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

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This notice describes a forthcoming Request for Proposal for the Human Space Flight Technical Integration Contract. The solicitation will be issued by NASA's Johnson Space Center on or about November 1, 2019, with proposals due on or about December 11, 2019. The procurement is a total small business set-aside under NAICS code 541715 with a size standard of 1,250 employees. The contract will provide technical integration services in support of human space flight programs. Interested parties should monitor the Federal Business Opportunities and NASA Johnson procurement websites for release of the RFP and any amendments. All technical questions must be submitted in writing.

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Russian Segment Specification

International Space Station Program

Revision L

November 2018

EAR 99. This document contains data within the purview of the U.S. Export Administration Regulations (EAR), 15 CFR 730-774, and is export controlled. The document may be used only in the International Space Station (ISS) program to fulfill responsibilities of the Parties or of a Cooperating Agency of an ISS Partner in furtherance of the ISS Intergovernmental Agreement. Re-transfer or disclosure to, or use by, any persons other than citizens of ISS Program International Partner countries, or use for any other purpose, requires prior U.S. Government authorization.

National Aeronautics and Space Administration International Space Station Program Johnson Space Center Houston, Texas Contract No.: NNJ12GA46C

SSP 41163

Revision L

REVISION AND HISTORY

REVISION AND HISTORY – Continued

REVISION AND HISTORY – Continued

REVISION AND HISTORY – Continued

REV.
DESCRIPTION
PUB. DATE

J

05-05-10

K
Revision K, Final Document (SSCD 014445 EFF, 01-21-16)

Incorporates the following changes: 011497, 011768R1, 012028, 012097, 012507R1, 012701, and 014445.

02-24-16

REVISION AND HISTORY – Continued

REV.
DESCRIPTION
PUB. DATE

This document has been converted from the Original Interleaf format to MS Word format. Differences in format are due to this conversion.

L The following NDCs have been incorporated into Revision L.

NDC 41163-064 (SSCN N/A)

NDC 41163-065 (SSCN N/A)

NDC 41163-068 (SSCN N/A)

NDC 41163-069 (SSCN N/A)

NDC 41163-070 (SSCN N/A)

NDC 41163-071 (SSCN N/A)

NDC 41163-072 (SSCN N/A)

NDC 41163-073 (SSCN N/A)

NDC 41163-074 (SSCN N/A)

NDC 41163-075 (SSCN N/A)

NDC 41163-076 (SSCN N/A)

NDC 41163-077 (SSCN N/A)

Revision L (Reference per SSCD 15981, EFF. 02-07-19)

Program Release
03-27-19

PREFACE

russian segment specification SSP 41163, (Russian Segment Specification) equally applies to NASA and the Roscosmos. This document is under the control of the Space Station Control Board (SSCB) with the concurrence of the respective International Partners, any changes or revisions will be approved by the SSCB and Roscosmos.

See Directive Approval

See Directive Approval

Kirk A. Shireman Program Manager International Space Station Program National Aeronautics and Space Administration

