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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 is a notice for a Request for Proposal (RFP) for the Human Space Flight Technical Integration Contract (HSFTIC). NASA/JSC plans to issue the RFP on or about November 1, 2019, with an anticipated offer due date of December 11, 2019. The procurement is a total small business set-aside with a NAICS code of 541715 and size standard of 1,250. All responsible sources may submit an offer, which will be considered by the agency. The solicitation and related documents will be available at the listed websites. Prospective offerors must notify the office of their intent to submit an offer and are responsible for monitoring the sites for solicitation releases and amendments. Technical questions must be submitted in writing.

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Text version

Segment Specification for the H−II Transfer Vehicle

International Space Station Program

Revision J

March 2019

This document contains information which falls under the purview of the U.S. Munitions List (USML), as defined in the International Traffic in Arms Regulations (ITAR), 22 CFR 120−130, and is export controlled. It shall not be transferred to foreign nationals in the U.S. or abroad, without specific approval of a knowledgeable NASA export control official, and/or unless an export license/license exemption is obtained/available from the United States Department of State. Violations of these regulations are punishable by fine, imprisonment, or both.

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

REVISION AND HISTORY

REVISION AND HISTORY - Continued

REV.
DESCRIPTION
PUB. DATE

The following SCNs have been cancelled. The content of these SSCNs authorizing release of the SCNs has been incorporated into Revision H.

SCN 052 incorporates SSCN 011868 Administrative Cancel SCN 053 incorporates SSCN 011867 Administrative Cancel SCN 054 incorporates SSCN 010967 Administrative Cancel Overcome by events SCN 055 incorporates SSCN 010905 Administrative Cancel SCN 056 incorporates SSCN 011768 Administrative Cancel SCN 057 incorporates SSCN 011019 Administrative Cancel SCN 058 incorporates SSCN 012713 Administrative Cancel No impact SCN 059 incorporates SSCN 012693 Administrative Cancel Not incorporated SCN 060 incorporates SSCN 012902 Administrative Cancel SCN 061 incorporates SSCN 012906 Administrative Cancel

Revision H is the first revision of this Document to be produced in Microsoft Word after its conversion from Interleaf format.

(Draft – January 2018)
NDCs included in this revision:

HTV4-SPEC-001

HTV3 ENV-001

HTV3-EP-MP-003

HTV3 EP-MP-001

HTV3 EP-MP-002

HTV3 Robotics-001 HTV3 Robotics-2

HTV3 ENV-002

HTV3-SPEC-001

HTV3-SPEC-002A

HTV2 Cargo-001

HTV2 IVPAT-001

HTV2 Label-001 HTV2 Robotics-001

HTV2 ENV-001A

HTV2 PROX-001

HTV3 PROX-001

H
Revision H incorporates SSCNs 010905, 010967, 011019, 011867, 011868, 012028 R1, 012902, 012906, 013393, 013515, 013685, and 013686. (Reference per SSCD 013686, EFF. 03-26-15)
06-12-15

Errata to program released Rev H: Removed 011768 – Not Incorporated (deferred to later CR)

REV.
DESCRIPTION
PUB. DATE
J
Revision J incorporates NDCs HTV5-SPEC-002, HTV5-ENV-001 Rev A, HTV6-SPEC-001 Rev A, HTV6-SPEC-003, HTV6-SPEC-004, HTV6-SPEC-005, HTV6-SPEC-006 Rev B, HTV6-SPEC-007 Rev A, HTV6-SPEC-008, HTV6-SPEC-009, HTV6-SPEC-010, HTV7-SPEC-001, HTV7-SPEC-002, HTV7-SPEC-003, HTV7-SPEC-004, HTV7-SPEC-005, HTV7-SPEC-006, HTV7-SPEC-007, HTV7-SPEC-008, HTV7-SPEC-009 and HTV7-SPEC-011 and SSCN 15886 (Reference per SSCD 16005, EFF 05-15-19)
07-30-19

PREFACE

INTERNATIONAL SPACE STATION PROGRAM

SEGMENT SPECIFICATION FOR THE H-II TRANSFER VEHICLE

This document defines the performance and design requirements for the Japanese H-II Transfer Vehicle (HTV) to access the International Space Station, and will be controlled and maintained as described in the Joint Management Plan.

