SSP_50869-Rev_A.docx

DOCX document 3 MB Posted

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

This document provides details for a solicitation for the Human Space Flight Technical Integration Contract (HSFTIC). Key information includes that NASA/JSC plans to issue a Request for Proposal (RFP) with an anticipated release date of November 1, 2019 and offer due date of December 11, 2019. The NAICS code is 541715 with a size standard of 1,250 employees. The procurement is a total small business set-aside. The RFP and any associated documents will be available at the listed websites. Prospective offerors must notify the agency of their intent to submit an offer and are responsible for downloading solicitation documents. All contractual technical questions must be submitted in writing. The Center Ombudsman information is also provided.

SSP 50869-Rev A

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
HSFTIC J-17 placeholder (FRFP).docx DOCX document
HSFTIC Interested Parties List - Rev. 1.pdf PDF
MD_1015_RA_FINAL.docx DOCX document
SSP41142P1_RF_CD_012044_.pdf PDF
42097P1_AE_RF_012968.pdf PDF
SSP41017p1rG.pdf PDF
SSP41143Pt1RevC.PDF PDF
6.0.zip ZIP file
N_PR_9501_002E_.pdf PDF
SSP_50316-Rev_C.docx DOCX document
SSP_57011_Rev_E.docx DOCX document
Applicable_5.zip ZIP file
ISS_Program_Flight_Rate.pptx PPTX presentation
MD_1040_FINAL_PSF_US_Charter.docx DOCX document
SSP_50578-RevC.docx DOCX document
42097P2RE_AE_RE_012967.pdf PDF
DSG-PLAN-004_Gateway_Configuration_and_Data_Management_Plan_Baseline.pdf PDF
SSP_50826.doc DOC document
SSP-50615_Baseline.doc DOC document
Subsystem_&_Mission_Functions_to_Modules.xlsx XLSX spreadsheet
Gateway_generic_org_chart.pptx PPTX presentation
SSP_50038.DOC DOC document
SSP_50190-RevF.docx DOCX document
SSP-50715_RevA.docx DOCX document
SSP_50273_Rev_J.docx DOCX document
50281.DOC DOC document
SSP_50469-RevD-Retired.docx DOCX document
Initial_Baseline_DSG-CONOP-001_06_2019.docx DOCX document
POH_Vol_2_2-2-18.pdf PDF
SSP_50200-01-ANXZ-RevB_SPIP_OZ.docx DOCX document
SSP_50744-Rev_A.docx DOCX document
ssp42097_p2_rd.pdf PDF
SSP_52055_Revision_D.doc DOC document
Work_Load_Indicators_Matrix_FRFP.xlsx XLSX spreadsheet
SSP_41140_P2_RD_111010.pdf PDF
SSP_42007-Rev_L-SSCD_15992.docx DOCX document
SSP_50420-HTV3-Baseline.docx DOCX document
Signed_Approved_Charter_31Aug08_IRT_Charter.doc DOC document
SSP_41147,_Part_1_Rev_C.pdf PDF
SSP_42121-Part_1-RevC.docx DOCX document
SSP_50754-RevA-DCN001-EAR99.docx DOCX document
SSP_50839-RevB-DCN001-Collated_Master.pdf PDF
SSP41148.pdf PDF
PALSTORE.PROD.O0073170.G0000001.IL TXT text file
SSP_30575-RevF.docx DOCX document
SSP_41165-RevN.docx DOCX document
SSP_50005_Rev_G.pdf PDF
SSP_50309_Part_2.pdf PDF
DRFP_Industry_Questions_and_Answers.pdf PDF
Draft_HSFTIC_Request_for_Proposal.pdf PDF
Show all 50

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

On GovTribe

Work with this file on GovTribe

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

Text version

Prime Item Development Specification for the Permanent Multipurpose Module (PMM)

International Space Station Program

Revision A

September 2010

National Aeronautics and Space Administration International Space Station Program Johnson Space Center Houston, Texas Contract No. NNJ09GA18B

SSP 50869

Revision A

REVISION AND HISTORY PAGE

REV.
DESCRIPTION
PUB. DATE
-
Initial Release (Reference per SSCD 011801R2, EFF. 08/09/10)
08-16-10
A
Revision A (Reference per SSCD 012421, EFF. 09/22/10)
10-05-10

SSP 50869

Revision A

PREFACE

Prime Item Development Specification for the Permanent Multipurpose Module (PMM) This document is developed and maintained by the NASA PMM Project Office. This document is under the control of the Space Station Control Board (SSCB).

The initial baseline release of this document is under the control of the SSCB. The SSCB delegates control and approval authority for future updates and/or revisions to the Multilateral Vehicle Control Board (MVCB).

INTERNATIONAL SPACE STATION PROGRAM

for the Permanent Multipurpose Module (PMM)

CONCURRENCE

august 2010 for the Permanent Multipurpose Module (PMM)

CONCURRENCE

august 2010

Prime item development specification for the permanent Multipurpose module (pMm)

LIST OF CHANGES

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

Board Name

Entry Date

Change

Paragraph(s)

