ

NODE 3 BULKHEAD RECEPTACLE

JUMPER PLUG

ELECTRICAL JUMPER ASSEMBLY

NODE 3 TO HAB

ELECTRICAL

INTERFACE PLANE

JUMPER PLUG

HAB BULKHEAD RECEPTACLE

TBD

ÉÉÉÉÉ

HAB STBD

BULKHEAD

É É

NODE 3

PORT

BULKHEAD

VESTIBULE

AREA

ÉÉ

É É

ÉÉ

É É

ÉÉ

ASI/ALENIA

NASA

NOTE: BULKHEAD RECEPTACLES FOR NODE 3 AND HAB ARE IDENTICAL IN PART NUMBER,

REFERENCE DESIGNATOR, AND PIN FUNCTION UNLESS NOTED OTHERWISE IN

PIN FUNCTION TABLES

ÉÉ

É É

FIGURE 3.4–1 NODE 3 TO HAB GENERIC ELECTRICAL UTILITY INTERFACE

3–18

JUMPER CABLE ASSEMBLY DIAGRAM

J83

ASI/ALENIA NASA TBD TBD

W0401 W6003

J14

NATC77HF25N37PPE2

NODE 3 BULKHEAD HAB BULKHEAD

P 83

P83 P14

NATC06G25N37SE

PIN FUNCTION ASSIGNMENT

NODE 3/HAB FEEDTHROUGH

J83 & J14

EMC

CLASS

AWG CONNECTS TO

SIGNAL FUNCTION FO P CONTACT P CONTACT

a Video 1 – Hab to Node 3 VSU 5 16 83 a 14 a b Video 2 – Node 3 VSU 5 to Hab 16 83 b 14 b c Video 2 – Hab CVIU to Node 3 VSU 5 16 83 c 14 c d Video 1 – Node 3 VSU 5 to Hab 16 83 d 14 d e Hab SYNC 1 16 83 e 14 e f Hab SYNC 2 16 83 f 14 f r Audio Bus A N3 to Hab 1 16 83 r 14 r q Audio Bus A N3 to Hab 2 16 83 q 14 q h Audio Bus A N3 to Hab 3 16 83 h 14 h k Audio Bus A N3 to Hab 4 16 83 k 14 k m Audio Bus A Hab 1 to N3 16 83 m 14 m n Audio Bus A Hab 2 to N3 16 83 n 14 n p Audio Bus A Hab 3 to N3 16 83 p 14 p g Audio Bus A Hab 4 to N3 16 83 g 14 g

FIGURE 3.4–2 DETAILED ELECTRICAL DESCRIPTION OF NODE BULKHEAD J83 AND

HAB BULKHEAD J14

3–19

NATC06G25N35SC

J85

ASI/ALENIA NASA

JUMPER CABLE ASSEMBLY DIAGRAM

TBD TBD

W0205 W6001

J12

NATC77H25N35PPC

NODE 3 BULKHEAD HAB BULKHEAD

P85

NATC06G25N35SCP85

P12

PIN FUNCTION ASSIGNMENT

NODE 3/HAB FEEDTHROUGH

J85 & J12

EMC

CLASS

AWG CONNECTS TO

SIGNAL FUNCTION P CONTACT P CONTACT

87 CB CT–4A HI RF 22 85 TBD 12 TBD

75 CB CT–4A LO RF 22 85 TBD 12 TBD

53 LB CHeCS–HAB–1A HI RF 22 85 TBD 12 TBD

65 LB CHeCS–HAB–1A LO RF 22 85 TBD 12 TBD

76 LB SEPS–N3–14A HI RF 22 85 TBD 12 TBD

64 LB SEPS–N3–14A LO RF 22 85 TBD 12 TBD

63 LB SEPS–N3–23A HI RF 22 85 TBD 12 TBD

52 LB SEPS–N3–23A LO RF 22 85 TBD 12 TBD

41 LB SEPS–HCZ–14A HI RF 22 85 TBD 12 TBD

30 LB SEPS–HCZ–14A LO RF 22 85 TBD 12 TBD

42 LB SEPS–HCZ–23A HI RF 22 85 TBD 12 TBD

54 LB SEPS–HCZ–23A LO RF 22 85 TBD 12 TBD

66 LB SYS–HCZ–1A HI RF 22 85 TBD 12 TBD

77 LB SYS–HCZ–1A LO RF 22 85 TBD 12 TBD

FIGURE 3.4–3 DETAILED ELECTRICAL DESCRIPTION OF NODE BULKHEAD J85 AND

HAB BULKHEAD J12

3–20

PIN FUNCTION ASSIGNMENT (CONTINUED)