The Space Station Control Board delegates control and approval authority for future updates or revisions to the Transportation Integration Control Board (TICB) per Directive 009441.

INTERNATIONAL SPACE STATION PROGRAM

CONCURRENCE

SEGMENT SPECIFICATION FOR THE H-II TRANSFER VEHICLE

march 2019

TABLE OF CONTENTS

PARAGRAPHPAGE
1.0SCOPE.9
2.0APPLICABLE AND REFERENCE DOCUMENTS.10
2.1Government documents.10
2.1.1Specifications, standards, and handbooks.10
2.1.2Other government documents, drawings, and publications.10
2.2Reference documents.15
2.3Order of precedence.16
2.4Meet or exceed.17
3.0SYSTEM REQUIREMENTS.18
3.1System definition.18
3.1.1System description.18
3.1.1.1H−II Transfer Vehicle.18
3.1.1.2Deleted.18
3.1.1.3HTV Operations System.18
3.1.1.4HTV Proximity Communication System.18
3.1.1.5Laser radar reflector.19
3.1.2Design reference mission.19
3.1.2.1Deleted.19
3.1.2.2Deleted.19
3.1.3Reserved.19
3.1.4Reserved.19
3.1.5Interface requirements.19
3.1.5.1External interfaces.19
3.1.5.1.1International Space Station interface description.19
3.1.5.1.2Space Station Ground Segment interface description.22
3.1.5.1.3HTV cargo interface description.22
3.1.5.1.4Japanese Experiment Module interface description.22
3.1.5.1.5TDRSS interface description.22
3.1.5.1.6Global positioning system interface description.22
3.1.5.1.7Data Relay Technology Satellite interface description.22
3.1.5.1.8Launch vehicle and launch site interface description.22
3.1.5.2Deleted.22
3.1.6Operations definition.22
3.1.6.1Integrated operation definition.23
3.1.6.2Operation phase definition.23
3.1.6.2.1Preparation and prelaunch phase.24
3.1.6.2.2Launch phase.24
3.1.6.2.3Rendezvous phase.24
3.1.6.2.4Proximity operation phase.24
3.1.6.2.5Attached phase.24
3.1.6.2.6Departure phase.24
3.1.6.2.7Reentry phase.24
3.2Characteristics.24
3.2.1Performance characteristics.24
3.2.1.1Launch phase capability.24
3.2.1.2Mode: Rendezvous phase capability.25
3.2.1.2.1Capability: Trajectory.25
3.2.1.2.2Capability: Communication.25
3.2.1.2.2.1Capability: Communication with HTVCC via TDRSS.25
3.2.1.2.2.2Capability: Ranging support via TDRSS.25
3.2.1.2.2.3Capability: RF Communication interface.26
3.2.1.3Proximity operation phase and departure phase capability.26
3.2.1.3.1Trajectory.26
3.2.1.3.1.1Capability: Predefined trajectory.26
3.2.1.3.1.2Capability: Trajectory prior to AI.26
3.2.1.3.1.3Capability: Time adjustment prior to Integrated Operation.26
3.2.1.3.1.4Capability: Proximity operation time capability.26
3.2.1.3.1.5Capability: Nominal proximity operation phase duration.26
3.2.1.3.1.6Capability: Approach Trajectory after AI.26
3.2.1.3.1.7Capability: Hold point inside AE.26
3.2.1.3.1.8Capability: Visibility to ISS.27
3.2.1.3.1.9Capability: Keep out sphere penetration and approach corridor.27
3.2.1.3.1.10Capability: Range rate and braking.27
3.2.1.3.1.11Capability: Safe free drift trajectory after AI.27
3.2.1.3.1.12Capability: Abort.27
3.2.1.3.1.13Capability: Safe retreat to hold point.27
3.2.1.3.1.14Capability: Condition for SSRMS capture.27
3.2.1.3.1.15Capability: Maximum free drift time for capture.27
3.2.1.3.1.16Capability: Capture abort.28
3.2.1.3.1.17Capability: Backup separation.28
3.2.1.3.1.18Capability: Condition for SSRMS release.28