August 2010

Baseline

All

October 2010

Revision A

All v

TABLE OF CONTENTS

PARAGRAPHPAGE
1.0SCOPE1-1
1.1Identification1-1
1.2System overview1-1
2.0documents2-1
2.1applicable documents2-1
2.1.1specifications, standards, and handbooks2-1
2.1.2Other government documents, drawings, and publications2-2
2.2Meet or exceed2-9
3.0system requirements3-1
3.1system definition3-1
3.1.1System functional description3-1
3.1.2Mission Scenario3-1
3.1.2.1Ground Operations Scenario3-1
3.1.2.2Launch and On-Orbit Scenario3-1
3.1.2.3Contingency Scenarios3-2
3.1.3Integrated system functional diagram3-3
3.1.4Interface requirements3-4
3.1.4.1External interfaces3-4
3.1.4.1.1Orbiter external interface description3-4
3.1.4.1.2Launch/landing site support facilities external interface description3-4
3.1.4.1.3United States On-orbit Segment (USOS) external interface description3-4
3.1.4.1.3.1Portable Fire Extinguisher (PFE) external interface description3-4
3.1.4.1.3.2Portable Breathing Apparatus (PBA) external interface description3-4
3.1.4.1.3.3IntraVehicular Activity restraints and mobility aids interfaces3-5
3.1.4.1.3.4EXtraVehicular Activity translation aids and attachments Interfaces3-5
3.1.4.1.3.5CAUTION AND WARNING (C&W) DEVICE INTERFACES3-5
3.1.4.1.3.6PMM pcbm TO Node 1 acbm Thermal Conduction interface3-5
3.1.4.1.4Space Station Remote Manipulator System (SSRMS) external interface description3-11
3.1.4.1.5Rack external interface3-11
3.1.4.1.6Refrigerator/Freezer Rack external interface description3-11
3.1.4.1.7Re-supply stowage platform external interface3-11
3.1.4.1.8PMM to Ground Support Equipment interface description3-11
3.1.4.2Internal interfaces3-11
3.1.4.2.1PCBM interface3-11
3.1.4.2.2Hatch interface3-11
3.2Characteristics3-11
3.2.1Performance characteristics3-11
3.2.1.1State: Perform mission on-orbit3-11
3.2.1.1.1Capability3-12
3.2.1.1.1.1Relieve overpressure3-12
3.2.1.1.1.2Equalize pressure3-12
3.2.1.1.1.3Circulate atmosphere3-12
3.2.1.1.1.4Control internal lighting3-12
3.2.1.1.1.5Illuminate internal areas3-12
3.2.1.1.1.6Isolate to recovery level3-13
3.2.1.1.1.7Recover lost function3-13
3.2.1.1.1.8Isolate for safing3-13
3.2.1.1.1.9Safe3-13
3.2.1.1.1.9.1Re-attempt safing3-13
3.2.1.1.1.9.2Demand safing3-13
3.2.1.1.1.9.3Confirm successful safing3-13
3.2.1.1.1.10Maintain station mode3-13
3.2.1.1.1.11Transition station modes3-14
3.2.1.1.1.12Generate functional data3-14
3.2.1.1.1.13Assess functional status data3-14
3.2.1.1.1.14Acquire hazardous condition data3-14
3.2.1.1.1.15Identify hazardous condition3-14
3.2.1.1.1.16Respond to fire3-14
3.2.1.1.1.17Respond to hazardous atmosphere3-15
3.2.1.1.1.18Deleted3-15
3.2.1.1.1.19Deleted3-15
3.2.1.1.1.20Distribute power3-15
3.2.1.1.1.21Collect thermal energy3-19
3.2.1.1.1.22Distribute thermal energy3-19
3.2.1.1.1.23Distribute time3-19
3.2.1.1.1.24Support internal crew restraint and mobility3-19
3.2.1.1.1.25Provide direct visual access3-19
3.2.1.1.1.26Deleted3-19
3.2.1.1.1.27Provide data for downlink3-19
3.2.1.1.1.28Deleted3-19
3.2.1.1.1.29Deleted3-19
3.2.1.1.1.30Manage time3-19
3.2.1.1.1.30.1Maintain time3-19
3.2.1.1.1.30.2Control Time3-20
3.2.1.1.1.31Provide time interface3-20
3.2.1.1.1.31.1Receive time3-20
3.2.1.1.1.31.2Provide time services3-20
3.2.1.1.1.31.3Distribute time3-20
3.2.1.1.1.32Atmosphere sampling3-20
3.2.1.1.1.33Respond to rapid decompression3-20
3.2.1.1.1.34Annunciate alarms3-20
3.2.1.1.1.35Micro-gravity disturbances3-20
3.2.1.1.1.35.1Limit quasi−steady accelerations3-20
3.2.1.1.1.35.2Limit vibratory accelerations3-20
3.2.1.1.1.36Limit angular momentum disturbances3-21
3.2.1.1.1.36.1Limit disturbance induced ISS attitude rate Limit disturbance3-21
3.2.1.1.1.36.2Limit disturbance induced CMG MOMENTUM3-22
3.2.1.2DELETED3-23
3.2.1.3State: Support mission3-23
3.2.1.3.1Mode: Ground processing3-23
3.2.1.3.1.1Load and unload cargo items3-23
3.2.1.3.1.2Support system check-out and monitoring.3-23
3.2.1.3.2Mode: Space transport3-24
3.2.1.3.2.1Transport internal cargo3-24
3.2.2Physical characteristics3-24
3.2.2.1Tare weight3-24
3.2.2.2Launch envelope3-25
3.2.2.2.1External diameter3-25
3.2.2.2.2Axial length3-25
3.2.2.3Distribute commands and data3-25
3.2.2.4External NASA/ASI insignia emblem3-25
3.2.2.4.1External NASA insignia emblem3-25
3.2.2.4.2External ASI insignia emblem3-25
3.2.3Reliability3-25
3.2.3.1Flight system reliability3-25
3.2.3.1.1Failure tolerance3-25
3.2.3.1.2Failure propagation3-25
3.2.3.1.3Separation of redundant paths3-25
3.2.3.1.4Redundancy3-26
3.2.4Maintainability3-26
3.2.4.1Flight system maintainability3-26
3.2.4.1.1Qualitative maintainability design3-26
3.2.4.1.1.1Equipment item interconnecting devices3-26
3.2.4.1.1.2Incorrect equipment installation3-26
3.2.4.1.1.3Lockwiring and staking3-26
3.2.4.1.1.4PMM Mean Maintenance Crew Hours Per Year3-26
3.2.4.1.1.5Access item retention3-26
3.2.4.1.2Failure Detection, Isolation, and Recovery (FDIR)3-26
3.2.4.1.2.1Automatic hazard and hazardous condition detection3-26
3.2.4.1.2.2Automatic anomaly detection3-26
3.2.4.1.2.3Manual FDIR3-27
3.2.4.1.2.4Manual control of FDIR3-28
3.2.4.1.2.5Deleted3-28
3.2.4.1.2.6Automatic safing verification3-28
3.2.4.1.2.7Testing at operation location3-28
3.2.4.1.2.8Ambiguity resolution3-28
3.2.4.1.2.9Data availability3-28
3.2.4.1.2.10False alarm mitigation3-28
3.2.5Availability3-28
3.2.6Environmental conditions3-28
3.2.6.1Flight system environmental conditions3-28
3.2.6.1.1On-orbit environmental conditions3-28
3.2.6.1.1.1Thermal environment3-29
3.2.6.1.1.2Neutral atmosphere3-31
3.2.6.1.1.3External contamination3-31
3.2.6.1.1.4Electric and geomagnetic fields3-31
3.2.6.1.1.5Plasma3-32
3.2.6.1.1.6Ionizing radiation3-32
3.2.6.1.1.7Solar ultraviolet radiation3-32
3.2.6.1.1.8Micro Meteoroids and Orbital Debris (MMOD)3-33
3.2.6.1.1.9Deleted3-33
3.2.6.1.1.10Plume impingement pressures3-33
3.2.6.1.1.11Atomic oxygen3-33
3.2.6.1.2ascent/descent thermal environment3-33
3.2.7Transportability3-33
3.2.7.1PMM transportability3-33
3.2.8PLANAR REFLECTOR INTERFACE REQUIREMENTS3-34
3.2.8.1PLAnar reflector location3-34
3.2.8.2PLAnar reflector structural interface3-34
3.2.8.2.1Alignment tolerance3-34
3.2.8.2.2planar reflector flatness3-34
3.2.8.2.3planar reflector Structural Interface Temperature limits3-34
3.2.8.2.4planar reflector vibration limits3-34
3.3Design and construction3-35
3.3.1Materials, processes, and parts3-35
3.3.1.1PMM materials, processes, and parts3-35
3.3.1.1.1Materials and processes3-35
3.3.1.1.2Electrical, Electronic, and Electromechanical (EEE) parts3-35
3.3.1.1.2.1EEE parts selection3-35
3.3.1.1.3Static age life3-36
3.3.2Electromagnetic Radiation (EMR)3-36
3.3.2.1PMM Electromagnetic Compatibility (EMC) requirements3-36
3.3.2.1.1Grounding3-36
3.3.2.1.2Cabling and wire design3-36
3.3.2.1.3Electrical bonding3-36
3.3.2.1.4Power conducted disturbance3-36
3.3.2.1.5Equipment Electromagnetic Interference (EMI) requirements3-37
3.3.2.1.6Electromagnetic interference safety margins for critical circuits3-37
3.3.2.1.7Launch element transportation, storage, and launch environment3-37