NODE 3/HAB FEEDTHROUGH

J85 & J12

EMC

CLASS

AWG CONNECTS TO

SIGNAL FUNCTION P CONTACT P CONTACT

88 SPARE 1 HI RF 22 85 TBD 12 TBD

99 SPARE 1 LO RF 22 85 TBD 12 TBD

62 LB SYS–HCZ–2A HI RF 22 85 TBD 12 TBD

51 LB SYS–HCZ–2A LO RF 22 85 TBD 12 TBD

40 SPARE 2 HI RF 22 85 TBD 12 TBD

29 SPARE 2 LO RF 22 85 TBD 12 TBD

86 CB CT–BIA–23A HI RF 22 85 TBD 12 TBD

74 CB CT–BIA–23A LO RF 22 85 TBD 12 TBD

89 SPARE 3 HI RF 22 85 TBD 12 TBD

100 SPARE 3 LO RF 22 85 TBD 12 TBD

43 SPARE 4 HI RF 22 85 TBD 12 TBD

55 SPARE 4 LO RF 22 85 TBD 12 TBD

TBD NOT USED 22

HAB BULKHEAD J12 (cont.)

3–21

PIN FUNCTION ASSIGNMENT (CONTINUED)

NODE 3/HAB FEEDTHROUGH

J85 & J12

EMC

CLASS

AWG CONNECTS TO

SIGNAL FUNCTION P CONTACT P CONTACT

TBD NOT USED 22

3–22

PIN FUNCTION ASSIGNMENT (CONTINUED)

NODE 3/HAB FEEDTHROUGH

J85 & J12

EMC

CLASS

AWG CONNECTS TO

SIGNAL FUNCTION P CONTACT P CONTACT

TBD NOT USED 22

3–23

PIN FUNCTION ASSIGNMENT (CONCLUDED)

NODE 3/HAB FEEDTHROUGH

J85 & J12

EMC

CLASS

AWG CONNECTS TO

SIGNAL FUNCTION P CONTACT P CONTACT

TBD NOT USED 22

HAB BULKHEAD J12 (conc.)

3–24

NATC66G25N37SN

J125

ASI/ALENIA NASA

JUMPER CABLE ASSEMBLY DIAGRAM

TBD TBD

W0402 W6004

NATC77HF25N37PPN2

NODE 3 BULKHEAD HAB BULKHEAD

NATC06G25N37SNP125

P125

PIN FUNCTION ASSIGNMENT

NODE 3/HAB FEEDTHROUGH

J125 & J2

EMC

CLASS

AWG CONNECTS TO

SIGNAL FUNCTION P CONTACT P CONTACT

r Audio Bus B N3 to Hab 1 16 125 r 2 r q Audio Bus B N3 to Hab 2 16 125 q 2 q h Audio Bus B N3 to Hab 3 16 125 h 2 h k Audio Bus B N3 to Hab 4 16 125 k 2 k m Audio Bus B Hab 1 to N3 16 125 m 2 m n Audio Bus B Hab 2 to N3 16 125 n 2 n p Audio Bus B Hab 3 to N3 16 125 p 2 p g Audio Bus B Hab 4 to N3 16 125 g 2 g

FIGURE 3.4–4 DETAILED ELECTRICAL DESCRIPTION OF NODE BULKHEAD J125 AND

HAB BULKHEAD J2

3–25

JUMPER CABLE ASSEMBLY DIAGRAM

J128

ASI/ALENIA NASA TBD TBD

W0202 W6002

NATC77H25N35PPC

NODE 3 BULKHEAD HAB BULKHEAD

P128

P128 P3

NATC06G25N35SC

PIN FUNCTION ASSIGNMENT

NODE 3/HAB FEEDTHROUGH

J128 & J3

EMC

CLASS

AWG CONNECTS TO

SIGNAL FUNCTION P CONTACT P CONTACT

87 CB CT–4B HI RF 22 128 TBD 3 TBD

75 CB CT–4B LO RF 22 128 TBD 3 TBD

76 LB SEPS–N3–14B HI RF 22 128 TBD 3 TBD

64 LB SEPS–N3–14B LO RF 22 128 TBD 3 TBD

63 LB SEPS–N3–23B HI RF 22 128 TBD 3 TBD

52 LB SEPS–N3–23B LO RF 22 128 TBD 3 TBD

41 LB SEPS–HCZ–14B HI RF 22 128 TBD 3 TBD

30 LB SEPS–HCZ–14B LO RF 22 128 TBD 3 TBD

42 LB SEPS–HCZ–23B HI RF 22 128 TBD 3 TBD

54 LB SEPS–HCZ–23B LO RF 22 128 TBD 3 TBD

FIGURE 3.4–5 DETAILED ELECTRICAL DESCRIPTION OF NODE BULKHEAD J128 AND

HAB BULKHEAD J3

3–26

PIN FUNCTION ASSIGNMENT (CONTINUED)