Date

Alexey A. Strelnikov Roscosmos ISS Program Manager

Date

INTERNATIONAL SPACE STATION PROGRAM

russian segment specification

CONCURRENCE

November 2018 i

TABLE OF CONTENTS

PARAGRAPHPAGE
1.0SCOPE.1
1.1Identification.1
1.2System overview.1
2.0APPLICABLE DOCUMENTS.2
2.1Government documents.2
2.1.1Specifications, standards, and handbooks.2
2.1.2Other Government documents, drawings, and publications.2
2.2Non-Government documents.4
2.3Order of precedence.4
3.0SYSTEM REQUIREMENTS.5
3.1System definition.5
3.1.1System description.5
3.1.1.1Functional Cargo Block description.5
3.1.1.2Service Module description.5
3.1.1.3Reserved.5
3.1.1.4Docking Compartment 1 description.5
3.1.1.5Mini Research Module 2.5
3.1.1.6Soyuz vehicle description.6
3.1.1.7Cargo vehicle description.6
3.1.1.8Mini Research Module 1.6
3.1.1.9Multipurpose Laboratory Module.6
3.1.1.10Node Module.7
3.1.1.11Russian Ground Segment.7
3.1.2Missions.7
3.1.3Threat.7
3.1.4Reserved.8
3.1.5Interface requirements.8
3.1.5.1External interfaces.8
3.1.5.1.1United States On-orbit Segment external interface description.9
3.1.5.1.2USGS external interface description.9
3.1.5.1.3Grapple fixture interfaces.9
3.1.5.1.3.1FGB Power Data Grapple Fixture and Video Signal Converter interfaces.9
3.1.5.1.4RS/SSRMS interface.9
3.1.5.1.4.1MRM1 PVGF interface.10
3.1.5.1.5Orbiter external interface description.10
3.1.5.1.5.1FGB Orbiter external interface description.10
3.1.5.1.5.2MRM1 to Orbiter external interface description.10
3.1.5.1.6RS to ATV interface description.10
3.1.5.1.7Crew external interface description.10
3.1.5.1.8Orlan pressure suit.10
3.1.5.2Internal interfaces.11
3.1.5.2.1FGB interface.11
3.1.5.2.2SM interface.12
3.1.5.2.3SPM Interface.13
3.1.5.2.4DC interface.13
3.1.5.2.5MRM2 interfaces.13
3.1.5.2.6Soyuz vehicle interface.13
3.1.5.2.7CV interface.13
3.1.5.2.8MRM1 interface.14
3.1.5.2.9MLM interface.14
3.1.5.2.10NM Interfaces.14
3.1.5.2.11Russian ground segment.15
3.1.5.2.12Reserved.15
3.1.5.2.13PDGF stand Interface.15
3.2Characteristics.15
3.2.1Performance characteristics.15
3.2.1.1State: perform mission.15
3.2.1.1.1Mode: standard.15
3.2.1.1.1.1Control atmospheric pressure.15
3.2.1.1.1.1.1Capability: Control total pressure.15
3.2.1.1.1.1.2Capability: Control oxygen partial pressure.15
3.2.1.1.1.1.3Capability: Relieve overpressure.16
3.2.1.1.1.1.4Capability: Equalize pressure.16
3.2.1.1.1.2Condition atmosphere.16
3.2.1.1.1.2.1Capability: Control atmosphere temperature.16
3.2.1.1.1.2.2Capability: Control atmosphere moisture.16
3.2.1.1.1.2.3Capability: Circulate atmosphere.16
3.2.1.1.1.3Light station.16
3.2.1.1.1.3.1Capability: Control internal lighting.16
3.2.1.1.1.3.2Capability: Illuminate internal areas.17
3.2.1.1.1.3.3Deleted.17
3.2.1.1.1.4Respond to loss of function.17
3.2.1.1.1.4.1Capability: Isolate to recovery level.17
3.2.1.1.1.4.2Capability: Recover lost function.19
3.2.1.1.1.4.3Capability: Isolate for safing.19
3.2.1.1.1.4.4Capability: Safe.19
3.2.1.1.1.5Control station modes.19
3.2.1.1.1.5.1Capability: Maintain station modes.19
3.2.1.1.1.5.2Capability: Transition station modes.21
3.2.1.1.1.5.3Capability: Support execute attitude control handover operations.23
3.2.1.1.1.6Support crew control interface.24
3.2.1.1.1.6.1Capability: Provide data to crew.24
3.2.1.1.1.6.2Capability: Accept crew inputs and commands.24
3.2.1.1.1.6.3Capability: Provide Crew Control Interface.24
3.2.1.1.1.6.4Capability: Provide crew control of Russian payloads.25
3.2.1.1.1.6.5Capability: Provide Ethernet Interfaces for JSL Devices.25
3.2.1.1.1.7Monitor system status.25
3.2.1.1.1.7.1Capability: Acquire function status data.25
3.2.1.1.1.7.2Capability: Assess function status data.25
3.2.1.1.1.8Respond to emergency conditions.25
3.2.1.1.1.8.1Capability: Respond to fire.25
3.2.1.1.1.8.2Capability: Respond to rapid decompression.30
3.2.1.1.1.8.3Capability: Respond to hazardous atmosphere.30
3.2.1.1.1.9Provide electrical power.30
3.2.1.1.1.9.1Capability: Generate power.30
3.2.1.1.1.9.2Capability: Distribute power.30
3.2.1.1.1.9.3Capability: Store energy.33
3.2.1.1.1.10Maintain thermal conditioning.33
3.2.1.1.1.10.1Capability: Collect thermal energy.33
3.2.1.1.1.10.2Capability: Transmit thermal energy.33
3.2.1.1.1.10.3Capability: Dispose of thermal energy.33
3.2.1.1.1.11Maintain time reference.33
3.2.1.1.1.11.1Capability: Distribute time.33
3.2.1.1.1.12Support flight crew.33
3.2.1.1.1.12.1Capability: Accommodate crew hygiene and wastes.33
3.2.1.1.1.12.2Capability: Support radiation exposure monitoring.34
3.2.1.1.1.12.3Capability: Accommodate crew privacy.34
3.2.1.1.1.12.4Capability: Support crew personal items.34
3.2.1.1.1.12.5Capability: Support housekeeping.34
3.2.1.1.1.12.6Capability: Support crew health.34
3.2.1.1.1.12.7Capability: Support food and water consumption and cleanup.35
3.2.1.1.1.12.8Capability: Support food processing.35
3.2.1.1.1.12.9Capability: Provide food.35
3.2.1.1.1.12.10Capability: Support internal crew restraint and mobility.35
3.2.1.1.1.13Control internal carbon dioxide and contaminants.36
3.2.1.1.1.13.1Capability: Control carbon dioxide.36
3.2.1.1.1.13.2Capability: Control gaseous contaminants.37
3.2.1.1.1.13.3Capability: Control airborne particulate contaminants.37
3.2.1.1.1.13.4Capability: Control airborne microbial growth.37
3.2.1.1.1.14Provide water.37
3.2.1.1.1.14.1Capability: Provide water for crew use.37
3.2.1.1.1.14.2Monitor water quality.38
3.2.1.1.1.15Provide visual access.38
3.2.1.1.1.15.1Capability: Provide direct visual access.38
3.2.1.1.1.15.2Capability: Provide remote internal visual access.38
3.2.1.1.1.15.3Reserved.38
3.2.1.1.1.15.4Capability: Accommodation of PDGF video cable.38
3.2.1.1.1.16Facilitate internal voice communication.38
3.2.1.1.1.16.1Capability: Transmit voice communications.38
3.2.1.1.1.16.2Capability: Receive voice communications.38
3.2.1.1.1.17Reserved.39
3.2.1.1.1.18Determine navigation parameters.39
3.2.1.1.1.18.1Capability: Determine state vector and attitude.39
3.2.1.1.1.18.2Capability: Generate pointing and support data.40
3.2.1.1.1.19Maintain attitude - nonpropulsive.40
3.2.1.1.1.19.1Capability: Maintain attitude - nonpropulsive.40
3.2.1.1.1.20Support on-orbit to ground communication.41
3.2.1.1.1.20.1Capability: Support uplinked data.41
3.2.1.1.1.20.2Capability: Provide data for downlink.41
3.2.1.1.1.21Support internal equipment manipulation and maintenance.41
3.2.1.1.1.21.1Capability: Support internal equipment translation.41
3.2.1.1.1.21.2Capability: Support internal equipment removal and replacement.41
3.2.1.1.1.21.3Capability: Support internal equipment identification.41
3.2.1.1.1.21.4Capability: Support internal equipment restraint.41
