SSP_50621-RevF-DCN001-Collated_Master.pdf

SSP 50621

Revision F

Generic On-Orbit Stowage Capabilities and Requirements: Pressurized Volume

International Space Station Program

Incorporates DCN 001

January 2013

National Aeronautics and Space Administration International Space Station Program Johnson Space Center Houston, Texas Contract Number: NNJ10GA20B

Revision F 16 August 2016

REVISION AND HISTORY PAGE

REV. DESCRIPTION PUB.

DATE

- Initial Release (per SSCD 006076, EFF. 02-05-02)

Early Release 04-02-02

Program Release 07-29-02

A Revision A (per SSCCD 006595, EFF. 03-07-02)

Early Release 04-13-02

Program Release 11-08-02

B Revision B (per SSCCD 007137, EFF. 09-18-02)

Early Release 10-01-02

Program Release 11-08-02

C Revision C (per SSCCD 008552 EFF. 04-15-04)

Early Release 04-19-04

Program Release 05-25-05

D Revision D (Reference per SSCD 009046, EFF. 12-02-04;

SSCD 009046R1, EFF. 02-25-05; SSCD 009046R2,

EFF. 06-17-05)

Early Release 09-05-05

Program Release 02-01-06

DCN 001 (Reference per SSCD 010012, EFF. 12-14-06)

Early Release 12-21-06

Program Release 03-20-07

E Revision E (Reference per SSCD 010207, EFF. 12-14-06)

Early Release 12-21-06

Program Release 06-03-08

F Revision F (Reference per SSCD 013288, EFF. 02-13-13)

Early Release 03-01-13

Program Release 11-20-13

REVISION AND HISTORY PAGE

REV. DESCRIPTION PUB.

DATE

F DCN 001 (Reference SSCD 15150, EFF 04-22-16)

Program Release 08-17-16 i

PREFACE

GENERIC ON-ORBIT STOWAGE CAPABILITIES AND REQUIREMENTS

PRESSURIZED VOLUME

SSP 50621, Generic On-orbit Stowage Capabilities and Requirements: Pressurized Volume, describes the generic capabilities of the on-orbit Station to accommodate stowage of cargo in each International Space Station (ISS) module.

The Generic On-orbit Stowage Capabilities and Requirements (OSCAR) documents the approval of the National Aeronautics and Space Administration (NASA) and the applicable International Partners (IPs) of the generic stowage capabilities for ISS modules.

This document is under the control of the Multilateral Mission Integration and

Operations Control Board (MMIOCB). The technical concurrences represented in this document apply to those sections of the document specific to each respective partner.

ii

INTERNATIONAL SPACE STATION PROGRAM

GENERIC ON-ORBIT STOWAGE CAPABILITIES AND REQUIREMENTS:

PRESSURIZED VOLUME

CONCURRENCE

JANUARY 2013

iii

INTERNATIONAL SPACE STATION PROGRAM

GENERIC ON-ORBIT STOWAGE CAPABILITIES AND REQUIREMENTS:

PRESSURIZED VOLUME

iv

INTERNATIONAL SPACE STATION PROGRAM

GENERIC ON-ORBIT STOWAGE CAPABILITIES AND REQUIREMENTS:

PRESSURIZED VOLUME

v

INTERNATIONAL SPACE STATION PROGRAM

GENERIC ON-ORBIT STOWAGE CAPABILITIES AND REQUIREMENTS:

PRESSURIZED VOLUME

SSP 50621 16 August 2016 vi

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 ................................................................................................ 2-1

3.0 APPROVED STOWAGE CAPABILITY (ASC) SUMMARY .................................................... 3-1

3.1 SUMMARY OF ASC BY MODULE ........................................................................................ 3-1

4.0 NATIONAL AERONAUTICS AND SPACE ADMINISTRATION ELEMENTS ........................ 4-1

4.1 FUNCTIONAL CARGO BLOCK (FGB) .................................................................................. 4-1

4.2 NODE 1 (ZENITH 1 INCLUDED) ........................................................................................... 4-12

4.3 UNITED STATES LABORATORY ......................................................................................... 4-17

4.4 JOINT AIRLOCK ................................................................................................................... 4-22

4.5 NODE 2 ................................................................................................................................. 4-25

4.6 PRESSURIZED MATING ADAPTER 1 (PMA-1) ................................................................... 4-29

4.7 PRESSURIZED MATING ADAPTER 2 (PMA-2) .................................................................. 4-29

4.8 PRESSURIZED MATING ADAPTER 3 (PMA-3) ................................................................... 4-30

4.9 NODE 3 ................................................................................................................................. 4-31

4.10 CUPOLA ................................................................................................................................ 4-37

4.11 PERMANENT MULTIPURPOSE MODULE (PMM) ............................................................... 4-37

5.0 RUSSIAN SPACE AGENCY MODULES ............................................................................... 5-1

5.1 SERVICE MODULE (SM) ...................................................................................................... 5-1

5.1.1 CONSTRAINTS ON STOWING CARGO IN THE SM ........................................................... 5-1

5.1.2 CARGO STOWAGE CAPABILITIES IN THE SM .................................................................. 5-3

5.2 DOCKING COMPARTMENT 1 (DC-1) .................................................................................. 5-11

5.2.1 DC-1 STOWAGE CONSTRAINTS ........................................................................................ 5-11

5.3 MINI RESEARCH MODULE NO. 1 (MRM1).......................................................................... 5-18

5.4 MINI RESEARCH MODULE NO. 2 (MRM2).......................................................................... 5-27

6.0 EUROPEAN SPACE AGENCY MODULE ............................................................................. 6-34

6.1 COLUMBUS .......................................................................................................................... 6-34

7.0 JAPAN AEROSPACE EXPLORATION AGENCY MODULE ................................................. 7-40

7.1 JAPANESE EXPERIMENT MODULE EXPERIMENT LOGISTICS MODULE -

PRESSURIZED SECTION (JLP) ........................................................................................... 7-40

7.2 JEM EXPERIMENT MODULE PRESSURIZED MODULE (JPM) .......................................... 7-43

APPENDIX

A ACRONYMS AND ABBREVIATIONS ................................................................................... A-1

B GLOSSARY OF TERMS ....................................................................................................... B-1

C OPEN WORK ........................................................................................................................ C-1 vii

TABLE

3.1-1 SUMMARY OF ASC .............................................................................................................. 3-1

4.1-1 FGB STOWAGE CLEARANCE REQUIREMENTS ............................................................... 4-2

4.1-2 FGB ASC (PAGE 1 OF 2) ..................................................................................................... 4-3

4.2-1 NODE 1 ASC ......................................................................................................................... 4-13

4.2-1 NODE 1 ASC ......................................................................................................................... 4-14

4.3-1 U.S. LABORATORY ASC ...................................................................................................... 4-18

4.4-1 JOINT AIRLOCK ASC ........................................................................................................... 4-23

4.5-1 NODE 2 ASC ......................................................................................................................... 4-26

4.6-1 PMA-1 ASC ........................................................................................................................... 4-29

4.7-1 PMA-2 ASC ........................................................................................................................... 4-30

4.8-1 PMA-3 ASC ........................................................................................................................... 4-30

4.9-1 NODE 3 ASC ......................................................................................................................... 4-32