NODE 3/HAB FEEDTHROUGH

J128 & J3

EMC

CLASS

AWG CONNECTS TO

SIGNAL FUNCTION P CONTACT P CONTACT

66 LB SYS–HCZ–1B HI RF 22 128 TBD 3 TBD

77 LB SYS–HCZ–1B LO RF 22 128 TBD 3 TBD

88 SPARE 1 HI RF 22 128 TBD 3 TBD

99 SPARE 1 LO RF 22 128 TBD 3 TBD

53 LB CHeCS–HAB–1B HI RF 22 128 TBD 3 TBD

65 LB CHeCS–HAB–1B LO RF 22 128 TBD 3 TBD

40 SPARE 2 HI RF 22 128 TBD 3 TBD

29 SPARE 2 LO RF 22 128 TBD 3 TBD

89 SPARE 3 HI RF 22 128 TBD 3 TBD

100 SPARE 3 LO RF 22 128 TBD 3 TBD

86 CB CT–BIA–23B HI RF 22 128 TBD 3 TBD

74 CB CT–BIA–23B LO RF 22 128 TBD 3 TBD

TBD Not Used 22 128 TBD 3 TBD

HAB BULKHEAD J3 (CONT)

3–27

PIN FUNCTION ASSIGNMENT (CONTINUED)

NODE 3/HAB FEEDTHROUGH

J128 & J3

EMC

CLASS

AWG CONNECTS TO

SIGNAL FUNCTION P CONTACT P CONTACT

TBD Not Used 22 128 TBD 3 TBD

3–28

PIN FUNCTION ASSIGNMENT (CONTINUED)

NODE 3/HAB FEEDTHROUGH

J118 & J3

EMC

CLASS

AWG CONNECTS TO

SIGNAL FUNCTION P CONTACT P CONTACT

TBD NOT USED 22 128 TBD 3 TBD

TBD NOT USED 22 TBD TBD

43 SPARE 4 HI RF 22 128 TBD 3 TBD

55 SPARE 4 LO RF 22 128 TBD 3 TBD

62 LB SYS–HCZ–2B HI RF 22 128 TBD 3 TBD

61 LB SYS–HCZ–2B LO RF 22 128 TBD 3 TBD

TBD NOT USED 22

3–29

PIN FUNCTION ASSIGNMENT (CONTINUED)

NODE 3/HAB FEEDTHROUGH

J118 & J3

EMC

CLASS

AWG CONNECTS TO

SIGNAL FUNCTION P CONTACT P CONTACT

TBD NOT USED 22

3–30

PIN FUNCTION ASSIGNMENT (CONCLUDED)

NODE 3/HAB FEEDTHROUGH

J128 & J3

EMC

CLASS

AWG CONNECTS TO

SIGNAL FUNCTION P CONTACT P CONTACT

TBD NOT USED 22

HAB BULKHEAD J3 (CONC)

3–31

JUMPER CABLE ASSEMBLY DIAGRAM

NATC66G25N8SE

J120

ASI/ALENIA NASA TBD TBD

W0404 W6008

J20

NATC77H25N8PPE

NODE 3 BULKHEAD HAB BULKHEAD

P120

P120 P20

NATC06G25N8SE

PIN FUNCTION ASSIGNMENT

NODE 3/HAB FEEDTHROUGH

J120 & J20

EMC

CLASS

AWG

(COAX)

CONNECTS TO

SIGNAL FUNCTION (COAX) P CONTACT P CONTACT

H IAA TO HAB RF 8 120 H 20 H

A IAA TO TERMINATOR * RF 8

B NOT USED 8

C NOT USED 8

D NOT USED 8

E NOT USED 8

F NOT USED 8

G NOT USED 8

* This pin reserved on J120 for looping book into N3 prior to HAB on orbit and is not used in N3 to HAB jumper assembly.