3.2.1.1.1.21.5Capability: Support orbital replaceable unit repair.42
3.2.1.1.1.21.6Capability: Store internal equipment.42
3.2.1.1.1.22Support Station to external vehicle proximity operations communications.42
3.2.1.1.1.22.1Capability: Support external input data.42
3.2.1.1.1.22.2Capability: Provide data for external vehicles.42
3.2.1.1.1.22.3Capability: Support external vehicle wave-off.42
3.2.1.1.1.23Reserved.42
3.2.1.1.1.24Capabilities during pressure change.42
3.2.1.1.2Mode: Reboost.44
3.2.1.1.2.1Execute translation maneuvers.44
3.2.1.1.2.1.1Capability: Execute maneuver guidance.44
3.2.1.1.2.1.2Capability: Execute translational thrust.45
3.2.1.1.2.2Capability: Control attitude - propulsive.50
3.2.1.1.2.2.1Rotational control.51
3.2.1.1.2.2.2Provide desaturation torque.54
3.2.1.1.3Reserved.55
3.2.1.1.4Mode: microgravity.55
3.2.1.1.4.1Support microgravity experiments.55
3.2.1.1.4.1.1Capability: Limit accelerations.55
3.2.1.1.4.1.2Limit angular momentum disturbance.59
3.2.1.1.5Mode: Survival.60
3.2.1.1.6Mode: Proximity operations.61
3.2.1.1.6.1Capability: Provide automated collision avoidance maneuvers.61
3.2.1.1.6.2Reserved.61
3.2.1.1.6.3Capability: Provide docking status.61
3.2.1.1.6.4Capability: Support external vehicle to ISS relative navigation.61
3.2.1.1.6.5Capability: External vehicle monitoring during rendezvous approach.61
3.2.1.1.6.6Capability: Mission planning - rendezvous and docking.61
3.2.1.1.6.7Capability: External vehicle video transmission.62
3.2.1.1.7Mode: External operations.62
3.2.1.1.7.1Support EVA operations.62
3.2.1.1.7.1.1Capability: Support voice and data communications.62
3.2.1.1.7.1.2Communication with U.S. Airlock Orlan suits.62
3.2.1.1.7.1.3Reserved.62
3.2.1.1.7.1.4Capability: Support station ingress.62
3.2.1.1.7.1.5Capability: Illuminate external worksites and translation paths.62
3.2.1.1.7.1.6Capability: Track external crew.62
3.2.1.1.7.1.7Capability: Self rescue of EVA crew.63
3.2.1.1.7.2Accommodate mobile servicing system.63
3.2.1.1.8Mode: Crew delivery and return.63
3.2.1.1.8.1Support scheduled crew delivery and return.63
3.2.1.1.8.1.1Capability: Scheduled crew delivery and return.63
3.2.1.1.8.2Support unplanned crew return.64
3.2.1.1.8.2.1Capability: Support unplanned crew return.64
3.2.1.2External and proximity operations.64
3.2.1.2.1Mode: Proximity operations.64
3.2.1.2.2Mode: External operations.64
3.2.1.3State: Support mission.64
3.2.1.3.1Reserved.64
3.2.1.3.2Mode: Space transport.64
3.2.1.3.2.1Support resupply and return.64
3.2.1.3.2.1.1Capability: Transport cargo.64
3.2.2Physical characteristics.65
3.2.2.1Visiting vehicle approach and departure corridor.65
3.2.2.1.1Approach and departure corridor for the Orbiter.65
3.2.2.1.2Approach corridor for the Russian Visiting Vehicle.66
3.2.2.1.3Departure corridor for the Russian Visiting Vehicle.69
3.2.2.2Establish translation paths.69
3.2.2.3Establish worksites.70
3.2.2.3.1Common restraint hardware.70
3.2.2.4Provide external and internal stowage of tools and hardware.70
3.2.2.5ISS storage requirements.70
3.2.2.6Transfer crew and external hardware.70
3.2.2.7Distribute commands and data.71
3.2.2.7.1Provide output amplitude.71
3.2.2.8MRM1 Shuttle interface.71
3.2.2.9ATV.71
3.2.3Reliability.71
3.2.3.1Failure tolerance.71
3.2.3.2Service life.75
3.2.3.3Failure propagation.75
3.2.3.4Redundancy status.75
3.2.4Maintainability.75
3.2.4.1Qualitative maintainability requirements.75
3.2.4.1.1Reserved.75
3.2.4.1.2Procedures and tools.75
3.2.4.2Quantitative maintainability requirements.75
3.2.4.2.1Equipment maintenance time in nonpressurized areas.75
3.2.4.2.2Capability: Total Mean Maintenance Crew Hours/Year.76
3.2.4.2.2.1EVA TMMCH/Y.76
3.2.4.2.2.2IVA TMMCH/Y.76
3.2.4.2.2.2.1IVA in support of EVA.76
3.2.4.2.3Airlock cycles to support EVA.76
3.2.4.3Failure Detection, Isolation and Recovery.76
3.2.4.3.1Manual control of FDIR.76
3.2.4.3.2Testing at operating location.76
3.2.4.3.3Manual FDIR.76
3.2.4.3.4Automatic functional recovery confirmation.77
3.2.4.3.5Automatic safing confirmation.77
3.2.4.3.6False alarm mitigation.77
3.2.4.4Pressure integrity.77
3.2.5Docking mechanism and contact conditions.77
3.2.6Environmental conditions.79
3.2.6.1On-orbit environmental conditions.79
3.2.6.1.1Thermal environment.79
3.2.6.1.2Neutral atmosphere.84
3.2.6.1.3External contamination.85
3.2.6.1.4Electromagnetic and geomagnetic fields.85
3.2.6.1.5Plasma.85
3.2.6.1.6Ionizing radiation.86
3.2.6.1.7Reserved.86
3.2.6.1.8Meteoroids and Orbital Debris.86
3.2.6.1.9Reserved.86
3.2.6.1.10Plume impingement pressures.86
3.2.6.1.11Flight attitude table.87
3.3Design and construction.90
3.3.1Materials, processes and parts.90
3.3.1.1Reserved.90
3.3.1.2Reserved.90
3.3.1.3Materials and processes.90
3.3.1.4Electrical, Electronic, and Electromechanical parts.90
3.3.1.5Seal life.90
3.3.1.6Fluid and Connector standards.90
3.3.1.7Capability: Provide propellants and pressurant gases.90
3.3.2Electromagnetic radiation.91
3.3.2.1Electromagnetic compatibility.91
3.3.3Nameplates and product marking.91
3.3.3.1Labeling.91
3.3.3.1.1Vendor labels.91
3.3.3.2On-orbit labels.91
3.3.4Workmanship.91
3.3.4.1Cleanliness.91
3.3.4.2Cleanliness of surfaces in contact with fluids.91
3.3.5Reserved.92
3.3.6Safety.92
3.3.6.1General.92
3.3.6.1.1Catastrophic hazards.92
3.3.6.1.2Critical hazards.92
3.3.6.1.3Design for minimum risk.92
3.3.6.1.4Control of functions resulting in critical hazards.92
3.3.6.1.4.1Inadvertent operation resulting in a critical hazard.92
3.3.6.1.4.2Loss of a function resulting in a critical hazard.92
3.3.6.1.5Control of functions resulting in catastrophic hazards.93
3.3.6.1.5.1Inadvertent operation resulting in a catastrophic hazard.93
3.3.6.1.5.2Loss of function resulting in a catastrophic hazard.93
3.3.6.1.6Subsequent induced loads.93
3.3.6.1.7Safety interlocks.93
3.3.6.1.8Environmental compatibility.93
3.3.6.1.9Redundant functions.93
3.3.6.2Hazard detection and safing.94
3.3.6.2.1Safing prior to return/resupply/refurbishment.94
3.3.6.2.2Monitors.94
3.3.6.2.2.1Status information.94
3.3.6.2.2.2Hazardous function operation prevention.94
3.3.6.2.2.3Loss of input or failure.94
3.3.6.2.2.4Launch site availability.94
3.3.6.2.2.5Flight crew availability.94
3.3.6.2.3Near real-time monitoring.94
3.3.6.2.4Real-time monitoring.94
3.3.6.2.4.1Maintain status of hazard controls.94
3.3.6.2.4.2Crew response time and safing procedures.95
3.3.6.2.4.3Ground monitoring.95
3.3.6.3Command and computer control of hazardous functions.95
3.3.6.3.1Computer control of hazardous functions.95
3.3.6.3.1.1Detection and recovery.95
3.3.6.3.1.2Independent safing action.95
3.3.6.4Hazardous materials.95
3.3.6.4.1Hazardous fluid containment failure tolerance.95