3.2.1.3.1.19Capability: Departure from ISS and departure corridor.28
3.2.1.3.1.20Capability: Maintain positive opening rate during departure.28
3.2.1.3.1.21Capability: Time for exiting AE.28
3.2.1.3.1.22Capability: Reintersection with AE after departure.28
3.2.1.3.1.23Capability: Deorbit and reentry maneuver.28
3.2.1.3.1.24Capability: HTV motions in Berthing Box.29
3.2.1.3.1.25Disturbance induced by SSRMS.29
3.2.1.3.1.26Minimum clearance with ISS during capturing and release
operations.29
3.2.1.3.2Communication.29
3.2.1.3.2.1Capability: Communication with ISS.29
3.2.1.3.2.2Capability: Communication with HTVCC via data relay satellites.30
3.2.1.3.2.3Capability: Communication with HTVCC via SSCC.30
3.2.1.3.2.4Capability: Loss of communication.30
3.2.1.3.2.5Capability: Command protection.30
3.2.1.3.2.6Capability: Omni−Communication coverage.30
3.2.1.3.2.7Capability: Independent means of range and range rate.31
3.2.1.3.2.8RF Communication interference.32
3.2.1.3.3Telemetry and command.33
3.2.1.3.3.1Capability: Telemetry.33
3.2.1.3.3.2Capability: Command.33
3.2.1.3.3.3Capability: GPS data and ISS attitude data.33
3.2.1.3.3.4Capability: Space Station crew command capability.33
3.2.1.3.3.5Capability: Abort command execution.34
3.2.1.3.3.6Capability: Command verification.34
3.2.1.3.3.7Crew display of telemetry.34
3.2.1.3.3.8Capability: Hazard identification.34
3.2.1.3.4Capability: Guidance, Navigation, and Control.34
3.2.1.3.4.1Capability: General design.34
3.2.1.3.4.2Capability: GPS absolute navigation.34
3.2.1.3.4.3Capability: GPS Relative navigation.34
3.2.1.3.4.4Capability: Rendezvous sensor relative navigation.35
3.2.1.3.4.5Capability: Proximity rendezvous maneuver plan.35
3.2.1.3.4.6Capability: Departure and reentry maneuver plan.35
3.2.1.3.4.7Capability: Initiation of AI maneuver.35
3.2.1.3.4.8Capability: Approach maneuver.35
3.2.1.3.4.9Capability: Departure maneuver.35
3.2.1.3.4.10Capability: Automatic abort.35
3.2.1.3.4.11Capability: Motion actuator inhibit and enable.35
3.2.1.3.4.12Capability: Rerendezvous.35
3.2.1.4Mode: Functional capability for pressurized section of HTV LC.35
3.2.1.4.1Capability: Relieve overpressure.36
3.2.1.4.2Capability: Equalize pressure.36
3.2.1.4.3Capability: Monitor atmosphere temperature.36
3.2.1.4.4Reserved.36
3.2.1.4.5Capability: Circulate atmosphere.36
3.2.1.4.6Capability: Illuminate internal area.36
3.2.1.4.7Capability: Monitor total pressure.36
3.2.1.4.8Capability: Support internal crew restraint and mobility.37
3.2.1.4.9Capability: Support internal items translations.37
3.2.1.4.10Capability: Hazardous atmosphere.37
3.2.1.4.11Capability: Respond to fire.37
3.2.1.4.12Capability: Internal user payload volume.37
3.2.1.4.13Capability: Sample atmosphere.37
3.2.1.5Mode: FDIR functional capability during integrated operation.37
3.2.1.5.1Capability: Isolate for safing.37
3.2.1.5.2Capability: Safe.37
3.2.1.5.3Capability: Annunciate alarms.38
3.2.1.5.4Capability: Acquire function status data.38
3.2.1.5.5Capability: Assess functional status data.38
3.2.1.5.6Capability: Manual control of failure, detection, isolation and
recovery.38
3.2.1.6Mode: Functional capability during attached phase.38