FIGURE 3.4–6 DETAILED ELECTRICAL DESCRIPTION OF NODE BULKHEAD J120 AND

HAB BULKHEAD J20

3–32

JUMPER CABLE ASSEMBLY DIAGRAM

J123

ASI/ALENIA NASA TBD TBD

W(TBD)

J23

NATC77H33N3PPN

NODE 3 BULKHEAD HAB BULKHEAD

P 123

P123 P23

NATC06G33N3SN

PIN FUNCTION ASSIGNMENT

NODE 3/HAB FEEDTHROUGH

J123 & J23

EMC

CLASS

AWG CONNECTS TO

SIGNAL FUNCTION FO J CONTACT J CONTACT

A Power Supply (IB4A) EO 1/0 123 TBD 23 TBD

C Power Return (IB4A) EO 1/0 123 TBD 23 TBD

B Ground (IB4A) EO 4 123 TBD 23 TBD

FIGURE 3.4–7 DETAILED ELECTRICAL DESCRIPTION OF NODE BULKHEAD J123 AND

HAB BULKHEAD J23

3–33

JUMPER CABLE ASSEMBLY DIAGRAM

J126

ASI/ALENIA NASA TBD TBD

W(TBD)

J22

NATC77H23N3PPN

NODE 3 BULKHEAD HAB BULKHEAD

P 126

P126 P22

NATC06G33N3SN

PIN FUNCTION ASSIGNMENT

NODE 3/HAB FEEDTHROUGH

J126 & J22

EMC

CLASS

AWG CONNECTS TO

SIGNAL FUNCTION FO J CONTACT J CONTACT

A Power Supply (2A2B) E0 1/0 126 TBD 22 TBD

C Power Return (2A2B) E0 1/0 126 TBD 22 TBD

B Ground (2A2B) E0 4 126 TBD 22 TBD

FIGURE 3.4–8 DETAILED ELECTRICAL DESCRIPTION OF NODE BULKHEAD J126 AND

HAB BULKHEAD J22

3–34

JUMPER CABLE ASSEMBLY DIAGRAM

J124

ASI/ALENIA NASA TBD TBD

W0401 W6003

J24

NODE 3 BULKHEAD HAB BULKHEAD

P 124

P124 P24

PIN FUNCTION ASSIGNMENT

NODE 3/HAB FEEDTHROUGH

J124 & J24

EMC

CLASS

AWG CONNECTS TO

SIGNAL FUNCTION FO J CONTACT J CONTACT

1 HAB/MPLM REC–LO E0 1/0 124 11 24 TBD

2 HAB/MPLM REC–HI E0 1/0 124 12 24 TBD

3 HAB/MPLM TR–LO E0 1/0 124 13 24 TBD

4 HAB/MPLM TR–HI E0 1/0 124 14 24 TBD

5 Node 1/HAB REC–LO E0 1/0 124 15 24 TBD

6 Node 1/HAB REC–HI E0 1/0 124 16 24 TBD

7 HAB/Node 3 TR–LO E0 1/0 124 17 24 TBD

8 HAB/Node 3 REC–LO E0 1/0 124 18 24 TBD

9 HAB/Node 3 REC–HI E0 1/0 124 19 24 TBD

10 Node 1/HAB TR–LO E0 1/0 124 20 24 TBD

11 Node 1/HAB TR–HI E0 1/0 124 21 24 TBD

12 HAB/Node 3 TR–HI E0 1/0 124 22 24 TBD

FIGURE 3.4–9 DETAILED ELECTRICAL DESCRIPTION OF NODE BULKHEAD J124 AND

HAB BULKHEAD J24

3–35 class R bonds

NODE 3 ACBM PCBM HAB

FIGURE 3.4.1–1 NODE 3 TO HAB ELECTRICAL BONDING

A - 1

APPENDIX A ABBREVIATIONS AND ACRONYMS

A.1 ABBREVIATIONS AND ACRONYMS

ACA Associate Contractor Agreement

ACBM Active Common Berthing Mechanism

ARS Air Revitalization System

ASI Agenzia Spaziale Italiana

CBM Common Berthing Mechanism

CHeCS Crew Health Care Systems

CVIU Common Video Interface Units

HAB Habitation Module

ICD Interface Control Document

ICWG Interface Control Working Group

IMV Intermodule Ventilation

ISS International Space Station

LAN Local Area Network

LTL Low Temperature Loop

MPLM Mini Pressurized Logistics Module

MTL Moderate Temperature Loop

N2 Nitrogen

O2 Oxygen

P/N Part Number

PCBM Passive Common Berthing Mechanism

SSP Space Station Program

TBD To Be Determined

UHF Ultrahigh Frequency

VSU Video Switch Unit

B – 1

APPENDIX B

ISSUE LIST FOR SSP 50309

B – 2

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