3.3.6.5Pyrotechnics for RS applications.95
3.3.6.6Radiation.96
3.3.6.6.1Reserved.96
3.3.6.6.2Nonionizing radiation.96
3.3.6.6.3Spacesuit electric field radiation.98
3.3.6.6.4Spacesuit magnetic field radiation.98
3.3.6.7Optics and lasers.98
3.3.6.7.1Lasers.98
3.3.6.7.2Optical requirements.98
3.3.6.7.2.1Optical instruments.98
3.3.6.7.2.2Personnel protection.99
3.3.6.7.2.3Direct viewing optical systems.99
3.3.6.8Electrical safety.99
3.3.6.8.1Electrical power circuit overloads.99
3.3.6.8.1.1Circuit overload protection.99
3.3.6.8.1.2Protective device sizing.99
3.3.6.8.1.3Bent pin or conductive contamination.99
3.3.6.8.2Crew protection for electrical shock.99
3.3.6.8.2.1EVA crew protection for electric shock.99
3.3.6.8.3Reapplication of power.99
3.3.6.8.4Batteries.99
3.3.6.9Liquid propellant propulsion systems.100
3.3.6.9.1Inadvertent engine firings.100
3.3.6.9.1.1Propellant flow control devices.100
3.3.6.9.1.1.1Thruster valves.100
3.3.6.9.1.1.2Operations.100
3.3.6.9.1.2Electrical inhibits.100
3.3.6.9.1.3Monitoring of electrical inhibits to prevent catastrophic thruster firing.100
3.3.6.9.2Propellant overheating.101
3.3.6.9.3Propellant leakage.101
3.3.6.9.4Reserved.101
3.3.6.9.5Plume impingement.101
3.3.6.9.6Hazardous venting.101
3.3.6.9.7Monitoring propulsion system status.101
3.3.6.9.8The RS MCS.101
3.3.6.10Fire protection.101
3.3.6.10.1Manual activation.101
3.3.6.10.2Isolation.101
3.3.6.10.3Suppression.101
3.3.6.10.4Suppressant.102
3.3.6.10.4.1Suppressant material.102
3.3.6.10.4.2Toxicity level.102
3.3.6.10.5Contamination.102
3.3.6.10.6Portable equipment.102
3.3.6.10.6.1Proximity to entrance.102
3.3.6.10.6.2Location within element.102
3.3.6.10.6.3Set co-location.102
3.3.6.11Constraints.102
3.3.6.11.1Pressurized volume depressurization and repressurization tolerance.102
3.3.6.11.1.1Hazards during depressurization.102
3.3.6.11.2Emergency egress.102
3.3.6.11.2.1No drag-throughs.103
3.3.6.11.3Translation entry/exit paths.103
3.3.6.11.4Component hazardous energy provision.103
3.3.6.11.5Hatch opening.103
3.3.6.11.6Hatch operations.103
3.3.6.11.7Pins or detachable parts.103
3.3.6.11.8Single crewmember entry/exit.103
3.3.6.11.9Reserved.103
3.3.6.11.10Equipment clearance for entrapment hazard.103
3.3.6.11.11Light fixture.103
3.3.6.12Human factors.104
3.3.6.12.1Internal volume touch temperature.104
3.3.6.12.1.1Continuous contact-high temperature.104
3.3.6.12.1.2Incidental or momentary contact-high temperature.104
3.3.6.12.1.3Internal volume low touch temperature.104
3.3.6.12.2External touch temperature for U.S. EVA.104
3.3.6.12.3External edge, corner, and protrusion radii.105
3.3.6.12.4IVA internal corner and edge protection.105
3.3.6.12.5Reserved.106
3.3.6.12.6Latches.106
3.3.6.12.6.1Design.106
3.3.6.12.6.2Protective covers or guards.106
3.3.6.12.7Screws and bolts.106
3.3.6.12.8Safety critical fasteners.106
3.3.6.12.9Levers, cranks, hooks and controls.106
3.3.6.12.10Burrs.106
3.3.6.12.11Reserved.106
3.3.6.12.12Protrusions.106
3.3.6.12.13Pinch points.106
3.3.6.12.14Emergency ingress for a non-impaired crew member.106
3.3.6.12.15Flex hoses, lines, and cables.107
3.3.6.12.16Translation routes and established worksites.107
3.3.6.12.16.1Primary translation routes and established worksites.107
3.3.6.12.16.2Secondary translation routes and established worksites.107
3.3.6.12.16.3EVA crewmember contact isolation.107
3.3.6.12.17Moving or rotating equipment.107
3.3.6.13Deleted.108
3.3.6.13.1Deleted.108
3.3.6.13.1.1Deleted.108
3.3.6.13.1.2Deleted.108
3.3.6.13.2Deleted.108
3.3.6.13.3Deleted.108
3.3.6.13.4Deleted.108
3.3.6.13.4.1Deleted.108
3.3.6.13.4.2Deleted.108
3.3.6.13.5Deleted.108
3.3.6.13.6Deleted.108
3.3.6.13.6.1Deleted.108
3.3.6.13.6.2Deleted.108
3.3.6.13.6.3Deleted.108
3.3.6.13.6.4Deleted.108
3.3.6.13.7Deleted.108
3.3.6.13.8Deleted.108
3.3.6.13.9Deleted.108
3.3.6.13.9.1Deleted.108
3.3.6.13.9.2Deleted.108
3.3.6.13.10Deleted.108
3.3.6.14Deleted.108
3.3.6.14.1Deleted.108
3.3.6.14.2Deleted.108
3.3.6.14.3Deleted.108
3.3.6.14.4Deleted.108
3.3.6.15Ground interfaces and services - Russian launch vehicle.108
3.3.6.16Deleted.109
3.3.7Human engineering.109
3.3.7.1Anthropometric requirements.109
3.3.7.2External task location requirements.109
3.3.7.3Strength requirements.110
3.3.7.3.1Normal operations.110
3.3.7.3.2Maintenance.111
3.3.7.3.3Emergency controls.111
3.3.7.4Gloved operation.111
3.3.7.5Location coding.112
3.3.7.5.1Alphanumeric coding.112
3.3.7.5.2Accommodate changes.112
3.3.7.5.3Reserved.112
3.3.7.5.4EVA primary translation path.112
3.3.7.6Housekeeping.112
3.3.8Reserved.112
3.3.9System security.112
3.3.10Environmental constraints.112
3.3.10.1Acoustic emission limits.112
3.3.10.2External contamination releases.112
3.3.11Design for remote controlled external operations.112
3.3.11.1SRMS robotic support of the MRM1.113
3.3.11.2SRMS to SSRMS robotic hand-off.113
3.3.11.3SSRMS support of the RS.113
3.3.11.3.1MRM1 support of the PVGF.116
3.3.12Design requirements.117
3.3.12.1Structural design requirements.117
3.3.12.1.1Structural design life for meteoroid and orbital debris analyses.117
3.3.12.1.1.1Probability of No Penetration.118
3.3.12.1.1.1.1Structure penetration.118
3.3.12.1.1.2Reserved.118
3.3.12.1.2EVA on-orbit induced loads.118
3.3.12.1.3Additional M/OD space protections.118
3.3.12.2Window, glass and ceramic structural design.118
3.3.12.3Fracture control.118
3.3.12.4Structural design constraints.118
3.3.12.4.1FGB structural design constraint.119
3.3.12.4.2SM structural design constraint.119
3.3.12.5Fluid handling requirements.119
3.3.12.5.1Fluid quantity determination.119
3.3.12.5.2Interface hardware.119
3.3.12.5.3Flexible lines and bellows design.119
3.3.12.6Knobs and fasteners.119
3.3.12.7Atmosphere leakage.119
3.3.12.8Operational altitude.120
3.3.12.9Preclude condensation.120
3.3.12.10Venting/dumping.120
3.3.13EVA equipment handling capabilities.120
3.3.14MIL-STD-1553 data bus addresses.121
3.3.15MIL-STD-1553 data bus constraints.121
3.3.15.1SSQ components.121
3.3.15.1.1Bus coupler type.121
3.3.15.2Bus stub length.122
3.3.15.3Bus coupling.123
3.3.16Terminal interface units.123
3.3.16.1TIU multiple bus isolation.123
3.3.17RS not-to-exceed bus length.123
3.4Computer resource requirements.123
3.4.1Computer hardware design considerations.123
3.4.2Flexibility and expansion.123
3.5Logistics.124
3.5.1Maintenance.124
3.5.1.1General maintenance requirements.124
3.5.1.1.1RS logistics infrastructure.124
3.5.1.1.2ORU maintenance level distribution.124
3.5.1.2Perform on-orbit maintenance.124
3.5.1.2.1ORU removal and replacement.124
3.5.1.2.2In situ maintenance.124
3.5.1.2.3Maintenance coordination.124
3.5.1.2.4ORU packaging.124
3.5.1.2.5Procedure storage.124