3.3.2.1.8Static electricity3-37
3.3.2.1.9Corona3-37
3.3.2.1.10Selection and use of equipment3-37
3.3.3Nameplates and product markings3-37
3.3.3.1PMM nameplates and product markings3-37
3.3.3.1.1Labeling3-38
3.3.4Workmanship3-38
3.3.4.1PMM workmanship3-38
3.3.4.2PMM cleanliness3-38
3.3.5Interchangeability3-38
3.3.6Safety3-38
3.3.6.1General3-38
3.3.6.1.1Catastrophic hazards3-38
3.3.6.1.1.1Deleted3-39
3.3.6.1.1.2Deleted3-39
3.3.6.1.2Critical hazards3-39
3.3.6.1.3Design for minimum risk3-39
3.3.6.1.4Control of functions resulting in critical hazards3-39
3.3.6.1.4.1Inadvertent operation resulting in critical hazards3-39
3.3.6.1.4.2Loss of function resulting in critical hazards3-39
3.3.6.1.5Control of functions resulting in catastrophic hazards3-39
3.3.6.1.5.1Inadvertent operation resulting in catastrophic hazards3-39
3.3.6.1.5.2Loss of function resulting in catastrophic hazards3-40
3.3.6.1.6Subsequent induced loads3-40
3.3.6.1.6.1Deleted3-40
3.3.6.1.7Safety interlocks3-40
3.3.6.1.8Environmental compatibility3-40
3.3.6.2Hazard detection and safing3-40
3.3.6.2.1Reserved3-40
3.3.6.2.2Monitors3-40
3.3.6.2.2.1Status information3-40
3.3.6.2.2.2Hazardous function operation prevention3-41
3.3.6.2.2.3Loss of input or failure3-41
3.3.6.2.2.4Launch site availability3-41
3.3.6.2.2.5Flight crew availability3-41
3.3.6.2.3Near-real-time monitoring3-41
3.3.6.2.4Real-time monitoring3-41
3.3.6.2.4.1Maintain status of hazard controls3-41
3.3.6.2.4.2Crew response time and safing procedures3-41
3.3.6.2.4.3Deleted3-41
3.3.6.3Command and computer control of hazardous functions3-41
3.3.6.3.1Computer control of hazardous functions3-41
3.3.6.4Hazardous materials3-47
3.3.6.4.1Hazardous fluid containment3-47
3.3.6.5Pyrotechnics3-47
3.3.6.6Radiation3-47
3.3.6.6.1Non-ionizing radiation3-47
3.3.6.6.2Ionizing radiation crew limits3-47
3.3.6.6.3PMM transmitters3-47
3.3.6.7optics and lasers3-47
3.3.6.8electical safety3-47
3.3.6.8.1electrical power circuit overloads3-47
3.3.6.8.1.1circuit overload protection3-47
3.3.6.8.1.2protective device sizing3-47
3.3.6.8.1.3bent pin or conductive contamination3-47
3.3.6.8.2crew protection for electrical shock3-47
3.3.6.8.3reapplication of power3-48
3.3.6.8.4batteries3-48
3.3.6.9cryogenics3-48
3.3.6.10fire protection3-48
3.3.6.10.1reserved3-48
3.3.6.10.2isolation3-48
3.3.6.10.3suppression3-48
3.3.6.10.4suppressant3-48
3.3.6.10.5restorable suppression3-48
3.3.6.10.6power removal3-48
3.3.6.10.7portable equipment3-48
3.3.6.10.7.1set co-location3-48
3.3.6.10.8confirmation3-50
3.3.6.11constraints3-50
3.3.6.11.1reserved3-50
3.3.6.11.2pressurized volume depressurization and re-pressurization tolerance3-50
3.3.6.11.2.1pressure differential tolerance3-50
3.3.6.11.2.2operation during pressure changes3-50
3.3.6.11.3emergency egress3-50
3.3.6.11.4reserved3-51
3.3.6.11.5reserved3-51
3.3.6.11.6component hazardous energy provision3-51
3.3.6.11.7hatch opening3-51
3.3.6.11.8reserved3-51
3.3.6.11.9reserved3-51
3.3.6.11.10reserved3-51
3.3.6.11.11reserved3-51
3.3.6.11.12hazardous Gas accumulation3-51
3.3.6.11.12.1accumulation prevention3-51
3.3.6.11.13equipment clearance for entrapment hazard3-51
3.3.6.11.14light fixture3-51
3.3.6.12human engineering safety3-51
3.3.6.12.1internal volume touch temperature3-51
3.3.6.12.1.1continuous contact - high temperature3-51
3.3.6.12.1.2incidental or momentary contact - high temperature3-51
3.3.6.12.1.3internal volume low touch temperature3-52
3.3.6.12.2external touch temperature3-52
3.3.6.12.2.1incidental contact3-52
3.3.6.12.2.2unlimited contacT3-52
3.3.6.12.3external corner and edge protection3-52
3.3.6.12.3.1sharp edges3-52
3.3.6.12.3.2thin materials3-53
3.3.6.12.4internal corner and edge protection3-53
3.3.6.12.4.1equipment exposed to crew activity3-53
3.3.6.12.5reserved3-53
3.3.6.12.6latches3-53
3.3.6.12.7screws and bolts3-53
3.3.6.12.8safety critical fasteners3-53
3.3.6.12.9levers, cranks, hooks and controls3-53
3.3.6.12.10burrs3-53
3.3.6.12.11holes3-54
3.3.6.12.11.1equipment located inside habitable volumes3-54
3.3.6.12.11.2equipment located outside habitable volumes3-54
3.3.6.12.12protrusions3-54
3.3.6.12.13pinch points3-54
3.3.6.12.14reserved3-54
3.3.6.12.15reserved3-54
3.3.6.12.16flexhoses3-54
3.3.6.12.17translation routes and established worksites3-54
3.3.6.12.17.1Primary translation routes and established worksites3-54
3.3.6.12.17.2secondary translation routes and eStablished worksites3-54
3.3.6.12.17.3eva crewmember contact isolation3-54
3.3.6.12.18moving or rotating equipment3-55
3.3.6.13launch vehicle interfaces and services3-56
3.3.6.13.1safe without space shuttle program services3-56
3.3.6.13.1.1fault tolerance/safety margins3-56
3.3.6.13.1.2termination of services due to orbiter emergency conditions3-56
3.3.6.13.2critical orbiter services3-56
3.3.6.13.3inadvertent deployment, separation, and jettison functions3-56
3.3.6.13.4planned deployment/extension functions3-56
3.3.6.13.4.1violation of orbiter payload door envelope3-56
3.3.6.13.4.2method of fault tolerance3-56
3.3.6.13.5contingency return and rapid safing3-56
3.3.6.13.5.1deleted3-56
3.3.6.13.5.2deleted3-56
3.3.6.14flammable atmosphere3-56
3.3.6.14.1normal functions3-56
3.3.6.14.2electrical ignition sources3-57
3.3.6.14.3surface temperatures3-57
3.3.6.14.4conductive surfaces3-57
3.3.6.15reserved3-57
3.3.6.16lightning protection3-57
3.3.6.17orbiter vent/dump provisions3-57
3.3.6.17.1release or ejection of hazardous materials3-57
3.3.6.17.2fluid system containment3-57
3.3.6.18sealed compartments3-57
3.3.6.19ground safety requirements for space shuttle launch of PMM hardware3-57
3.3.6.20Indicate emergency egress hatches3-57
3.3.7human engineering3-57
3.3.7.1internal hardware3-57
3.3.7.1.1anthropometric requirements3-57
3.3.7.1.2strength requirements3-58
3.3.7.1.2.1normal and maintenance operations3-58
3.3.7.1.2.2emergency controls3-58
3.3.7.1.3gloved operation3-58
3.3.7.1.4location coding3-58
3.3.7.1.4.1alphanumeric coding3-58
3.3.7.1.4.2reference configuration coordinate system3-58
3.3.7.1.4.3deleted3-58
3.3.7.1.4.4deleted3-58
3.3.7.1.4.5deleted3-58
3.3.7.1.4.6deleted3-58
3.3.7.1.4.7deleted3-58
3.3.7.1.4.8utility accessibility3-58
3.3.7.1.5iva closures and design requirements3-58
3.3.7.1.6iva housekeeping3-58
3.3.7.1.7controls and displays3-59
3.3.7.1.8interior colors3-59
3.3.7.1.9Hand Holds and Hand Rails3-59
3.3.7.1.10Maintenance of Crew Position3-59
3.3.7.2external eva hardware3-59
3.3.7.2.1external task location requirements3-59
3.3.7.2.2eva crewmember field of view3-59
3.3.7.2.3working volume3-59
3.3.7.2.4eva induced loads3-59
3.3.7.2.5repetitive actuation forces3-61
3.3.7.2.6crew aids for worksite stability3-61
3.3.7.2.6.1placement for worksite tasks3-61
3.3.7.2.6.2proximity to foot restraint3-61
3.3.7.2.6.3foot restraing ingress and egress aid3-61
3.3.7.2.6.4height considerations3-61
3.3.7.2.6.5centering3-61
3.3.7.2.7glove clearance3-61
3.3.7.2.8primary translation path marking3-61
3.3.7.2.9translation path3-61
3.3.7.2.10handrail spacing3-61
3.3.8nuclear control3-62