4.11-1 PMM ASC (PAGE 1 OF 2)..................................................................................................... 4-39

5.1.1 CLEARANCE REQUIREMENTS FOR STOWING CARGO IN THE SM ............................... 5-2

5.1.2.-1 CARGO STOWAGE CAPABILITIES IN THE SM .................................................................. 5-3

5.2-1 ASC IN DC-1 ......................................................................................................................... 5-11

5.2.1-1 DC-1 CARGO STOWAGE CLEARANCE REQUIREMENTS ................................................ 5-12

5.3-2 STORAGE CAPABILITIES IN MRM1 .................................................................................... 5-19

5.4-1 ASC IN MRM2 ....................................................................................................................... 5-28

6.1-1 COLUMBUS ASC .................................................................................................................. 6-35

7.1-1 JLP ASC ................................................................................................................................ 7-41

7.2-1 JPM ASC ............................................................................................................................... 7-44

C-1 TO BE DETERMINED ITEMS ............................................................................................... C-1

C-2 TO BE RESOLVED ISSUES ................................................................................................. C-1

FIGURE

4.1-1 DIAGRAM OF CARGO STOWAGE ZONES BEHIND STARBOARD PANELS (PLANE IV) IN

THE FGB ............................................................................................................................... 4-5

4.1-2 DIAGRAM OF CARGO STOWAGE ZONES BEHIND PORT PANELS (PLANE II) IN THE

FGB ....................................................................................................................................... 4-6

4.1-3 DIAGRAM OF CARGO STOWAGE ZONES ON DECK INTERIOR PANELS ....................... 4-7

4.1-4 STOWAGE CAPABILITY OF FGB ENCLOSURES ............................................................... 4-8

4.1-5 STOWAGE CAPABILITY OF FGB ENCLOSURES ............................................................... 4-9

4.1-6 STOWAGE CAPABILITY OF FGB ENCLOSURES ............................................................... 4-10

4.1-7 STOWAGE CAPABILITY OF FGB ENCLOSURES ............................................................... 4-11

4.2-1 NODE 1 LOCATION REFERENCE ....................................................................................... 4-14

4.2-2 NODE 1 PORT/OVERHEAD ‘RACK FRONT’ STOWAGE CAPABILITY .............................. 4-15

4.2-3 NODE 1 STARBOARD/DECK ‘RACK FRONT’ STOWAGE CAPABILITY ............................ 4-16

4.3-1 U.S. LABORATORY LOCATION REFERENCE .................................................................... 4-19

4.3-2 U.S. LABORATORY STBD/DECK STOWAGE CAPABILITY ................................................ 4-20

4.3-3 U.S. LABORATORY OVERHEAD/PORT STOWAGE CAPABILITY ..................................... 4-21

4.4-1 JOINT AIRLOCK LOCATION REFERENCE ......................................................................... 4-24

4.5-1 NODE 2 LOCATION REFERENCE ....................................................................................... 4-27

4.5-2 NODE 2 FORWARD/DECK/PORT ‘RACK FRONT’ STOWAGE CAPABILITY ..................... 4-28 viii

4.5-3 NODE 2 FORWARD STOWAGE CAPABILITY ..................................................................... 4-29

4.9-1 NODE 3 LOCATION REFERENCE ....................................................................................... 4-34

4.9-2 NODE 3 PORT/AFT/DECK ‘RACK FRONT’ STOWAGE CAPABILITY ................................. 4-35

4.9-3 NODE 3 OVERHEAD/FORWARD ‘RACK FRONT’ STOWAGE CAPABILITY ...................... 4-36

4.11-1 PMM DIFFUSER KEEP OUT ZONES ................................................................................... 4-38

4.11-2 PMM LOCATIONS ................................................................................................................ 4-41

4.11-3 PMM ‘RACK FRONT’ AND CORRIDOR STOWAGE CAPABILITY ...................................... 4-42

4.11-4 PMM ‘END CONE’ STOWAGE CAPABILITY ........................................................................ 4-43

5.1.2-1 SM STOWAGE ZONES DECK (PLANE I) AND STARBOARD (PLANE IV) (PAGE 1 OF 2) 5-4

5.1.2-2 SM STOWAGE ZONES, TRANSFER TUNNEL (PAGE 1 OF 2) ........................................... 5-6

5.1.2-3 SM STOWAGE ZONES, TRANSFER COMPARTMENT (PAGE 1 OF 2) ............................. 5-8

5.1.2-4 SM STOWAGE ZONES, TOILET COMPARTMENT ............................................................. 5-10

5.2-1 GENERAL CONFIGURATION OF DC-1 INTERIOR VOLUME ............................................. 5-13

5.2-2 CARGO STORAGE ZONES IN DC1 (ВЛ1 & ВЛ2 SIDES) (PAGE 1 OF 3) ........................... 5-14

5.2-3 PLACEMENT OF SPACESUITS DURING STOWAGE IN DC-1 ........................................... 5-17

5.3-1 GENERAL CONFIGURATION OF MRМ1 - INTERNAL VOLUME ........................................ 5-20

5.3-2 CARGO STORAGE ZONES IN MRM1 (STARBOARD) (PAGE 1 OF 6) ............................... 5-21

5.3-2 CARGO STORAGE ZONES IN MRM1 (PORT) (PAGE 2 OF 6) ........................................... 5-22

5.3-3 TYPICAL STANDARD ENCLOSURE IN MRM1 .................................................................... 5-27

5.4-1 GENERAL CONFIGURATION OF MRM2 INTERNAL VOLUME .......................................... 5-29

5.4-2 CARGO STORAGE ZONES IN MRM2 (ВЛ1 & ВЛ2 SIDES) (PAGE 1 OF 3) ....................... 5-30

5.4-3 PLACEMENT OF SPACESUITS DURING STORAGE IN MRM2 ......................................... 5-33

6.1-1 COLUMBUS LOCATIONS, TOPOGRAPHIC REFERENCE ................................................. 6-36

6.1-2 COLUMBUS OVERHEAD/FORWARD RACK FRONT APPROVED STOWAGE ................. 6-37

6.1-3 COLUMBUS RACK DECK/AFT APPROVED STOWAGE .................................................... 6-38

6.1-4 COLUMBUS END CONE APPROVED STOWAGE .............................................................. 6-39

7.1-1 JLP LOCATION REFERENCE .............................................................................................. 7-42

7.2-1 JPM LOCATION REFERENCE ............................................................................................. 7-45

1-1 DCN 001

1.0 INTRODUCTION

1.1 PURPOSE

This document, SSP 50621, Generic On-orbit Stowage Capabilities and Requirements (OSCAR): Pressurized Volume, documents approved stowage capabilities for all International Space Station (ISS) pressurized modules/elements, and also documents the approval of National Aeronautics and Space Administration (NASA) and applicable International Partners (IP’s) of those approved stowage capabilities.

1.2 SCOPE

The scope of this document is limited to Approved Stowage Capability (ASC) which can be utilized without violating generic and module-specific groundrules or constraints.

The ISS configuration used for this document is post-ULF7.

There are certain locations that are not used for permanent stowage due to crew efficiency (e.g. not stowing on rack fronts in dwellings due to high amounts of translation) and cargo operations (e.g. trash staging and docking/berthing ports). Locations that impact crew efficiency are only used temporary and will be removed as quickly as possible. This applies to USOS modules only.