3.5.1.2.6Liquid or gas venting.124
3.5.2Supply.125
3.5.2.1General supply requirements.125
3.5.2.1.1Sustaining fleet resources.125
3.5.2.1.2Missed resupply crew provisions.125
3.5.2.1.3Maintenance resources.125
3.5.2.1.4On-orbit propellant reserve.125
3.5.2.2Provide inventory management capability.125
3.5.2.2.1Critical item storage.125
3.6Reserved.125
3.7Characteristics of major functional elements.125
3.7.1Functional cargo block.125
3.7.1.1Purpose.125
3.7.1.2Description.126
3.7.1.3Capabilities.126
3.7.1.3.1Control total pressure.126
3.7.1.3.1.1Monitor total pressure.126
3.7.1.3.2Control oxygen partial pressure.126
3.7.1.3.2.1Monitor oxygen partial pressure.126
3.7.1.3.3FGB to PMA1 leak seal monitoring and repressurization.126
3.7.1.3.4Equalize pressure.127
3.7.1.3.4.1Control atmosphere temperature.127
3.7.1.3.4.1.1Monitor atmosphere temperature.127
3.7.1.3.4.1.2Remove atmosphere heat.127
3.7.1.3.4.2Control atmosphere moisture.127
3.7.1.3.4.2.1Monitor humidity.127
3.7.1.3.5Circulate atmosphere.127
3.7.1.3.5.1Circulate atmosphere intra-module.127
3.7.1.3.5.2Circulate atmosphere inter-module.127
3.7.1.3.6Isolate to recovery level.128
3.7.1.3.7Recover lost function.129
3.7.1.3.8Safe.130
3.7.1.3.9Reserved.130
3.7.1.3.10Reserved.130
3.7.1.3.11Distribute time.130
3.7.1.3.12Provide data to crew.130
3.7.1.3.13Acquire function status data.130
3.7.1.3.13.1Collect function status data.130
3.7.1.3.14Assess function status data.130
3.7.1.3.15Provide crew control interface.131
3.7.1.3.16Reserved.131
3.7.1.3.17Respond to fire.131
3.7.1.3.17.1Detect fire event.131
3.7.1.3.17.2Isolate fire control zone.131
3.7.1.3.17.3Extinguish fire.131
3.7.1.3.17.4Recover from fire.131
3.7.1.3.18Reserved.131
3.7.1.3.19Respond to hazardous atmosphere.131
3.7.1.3.20Provide electrical power.131
3.7.1.3.20.1Generate power.131
3.7.1.3.20.2Distribute power.131
3.7.1.3.20.3Store energy.132
3.7.1.3.21Reserved.132
3.7.1.3.22Maintain thermal conditioning.132
3.7.1.3.22.1Collect thermal energy.132
3.7.1.3.22.2Transmit thermal energy.132
3.7.1.3.22.3Dispose of thermal energy.132
3.7.1.3.22.4Passive thermal energy.132
3.7.1.3.23Provide ethernet interfaces for JSL devices.132
3.7.1.3.24Support internal crew restraint and mobility.132
3.7.1.3.25Control carbon dioxide.134
3.7.1.3.25.1Monitor carbon dioxide.134
3.7.1.3.26Control airborne particulate contaminants.134
3.7.1.3.26.1Remove airborne particulate contaminants.134
3.7.1.3.27Provide remote internal visual access.134
3.7.1.3.27.1Transmit video signal.134
3.7.1.3.27.2Receive video signal.134
3.7.1.3.28Transmit voice communications.134
3.7.1.3.28.1Transmit hardwire.134
3.7.1.3.29Receive voice communication.135
3.7.1.3.29.1Receive hardwire.135
3.7.1.3.30Support uplinked data.135
3.7.1.3.30.1Receive uplinked data.135
3.7.1.3.30.2Prepare uplinked data for on-board distribution.135
3.7.1.3.30.3Distribute uplinked data.135
3.7.1.3.31Provide data for downlink.135
3.7.1.3.31.1Prepare data for downlink.135
3.7.1.3.31.2Transmit data for downlink.136
3.7.1.3.32Support internal equipment translation.136
3.7.1.3.33Support internal equipment removal and replacement.136
3.7.1.3.34Support internal equipment identification.136
3.7.1.3.35Support internal equipment restraint.136
3.7.1.3.36Execute maneuver guidance.136
3.7.1.3.37Execute translation thrust.136
3.7.1.3.38Control attitude - propulsive.137
3.7.1.3.38.1FGB attitude control requirements.139
3.7.1.3.38.2Indicate status of motion control system.142
3.7.1.3.38.3Maneuvering on orbit with additional cargo (Flight 2A.1).142
3.7.1.3.39Limit accelerations.142
3.7.1.3.40Light FGB.142
3.7.1.3.40.1Control internal lighting.142
3.7.1.3.40.2Illuminate internal areas.143
3.7.1.3.41Support housekeeping.143
3.7.1.3.42Store internal equipment.143
3.7.1.3.43Support orbital replacement unit repair.143
3.7.1.3.44Capability: Provide automated collision avoidance maneuvers.144
3.7.1.3.45Capability: Provide docking status.144
3.7.1.3.46Capability: FGB relative navigation support.144
3.7.1.3.47Capability: FGB video transmission.145
3.7.1.3.48Automatic power reduction.145
3.7.1.3.49Communication with US Airlock Orlan suits.145
3.7.2Service Module.145
3.7.2.1Purpose.145
3.7.2.2Description.145
3.7.2.3Capabilities.145
3.7.2.3.1Control total pressure.145
3.7.2.3.1.1Monitor total pressure.145
3.7.2.3.2Control oxygen partial pressure.146
3.7.2.3.2.1Monitor oxygen partial pressure.146
3.7.2.3.2.2Introduce oxygen.146
3.7.2.3.3Reserved.146
3.7.2.3.4Equalize pressure.146
3.7.2.3.5Control atmosphere temperature.146
3.7.2.3.5.1Monitor atmosphere temperature.146
3.7.2.3.5.2Remove atmospheric heat.146
3.7.2.3.6Control atmosphere moisture.146
3.7.2.3.6.1Remove excess moisture from cabin atmosphere.146
3.7.2.3.6.2Dispose of removed moisture.147
3.7.2.3.6.3Monitor humidity.147
3.7.2.3.7Circulate atmosphere.147
3.7.2.3.7.1Circulate atmosphere intra-module.147
3.7.2.3.7.2Circulate atmosphere inter-module.147
3.7.2.3.8Light station.147
3.7.2.3.8.1Control internal lighting.147
3.7.2.3.8.2Accommodate on SM a source of light for Shuttle Star Tracker.147
3.7.2.3.8.3Illuminate internal area.147
3.7.2.3.9Isolate to recovery level.148
3.7.2.3.10Recover lost function.148
3.7.2.3.11Safe.148
3.7.2.3.12Maintain station modes.148
3.7.2.3.13Transition station modes.149
3.7.2.3.14Provide data to crew.150
3.7.2.3.15Accept crew inputs and commands.150
3.7.2.3.16Acquire function status data.150
3.7.2.3.17Assess function status data.150
3.7.2.3.18Respond to fire.151
3.7.2.3.18.1Detect fire event.151
3.7.2.3.18.2Isolate fire control zone.151
3.7.2.3.18.3Extinguish fire.151
3.7.2.3.18.4Recover from fire.151
3.7.2.3.19Respond to decompression.151
3.7.2.3.19.1Detect rapid decompression.151
3.7.2.3.19.2Isolate rapid decompression.151
3.7.2.3.19.3Identify depressurizing module.152
3.7.2.3.20Respond to hazardous atmosphere.152
3.7.2.3.21Maintain thermal conditioning.152
3.7.2.3.21.1Collect thermal energy.152
3.7.2.3.21.2Transmit thermal energy.152
3.7.2.3.21.3Dispose of thermal energy.152
3.7.2.3.22Provide crew control interface.152
3.7.2.3.23Distribute time.152
3.7.2.3.24Accommodate crew hygiene and wastes.153
3.7.2.3.25Support radiation exposure monitoring.153
3.7.2.3.26Accommodate crew privacy.153
3.7.2.3.27Support crew personal items.153
3.7.2.3.28Support housekeeping.153
3.7.2.3.29Support crew health.153
3.7.2.3.29.1Monitor crew health.153
3.7.2.3.29.2Respond to crew illness or injury.154
3.7.2.3.29.3Provide preventive crew health care.154
3.7.2.3.29.4Support microgravity countermeasures and exercise.154
3.7.2.3.30Support food and water consumption and cleanup.154
3.7.2.3.31Support food processing.154
3.7.2.3.32Provide food.154
3.7.2.3.33Support internal crew restraint and mobility.154