3.3.9system security3-62
3.3.10environmental constraints3-62
3.3.10.1flight system environmental constaints3-62
3.3.10.1.1acoustic emission limits3-62
3.3.10.1.2external contamination releases3-62
3.3.10.1.3ionizing radiation emission limits3-62
3.3.10.1.4internal temperature limits during transfer of PMM3-63
3.3.10.1.5internal temperature limits edward afb operations and ferry flight of PMM3-63
3.3.11design for remote controlled external operations3-63
3.3.11.1equipment requiring shuttle robotic support3-63
3.3.11.2external equipment requiring robotic hand-off3-63
3.3.11.3External equipment requiring ssrms support3-63
3.3.11.3.1equipment requiring ssrms support using an nsts gf3-65
3.3.12design requirements3-65
3.3.12.1PMM design requirements3-65
3.3.12.1.1structural design requirements3-65
3.3.12.1.1.1structure penetrations3-65
3.3.12.1.1.2window, glass, and ceramic structural design3-65
3.3.12.1.1.3fracture control3-66
3.3.12.1.1.4allowabLE mechanical properties3-66
3.3.12.1.1.5on-orbit loads3-66
3.3.12.1.1.5.1on-orbit pressure spectra3-66
3.3.12.1.1.5.2on-orbit transient loads3-66
3.3.12.1.1.5.3on-orbit thermally induced loads3-68
3.3.12.1.2fluid handling requirements3-68
3.3.12.1.2.1fluid standards3-68
3.3.12.1.2.2fluid quantity3-68
3.3.12.1.2.3interface hardware3-69
3.3.12.1.2.4flexible lines and bellows design3-69
3.3.12.1.3fasteners3-69
3.3.12.1.4internal atmosphere3-69
3.3.12.1.4.1maximum design pressure3-69
3.3.12.1.4.2atmospheric leakage3-69
3.3.12.1.5operational life3-69
3.3.12.1.6carrier mating/de-mating3-69
3.3.12.1.6.1bertHing stay - out zones3-69
3.3.12.1.7element access3-69
3.3.12.1.8preclude condensation3-70
3.3.12.1.9support internal equipment removal and replacement3-70
3.3.12.1.10iva translation path obstructions3-70
3.3.12.1.11iva restrainT for non - permanent equipment3-70
3.3.12.1.12GENERAL MOUNTING3-70
3.3.12.2iva connectors3-70
3.3.12.3external hardware3-70
3.3.12.3.1eva equipment handling capabilities3-70
3.3.12.4alignment devices3-70
3.3.12.5cable management3-71
3.3.13mil-std-1553 data bus addresses3-71
3.3.14mil-std-1553 data bus constraints3-71
3.3.14.1ssq components3-71
3.3.14.1.1bus coupler type3-71
3.3.14.2bus stub length3-71
3.3.14.3bus coupling3-72
3.3.15terminal interface units3-72
3.3.15.1input impedance3-72
3.3.15.2tiu multiple bus isolation3-73
3.3.16PMM not-to exceed bus length3-73
3.4computer resource requirements3-73
3.4.1flexibility and expansion3-73
3.5logistics3-73
3.5.1maintenance3-73
3.5.1.1on-orbit maintenance3-73
3.5.1.1.1corrective maintenance3-74
3.5.1.1.2in situ maintenance3-74
3.5.1.1.3oru intermediate maintenance3-74
3.5.1.1.4preventive maintenance3-74
3.5.1.1.5pressurized volume rack rotation3-74
3.5.1.2on-orbit maintenance backup3-74
3.5.1.3access for on-orbit maintenance3-74
3.5.1.3.1access for on-orbit inspection3-74
3.5.1.3.2visual access3-74
3.5.1.3.3eva access to fasteners3-74
3.5.1.3.4physical access3-74
3.5.1.3.4.1deleted3-74
3.5.1.3.5removal, replacement, and modularity design3-74
3.5.1.4standard on-orbit tools3-75
3.5.1.5standard on-orbit diagnostic equipment3-76
3.5.1.6ground maintenance3-76
3.6personnel and training3-76
3.7chAracteristics3-76
3.8precedence3-77
4.0quality assurance provisions4-1
4.1general4-2
4.1.1responsibility for verifications4-3
4.1.2particular instructions applicable to PMM verification4-3
4.2PMM quality conformance inspections4-3
4.3system requirements4-4
4.3.1system definition4-4
4.3.1.1system functional description4-4
4.3.1.2mission sCENARIO4-4
4.3.1.2.1GROUND OPERATIONS sCENARIO4-4
4.3.1.2.2LAUNCH AND ON-ORBIT sCENARIO4-4
4.3.1.2.3CONTINGENCY sCENARIO4-4
4.3.1.3integrated system functional diagram4-4
4.3.1.4interface requirements4-4
4.3.1.4.1external interfaces4-4
4.3.1.4.1.1orbiter external interface description4-4
4.3.1.4.1.2launch/landing site support facilities external interface description4-4
4.3.1.4.1.3united states on-orbit segment (usos) external interface description4-4
4.3.1.4.1.3.1portable fire extinguisher (pfe) external interface description4-4
4.3.1.4.1.3.2portable breathing apparatus (pba) external interface description4-4
4.3.1.4.1.3.3intravehicular activity restraints and mobility aids interface4-5
4.3.1.4.1.3.4extravehicular activity translation aids and attachments interfaces4-5
4.3.1.4.1.3.5CAUTION & WARNING (C&w) DEVICE interfaces4-5
4.3.1.4.1.3.6PMM pcbm TO Node 1 acbm interface4-5
4.3.1.4.1.4space station remote manipulator system (ssrms) external interface description4-5
4.3.1.4.1.5rack external interface4-5
4.3.1.4.1.6refrigerator/freezer rack external interface description4-5
4.3.1.4.1.7re-supply stowage platform external interface4-5
4.3.1.4.1.8PMM to ground support equipment interface description4-5
4.3.1.4.1.9K-BAR/PIVOT PIN INTERFACES4-5
4.3.1.4.2INTERNAL INTERFACES4-5
4.3.1.4.2.1PCBM INTERFACE4-5
4.3.1.4.2.2hatch interface4-5
4.3.2characteristics4-6
4.3.2.1performance characteristics4-6
4.3.2.1.1state: perform mission on-orbit4-6
4.3.2.1.1.1capability4-6
4.3.2.1.1.1.1relieve overpressure4-6
4.3.2.1.1.1.2equalize pressure4-6
4.3.2.1.1.1.3circulate atmosphere4-6
4.3.2.1.1.1.4control internal lighting4-7
4.3.2.1.1.1.5illumination internal areas4-7
4.3.2.1.1.1.6isolate to recovery level4-8
4.3.2.1.1.1.7recover lost function4-8
4.3.2.1.1.1.8isolate for safing4-8
4.3.2.1.1.1.9safe4-8
4.3.2.1.1.1.9.1re-attempt safing4-8
4.3.2.1.1.1.9.2demand safing4-9
4.3.2.1.1.1.9.3confirm successful safing4-9
4.3.2.1.1.1.10maintain station mode4-9
4.3.2.1.1.1.11transition station modes4-9
4.3.2.1.1.1.12generate functional data4-9
4.3.2.1.1.1.13assess functional status data4-9
4.3.2.1.1.1.14acquire hazardous condition data4-10
4.3.2.1.1.1.15identify hazardous condition4-10
4.3.2.1.1.1.16respond to fire4-10
4.3.2.1.1.1.17respond to hazardous atmosphere4-11
4.3.2.1.1.1.18deleted4-11
4.3.2.1.1.1.19deleted4-11
4.3.2.1.1.1.20distribute power4-11
4.3.2.1.1.1.21collect thermal energy4-11
4.3.2.1.1.1.22distribute thermal energy4-12
4.3.2.1.1.1.23distribute time4-12
4.3.2.1.1.1.24Support internal crew restraint and mobility4-12
4.3.2.1.1.1.25provide direct visual access4-13
4.3.2.1.1.1.26deleted4-13
4.3.2.1.1.1.27provide data for downlink4-13
4.3.2.1.1.1.28deleted4-13
4.3.2.1.1.1.29deleted4-13
4.3.2.1.1.1.30manage time4-13
4.3.2.1.1.1.30.1maintain time4-13
4.3.2.1.1.1.30.2control time4-13
4.3.2.1.1.1.31provide time interface4-14
4.3.2.1.1.1.31.1receive time4-14
4.3.2.1.1.1.31.2provide time services4-14
4.3.2.1.1.1.31.3distribute time4-14
4.3.2.1.1.1.32ATMOSPHERE SAMPLING4-14
4.3.2.1.1.1.33respond to rapid decompression4-15
4.3.2.1.1.1.34annunciate alarms4-15
4.3.2.1.1.1.35micro-gravity distrubances4-15
4.3.2.1.1.1.35.1limit quasi-steady accelerations4-15
4.3.2.1.1.1.35.2Limit vibratory accelerations4-15
4.3.2.1.1.1.36limit angular momentum disturbances4-15
4.3.2.1.1.1.36.1limit disturbance induced iss attitude rate4-15
4.3.2.1.1.1.36.2limit disturbance induced cmg momentum usage4-16
4.3.2.1.2deleted4-16
4.3.2.1.3state: support mission4-16
4.3.2.1.3.1mode: ground processing4-17