Any identified temporary stowage capability which violates a hazard control, GGR&C (Generic Groundrule and Constraint), United States On-orbit Segment (USOS) constraint, or documented Russian Segment (RS) constraint and requires a waiver or deviation, is out of the scope of this document. Waivers or deviations are documented in the applicable ISS safety documentation or operations planning document (i.e., Non-Compliance Reports, Increment Definition & Requirements Document, etc.).

U.S. Segment Stowage values are per GGR&C 13159 <TBD 1-1>.

The definition of waivers and deviations are provided in the NASA/Partners’ Joint Management Plans/Protocol (SSP 50019, NASA/ESA Joint Management Plan;

SSP 50022, NASA/CSA Joint Management Plan; SSP 50030, NASA/NASDA Joint Management Plan; SSP 50107, NASA/Roscosmos Joint Management Protocol).

This Generic OSCAR will be updated, as necessary, to incorporate changes to the on-orbit module ASC’s (e.g., relocating a module, the addition of a new module, or rack changes to current modules).

1.3 PRECEDENCE

If there are any discrepancies between the information contained in this document and

SSP 50261-01, Generic Groundrules, Requirements, and Constraints Part 1: Strategic and Tactical Planning, SSP 50128, Specification of Technical Requirements for the FGB Functional Cargo Block, and SSP 41163, ISS Russian Segment Specification, the aforementioned documents take precedence.

1.4 DELEGATION OF AUTHORITY

The Generic OSCAR document is the responsibility of the Multilateral Mission Integration and Operations Control Board (MMIOCB). All changes to this document will

1-2 be processed in accordance with the procedures as specified in SSP 41170, Configuration Management Requirements.

2-1 DCN 001

2.0 DOCUMENTS

2.1 APPLICABLE DOCUMENTS

The following documents include specifications, models, standards, guidelines, handbooks, and other special publications. The documents listed in this paragraph are applicable to the extent specified herein. Inclusion of applicable documents herein does not in any way supersede the order of precedence identified in Paragraph 1.3 of this document.

ISS-STO-801-### Safety Hazard Report (Latest Available Version)

KhSC-0050-10 KhSC Salyut Design Bureau International Space Station Alpha FGB Hazard Analysis Report (or Latest Available

Version)

RSCE-C148 Hazard Report: Damage To Spacesuit While It Is Stowed In The Docking Compartment 1 (DC1)

SSP 41163 Russian Segment Specification

SSP 41170 Configuration Management Requirements

SSP 50019 NASA/ESA Joint Management Plan

SSP 50022 NASA/CSA Joint Management Plan

SSP 50030 NASA/NASADA Joint Management Plan

SSP 50128 Specification of Technical Requirements for the FGB, (Functional Cargo Block)

SSP 50261-01 Generic Groundrules, Requirements, and Constraints Part 1: Strategic and Tactical Planning

2.2 REFERENCE DOCUMENTS

The following documents contain supplemental information to guide the user in the application of this document. These reference documents may or may not be specifically cited within the text of this document.

SSP 30219 Space Station Reference Coordinate Systems

SSP 50200 11 Station Program Implementation Plan; Volume 11: ISS Cargo Integration Process

SSP 50564 ISS Interior Volume Configuration Document

2-2

SE-XBA 031699-003 Boeing: Sustaining Engineering Analysis Report: Node 1 Non-standard Stowage Constraints and Guidelines, March 17, 1999 - Vehicle Integrated Performance and Resources (VIPeR)

SE-XBA-100699-011 Boeing: Sustaining Engineering Analysis Report: Z1 Non-standard Stowage Constraints and Guidelines - Vehicle Integrated Performance and Resources (VIPeR)

SE-XBA 101399-013 Boeing: Sustaining Engineering Analysis Report: PMA-3 Non-standard Stowage Capability, January 25, 2000 - Vehicle Integrated Performance and Resources (VIPeR)

3-1 DCN 001

3.0 APPROVED STOWAGE CAPABILITY (ASC) SUMMARY

3.1 SUMMARY OF ASC BY MODULE

A summary of the ASC for each module and a combined total of the ASC for the ISS is shown in Table 3.1-1, Summary of ASC. One Cargo Transfer Bag Equivalent (CTBE) equals 0.053 m3 or 1.86 ft3.

TABLE 3.1-1 SUMMARY OF ASC

Section/Module

ASC

M^3 CTBE

4.1 FGB 14.70 278.1

4.2 Node1 (Z1 included) 9.3/7.9* 176.5/151.5*

4.3 U.S. Lab 6.6 93.7

4.4 A/L (Equip. Lock and Crewlock) 6.11/5** 116.5/95**

4.5 Node2 5.8/4.0* 150.5/115.5*

4.6 PMA-1 1.6 30.0

4.7 PMA-2 1.8 34.5

4.8 PMA-3 1.8 34.5

4.9 Node3 4.8 91.0

4.10 Cupola 0.0 0.0

4.11 PMM 37.3 710

5.1 SM 2.3 42.7

5.2 DC-1 1.6 30.0

5.3 MRM1 2.0 37.7

5.4 MRM2 1.6 30.0

6.1 Columbus 10.2 189.5

7.1 JLP 8.1 152.0

7.2 JPM 6.7 113.6

ISS Total **(w/o NORS/AIK installed) 122.3/119.1* 2310.8/2250.8*

**(w/ NORS/AIK installed) 121.2/118* 2289.3/2229.3*

* Stowage removed when VV is berthed

Acronyms and Abbreviations

A/L Airlock

DC Docking Compartment

FGB Functional Cargo Block

JEM Japanese Experiment Module

JLP JEM Experiment Logistics Module - Pressurized Section

JPM JEM-Pressurized Module

MRM Mini Research Module

PMA Pressurized Mating Adapter

PMM Permanent Multi-purpose Module

SM Service Module

Z1 Zenith 1 Truss

4-1

4.0 NATIONAL AERONAUTICS AND SPACE ADMINISTRATION ELEMENTS

4.1 FUNCTIONAL CARGO BLOCK (FGB)

The ASC for cargo stowage inside the FGB consists of stowage zones behind closeout panels and on the front of specific deck closeout panels in the FGB corridor. FGB enclosures have been installed behind appropriate closeout panels to prevent the cargo from coming in contact with the FGB pressurized hull, structure, and other equipment.

General Safety-Related cargo stowage constraints for the FGB are specified in KhSC-0050-10, KhSC Salyut Design Bureau International Space Station Alpha FGB Hazard Analysis Report including attachments.

Additional operational stowage constraints are listed below (from SSP 50261-01:

A. Maintain a minimum emergency translation corridor of 32 X 32 inches (in.)

(81 X 81 centimeters (cm)) within the FGB.

B. Cargo shall not interfere with the hatch operational envelopes.

C. Cargo shall not impede access to Portable Fire Extinguishers (PFE’s), gas masks, or quick disconnects on drag-through cabling.

D. Cargo shall not crush or damage the dragline flex hose.

E. Temperature sensors in the ГА in the hatches ГА-NODE1 and ГА-Soyuz (or Progress) shall remain free of equipment at all times to permit air circulation.

F. Ventilation grilles on panels 101, 116, 201, 231, 301, 316, 401, and 431 shall remain free of equipment at all times to permit air circulation.