3.7.2.3.34Control carbon dioxide.156
3.7.2.3.34.1Remove carbon dioxide.156
3.7.2.3.34.2Dispose of carbon dioxide.156
3.7.2.3.35Control gaseous contaminants.156
3.7.2.3.35.1Remove gaseous contaminants.156
3.7.2.3.35.2Dispose of gaseous contaminants.156
3.7.2.3.36Control airborne particulate contaminants.156
3.7.2.3.36.1Remove airborne particulate contaminants.156
3.7.2.3.37Control airborne microbial growth.156
3.7.2.3.37.1Remove airborne microbes.156
3.7.2.3.38Provide water for crew use.157
3.7.2.3.38.1Supply water for potable use.157
3.7.2.3.38.2Supply water for hygiene use.157
3.7.2.3.38.3Waste water management.157
3.7.2.3.38.4Monitor water quality.157
3.7.2.3.39Provide direct visual access.157
3.7.2.3.40Provide remote internal visual access.158
3.7.2.3.40.1Create video signal.158
3.7.2.3.40.2Reserved.158
3.7.2.3.41Transmit voice communications.158
3.7.2.3.41.1Transmit hardwire.158
3.7.2.3.42Receive voice communication.158
3.7.2.3.42.1Receive hardwire.158
3.7.2.3.43Determine state vector and attitude.158
3.7.2.3.43.1Provide state vector and attitude.158
3.7.2.3.43.2Deleted.159
3.7.2.3.44Maintain attitude - nonpropulsive.159
3.7.2.3.45Support uplinked data.160
3.7.2.3.45.1Receive uplinked data.160
3.7.2.3.45.2Prepare uplinked data for on-board distribution.160
3.7.2.3.45.3Distribute uplinked data.160
3.7.2.3.46Provide data for downlink.160
3.7.2.3.46.1Prepare data for downlink.160
3.7.2.3.46.2Transmit data for downlink.161
3.7.2.3.47Support internal equipment translation.161
3.7.2.3.48Support internal equipment removal and replacement.161
3.7.2.3.49Support internal equipment identification.161
3.7.2.3.50Support internal equipment restraint.161
3.7.2.3.51Support orbital replaceable unit repair.161
3.7.2.3.52Store internal equipment.161
3.7.2.3.53Support external vehicle input data for proximity operations.161
3.7.2.3.53.1Receive external vehicle input data.161
3.7.2.3.53.2Prepare external input data for on-board distribution.162
3.7.2.3.54Provide data for external vehicles for proximity operations.162
3.7.2.3.54.1Prepare data for external vehicles.162
3.7.2.3.54.2Transmit data to external vehicles.162
3.7.2.3.55Support external vehicle wave-off.162
3.7.2.3.55.1Determine external vehicle wave-off.162
3.7.2.3.55.2Communicate wave-off to external vehicle.162
3.7.2.3.56Execute translation maneuvers.162
3.7.2.3.56.1Execute maneuver guidance.162
3.7.2.3.56.2Execute translation thrust.163
3.7.2.3.57Control attitude - propulsive.164
3.7.2.3.58Provide desaturation torque.168
3.7.2.3.59Provide depressurization capabilities.169
3.7.2.3.60Communications with US Airlock Orlan suits.170
3.7.2.3.61Support attitude control handover operations.170
3.7.2.3.62Provide ethernet interfaces for JSL devices.170
3.7.3MRM1.170
3.7.3.1Purpose.170
3.7.3.2Description.171
3.7.3.3Capabilities.171
3.7.3.3.1Reserved.171
3.7.3.3.2Reserved.171
3.7.3.3.3Reserved.171
3.7.3.3.4Equalize pressure.171
3.7.3.3.5Control atmosphere temperature.171
3.7.3.3.5.1Monitor atmosphere temperature.171
3.7.3.3.5.2Remove atmosphere heat.171
3.7.3.3.6Reserved.171
3.7.3.3.7Circulate atmosphere.171
3.7.3.3.7.1Circulate atmosphere intra-module.171
3.7.3.3.7.2Circulate atmosphere inter-modules.171
3.7.3.3.8Light station.171
3.7.3.3.8.1Control internal lighting.171
3.7.3.3.9Isolate to recovery level.172
3.7.3.3.10Recover lost function.172
3.7.3.3.11Safety.172
3.7.3.3.12Reserved.172
3.7.3.3.13Reserved.172
3.7.3.3.14Provide data to crew.172
3.7.3.3.15Accept crew inputs and commands.172
3.7.3.3.16Acquire function status data.172
3.7.3.3.17Assess function status data.173
3.7.3.3.18Respond to fire.173
3.7.3.3.18.1Detect fire event.173
3.7.3.3.18.2Isolate fire control zone.173
3.7.3.3.18.3Extinguish fire.173
3.7.3.3.18.4Recover from fire.173
3.7.3.3.19Respond to decompression.174
3.7.3.3.19.1Reserved.174
3.7.3.3.19.2Isolate rapid decompression.174
3.7.3.3.20Respond to hazardous atmosphere.174
3.7.3.3.21Maintain thermal conditioning.174
3.7.3.3.21.1Collect thermal energy.174
3.7.3.3.21.2Transmit thermal energy.174
3.7.3.3.21.3Dispose of thermal energy.174
3.7.3.3.22Provide crew control interface.174
3.7.3.3.23Reserved.175
3.7.3.3.24Reserved.175
3.7.3.3.25Reserved.175
3.7.3.3.26Reserved.175
3.7.3.3.27Reserved.175
3.7.3.3.28Reserved.175
3.7.3.3.29Reserved.175
3.7.3.3.30Reserved.175
3.7.3.3.31Reserved.175
3.7.3.3.32Reserved.175
3.7.3.3.33Support internal crew restraint and mobility.175
3.7.3.3.34Reserved.176
3.7.3.3.35Reserved.176
3.7.3.3.36Reserved.176
3.7.3.3.37Reserved.176
3.7.3.3.38Reserved.176
3.7.3.3.39Reserved.176
3.7.3.3.40Provide remote internal visual access.176
3.7.3.3.40.1Create video signal.176
3.7.3.3.41Transmit voice communications.176
3.7.3.3.41.1Transmitting hardwire.176
3.7.3.3.42Receive voice communications.176
3.7.3.3.42.1Receiving hardwire.176
3.7.3.3.43Reserved.177
3.7.3.3.44Reserved.177
3.7.3.3.45Support uplink data.177
3.7.3.3.45.1Receive uplinked data.177
3.7.3.3.46Provide data for downlink.177
3.7.3.3.46.1Data downlink.177
3.7.3.3.47Support internal equipment translation.177
3.7.3.3.48Support removal and replacement of internal equipment.177
3.7.3.3.49Support internal equipment identification.177
3.7.3.3.50Support internal equipment restraints.177
3.7.3.3.51Reserved.177
3.7.3.3.52Reserved.177
3.7.3.3.53Support transport vehicle data input for rendezvous operations.177
3.7.3.3.53.1Baseline data exchange with docking transport vehicle.177
3.7.3.3.54MRM1 electric power supply.178
3.7.3.3.55MLM resupply cargo items.178
3.7.3.3.56NASA cargo items.178
3.7.4MRM2.178
3.7.4.1Purpose.178
3.7.4.2Description.178
3.7.4.3Capabilities (functions).179
3.7.4.3.1Reserved.179
3.7.4.3.2Reserved.179
3.7.4.3.3Reserved.179
3.7.4.3.4Equalize pressure.179
3.7.4.3.5Control atmosphere temperature.179
3.7.4.3.5.1Monitor atmosphere temperature.179
3.7.4.3.5.2Remove atmosphere heat.179
3.7.4.3.6Reserved.179
3.7.4.3.7Circulate atmosphere.179
3.7.4.3.7.1Circulate atmosphere intra-module.179
3.7.4.3.7.2Circulate atmosphere inter-module.179
3.7.4.3.8Lighting.179
3.7.4.3.8.1Control internal lighting.179
3.7.4.3.9Isolate to recovery level.179
3.7.4.3.10Recover lost function.180
3.7.4.3.11Safety.180
3.7.4.3.12Reserved.180
3.7.4.3.13Reserved.180
3.7.4.3.14Provide data to crew.180
3.7.4.3.15Accept crew inputs and commands.180
3.7.4.3.16Acquire function status data.180
3.7.4.3.17Assess function status data.180
3.7.4.3.18Respond to fire.181
3.7.4.3.18.1Detect fire event.181
3.7.4.3.18.2Isolate fire control zone.181
3.7.4.3.18.3Extinguish fire.181
3.7.4.3.18.4Recover from fire.181
3.7.4.3.19Respond to depressurization.181
3.7.4.3.19.1Reserved.181
3.7.4.3.19.2Isolate rapid depressurization.181