4.3.2.1.3.1.1load and unload cargo items4-17
4.3.2.1.3.1.2support system checkout and monitoring4-17
4.3.2.1.3.2mode: space transport4-17
4.3.2.1.3.2.1transport internal cargo4-17
4.3.2.2physical characteristics4-18
4.3.2.2.1tare weight4-18
4.3.2.2.2launch envelope4-18
4.3.2.2.2.1external diameter4-18
4.3.2.2.2.2axial length4-18
4.3.2.2.3distribute commands and data4-18
4.3.2.2.4external nasa/ASI insignia emblem4-18
4.3.2.2.4.1external nasa insignia emblem4-18
4.3.2.2.4.2No verification required. external ASI insignia emblem4-18
4.3.2.3reliability4-19
4.3.2.3.1flight system reliability4-19
4.3.2.3.1.1failure tolerance4-19
4.3.2.3.1.2failure propagation4-19
4.3.2.3.1.3separation of redundant path4-19
4.3.2.3.1.4redundancy4-19
4.3.2.4maintainability4-19
4.3.2.4.1flight system maintainability4-19
4.3.2.4.1.1qualitative maintainability design4-19
4.3.2.4.1.1.1equipment item interconnecting devices4-19
4.3.2.4.1.1.2incorrect equipment installation4-20
4.3.2.4.1.1.3lockwiring and staking4-20
4.3.2.4.1.1.4PMM mean maintenance crew hours per year4-20
4.3.2.4.1.1.5ACCESS ITEM RETENTION4-20
4.3.2.4.1.2failure detection, isolation, and recovery (fdir)4-20
4.3.2.4.1.2.1automatic hazard and hazardous condition detection4-20
4.3.2.4.1.2.2automatic anomaly detection4-20
4.3.2.4.1.2.3manual fdir4-20
4.3.2.4.1.2.4manual control of fdir4-20
4.3.2.4.1.2.5deleted4-21
4.3.2.4.1.2.6automatic safing verification4-21
4.3.2.4.1.2.7testing at operation location4-21
4.3.2.4.1.2.8ambiguity resolution4-22
4.3.2.4.1.2.9data availability4-22
4.3.2.4.1.2.10false alarm mitigation4-22
4.3.2.5availability4-22
4.3.2.6environmental conditions4-23
4.3.2.6.1flight system environmental conditions4-23
4.3.2.6.1.1on-orbit environmental conditions4-23
4.3.2.6.1.1.1thermal environment4-23
4.3.2.6.1.1.2neutral atmosphere4-28
4.3.2.6.1.1.3external contamination4-28
4.3.2.6.1.1.4electromagnetic and geomagnetic fields4-28
4.3.2.6.1.1.5plasma4-28
4.3.2.6.1.1.6ionizing radiation4-28
4.3.2.6.1.1.7solar ultraviolet radiation4-29
4.3.2.6.1.1.8micro meteoroids and orbital debris (mmod)4-29
4.3.2.6.1.1.9deleted4-29
4.3.2.6.1.1.10plume impingement pressures4-29
4.3.2.6.1.1.11atomic oxygen4-29
4.3.2.6.1.2ascent/descent thermal environment4-29
4.3.2.7transportability4-29
4.3.2.7.1PMM transportability4-29
4.3.3design and construction4-30
4.3.3.1materials, processes, and parts4-30
4.3.3.1.1PMM materials, processes, and parts4-30
4.3.3.1.1.1materials and processes4-30
4.3.3.1.1.2electrical, electronic, and electromechanical (eee) parts4-31
4.3.3.1.1.2.1eee parts seLEction4-31
4.3.3.1.1.3static age life4-31
4.3.3.2electromagnetic radiation (emr)4-31
4.3.3.2.1PMM electromagnetic compatibility (emc) requirements4-31
4.3.3.2.1.1grounding4-31
4.3.3.2.1.2cabling and wire design4-32
4.3.3.2.1.3electrical bonding4-32
4.3.3.2.1.4power conducted disturbances4-32
4.3.3.2.1.5equipment electromagnetic interference (emi) requirements4-32
4.3.3.2.1.6electromagnetic interference safety margins for critical circuits4-32
4.3.3.2.1.7launch element transportation, storage, and launch environment4-32
4.3.3.2.1.8static electricity4-32
4.3.3.2.1.9corona4-33
4.3.3.2.1.10selection and use of equipment4-33
4.3.3.3nameplates and product markings4-33
4.3.3.3.1PMM nameplates and product markings4-33
4.3.3.3.1.1labeling4-33
4.3.3.4workmanship4-34
4.3.3.4.1PMM workmanship4-34
4.3.3.4.2PMM cleanliness4-34
4.3.3.5interchangeability4-35
4.3.3.6safety4-35
4.3.3.6.1general4-35
4.3.3.6.1.1catastrophic hazards4-35
4.3.3.6.1.1.1deleted4-35
4.3.3.6.1.1.2deleted4-35
4.3.3.6.1.2critical hazards4-35
4.3.3.6.1.3design for minimum risk4-35
4.3.3.6.1.4control of functions of resulting in critical hazards4-35
4.3.3.6.1.4.1inadvertent operations resulting in a critical hazard4-35
4.3.3.6.1.4.2loss of a function resulting in a critical hazard4-36
4.3.3.6.1.5control of functions resulting in a catastrophic hazards4-36
4.3.3.6.1.5.1inadvertent operation resulting in caTastrophic hazards4-36
4.3.3.6.1.5.2loss of function resulting in carastrophic hazards4-36
4.3.3.6.1.6subsequent induced loads4-36
4.3.3.6.1.6.1deleted4-36
4.3.3.6.1.7safety interlocks4-36
4.3.3.6.1.8environmental compatibility4-37
4.3.3.6.2hazard detection and safing4-37
4.3.3.6.2.1reserved4-37
4.3.3.6.2.2monitors4-37
4.3.3.6.2.2.1status information4-37
4.3.3.6.2.2.2hazardous function operation prevention4-37
4.3.3.6.2.2.3loss of input or failure4-37
4.3.3.6.2.2.4launch site availability4-38
4.3.3.6.2.2.5flight crew availability4-38
4.3.3.6.2.3near real - time monitoring4-38
4.3.3.6.2.4real - time monitoring4-38
4.3.3.6.2.4.1maintain status of hazard condtrols4-38
4.3.3.6.2.4.2crew response time and safing procedures4-38
4.3.3.6.2.4.3deleted4-39
4.3.3.6.3command and computer control of hazardous functions4-39
4.3.3.6.3.1computer control of hazardous functions4-39
4.3.3.6.4hazardous materials4-39
4.3.3.6.4.1hazardous fluid containment4-39
4.3.3.6.5pyrotechnics4-39
4.3.3.6.6radiation4-39
4.3.3.6.6.1non - ionizing radiation4-39
4.3.3.6.6.2ionizing radiation crew limits4-39
4.3.3.6.6.3PMM transmitters4-39
4.3.3.6.7optics and lasers4-39
4.3.3.6.8electrical safety4-40
4.3.3.6.8.1electrical power circuit overloads4-40
4.3.3.6.8.1.1circuit overload protection4-40
4.3.3.6.8.1.2protective device sizing4-40
4.3.3.6.8.1.3bent pin or conductive contamination4-40
4.3.3.6.8.2crew protection for electrical shock4-40
4.3.3.6.8.3reapplication of power4-40
4.3.3.6.8.4batteries4-40
4.3.3.6.9cryogenics4-41
4.3.3.6.10fire protection4-41
4.3.3.6.10.1reserved4-41
4.3.3.6.10.2isolation4-41
4.3.3.6.10.3suppression4-41
4.3.3.6.10.4suppressant4-41
4.3.3.6.10.5restorable suppression4-41
4.3.3.6.10.6power removal4-41
4.3.3.6.10.7portable equipment4-41
4.3.3.6.10.7.1set co - location4-41
4.3.3.6.10.8confirmation4-42
4.3.3.6.11constraints4-42
4.3.3.6.11.1reserved4-42
4.3.3.6.11.2pressurized volume depressurization and re - pressurization tolerance4-42
4.3.3.6.11.2.1pressure differential tolerance4-42
4.3.3.6.11.2.2operation during pressure changes4-42
4.3.3.6.11.3emergency egress4-42
4.3.3.6.11.4reserved4-43
4.3.3.6.11.5reserved4-43
4.3.3.6.11.6component hazardous energy provision4-43
4.3.3.6.11.7hatch opening4-43
4.3.3.6.11.8reserved4-43
4.3.3.6.11.9reserved4-43
4.3.3.6.11.10reserved4-43
4.3.3.6.11.11reserved4-43
4.3.3.6.11.12hazardous gas accumulation4-43
4.3.3.6.11.12.1accumulation prevention4-43
4.3.3.6.11.12.2reserved4-43
4.3.3.6.11.13equipment clearance for entrapment hazard4-43
4.3.3.6.11.14light fixture4-44
4.3.3.6.12human engineering safety4-44
4.3.3.6.12.1internal volume touch temperature4-44
4.3.3.6.12.1.1continuous contact - high temperature4-44
4.3.3.6.12.1.2incidental or momentary contact - high temperature4-44
4.3.3.6.12.1.3internal volume low touch temperature4-44
4.3.3.6.12.2external touch temperature4-45
4.3.3.6.12.2.1incidental contact4-45
4.3.3.6.12.2.2unlimited contact4-45
4.3.3.6.12.3external corner and edge protection4-45
4.3.3.6.12.3.1sharp edges4-45
4.3.3.6.12.3.2thin materials4-45
4.3.3.6.12.4internal corner and edge protection4-46