G. Equipment panels to be removed (opened) for fire extinguishing purposes shall be accessible within 1 minute.

H. Cargo shall adhere to the clearance requirements referenced in Table 4.1-1, FGB Stowage Clearance Requirements.

4-2

TABLE 4.1-1 FGB STOWAGE CLEARANCE REQUIREMENTS

Hardware Required Clearance

Pressure Equalization Valves (КВД) located (1) in ПГО-2, (1) in ПГО-3, and (2) in ГА

Cargo may be stowed in the area of the PEV so long as it does not hinder access to the PEV adjacent volume of 25.6 inch (65 cm) in diameter and 39 inch (100 cm) in length for PEV access.

Smoke Detectors Air Inlets 5 cm (2 In.)

Fan Inlet and Outlets 10 cm (3.9 in)

Gas Analyzer 15 cm (5.9 In.)

Cabin Air Sensible Heat Exchanger 20 cm (7.9 In.) from Fan inlet 10 cm (3.9 in) above assembly and fan outlets

Power Outlets, Control Panels, Portable Flashlights, and Fuse Plug Panels

30 cm (11.8 In.)

Overhead Lights Lighting in the FGB Corridor must not be impeded in the 800 mm diameter translation path and in locations of control panels, UOPs (Utility Outlet Panels), etc.

FGB ASC is shown by location in Table 4.1-2, FGB ASC, with stowage operational impacts identified for those relevant locations. FGB ASC locations are identified pictorially in Figures 4.1-1, Diagram of Cargo Stowage Zones Behind Starboard Panels (Plane IV) in the FGB, thru 4.1-3, Diagram of Cargo Stowage Zones on Deck Interior Panels. Figures 4.1-4, Stowage Capability of FGB Enclosures, thru 4.1-7, Stowage Capability of FGB Enclosures, depict FGB stowage enclosures with CTB’s (Cargo Transfer Bags) shown only for size reference. The bags have not been fit-checked inside the enclosures.

4-3

TABLE 4.1-2 FGB ASC (PAGE 1 OF 2)

Zone ASC

Number Enclosure Location CTBE m3 Comments

On panel front

8.54 0.45 Remove for access behind panel

On panel front

7.78 0.41 Remove for access behind panel

On panel front

5.51 0.29 Remove for access behind panel

On panel front

9.49 0.50 Remove for access behind panel

On panel front

6.84 0.36 Remove for access behind panel

On panel front

9.11 0.48 Remove for access behind panel

On panel front

12.34 0.65 Remove for access behind panel

On panel front

7.40 0.39 Remove for access behind panel

On panel front

3.99 0.21 Remove for access behind panel

On panel front

11.96 0.63 Remove for access behind panel

On panel front

1.14 0.06 Remove for access behind panel

On panel front

3.61 0.19 Remove for access behind panel

112_1 113_1

22 Behind panel

17.66 0.93

114_1 115_1

36 Behind panel

2.85 0.15

213_1 42A Behind panel 0.95 0.05

213_1 214_1

42Б Behind panel

3.99 0.21

215_1 40Б Behind panel 0.57 0.03

217_1 40A Behind panel 1.71 0.09

218_1 41 Behind panel 1.52 0.08

219_1 39 Behind panel 3.23 0.17

221_1 38 Behind panel 4.37 0.23

224_1 16 Behind panel 9.11 0.48

225_1 19 Behind panel 9.11 0.48

226_1 15 Behind panel 12.72 0.67

227_1 18 Behind panel 4.37 0.23

227_1 18R Behind panel 1.33 0.07

229_1 14 Behind panel 3.99 0.21

230_1 17 Behind panel 1.52 0.08

302_1 1 Behind panel 3.99 0.21

303_1 2 Behind panel 4.94 0.26

4-4

TABLE 4.1-2 FGB ASC (PAGE 2 OF 2)

Zone ASC

Number Enclosure Location CTBE m3 Comments

304_1 305_1

3 Behind panel

5.89 0.31

306_1 4 Behind panel 1.71 0.09

307_1 24A Behind panel 2.66 0.14

308_1 24Б Behind panel 4.75 0.25

309_1 24B Behind panel 3.42 0.18

312_1 21 Behind panel 4.18 0.22

403_1 35A Behind panel 0.95 0.05

404_1 5 Behind panel 2.78 0.12

404_1 8 Behind panel 4.56 0.24

405_1 9 Behind panel 4.37 0.23

407_1 35Б Behind panel/ 0.60 0.03

407_1 35B Behind panel 0.76 0.04

409_1 35Г Behind panel 1.71 0.09

412_1 23A Behind panel 2.47 0.13

414_1 23Б Behind panel 1.90 0.10

415_1 25A Behind panel 3.04 0.16

416_1 26 Behind panel 2.47 0.13

417_1 25Б Behind panel 3.04 0.16

418_1 27 Behind panel 2.85 0.15

419_1 28A Behind panel 2.09 0.11

419_1 28Б Behind panel 2.09 0.11

420_1 29 Behind panel 2.66 0.14

420_1 31 Behind panel 0.95 0.05

421_1 30A Behind panel 0.95 0.05

421_1 30Б Behind panel 0.76 0.04

422_1 32 Behind panel 1.14 0.06

424_1 10 Behind panel 9.11 0.48

425_1 12 Behind panel 9.11 0.48

426_1 11 Behind panel 12.72 0.67

427_1 13 Behind panel 4.37 0.23

427_1 13R Behind panel 0.95 0.05

ФГБ1ГА_K_2 48 2.28 0.12

278.13 14.70

4-5

FIGURE 4.1-1 DIAGRAM OF CARGO STOWAGE ZONES BEHIND STARBOARD PANELS (PLANE IV) IN THE FGB

4-6

FIGURE 4.1-2 DIAGRAM OF CARGO STOWAGE ZONES BEHIND PORT PANELS (PLANE II) IN THE FGB

4-7

Stowage permitted on shaded deck areas up to 750 mm from the deck panels.

Cargo Stowage on the overhead, port, and starboard panels is prohibited.

FIGURE 4.1-3 DIAGRAM OF CARGO STOWAGE ZONES ON DECK INTERIOR PANELS

4-8

FIGURE 4.1-4 STOWAGE CAPABILITY OF FGB ENCLOSURES

4-9

FIGURE 4.1-5 STOWAGE CAPABILITY OF FGB ENCLOSURES

4-10

FIGURE 4.1-6 STOWAGE CAPABILITY OF FGB ENCLOSURES

4-11

FIGURE 4.1-7 STOWAGE CAPABILITY OF FGB ENCLOSURES

4-12

DCN XXX

DCN 001

4.2 NODE 1 (ZENITH 1 INCLUDED)

The ASC for cargo stowage inside Node 1 consists of two ZSR’s (Zero-gravity Stowage Rack) and one RSR (Resupply Stowage Rack) and Node 1 Galley with minimal stowage capability (5 CTBE). Each ZSR has front adjustable shelves and a rear ‘pocket’ which is only accessible when the ZSR is rotated outward. The RSR has front accessible fixed shelves. Additional ASC is available in the alcove corridor, on panel fronts, in the overhead docking port, and in the Z1 vestibule (see location NOD1O2).