3.7.4.3.20Respond to hazardous atmosphere.182
3.7.4.3.21Maintain thermal conditioning.182
3.7.4.3.21.1Collect thermal energy.182
3.7.4.3.21.2Transmit thermal energy.182
3.7.4.3.21.3Reserved.182
3.7.4.3.22Provide crew control interface.182
3.7.4.3.23Reserved.182
3.7.4.3.24Reserved.182
3.7.4.3.25Reserved.182
3.7.4.3.26Reserved.182
3.7.4.3.27Reserved.182
3.7.4.3.28Reserved.182
3.7.4.3.29Reserved.182
3.7.4.3.30Reserved.182
3.7.4.3.31Reserved.182
3.7.4.3.32Reserved.182
3.7.4.3.33Support internal crew restraint and mobility.182
3.7.4.3.34Reserved.183
3.7.4.3.35Reserved.183
3.7.4.3.36Reserved.183
3.7.4.3.37Reserved.183
3.7.4.3.38Reserved.183
3.7.4.3.39Reserved.183
3.7.4.3.40Provide remote visual access.183
3.7.4.3.40.1Reserved.183
3.7.4.3.41Transmit voice communications.183
3.7.4.3.41.1Transmitting wired communications.183
3.7.4.3.42Receive voice communications.184
3.7.4.3.42.1Receiving wired communications.184
3.7.4.3.43Reserved.184
3.7.4.3.44Reserved.184
3.7.4.3.45Data uplink.184
3.7.4.3.45.1Receive uplinked data.184
3.7.4.3.46Provide data for downlink.184
3.7.4.3.46.1Data downlink.184
3.7.4.3.47Support internal equipment translation.184
3.7.4.3.48Support removal and replacement of internal equipment.184
3.7.4.3.49Support internal equipment identification.184
3.7.4.3.50Support internal equipment restraints.185
3.7.4.3.51Reserved.185
3.7.4.3.52Reserved.185
3.7.4.3.53Support transport vehicle data transmission for rendezvous operations.185
3.7.4.3.53.1Baseline data exchange with transport vehicle during docking.185
3.7.4.3.54MRM2 electrical power supply.185
3.7.5MLM.185
3.7.5.1Purpose.185
3.7.5.2Description.186
3.7.5.3Capabilities.186
3.7.5.3.1Control total pressure.186
3.7.5.3.1.1Monitor total pressure.186
3.7.5.3.2Control oxygen partial pressure.186
3.7.5.3.2.1Reserved.186
3.7.5.3.2.2Control Oxygen.186
3.7.5.3.3Reserved.186
3.7.5.3.4Reserved.186
3.7.5.3.5Control atmosphere temperature.186
3.7.5.3.5.1Monitor atmosphere temperature.186
3.7.5.3.5.2Remove atmospheric heat.186
3.7.5.3.6Control atmosphere humidity.187
3.7.5.3.6.1Removal excess moisture from cabin atmosphere.187
3.7.5.3.7Circulate atmosphere.187
3.7.5.3.7.1Circulate atmosphere intra-module.187
3.7.5.3.7.2Circulate atmosphere inter-module.187
3.7.5.3.8Station lighting.187
3.7.5.3.8.1Control internal lighting.187
3.7.5.3.8.2Reserved.187
3.7.5.3.8.3Illuminate internal areas.187
3.7.5.3.9Isolate to recovery level.187
3.7.5.3.10Recover lost function.187
3.7.5.3.11Safe.188
3.7.5.3.12Maintain station modes.188
3.7.5.3.13Transition station modes.188
3.7.5.3.14Provide data to crew.189
3.7.5.3.15Accept crew inputs and commands.189
3.7.5.3.16Acquire function status data.189
3.7.5.3.17Access to function status data.189
3.7.5.3.18Respond to fire.190
3.7.5.3.18.1Detect fire event.190
3.7.5.3.18.2Isolate fire control zone.190
3.7.5.3.18.3Extinguish fire.190
3.7.5.3.18.4Recover from fire.190
3.7.5.3.19Respond to depressurization.190
3.7.5.3.19.1Detect rapid depressurization.190
3.7.5.3.19.2Isolate rapid depressurization.190
3.7.5.3.20Respond to hazardous atmosphere.190
3.7.5.3.21Maintain thermal conditioning.191
3.7.5.3.21.1Collect thermal energy.191
3.7.5.3.21.2Transmit thermal energy.191
3.7.5.3.21.3Dispose of thermal energy.191
3.7.5.3.22Provide crew control interface.191
3.7.5.3.23Distribute power.191
3.7.5.3.24Accommodate crew hygiene and wastes.191
3.7.5.3.25Provide ethernet interfaces for JSL devices.191
3.7.5.3.26Crew cabins.191
3.7.5.3.27Support crew personal items.192
3.7.5.3.28Support housekeeping.192
3.7.5.3.29Respond to crew illness or injury.192
3.7.5.3.30Reserved.192
3.7.5.3.31Reserved.192
3.7.5.3.32Reserved.192
3.7.5.3.33Support internal crew restraint and mobility.192
3.7.5.3.34Reserved.194
3.7.5.3.35Control gaseous contaminants.194
3.7.5.3.35.1Remove gaseous contaminants.194
3.7.5.3.36Control airborne particulate contaminants.194
3.7.5.3.36.1Remove airborne particulate contaminants.194
3.7.5.3.37Control airborne microbial growth.194
3.7.5.3.37.1Remove airborne microbes.194
3.7.5.3.38Reserved.194
3.7.5.3.39Reserved.194
3.7.5.3.40Provide remote internal visual access.194
3.7.5.3.40.1Create video signal.194
3.7.5.3.40.2Receive video signal.194
3.7.5.3.41Transmit voice communications.195
3.7.5.3.41.1Transmit hardwire.195
3.7.5.3.42Receive voice communication.195
3.7.5.3.42.1Receive hardwire.195
3.7.5.3.43Transmit video data from MLM.195
3.7.5.3.44Provide docking status.195
3.7.5.3.45Support uplinked data.196
3.7.5.3.45.1Receive uplinked data.196
3.7.5.3.45.2Reserved.196
3.7.5.3.45.3Distribute uplinked data.196
3.7.5.3.46Provide data for downlink.196
3.7.5.3.46.1Reserved.196
3.7.5.3.46.2Transmit data for downlink.196
3.7.5.3.47Support internal equipment translation.196
3.7.5.3.48Support internal equipment removal and replacement.196
3.7.5.3.49Support internal equipment identification.196
3.7.5.3.50Support internal equipment restraint.196
3.7.5.3.51Support orbital replaceable unit repair.196
3.7.5.3.52Store internal equipment.197
3.7.5.3.53Support external vehicle input data for rendezvous operations.197
3.7.5.3.54Exchange data with docked vehicles.197
3.7.5.3.55Provide depressurization capabilities.197
3.7.5.3.56Control attitude - propulsive.197
3.7.5.3.57Provide desaturation torque.198
3.7.6Soyuz Vehicle.198
3.7.6.1Purpose.198
3.7.6.2Description.198
3.7.6.3Physical characteristics.198
3.7.6.3.1Reserved.198
3.7.6.3.2Reserved.198
3.7.6.3.3Soyuz vehicle dimensional envelope.198
3.7.6.3.4Soyuz vehicle body coordinate system.199
3.7.6.3.5Soyuz vehicle crew delivery and return.200
3.7.6.3.5.1Scheduled crew delivery and return.200
3.7.6.3.5.2Support unplanned crew return.201
3.7.6.3.6Personnel size and mass.201
3.7.6.4Safety.205
3.7.6.4.1Internal volume touch temperature.205
3.7.6.4.1.1Internal volume high temperature.205
3.7.6.4.1.2Internal volume low temperature.205
3.7.6.4.2Single failure tolerance.206
3.7.6.4.3Safe.206
3.7.6.4.4Computer control of hazardous functions.206
3.7.6.4.5Hazards during depressurization.206
3.7.6.4.6Hatch opening.206
3.7.6.5Capabilities.206
3.7.6.5.1Control atmospheric pressure.206
3.7.6.5.1.1Control total pressure.206
3.7.6.5.1.2Control oxygen partial pressure.206
3.7.6.5.1.3Equalize pressure.207
3.7.6.5.2Maintain thermal conditioning.207
3.7.6.5.2.1Thermal control system fluid standards.207
3.7.6.5.3Control atmosphere temperature.207
3.7.6.5.4Control atmosphere moisture.207
3.7.6.5.5Circulate atmosphere.207
3.7.6.5.6Support food and water consumption.207
3.7.6.5.7Control carbon dioxide.207
3.7.6.5.8Provide data for downlink.207
3.7.6.5.8.1Transmission of subsystem status while attached to RS.207
3.7.6.5.8.2Soyuz vehicle readiness information.207
3.7.6.5.8.3Vehicle operational support.208