4.3.3.6.12.4.1equipment exposed to crew activity4-46
4.3.3.6.12.5reserved4-46
4.3.3.6.12.6latches4-46
4.3.3.6.12.7screws and bolts4-46
4.3.3.6.12.8safety critical fasteners4-46
4.3.3.6.12.9levers, cranks, hooks, and controls4-46
4.3.3.6.12.10burrs4-47
4.3.3.6.12.11holes4-47
4.3.3.6.12.11.1equpment located inside habitable volumes4-47
4.3.3.6.12.11.2equipment located outside habitable volumes4-47
4.3.3.6.12.12protrusions4-47
4.3.3.6.12.13pinch points4-47
4.3.3.6.12.14reserved4-48
4.3.3.6.12.15reserved4-48
4.3.3.6.12.16flexhoses4-48
4.3.3.6.12.17translation routes and established worksites4-48
4.3.3.6.12.17.1primary translation routes and established worksites4-48
4.3.3.6.12.17.2secondary translation routes and established worksited4-48
4.3.3.6.12.17.3eva crewmember contact isolation4-48
4.3.3.6.12.18moving or rotating equipment4-48
4.3.3.6.13launch vehicle interfaces and services4-49
4.3.3.6.13.1safe without space shuttle program services4-49
4.3.3.6.13.1.1fault tolerance/safety margins4-49
4.3.3.6.13.1.2termination of services due to orbiter emergency conditions4-49
4.3.3.6.13.2critical orbiter services4-49
4.3.3.6.13.3inadvertent deployment, separation, and jettison functions4-49
4.3.3.6.13.4planned deployment/extension functions4-49
4.3.3.6.13.4.1violation of orbiter payload door envelope4-49
4.3.3.6.13.4.2method of fault tolerance4-50
4.3.3.6.13.5contingency return and rapid safing4-50
4.3.3.6.13.5.1deleted4-50
4.3.3.6.13.5.2deleted4-50
4.3.3.6.14flammable atmosphere4-50
4.3.3.6.14.1normal functions4-50
4.3.3.6.14.2electrical ignition sources4-50
4.3.3.6.14.3surface temperatures4-51
4.3.3.6.14.4conductive surfaces4-51
4.3.3.6.15reserved4-51
4.3.3.6.16lightning protection4-51
4.3.3.6.17orbiter vent/dump provisions4-51
4.3.3.6.17.1release or ejection of hazardous material4-51
4.3.3.6.17.2fluid system containment4-51
4.3.3.6.18sealed compartments4-51
4.3.3.6.19ground safety requirements for space shuttle launch of PMM hardware4-52
4.3.3.6.20Indicate emergency egress hatches4-52
4.3.3.7human engineering4-52
4.3.3.7.1internal hardware4-52
4.3.3.7.1.1anthropometric requirements4-52
4.3.3.7.1.2strength requirements4-52
4.3.3.7.1.2.1normal and maintenance operations4-52
4.3.3.7.1.2.2emergency controls4-53
4.3.3.7.1.3gloved operation4-53
4.3.3.7.1.4location coding4-53
4.3.3.7.1.4.1alphanumeric coding4-53
4.3.3.7.1.4.2reference configuration coordinate system4-53
4.3.3.7.1.4.3deleted4-54
4.3.3.7.1.4.4deleted4-54
4.3.3.7.1.4.5deleted4-54
4.3.3.7.1.4.6deleted4-54
4.3.3.7.1.4.7deleted4-54
4.3.3.7.1.4.8utility accessibility4-54
4.3.3.7.1.5iva closures and design requirements4-54
4.3.3.7.1.6iva housekeeping4-54
4.3.3.7.1.7colors and displays4-54
4.3.3.7.1.8interior colors4-55
4.3.3.7.1.9Hand Holds and Hand Rails4-55
4.3.3.7.1.10MAINTENANCE OF CREW POSITION4-55
4.3.3.7.2external eva hardware4-55
4.3.3.7.2.1external task location requirements4-55
4.3.3.7.2.2eva crewmember field of view4-55
4.3.3.7.2.3working volume4-55
4.3.3.7.2.4eva induced loads4-55
4.3.3.7.2.5repetitive actuation forces4-55
4.3.3.7.2.6crew aids for worksite stability4-55
4.3.3.7.2.6.1placement of worksite tasks4-55
4.3.3.7.2.6.2proximity of foot restraint4-56
4.3.3.7.2.6.3foot restraing ingress and egress aid4-56
4.3.3.7.2.6.4height considerations4-56
4.3.3.7.2.6.5centering4-56
4.3.3.7.2.7glove clearance4-56
4.3.3.7.2.8primary translation path marking4-56
4.3.3.7.2.9tranSlation path4-56
4.3.3.7.2.10hand rail spacing4-56
4.3.3.8Nuclear control4-56
4.3.3.9System security4-56
4.3.3.10Environmental constraints4-56
4.3.3.10.1Flight system environmental constraints4-56
4.3.3.10.1.1Acoustic emission limits4-56
4.3.3.10.1.2External contamination releases4-56
4.3.3.10.1.3Ionizing radiation emission limits4-57
4.3.3.10.1.4Internal temperature limits during transfer of PMM4-57
4.3.3.10.1.5Internal temperature limits during Edwards AFB operations and ferry flight of PMM4-57
4.3.3.11Design for remote controlled external operations4-57
4.3.3.11.1equipment requiring shuttle robotic support4-57
4.3.3.11.2External equipment requiring robotic hand-off4-57
4.3.3.11.3External equipment requiring SSRMS support4-57
4.3.3.11.3.1Equipment requiring SSRMS support using an NSTS GF4-58
4.3.3.12Design requirements4-59
4.3.3.12.1PMM design requirements4-59
4.3.3.12.1.1Structural design requirements4-59
4.3.3.12.1.1.1Structure penetrations4-59
4.3.3.12.1.1.2Window, glass, and ceramic structural design4-59
4.3.3.12.1.1.3Fracture control4-59
4.3.3.12.1.1.4Allowable mechanical properties4-59
4.3.3.12.1.1.5On-orbit loads4-60
4.3.3.12.1.1.5.1On-orbit pressure spectra4-60
4.3.3.12.1.1.5.2On-orbit transient loads4-60
4.3.3.12.1.1.5.3On-orbit thermally induced loads4-60
4.3.3.12.1.2Fluid handling requirements4-60
4.3.3.12.1.2.1Fluid standards4-60
4.3.3.12.1.2.2Fluid quantity determination4-60
4.3.3.12.1.2.3Interface hardware4-60
4.3.3.12.1.2.4Flexible lines and bellows design4-60
4.3.3.12.1.3Fasteners4-60
4.3.3.12.1.4Internal atmosphere4-61
4.3.3.12.1.4.1Maximum design pressure4-61
4.3.3.12.1.4.2Atmospheric leakage4-61
4.3.3.12.1.5Operational life4-61
4.3.3.12.1.6Carrier mating/de-mating4-61
4.3.3.12.1.6.1Berthing stay-out zones4-62
4.3.3.12.1.7Element access4-62
4.3.3.12.1.8Preclude condensation4-62
4.3.3.12.1.9Support internal equipment removal and replacement4-62
4.3.3.12.1.10IVA translation path obstructions4-62
4.3.3.12.1.11IVA restraint for non-permanent equipment4-63
4.3.3.12.1.12General Mounting4-63
4.3.3.12.2IVA Connectors4-63
4.3.3.12.3External Hardware4-63
4.3.3.12.3.1EVA equipment handling capabilities4-63
4.3.3.12.4Alignment devices4-63
4.3.3.12.5Cable management4-63
4.3.3.13MIL-STD-1553 data bus addresses4-63
4.3.3.14MIL-STD-1553 data bus constraints4-64
4.3.3.14.1SSQ components4-64
4.3.3.14.1.1Bus coupler type4-64
4.3.3.14.2Bus stub length4-64
4.3.3.14.3Bus coupling4-64
4.3.3.15Terminal interface units4-64
4.3.3.15.1Input impedance4-64
4.3.3.15.2TIU multiple bus isolation4-65
4.3.3.16PMM not-to-exceed bus length4-65
4.3.4Computer resource requirements4-65
4.3.4.1Flexibility and expansion4-65
4.3.5Logistics4-65
4.3.5.1Maintenance4-65
4.3.5.1.1On-orbit maintenance4-65
4.3.5.1.1.1Corrective maintenance4-65
4.3.5.1.1.2In situ maintenance4-65
4.3.5.1.1.3ORU intermediate maintenance4-66
4.3.5.1.1.4Preventive maintenance4-66
4.3.5.1.1.5Pressurized volume rack rotation4-66
4.3.5.1.2On-orbit maintenance back-up4-66
4.3.5.1.3Access for on-orbit maintenance4-66
4.3.5.1.3.1Access for on-orbit inspection4-66
4.3.5.1.3.2Visual access4-67
4.3.5.1.3.3EVA access to fasteners4-67
4.3.5.1.3.4Physical access4-67
4.3.5.1.3.4.1Deleted4-67
4.3.5.1.3.5Removal, replacement, and modularity design4-67
4.3.5.1.4Standard on-orbit tools4-67
4.3.5.1.5Standard on-orbit diagnostic equipment4-67
4.3.5.1.6Ground maintenance4-68
4.3.6Personnel and training4-68
4.3.7Characteristics4-68
4.3.8Precedence4-68
5.0preparation for delivery5-1
5.1general5-1
5.2detailed preparation5-1
5.2.1preservation and packaging5-1
6.0notes6-1
6.1definitions6-1
6.2acronyms and abbreviations6-8