3.2.1.6.1Capability: Distribute power from ISS.38
3.2.1.6.2Communication.38
3.2.1.6.2.1Capability: Command and data handling interface with ISS.38
3.2.1.6.2.2Deleted.39
3.2.1.6.2.3Deleted.39
3.2.1.6.2.4Deleted.39
3.2.1.6.3Deleted.39
3.2.1.6.4Deleted.39
3.2.1.7Functional capability during reentry phase.39
3.2.1.7.1Communication.39
3.2.1.7.1.1Capability: Communication with HTVCC via TDRSS.39
3.2.1.7.1.2RF communication interference.39
3.2.1.8Mode: Functional capability of HTV PROX and reflector.39
3.2.1.8.1Capability: Command and data handling interface with ISS.39
3.2.1.8.2Deleted.40
3.2.1.8.3Capability: Reflection of Laser Radar Reflectors.40
3.2.1.8.4Capability: Range and range rate measurement.40
3.2.1.8.5Capability: GPS navigation.41
3.2.1.8.6Crew commanding device HCP and command generation.41
3.2.1.8.6.1Capability: General.41
3.2.1.8.6.2Capability: Command from HCP to HTV.41
3.2.1.8.6.3Capability: Indication of PROX command receipt status.41
3.2.1.8.6.4Capability: Indication of HTV information.41
3.2.1.8.6.5Capability: Indication of communication link status.42
3.2.1.8.6.6Capability: HCP test.42
3.2.1.9System performance.42
3.2.1.9.1Capability: Cargo transportation.42
3.2.1.9.2Capability: Cargo disposal.42
3.2.1.9.3Capability: Rendezvous station altitude.42
3.2.1.9.4Capability: On−orbit life time.42
3.2.1.9.5Capability: Phase adjustment.43
3.2.1.9.6Capability: Launch window.43
3.2.1.9.7Deleted.43
3.2.1.9.8Deleted.43
3.2.1.9.9Late access.43
3.2.1.9.10Keep alive power capability.43
3.2.1.9.11resource margin.43
3.2.1.9.12Deberthing time.43
3.2.1.10Exposed Pallet.43
3.2.1.10.1Exposed Pallet Type I.43
3.2.1.10.1.1Unpressurized cargo transportation capability.43
3.2.1.10.1.2Berthing capability of Exposed Pallet Type I.44
3.2.1.10.1.2.1Resupply and reload of unpressurized cargo.44
3.2.1.10.1.2.2Power.44
3.2.1.10.1.2.3Communication.44
3.2.1.10.1.3Reserved.45
3.2.1.10.1.4Reserved.45
3.2.1.10.1.5Reserved.45
3.2.1.10.1.6Reserved.45
3.2.1.10.1.7Stay time.45
3.2.1.10.1.8Thermal protection.45
3.2.1.10.1.9Exposed Pallet Type Li-on battery oru plus45
3.2.1.10.1.10EVA worksite.45
3.2.1.10.1.11EVR worksite.45
3.2.1.10.2Deleted.46
3.2.1.10.3Deleted.46
3.2.1.10.4Deleted.46
3.2.1.10.5Deleted.46
3.2.1.10.6Deleted.46
3.2.1.10.7Deleted.46
3.2.1.10.8Exposed Pallet Type MP.46
3.2.1.10.8.1Unpressurized cargo transportation capability.46
3.2.1.10.8.2Berthing capability of EP−MP.46
3.2.1.10.8.2.1Resupply and reload of unpressurized cargo.47
3.2.1.10.8.2.2Power.47
3.2.1.10.8.2.2.1ISS provided power.47
3.2.1.10.8.2.2.2HTV provided power.47
3.2.1.10.8.2.2.3EP−MP power physical interface.47
3.2.1.10.8.2.2.3.1Connection responsibility.47
3.2.1.10.8.2.2.4Over−current protection.47
3.2.1.10.8.2.3Communication.47
3.2.1.10.8.3Structural compatibility.48
3.2.1.10.8.3.1Passive FRAM adapter plate.48
3.2.1.10.8.3.2Reserved.48
3.2.1.10.8.3.3FRAM accommodation.48
3.2.1.10.8.3.4DRC accommodation.48
3.2.1.10.8.4Reserved.48
3.2.1.10.8.5Reserved.48
3.2.1.10.8.6Reserved.48
3.2.1.10.8.7Stay time.48
3.2.1.10.8.8Thermal protection.48
3.2.1.10.8.9EP−MP EVA and EVR accommodation.48
3.2.1.10.8.9.1EVA worksite.48
3.2.1.10.8.9.2EVR worksite.49
3.2.1.10.8.10Deleted.49
3.2.1.10.9exposed pallet type li-ion battery oru plus.49