3.7.6.5.9Support crew delivery and return.208
3.7.6.5.9.1Environment of habitable volumes.208
3.7.6.5.9.2Provide translation path.209
3.7.6.5.9.3Launch and delivery.209
3.7.6.5.9.3.1Execute translation maneuvers.209
3.7.6.5.9.3.2Proximity operations.209
3.7.6.5.9.3.2.1Automated collision avoidance maneuvers.209
3.7.6.5.9.3.2.2Mission planning - rendezvous and docking.209
3.7.6.5.9.3.2.3Support external vehicle to ISS relative navigation.209
3.7.6.5.9.3.3Soyuz vehicle docking indication.210
3.7.6.5.9.3.4Soyuz vehicle voice communications.210
3.7.6.5.9.3.5Soyuz vehicle video transmission.210
3.7.6.5.9.3.6Docking mechanism and contact conditions.210
3.7.6.5.9.3.7Soyuz vehicle rendezvous abort command acceptance.210
3.7.6.5.9.3.8Launch.210
3.7.6.5.9.3.9Operational altitude.210
3.7.6.5.9.4Activation and separation.210
3.7.6.5.9.4.1Reserved.210
3.7.6.5.9.4.2Activation independent of ISS and the ground.210
3.7.6.5.9.4.3Reserved.210
3.7.6.5.9.4.4Independent separation capability.210
3.7.6.5.9.4.5Soyuz vehicle initiated separation.211
3.7.6.5.9.4.6Disconnection of utilities.211
3.7.6.5.9.4.7Reserved.211
3.7.6.5.9.4.8Reserved.211
3.7.6.5.9.4.9Separation clearance range.211
3.7.6.5.9.4.10Separation from a tumbling station.211
3.7.6.5.9.5Return mission.211
3.7.6.5.9.5.1Crew intervention.211
3.7.6.5.9.5.2Autonomous Soyuz vehicle operation.211
3.7.6.5.9.5.3Transmission of vehicle status after separation.211
3.7.6.5.9.5.4Orbit inclination.212
3.7.6.5.9.5.5State vector compatibility.212
3.7.6.5.9.5.6Recovery from missed deorbit opportunity.212
3.7.6.5.9.5.7Entry accelerations, nominal mode.212
3.7.6.5.9.5.8Landing cross range.212
3.7.6.5.9.5.9Landing accuracy at the ground.212
3.7.6.5.9.5.10Landing.212
3.7.6.5.9.5.11Automated operations.212
3.7.6.5.9.5.12Landing opportunities.212
3.7.6.5.9.5.13Landing accelerations.213
3.7.6.5.9.5.14Reserved.213
3.7.6.5.9.5.15Support from isolation to landing.213
3.7.6.5.9.5.16Reserved.213
3.7.6.5.9.5.17Ground support to flight operations.213
3.7.6.5.9.6Reserved.213
3.7.6.5.9.6.1Reserved.213
3.7.6.5.9.6.2Crew transport time from Soyuz vehicle separation.213
3.7.6.5.9.6.3Reserved.213
3.7.6.5.9.6.4Communications with mission support.213
3.7.6.5.9.6.5Reserved.213
3.7.6.5.9.6.6Entry accelerations.213
3.7.6.5.9.7Reserved.213
3.7.6.5.9.7.1Attached communications with mission support.213
3.7.6.5.9.7.2Attached Soyuz vehicle - Soyuz vehicle communications.214
3.7.6.5.9.7.3Detached Soyuz vehicle to Soyuz vehicle communication.214
3.7.6.5.9.7.4Attached Soyuz vehicle/RS voice communications.214
3.7.6.5.9.7.5Separation time limit.214
3.7.6.5.9.8Crew recovery, vehicle recovery, and post-recovery operations.214
3.7.6.5.9.8.1Reserved.214
3.7.6.5.9.8.2Post landing support.214
3.7.6.5.9.8.3Vehicle location aid.214
3.7.6.5.9.8.4Reserved.214
3.7.6.5.9.8.5Reserved.214
3.7.6.5.9.8.6Reserved.214
3.7.6.5.9.8.7Crew rescue procedures.214
3.7.6.5.9.8.8Vehicle recovery procedures.214
3.7.6.5.10Training.215
3.7.6.5.10.1Reserved.215
3.7.6.5.10.2Procedures training.215
3.7.6.5.10.3Functional systems training.215
3.7.6.5.11Light Soyuz vehicle.215
3.7.6.5.11.1Control internal lighting.215
3.7.6.5.11.2Illuminate internal areas.215
3.7.6.5.12Service life.215
3.7.6.5.12.1Seal life.215
3.7.7Cargo vehicle.215
3.7.7.1Purpose.215
3.7.7.2Description.215
3.7.7.3Capabilities.216
3.7.7.3.1Control total pressure.216
3.7.7.3.1.1Monitor total pressure.216
3.7.7.3.1.2Control nitrogen introduction.216
3.7.7.3.2Light Cargo vehicle.216
3.7.7.3.2.1Control internal lighting.216
3.7.7.3.2.2Illuminate internal areas.216
3.7.7.3.3Relieve over pressure.216
3.7.7.3.4Equalize pressure.216
3.7.7.3.5Safety.216
3.7.7.3.5.1Internal volume touch temperature.216
3.7.7.3.5.1.1Internal volume high temperature.216
3.7.7.3.5.1.2Internal low volume temperature.216
3.7.7.3.5.2Safe.217
3.7.7.3.5.3Computer control of hazardous functions.217
3.7.7.3.5.4Hatch opening.217
3.7.7.3.6Video transmission.217
3.7.7.3.7Determine state vector and attitude.217
3.7.7.3.8Support uplinked data.217
3.7.7.3.8.1Receive uplinked data.217
3.7.7.3.9Provide data for downlink.217
3.7.7.3.9.1Prepare data for downlink.217
3.7.7.3.9.2Transmit data for downlink.218
3.7.7.3.10Execute maneuver guidance.218
3.7.7.3.11Execute translation thrust.218
3.7.7.3.12Control attitude - propulsive.219
3.7.7.3.13Transport cargo.219
3.7.7.3.14Maintain thermal conditioning.219
3.7.7.3.14.1Thermal control system fluid standards.219
3.7.7.3.15Propellant transfer.219
3.7.7.3.16Trash disposal.220
3.7.7.3.17Capability: support prelaunch operations.220
3.7.7.3.17.1Load/unload cargo items.220
3.7.7.3.17.2Support system checkout and monitoring.220
3.7.7.3.18Cargo vehicle docking indication.220
3.7.7.3.19Independent separation capability.220
3.7.7.3.20Disconnection of utilities.220
3.7.7.3.21Separation clearance range.220
3.7.7.3.22Capability: Provide automated and manual collision avoidance maneuvers.220
3.7.7.3.23Capability: Mission planning - rendezvous and docking.221
3.7.7.3.24Service life.221
3.7.7.3.24.1Seal life.221
3.7.7.3.25Operational altitude.221
3.7.7.3.26Docking mechanism and contact conditions.221
3.7.7.3.27Support external vehicle to ISS relative navigation.221
3.7.8NM.221
3.7.8.1Purpose.221
3.7.8.2Description.221
3.7.8.3Capabilities.222
3.7.8.3.1Reserved.222
3.7.8.3.2Reserved.222
3.7.8.3.3Reserved.222
3.7.8.3.4Reserved.222
3.7.8.3.5Control atmosphere temperature.222
3.7.8.3.5.1Monitor atmosphere temperature.222
3.7.8.3.5.2Remove atmosphere heat.222
3.7.8.3.6Reserved.222
3.7.8.3.7Circulate atmosphere.222
3.7.8.3.7.1Circulate atmosphere intra-module.222
3.7.8.3.7.2Intermodule circulation.222
3.7.8.3.8Lighting.222
3.7.8.3.8.1Control internal lighting.222
3.7.8.3.9Isolate to recovery level.222
3.7.8.3.10Recover lost function.223
3.7.8.3.11Safety.223
3.7.8.3.12Reserved.223
3.7.8.3.13Reserved.223
3.7.8.3.14Reserved.223
3.7.8.3.15Reserved.223
3.7.8.3.16Reserved.223
3.7.8.3.17Assess function status data.223
3.7.8.3.18Respond to fire.223
3.7.8.3.18.1Detect fire event.223
3.7.8.3.18.2Isolate fire control zone.223
3.7.8.3.18.3Extinguish fire.223
3.7.8.3.18.4Recover from fire.224
3.7.8.3.19Respond to depressurization.224
3.7.8.3.19.1Reserved.224
3.7.8.3.19.2Isolate rapid depressurization.224
3.7.8.3.20Reserved.224
3.7.8.3.21Maintain thermal conditioning.224
3.7.8.3.21.1Collect thermal energy.224
3.7.8.3.22Provide crew control interface.224
3.7.8.3.23Reserved.224
3.7.8.3.24Reserved.224
3.7.8.3.25Reserved.224
3.7.8.3.26Reserved.224
3.7.8.3.27Reserved.224
3.7.8.3.28Reserved.224
3.7.8.3.29Reserved.224
3.7.8.3.30Reserved.224
3.7.8.3.31Reserved.224
3.7.8.3.32Reserved.224

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