APPENDIX

arequirement exceptionsA-1
Bopen workB-1
CPMM Bilateral Integrated Verification Plan (BIVP)C-1

TABLE

1PMM flight system power allocations3-15
2Maximum angular momentum impulse3-22
3CMG Momentum usage calculation3-23
4Functions required for 24-hour autonomous operation3-27
5FLIGHT ATTITUDE ENVELOPES FOR VEHICLE DESIGN – ORBITER ATTACHED OPERATIONS3-29
6FLIGHT ATTITUDE ENVELOPES FOR VEHICLE DESIGN – STAGE (ORBITER NOT ATTACHED) OPERATIONS3-29
7Hot and cold natural thermal environment3-30
8Extreme hot and cold natural thermal environment3-31
9Parameters for MMOD environment definition3-33
9.1pmm planar reflector vibration environment3-35
10Equivalent ESA/SCC parts3-36
11SSP 50038 applicability matrix3-42
12iva crew induced loads at the interface3-49
13fluid interfaces portable fire extinguisher3-49
14heat transfer rate3-52
15PMM interior colors3-59
16eva induced loads3-60
17moBile servicing centre robotic payload properties3-63
18berthing contact conditions3-64
19ssrms backdrive threshold3-64
20force/moment accommodation3-65
21on-orbit pressure spectra3-66
22limit load conditions3-66
23on-orbit transient load spectra3-67
24resultant berthing contact forces (limit)3-67
25constrainTs for single eva crewmember transport of objects3-70
26standard iva tool list3-75
26standard iva tool list - continued3-76
B-1to be determined itemsB-1
B-2TO BE RESOLVED ISSUESB-1

FIGURE

1Integrated system functional block diagram3-3
2PMM to PFE interface3-6
3PFE envelope3-7
4PMM side of R&MA structural interface3-8
5R&MA entry/exit envelope to PMM (Configuration 1)3-9
6R&MA entry/exit envelope to PMM (Configuration 2)3-10
7Fire protection selection criteria3-16
8PMM vibro−acoustic microgravity acceleration limits3-21
9PMM rack load envelope3-24
10On-orbit electric field environment3-32
11center of gravity (pfe)3-50
12eva zones - top view looking down into cargo bay3-55
13eva zones - end view looking at the PMM aft end cone in the cargo bay3-55
14Deleted3-55
15crewmember optimum work envelope3-59
16crewmember field of view3-59
17eva work volume and incidental contact volume3-60
18crew aids for stability3-61
19foot restraint ingress and egress aid3-61
20minimum clearance for gloved hand access3-62
21envelope for Handrail-assisted translation3-62
22load application diagram3-68
23typical bus3-72
24tiu minimum input impedance3-73
24design cold thermal environment profile4-24
25Design hot thermal environment profile4-25
26extreme cold thermal environment profile4-26
27EXTREME HOT THERMAL ENVIRONMENT PROFILE4-27

xxvii

SCOPE

This specification establishes the performance, design, development, and qualification requirements for the Permanent Multipurpose Module (PMM).

Identification This specification is for the PMM that will be a modification of the MPLM Flight Unit FM-1 (Leonardo) developed by ASI and delivered to NASA. The PMM Part Number: is 0000P001-805, the Serial Number is 00001 and the NASA ISS Configuration Item (CI) number of the upgraded MPLM is ISSA15A.

System overview The purpose of the PMM is to provide:

a. Logistics re-supply and transportation of user passive cargo and payloads for use by the on-orbit Space Station, as per the Flight ULF5 upload manifest;

b. Additional pressurized volume for stowage of cargo at the ISS, when docked to Node 1 Nadir.

1-1 documents applicable documents specifications, standards, and handbooks The following specifications, standards, and handbooks of the exact issue shown, form a part of this specification to the extent specified herein. In the event of a conflict between the documents referenced herein and the contents of this specification, the contents of this specification shall be considered a superseding requirement.

MILITARY STANDARDS

MIL-D-3464 Rev. E April 21, 1987 Desiccants, Activated, Bagged, Packaging Use and Static Dehumidification

MIL-STD-130 Rev. G October 11, 1988 Identification Marking of US Military Property

MIL-STD-1553 Rev. B, Notice 2 September 8, 1986 Digital Time Division Command/Response Multiplex Data Bus

MILITARY HANDBOOKS

MIL-HDBK-5, Rev. E June 1, 1987 Metallic Materials and Elements for Aerospace Vehicle Structures

MIL-HDBK-17 Rev. B, Notice 1 February 29, 1988 Polymer Matrix Composites Volume 1:Guidelines

MIL-HDBK-1553A plus Notice 1, 2, and 3 1 November 1998Multiplex Application Handbook

Other government documents, drawings, and publications The following other government documents, drawings, and publications of the exact issue shown, form a part of this specification to the extent specified herein.

SPECIFICATIONS

JSC-SN-C-0005 Rev. C February 15, 1989 NSTS Contamination Control Requirement Manual

JSC 27260, Rev. E Date: January, 2006 Decal Process Document and Catalog

KHB 1700.7, Rev. C August 19, 1999 STS Payload Ground Safety Handbook

NHB 6000.1, Rev. D September 30, 1990 Requirements for Packaging, Handling, and Transportation for Aeronautical and Space Systems, Equipment and Associated Components

NHB 8060.1, Rev. C April 2, 1991 Flammability, Odor, and Offgassing Requirements and Test Procedures for Materials in Environments that Support Combustion

NP 212 Current Issue NASA Graphics Standard, NASA Insignia

NSTS 1700.7 Rev. B, PCN 1 February 24, 1993 Safety Policy and Requirements for Payloads using the Space Transportation System

ICD-A-21499-MPLM-A ,

June 15, 2009 Shuttle Orbiter/MPLM-A Cargo Element Interfaces

NSTS 07700, Volume XIV June 1989 Space Shuttle System Payload Accommodations

NSTS 07700, Appendix 1 Rev. J, Change 1 June 1989 Contamination Environment

NSTS 07700, Appendix 2 Rev. J, Change 1 June 1989 System Description and Design Data-Thermal