Node 1 ASC by rack bay is shown in Table 4.2-1, Node 1 ASC, with stowage operational impacts identified for those relevant locations (e.g. rack front stowage).

Node 1 rack locations are identified in Figure 4.2-1, Node 1 Location Reference, (a topology type format), and can also be located pictorially in Figures 4.2-2, Node 1 Port/Overhead ‘Rack Front’ Stowage Capability, and 4.2-3, Node 1 Starboard/Deck ‘Rack Front’ Stowage Capability; the volumes shown in blue were determined by calculating the total bounded volume in each bay and hatchway to show the available stowage capability that is not within rack bays or racks which were designed specifically for stowage. Items of different sizes can be stowed within the volume available.

4-13

DCN XXX

DCN 001

TABLE 4.2-1 NODE 1 ASC

Node 1 Identifier m3 CTBE Comments

Bay 0 Hatch(Lab) 2 Fireports

Bay1 Alcove

Deck (on front) NOD1D1 0.37 7 3 Fireports

O/H (on front) NOD1O1 0.37 7 1 Fireport

Port (on front) NOD1P1

0.26 5

3 Fireports

1 RMO

Stbd (on front) NOD1S1 0.29 5.5 1 RMO

Bay2 Radial Ports

Stbd A/L NOD1S2

0 0

2 Fireports 2 RMOs

Not an Approved Stowage Location

Deck – Berthing Port NOD1D2

1.32/0* 25/0* 2 Fireports 2 RMOs

Port - Node 3 NOD1P2

0 0

2 Fireports

1 RMO

PEP LOCKER

Not an Approved Stowage Location

O/H (on front) NOD1O2

1.05 20

2 IMV I/Os 1 Diffuser

Z1 NOD1O2 0.74 14

Relocate overhead radial port stowage before access

Bay3 midbay

Stbd NOD1S3 0.32 6 2 Fireports

Deck NOD1D3 0 0

Not an Approved Stowage Location

Port NOD1P3

0 0

3 Fireports

1 RMO

Not an Approved Stowage Location

O/H NOD1O3 0.37 7 2 Fireports

Bay4 Racks EEGS

ZSR NOD1S4

1.16 22

1 Fireport

1 IMV I/O

RSR NOD1D4 0.95 18 2 Fireports

Rack front NOD1D4 0.68 13

Galley Rack NOD1P4 0.26 5

ZSR NOD1O4 1.16 22

4-14

DCN XXX

DCN 001

TABLE 4.2-1 NODE 1 ASC

Node 1 Identifier m3 CTBE Comments

Bay5 hatch

(PMA1)

1 Fireport 2 RMOs

Total Node 1

ASC

9.3/7.9 176.5/151.5*

* Stowage is removed when visiting vehicle is berthed

Acronyms and Abbreviations

EEGS Emergency Egress Guidance System

IMV I/O Intermodule Ventilation Inlet or Outlet

O/H Overhead

RMO Remote Manual Override

Stbd Starboard

(Shown is a typical rack/bay configuration which may be modified periodically as mission requirements dictate.

Current configuration can be accessed at https://iss-www.jsc.nasa.gov/nwo/seio/vcer/cammp/web/ic_WorkingTopologies.shtml)

FIGURE 4.2-1 NODE 1 LOCATION REFERENCE

4-15

DCN XXX

DCN 001

(Shown is a typical rack/bay configuration which may be modified periodically as mission requirements dictate.)

FIGURE 4.2-2 NODE 1 PORT/OVERHEAD ‘RACK FRONT’ STOWAGE CAPABILITY

4-16

(Shown is a typical rack/bay configuration which may modified periodically as mission requirements dictate.)

FIGURE 4.2-3 NODE 1 STARBOARD/DECK ‘RACK FRONT’ STOWAGE CAPABILITY

4-17

DCN XXX

4.3 UNITED STATES LABORATORY

The ASC for cargo stowage in the U.S. Lab (laboratory) consists of RSR’s, ZSRs, empty rack bays and portions of the payload racks. There is no ASC on U.S. Lab rack fronts.

U.S. Lab ASC is shown in Table 4.3-1, U.S. Laboratory ASC, with stowage operational impacts identified for those relevant locations (e.g. rack front stowage). U.S. Lab rack locations are identified in Figure 4.3-1, U.S. Laboratory Location Reference, (a topology type format) and can also be located pictorially in isometric type Figures 4.3-2, U.S.

Laboratory STBD/Deck Stowage Capability and 4.3-3, U.S. Laboratory Overhead/Port Stowage Capability.

The following Acronyms and Abbreviations relate to Table 4.3-1:

Acronyms and Abbreviations

ARS Air Revitalization System

AV Avionics

CHeCS Crew Health Care System

CIR Combustion Integrated Rack

CMRS Crew Medical restraint System

DDCU Direct Current-to-Direct Current Converter Unit

EEGS Emergency Egress Guidance System

EMER Emergency

Exp Experiment

EXPR Express Rack

FIR Fluids Integrated Rack

MELFI Minus Eighty-degree Laboratory Freezer for ISS

MSG Microgravity Science Glovebox

MSRR Material Science Research Rack

MSS Mission Specialist Station

RSR Resupply Stowage Rack

TCS Thermal Control System

U.S. United States

WORF Window Observational Research Facility

ZSR Zero-gravity Stowage Rack

4-18

DCN XXX

DCN 001

TABLE 4.3-1 U.S. LABORATORY ASC

Lab Identifier m3 CTBE Comments

Bay 1

MELFI-3 LAB1S1 0.05 1

Av-2 LAB1D1 0 0 Not an Approved Stowage Location

Rackless (Robonaut) LAB1P1 1.15 22

EXPR-2 LAB1O1 0.08 1.5 Varies based on exp installations

Bay 2

MSG LAB1S2 0.10 2

Av-3 LAB1D2 0 0 Not an Approved Stowage Location

EXPR-7 LAB1P2 0.08 1.5 Varies based on exp installations

EXPR-1 LAB1O2 0.08 1.5 Varies based on exp installations

Bay 3

CIR LAB1S3 0 0 Not an Approved Stowage Location

WORF Window LAB1D3 0 0 Not an Approved Stowage Location

DDCU-1 (CEVIS) LAB1P3 0.43 8.2

MSRR-1 LAB1O3 0 0

Bay 4

FIR LAB1S4 0 0 Not an Approved Stowage Location

RSR (CHeCS) LAB1D4 0.94 18

EXPR-8 LAB1P4 0.08 1.5 Varies based on exp installations

Galley (EXPR-6) LAB1O4 0.08 1.5 Varies based on exp installations

Bay 5

MSS/AV LAB1S5 0.34 6.5

Av-1 (CMRS) LAB1D5 0 0

Maintain access to CMRS

Not an Approved Stowage Location

MSS/AV LAB1P5 0.34 6.5

ZSR LAB1O5 1.15 22

Bay 6 EEGS

TCS LAB1S6 0 0 Not an Approved Stowage Location

ARS-1 (CMRS) LAB1D6

0 0

Maintain access to CMRS

Not an Approved Stowage Location

TCS LAB1P6 0 0 Not an Approved Stowage Location

DDCU-2 LAB1O6 0 0 Not an Approved Stowage Location aft hatch PEP LOCKER

Total Lab ASC 6.60 93.7

4-19

(Shown is a typical rack/bay configuration which may be modified periodically as mission requirements dictate.

https://iss-www.jsc.nasa.gov/nwo/seio/vcer/cammp/web/ic_WorkingTopologies.shtml. All ASC in the U.S. Laboratory is internal to rack bays, there is no rackfront ASC.)