NSTS 07700, Appendix 3 Rev. J, Change 2 June 1989 Electrical Power and Avionics

NSTS 07700, Appendix 4 Rev. J, Change 1 June 1989 Structures and Mechanisms

NSTS 07700, Appendix 5 Rev. K, Change 1 July 31, 1991 Ground Operations

NSTS 07700, Appendix 6 Rev. J October 4, 1988 Mission Planning and Flight Design

NSTS 07700, Appendix 7 Rev. J, Change 1 June 1989 Extravehicular Activities

NSTS 07700, Appendix 8 Rev. J, Change 1 June 1989 Payload Deployment and Retrieval System

NSTS 07700, Appendix 9 Rev. K December 16, 1992 Intravehicular Activities

NSTS 07700, Appendix 10 Rev. J, Change 1 June 1989 Integration Hardware

NSTS 08123 Rev. B March 28, 1991 Certification of Flex Hoses and Bellows for Flow Induced Vibration

NSTS 14046 Rev. C Including Numbered Updates 1 and 2 April 1994 Payload Verification Requirements

NSTS 20793

September 28, 1985 Manned Space Vehicle Battery Safety Handbook

SSP 30219, Rev. J Space Station Reference Coordinate Systems

SSP 30233, Rev. F March 6, 1998 Space Station Requirements for Materials and Processes

SSP 30234, Rev. D August 5, 1994 Instructions for Preparation of Failure Modes and Effects Analysis and Critical Items List for Space Station

SSP 30237, Rev. J Space Station Electromagnetic Emission and Susceptibility Requirements (except paragraph 3.2.1.3.2 for which Rev. B shall apply)

SSP 30238, Rev. C May 31, 1996 Space Station Electromagnetic Techniques (except paragraphs 3.2.4.1.3, 3.2.4.1.4.2, 3.2.4.1.5, Figures 3-1 and 3-6 for which Rev. B shall apply)

SSP 30240, Rev. F Space Station Grounding Requirements

SSP 30242, Rev. D, DCN 001, 002 May 31, 1996 Space Station Cable/Wire Design and Control Requirements for Electromagnetic Compatibility

SSP 30243, Rev. H Space Station Requirements for Electromagnetic Compatibility (except paragraphs 2.0, 3.2.2, 3.2.5, 3.2.10, 3.2.11, 3.5.3, 3.6.2.1, 3.6.2.1.1, 3.6.2.1.5, Appendix D, and Appendix E for which Rev. B shall apply)

SSP 30245, Rev. J Space Station Electrical Bonding Requirements (except paragraph 3.3.7 for which Rev. B shall apply)

SSP 30245

EMECB Tailoring Interpretation Agreement (TIA) 0031

SSP 30309 F

Safety Analysis and Risk Assessment Requirement Document

SSP 30312, Rev. J Electrical, Electronic, and Electromechanical and Mechanical Parts Management and Implementation Plan for Space Station Program

SSP 30420, Rev. B June 18, 1993 Space Station Electromagnetic, Ionizing Radiation and Plasma Environment Definition and Design Requirements

SSP 30423, Rev. F March 31, 1995 Space Station Approved Electrical, Electronic, and Electromechanical Parts List

SSP 30425, Rev. B February 8, 1994 Space Station Program Natural Environment Definition for Design

SSP 30426, Rev. D, DCN 001 January 21, 1994 Space Station External Contamination Control Requirements

SSP 30482, Vol. I Rev. A, DCN 001 January 2, 1994 Electrical Power Specifications and Standards: Vol. I, EPS Electrical Power Specifications

SSP 30482, Vol. II Rev. A, DCN 001, 002 January 1, 1994 Electrical Power Specifications and Standards: Vol. II, Consumer Constraints

SSP 30512, Rev. C June 3, 1994 Space Station Ionizing Radiation Design Environment

SSP 30558, Rev. B June 30, 1994 Fracture Control Requirements for Space Station

SSP 30559, D

Structural Design and Verification Requirements

SSP 30560, Rev. Basic June 1, 1991 Glass, Window and Ceramic Structural Design and Verification Requirements

SSP 30575, Rev. E April, 2007 Space Station Interior and Exterior Operational Location Coding System

SSP 30599, Rev. D September 2006 Safety Review Process

SSP 41004, Revision H, Part 1 October 25, 2005 Common Berthing Mechanism to Pressurized Elements Interface Control Document, Part 1

SSP 41004, Revision G, Part 2 Date: April 30, 1998 Common Berthing Mechanism to Pressurized Elements Interface Control Document, Part 2

SSP 41015, Rev. G, Part 1 Common Hatch and Mechanisms to Pressurized Elements Interface Control Document (Part 1)

SSP 41015, Rev. F Part 2 Date: July 29,1999 Common Hatch and Mechanisms to Pressurized Elements Interface Control Document (Part 2)

SSP 41017, Rev. G, Part 1 Rack To Mini-Pressurized Logistics Module Interface Control Document (Part 1)

SSP 41017, Rev. F, Part 2 November 13, 1998 Rack To Mini-Pressurized Logistics Module Interface Control Document (Part 2)

SSP 41172, Rev. J March 30, 2001 Qualification and Acceptance Environment Test Requirement

SSP 42004, Rev. H, Part 1 Mobile Servicing System (MSS) to User (Generic) Interface Control Document Part 1

SSP 42004, Rev. A, Part 2 Date: May 22, 1997 Mobile Servicing System (MSS) to User (Generic) Interface Control Document Part 2

SSP 42007, Rev. H, Part 1 December 31, 2002 United States On-orbit Segment to Italian to Mini-Pressurized Logistics Module Interface Control Document Part 1

SSP 42007, Rev. H, Part 2 Date:June 29, 1999 United States On-orbit Segment to Italian to Mini-Pressurized Logistics Module Interface Control Document Part 2

SSP 50004, Rev. Basic, DCN 001, 002 February 1, 1994 Ground Support Equipment Design Requirements (except paragraph 3.6.7.1 where Revision Basic plus CN001 shall apply)

SSP 50005, Rev. E June 30, 2006 International Space Station Flight Crew Integration Standard (NASA-STD-3000/T)

SSP 50007, Rev. D February, 2006 Space Station Inventory Management System Label Specification

SSP 50014, Rev. B September 3, 1997 International Space Station Utility Coding Specification

SSP 50023, Rev. Basic April 15, 1994 Thermal Control Plan

SSP 50038, Rev. B November 17, 1995 Computer Based Control System Safety Requirements

SSP 50104, Rev. A.

November 1996 Portable Breathing Apparatus Standard Interface Control Document Part 1

SSP 50110, Rev. J Multi-Increment Manifest Document

SSP 50228-6, Rev. Basic September, 1997 Space Station Program Configuration and Assembly Standard Interface Control Document, Volume 6: Advanced Vision Function To Multi Purpose Logistics Module

SSP 50699, Rev. B December, 2008 ISS Certification Baseline Volume 3: Flight Attitudes

SSQ 26000, Rev. Basic, October 16, 1996 Space Station Program Office Standard Repair for Sharp Edges on SSQ 21635 NZGL Type Connector Assemblies and Components

SSP 50342, Rev. Initial Release May 1998 MIL-STD-1553 Remote Terminal Test Exceptions Report

SSP 30256:001, Rev. H July 17, 2006 Extravehicular Activity (EVA) Standard Interface Control Document

SSP 30256:010 Basic
Portable Fire Extinguisher Interface Control Document

SSP 30257:004, Rev. E Space Station Program Intravehicular Activity Restraints and Mobility Aids Interface Control Document

SSP 41148, Rev. D September 30, 1998 Active Common Berthing Mechanism to Passive Common Berthing Mechanism Interface Control Document, Part 1

STANDARDS

OTHER PUBLICATIONS

SID 82K00760, Rev. D April 15, 1993 Standard Interface Document Space Station Processing Facility

D684-10058-2 Rev. A May 15, 1997 Plume Impingement Heat Rate Report, Volume 2

D684-10058-03-01 Rev. Basic December 1997 Integrated ISS Thermal Math Models, Volume 3, Book 1

D684-10058-03-02 Rev. Basic October 1997 Integrated ISS Thermal Math Models, Volume 3, Book 2

D684-10058-03-03 Rev. Basic March 2005 Integrated ISS Thermal Math Models, Volume 3, Book 3

Meet or exceed All the documents identified below have undergone…

This is the start of the file's text. The full file is on GovTribe.

File details come from the government source that posted it. Updated .