FIGURE 4.3-1 U.S. LABORATORY LOCATION REFERENCE

4-20

(Shown is a typical rack/bay configuration which may be modified periodically as mission requirements dictate. All ASC in the U.S. Laboratory is internal to rack bays, there is no rackfront ASC)

FIGURE 4.3-2 U.S. LABORATORY STBD/DECK STOWAGE CAPABILITY

4-21 DCN 001

(Shown is a typical rack/bay configuration which may be modified periodically as mission requirements dictate. All ASC in the U.S. Laboratory is internal to rack bays, there is no rackfront ASC)

FIGURE 4.3-3 U.S. LABORATORY OVERHEAD/PORT STOWAGE CAPABILITY

4-22 DCN 001

4.4 JOINT AIRLOCK

The ASC for cargo in the Joint A/L (Airlock) consists of racks, pallets, bins, bags, and behind closeouts in the Equipment Lock and Crewlock.

The Joint A/L is mainly used to stow EVA (Extravehicular Activity) equipment as well as EVA and A/L spares equipment. However, the Joint A/L can handle other hardware stowage as long as it is certified for vacuum operations or removed when the A/L atmospheric pressures will be reduced below certified levels. In addition to complying with Generic Groundrules and Constraints and HR ISS-STO-0801-AC, stowage should also:

1. Not block Relief Valve Outlet or Sample Probe

2. Not block or contact:

a) Nitrogen Oxygen Recharge System (NORS) Manifold Vent Holes,

b) NORS Closeout Cover,

c) NORS O2 (N2) Recharge Rank, or

d) The Recharge Regulators or Hoses

3. Not block screens on A/L1A2 Y4 panel and below the Umbilical Interface Assembly (UIA) Regulator.

4. Not block the oxygen venting pathway behind the closeout at A/L1D2 from the Prebreathe Regulator out to the top half of the Mesh Screen in the Cloth Panel.

5. Not block the operation of the Battery Stowage Assembly Door.

Joint Airlock ASC is shown in Table 4.4-1, Joint Airlock ASC, with stowage operational impacts identified for those relevant locations (e.g. rack front stowage). Joint Airlock rack locations are identified in Figure 4.4-1, Joint Airlock Location Reference, (a topology type format).

4-23 DCN 001

TABLE 4.4-1 JOINT AIRLOCK ASC

Airlock Identifier m3 CTBE Comments

Deck/Node behind close-out A/L1D0

0.21 4

Deck Pallet A/L1D1 0.21 4 EEGS

Deck Bins A/L1D1 0.26 5 EEGS

Deck/Crewlock behind close-out A/L1D2

0.15 3 Must not block Oxygen 'leak' vent and pathway

Overhead/Node behind close-out A/L1O0

0.21/0 4/0 Without/With NORS/AIK installed

Overhead Pallet A/L1O1 0.0.63/0.21 12/4 Without/With NORS/AIK installed.

Overhead Bins A/L1O1 0.26/0.13 5/2.5 Without/With NORS/AIK installed

CCAA Rack (on face) A/L1A1

0.42 8

Used only for EMU on EDDA Fireport clearance

Avionics Rack (on face) A/L1F1

0.42 8

Used only for EMU on EDDA Fireport clearance

Avionics Rack (in rack) A/L1F1 0.26 5 Fireport clearance

Crewlock nosecone bags A/L1C/L 0.24 4.5

Attic (behind Overhead Pallet) A/L1O1_1

0.36/0 7/0 Without/With NORS/AIK installed

Basement (behind Deck Pallet) A/L1D1_1

0.37 7

Crewlock 'corridor' A/L1C/L

2.11 40

Permanent NCR-ISS-STO-002-9S Relocate all items during U.S. EVA's or when crewlock UIA and /or GLAs are powered

Total Airlock ASC 6.11/4.99 116.5/95 Without/With NORS/AIK installed

Acronyms and Abbreviations

CCAA Common Cabin Air Assembly

C/L Crewlock

EDDA EMU Don/Doff Assembly

EEGS Emergency Egress Guidance System

EMU Extravehicular Mobility Unit

GLA General Luminaire Assembly

UIA Umbilical Interface Assembly

4-24 DCN 001

(Shown is a typical rack/bay configuration which may be modified periodically as mission requirements dictate.

https://iss-www.jsc.nasa.gov/nwo/seio/vcer/cammp/web/ic_WorkingTopologies.shtml.)

FIGURE 4.4-1 JOINT AIRLOCK LOCATION REFERENCE

4-25 DCN 001

4.5 NODE 2

The ASC for cargo inside Node 2 consists of small volumes within two DDCU racks, several panel fronts, and the three available docking ports when visiting vehicles are not docked or berthed.

Node 2 ASC is shown by location in Table 4.5-1, Node 2 ASC, with any stowage operational impacts identified for those relevant locations (e.g. rack front stowage). In addition to complying with Generic Groundrules and Constraints and HR ISS-STO- 0801-AC, stowage shall not block access to the Rack Power Switches (RPS’s ) of the Node 2 avionics rack.

Node 2 rack locations are identified in Figure 4.5-1, Node 2 Location Reference, (a topology type format) and can also be located pictorially in isometric type Figures 4.5-2, Node 2 Deck/Port ‘Rack Front” stowage Capability, and 4.5-3, Node 2 Forward Stowage

Capability; the volumes shown in blue were determined by calculating the total bounded volume in each bay and hatchway to show the available stowage capability that is not within rack bays or racks which were designed specifically for stowage. Items of different sizes can be stowed within the volume available.

The following Acronyms and Abbreviations relate to Table 4.5-1:

COL Columbus

CQ Crew Quarters

DDCU Direct Current-to-Direct Current Converter Unit

EEGS Emergency Egress Guidance System

ESA European Space Agency

IMV I/O Intermodule Ventilation Inlet or Outlet

JEM Japanese Experiment Module

JPM JEM Pressurized Module

O/H Overhead

RMO Remote Manual Override

Stbd Starboard

USL U.S. Laboratory

VV Visiting Vehicle

4-26 DCN 001

TABLE 4.5-1 NODE 2 ASC

Node 2 Identifier m3 CTBE Comments

0 hatch 0.89 17 4 Fireports

1 Alcove 2.11 40 IC-1509

Deck (on front) NOD2D1 1 IMV I/O

O/H (on front) NOD2O1 1 IMV I/O

Port (on front) NOD2P1 1 RMO

Stbd (on front) NOD2S1

1 RMO

1 IMV I/O

2 Ports

Stbd - COL NOD2S2 0 0

6 Fireports 2 RMOs

PEP LOCKER

Not an Approved Stowage Location

Deck (on front) NOD2D2 1.84/0* 35/0*

5 Fireports 2 RMOs (cover if no VV)

1 IMV I/O

Port - JPM NOD2P2 0 0

5 Fireports 2 RMOs

PEP LOCKER

Not an Approved Stowage Location

O/H (on front) NOD2O2 1.16 22 6 Fireports 2 RMOs (cover if no VV) 2 IMV I/Os

3 midbay

Deck NOD2D3 0.26 5 3 Fireports

O/H NOD2O3 0 0

2 Fireports

I IMV I/O

Not an Approved Stowage Location

Port NOD2P3 0.32 6 4 Fireports

Stbd NOD2S3 0 0

4 Fireports

1 IMV I/O

Not an Approved Stowage Location

Bay 4 11 total Fireports

DDCU JEM-2 NOD2S4 0 0

Not an Approved Stowage Location

DDCU ESA-1 NOD2D4 0.23 4.5

Rackfront NOD2D4 0.68 13 4 Fireports

DDCU ESA-2 NOD2P4 0 0

Not an Approved Stowage Location

DDCU JEM-1 NOD2O4 0.21 4

Rackfront NOD2O4 0.21 4 3 Fireports

Bay 5

EEGS

7 total Fireports

4-27 DCN 001

CQ-2 NOD2S5 0 0

Not an Approved Stowage Location

CQ-1 NOD2D5 0 0

Not an Approved Stowage Location

CQ-3 NOD2P5 0 0

Not an Approved Stowage Location

CQ-4 NOD2O5 0 0

Not an Approved Stowage Location

6 End cone 0 2 RMOs

Total ASC 5.8/4.0* 150.5/115.5*

* Stowage removed from hatchway when a visiting vehicle is berthed

(Shown is a typical rack/bay configuration which may be modified periodically as mission requirements dictate.

FIGURE 4.5-1 NODE 2 LOCATION REFERENCE

4-28 DCN 001

FIGURE 4.5-2 NODE 2 FORWARD/DECK/PORT ‘RACK FRONT’ STOWAGE CAPABILITY

4-29 DCN 001

FIGURE 4.5-3 NODE 2 FORWARD STOWAGE CAPABILITY

4.6 PRESSURIZED MATING ADAPTER 1 (PMA-1)

ASC for cargo inside PMA-1 is available only when lining the interior walls. PMA-1 ASC is shown in Table 4.6-1, PMA-1 ASC.

TABLE 4.6-1 PMA-1 ASC

Stowage Area

Stowage Identifier

ASC

m3 CTBEs Comments

PMA-1 Total 1.58 30 Maintain crew translation path

4.7 PRESSURIZED MATING ADAPTER 2 (PMA-2)

ASC for cargo inside PMA-2 is available for only those items which can survive the expected environmental conditions should a puncture occur as a result of an MMOD (Micrometeoroid Orbital Debris) impact. Normally pressure is maintained within PMA-2.

PMA-2 ASC is shown in Table 4.7-1, PMA-2 ASC, with stowage operational impacts identified.

4-30 DCN 001

TABLE 4.7-1 PMA-2 ASC

Stowage Area Stowage Identifier

ASC Comments m3 CTBEs

PMA-2 Total 1.82 34.5 Pressurized and isolated (hatch closed) from habitable volume MMOD and environmental concerns

Shell heaters nominally enabled

4.8 PRESSURIZED MATING ADAPTER 3 (PMA-3)

ASC for cargo inside PMA-3 is available for only those items which can survive the expected environmental conditions should a puncture occur as a result of an MMOD (Micrometeoroid Orbital Debris) impact. Normally pressure is maintained within PMA-3.

PMA-3 ASC is shown in Table 4.8-1, PMA-3 ASC, with stowage operational impacts identified

TABLE 4.8-1 PMA-3 ASC

PMA-3 Stowage Identifier

ASC Comments m3 CTBEs

PMA-3 Total 1.82 34.5 Pressurized and isolated (hatch closed) from habitable volume

MMOD and environmental concerns

Shell heaters nominally enabled

4-31 DCN 001

4.9 NODE 3

The ASC for cargo stowage inside Node 3 consists of the axial hatch port, the Alcove in bay 1, and bay 2 unused hatch port(s) because of ARED (Advanced Resistive Exercise Device) operations in Bay 2. The functionality of Node 3 for exercise and WHC (Waste and Hygiene Compartment) activities precludes using Bays 4 and 5 for rack front stowage.

Node 3 ASC is shown in Table 4.9-1, Node 3 ASC, with stowage operational impacts identified for those relevant locations (e.g. rack front stowage). Node 3 rack locations are identified in Figure 4.9-1, Node 3 Location Reference, (a topology type format) and can also be located pictorially in isometric type Figures 4.9-2, Node 3 Port/Aft/Deck ‘Rack Front’ Stowage Capability, 4.9-3, Node 3 Overhead/Forward ‘Rack Front’ Stowage Capability, and 4.9-4, Node 3 Axial Hatch Stowage Capability; the volumes shown in blue were determined by calculating the total bounded volume in each bay and hatchway to show the available stowage capability that is not within rack bays or racks which were designed specifically for stowage. Items of different sizes can be stowed within the volume available.

4-32 DCN 001

TABLE 4.9-1 NODE 3 ASC

Node 3 Identifier m3 CTBE Comments

0 hatch 0.95 18 4 Fireports

1 Alcove 2.27 43

Aft (on front) NOD3A1 1 Fireport

Deck (on front) NOD3D1

2 Fireports

PEPS LOCKER CTB

Fwd (on front) NOD3F1

1 Fireport

O/H (on front) NOD3O1 1 Fireport

2 Ports

Aft - (on front) ARED

(swinging) NOD3A2

0 0

7 Fireports

1 RMO

ARED

BEAM Berthed

Deck - Cupola NOD3D2

0 0

4 Fireports 2 RMOs

1 IMV I/O

Not an Approved Stowage Location

Fwd - (on front) PMM NOD3F2 0 0

6 Fireports

1 RMO

PMM

O/H - (on front) ARED (mount) NOD3O2

0.94 18

6 Fireports

1 RMO

1 IMV I/O

ARED

3 midbay

Aft NOD3A3 0.32 6 2 Fireports

Deck NOD3D3

0 0

3 Fireports

Not an Approved Stowage Location

Fwd NOD3F3

0.11 2

3 Fireports 2 IMV I/Os

O/H NOD3O3 0.21 4 1 Fireports

Bay 4 11 total Fireports

ARS-2 NOD3A4

0 0

Not an Approved Stowage Location

WRS-2 NOD3D4

0 0

Not an Approved Stowage Location

WHC NOD3F4

0 0

Not an Approved Stowage Location

AV-1 NOD3O4

0 0

Not an Approved Stowage Location

Bay 5

7 total Fireports

OGS NOD3A5

0 0

Not an Approved Stowage

4-33 DCN 001

Node 3 Identifier m3 CTBE Comments

WRS-1 NOD3D5

0 0

Not an Approved Stowage Location

T2 NOD3F5

0 0

Not an Approved Stowage Location

AV-2 NOD3O5

0 0

Not an Approved Stowage

6 Hatch

6 Fireports 2 RMOs

PEPS LOCKER

Total Node 3 ASC 4.79 91

4-34 DCN 001

Acronyms and Abbreviations

ARED Advanced Resistive Exercise Device

ARS Air Revitalization System

EEGS Emergency Egress Guidance System

Fwd Forward

OGS Oxygen Generation System

IMV I/O Intermodule Ventilation Inlet or Outlet

T2 Second generation Treadmill

PEPS Portable Emergency Provisions System

RMO Remote Manual Override

WHC Waste and Hygiene Compartment

WRS Water Recovery System

(Shown is a typical rack/bay configuration which may be modified periodically as mission requirements dictate.

FIGURE 4.9-1 NODE 3 LOCATION REFERENCE

4-35 DCN 001

(Shown is a typical rack/bay configuration which may be modified periodically as mission requirements dictate.)

FIGURE 4.9-2 NODE 3 PORT/AFT/DECK ‘RACK FRONT’ STOWAGE CAPABILITY

4-36 DCN 001

(Shown is a typical rack/bay configuration which may be modified periodically as mission requirements dictate.)

FIGURE 4.9-3 NODE 3 OVERHEAD/FORWARD ‘RACK FRONT’ STOWAGE CAPABILITY

4-37 DCN 001

4.10 CUPOLA

There is no stowage capability in the Cupola.

4.11 PERMANENT MULTIPURPOSE MODULE (PMM)

The ASC for cargo stowed inside PMM is contained in ZSR’s, RSR’s, RSP’s (Resupply Stowage Platforms), empty rack bays, standoff areas, End cone, on rack fronts, and in the corridor.

PMM ASC is shown in Table 4.11-1, PMM ASC, with stowage operational impacts identified for those relevant locations (e.g. rack front stowage). PMM rack locations are identified in Figure 4.11-2, PMM Locations, (a topology type format) and can be located pictorially in isometric type Figures 4.11-3, PMM ‘Rack Front’ and Corridor Stowage Capability, and 4.11-4, PMM ‘End Cone’ Stowage Capability, which use purple “boxes” to depict available stowage capability that is not within rack bays or racks which were designed specifically for stowage. Each purple box represents a single CTB. The purple boxes should only be used to determine available stowage capability in specific locations. Items of different sizes can be stowed within the volume available.

Limitations (reference Chit 9631):

1. Stowage on each rack front is limited to a 39” tall x 39.5” wide CTB footprint that extends 16.75” from the rack face and is centered on the rack to avoid impinging on the diffuser KOZ.

2. Stowage in the corridor is limited to a 50.25” tall x 39” wide x 39.5” deep footprint in each of bays 2, 3, and 4, leaving a 5.8” clear pathway from the Air Diffusers to the Air Returns on each side (Figure 4.11-1).

4-38 DCN 001

FIGURE 4.11-1 PMM DIFFUSER KEEP OUT ZONES

Image 2 – Ideal PMM Stowage configuration graphic

4-39 DCN 001

TABLE 4.11-1 PMM ASC (PAGE 1 OF 2)

PMM Identifier m3 CTBE Comments

Bay 1 EEGS

Corridor PMM1C1 0 0 See Limitation 2

Deck - Rack front PMM1D1 0.42 8 See Limitation 1

Port - Rack front PMM1P1 0.42 8 See Limitation 1

Ovhd - Rack front PMM1O1 0.42 8 See Limitation 1

Stbd - Rack front PMM1S1 0.42 8 1 Fireport See Limitation 1

Deck - ZSR PMM1D1 1.15 22 Relocate Rack front stowage before access

Port - <Rackless> PMM1P1 1.80 34 Relocate Rack front stowage before access

Ovhd - RSR 0007 PMM1O1 0.94 18 Relocate Rack front stowage before access

Stbd - <Rackless> PMM1S1 1.80 34 Relocate Rack front stowage before access

Deck/Port standoff PMM1DP1 0.21 4 Rack rotation or adjacent stowage removal required

Deck/Stbd standoff PMM1DS1 0.21 4 Rack rotation or adjacent stowage removal required

Bay 2

Corridor PMM1C2 0.84 16 Relocate before Rack front access See Limitation 2

Deck - Rack front PMM1D2 0.42 8 See Limitation 1

Port - Rack front PMM1P2 0.42 8 See Limitation 1

Ovhd - Rack front PMM1O2 0.42 8 See Limitation 1

Stbd - Rack front PMM1S2 0.42 8 See Limitation 1

Deck - ZSR PMM1D2 1.15 22 Relocate Rack front stowage before access

Port - RSP1008 PMM1P2 1.37 26 Relocate Rack front stowage before access

Ovhd - RSR 0014 PMM1O2 0.94 18 Relocate Rack front stowage before access

Stbd - RSP 1006 PMM1S2 1.37 26 Relocate Rack front stowage before access

Deck/Port standoff PMM1DP2 0.21 4 Rack rotation or adjacent stowage removal required

Deck/Stbd standoff PMM1DS2 0.21 4 Rack rotation or adjacent stowage removal required

Bay 3

Corridor PMM1C3 0.84 16 Relocate before Rack front access See Limitation 2

Deck - Rack front PMM1D3 0.42 8 See Limitation 1

Port - Rack front PMM1P3 0.42 8 See Limitation 1

Ovhd - Rack front PMM1O3 0.42 8 See Limitation 1

Stbd - Rack front PMM1S4 0.42 8 See Limitation 1

Deck - <Rackless> PMM1D3 1.80 34 Relocate Rack front stowage before access

4-40 DCN 001

TABLE 4.11-1 PMM ASC (PAGE 2 OF 2)

PMM Identifier m3 CTBE Comments

Port - <Rackless> PMM1P3 1.80 34 Relocate Rack front stowage before access

Ovhd - ZSR PMM1O3 1.15 22 Relocate Rack front stowage before access

Stbd - RSP 1010 PMM1S3 1.37 26 Relocate Rack front stowage before access

Deck/Port standoff PMM1DP3 0.21 4 Rack rotation or adjacent stowage removal required

Deck/Stbd standoff PMM1DS3 0.21 4 Rack rotation or adjacent stowage removal required

Bay 4

Corridor PMM1C4 0.84 16 Relocate before Rack front access See Limitation 2

Deck - Rack front PMM1D4 0.42 8 See Limitation 1

Port - Rack front PMM1P4 0.42 8 See Limitation 1

Ovhd - Rack front PMM1O4 0.42 8 See Limitation 1

Stbd - Rack front PMM1S4 0.42 8 See Limitation 1

Deck - RSR 0002 PMM1D4 0.94 18 Relocate Rack front stowage before access

Port - RSR 0016 PMM1P4 0.94 18 Relocate Rack front stowage before access

Ovhd - RSR 0008 PMM1O4 0.94 18 Relocate Rack front stowage before access

Stbd - ZSR PMM1S4 1.15 22 Relocate Rack front stowage before access

Deck/Port standoff PMM1DP4 0.21 4 Rack rotation or adjacent stowage removal required

Deck/Stbd standoff PMM1DS4 0.21 4 Rack rotation or adjacent stowage removal required

5 End cone 5.80 110

Total PMM ASC 37.33 710

4-41 DCN 001

(Shown is a typical rack/bay configuration which may be modified periodically as mission requirements dictate.

FIGURE 4.11-2 PMM LOCATIONS

4-42 DCN 001

(Boxes represent 1.0 CTB’s)

FIGURE 4.11-3 PMM ‘RACK FRONT’ AND CORRIDOR STOWAGE CAPABILITY

Bay 1

Bay 2

Bay 3

Bay 4

4-43 DCN 001

(Boxes represent 1.0 CTB’s)

FIGURE 4.11-4 PMM ‘END CONE’ STOWAGE…