3.2.1.10.9.1unpressurized cargo transportation capability.49
3.2.1.10.9.2berthing capability of EP-6B+.49
3.2.1.10.9.2.1resupply and reload of unpressurized cargo.49
3.2.1.10.9.2.2power.50
3.2.1.10.9.2.2.1iss provided power.50
3.2.1.10.9.2.2.2reserved.50
3.2.1.10.9.2.2.3EP-6B+ power physical interface.50
3.2.1.10.9.2.2.3.1connection responsibility.50
3.2.1.10.9.2.2.4over-current production.50
3.2.1.10.9.2.3communication.50
3.2.1.10.9.3reserved.51
3.2.1.10.9.4reserved.51
3.2.1.10.9.5reserved.51
3.2.1.10.9.6reserved.51
3.2.1.10.9.7stay time.51
3.2.1.10.9.8thermal protection.51
3.2.1.10.9.9ep-6b+ eva and evr accomodation.51
3.2.1.10.9.9.1eva worksite.51
3.2.1.10.9.9.2evr worksite.51
3.2.1.11Mode: Functional capability for unpressurized section of HTV LC.51
3.2.1.11.1Capability: Holding the Exposed Pallet.52
3.2.1.11.2Capability: Removal and capture of the Exposed Pallet.52
3.2.1.11.3Capability: Guide for the Exposed Pallet operations.52
3.2.2Physical and mechanical characteristics.52
3.2.2.1Coordinate systems.53
3.2.2.2Mass property.53
3.2.2.2.1Berthing configuration including cargo.53
3.2.2.2.2Deleted.53
3.2.2.2.3Unberthing configuration including cargo.53
3.2.2.2.4Deleted.53
3.2.2.3HTV grappling by SSRMS.53
3.2.2.4HTV berthing to ISS.53
3.2.2.4.1Alternate ISS berthing port.53
3.2.2.5External crew translation path.53
3.2.2.5.1External translation path interfaces.53
3.2.2.5.2Translation path aids and attachments.53
3.2.2.6Establish Extravehicular Activity translation paths.54
3.2.2.7Establish worksites.54
3.2.2.8Provide MIL−STD−1553B data buses.55
3.2.2.9Physical and Mechanical Characteristics of Exposed Pallet.55
3.2.2.9.1Deleted.55
3.2.2.9.2Size.55
3.2.2.10Structural envelope.55
3.2.3Reliability.55
3.2.3.1Failure tolerance.56
3.2.3.1.1Redundancy verification.56
3.2.3.1.2Illumination failure tolerance.56
3.2.3.2Reserved.56
3.2.3.3Failure propagation.56
3.2.3.4Separation of redundant paths.56
3.2.3.5Deleted.56
3.2.4Maitainability.56
3.2.4.1Maintenance.56
3.2.4.2Nonpressurized area equipment maintenance time.57
3.2.4.3Access item retainment.57
3.2.4.4Equipment item interconnecting devices.57
3.2.4.5Incorrect equipment installation.57
3.2.4.6Lockwiring and staking.57
3.2.4.7Restraining and handling devices for temporary storage.57
3.2.4.8Fluid Capture and Containment.58
3.2.5Reserved.58
3.2.6Environmental conditions.58
3.2.6.1On−orbit environmental conditions.58
3.2.6.1.1Thermal environment.58
3.2.6.1.2Neutral atmosphere.59
3.2.6.1.3External contamination.64
3.2.6.1.4Electromagnetic and geomagnetic fields.64
3.2.6.1.5Plasma.64
3.2.6.1.6Ionizing radiation.65
3.2.6.1.7Solar ultraviolet radiation.65
3.2.6.1.8Meteoroids and Orbital Debris.65
3.2.6.1.9Gravitational field.65
3.2.6.1.10Plume impingement pressures.66
3.2.6.2Launch environmental conditions.66
3.2.6.3Storage and transportation conditions.66
3.2.6.4Deleted.66
3.2.7ISS flight configuration and performance.66
3.2.7.1ISS flight attitude.66
3.2.7.2ISS orbit.68
3.2.7.3Air drag.68
3.2.7.4Solar array orientation.68
3.2.7.5ISS CG envelope.68
3.2.7.6Deleted.69
3.2.7.7Deleted.69
3.2.7.8Deleted.69
3.3Design and construction.69
3.3.1Material, process and parts.69
3.3.1.1Toxic products and formulations.69
3.3.1.2Protective coating.69
3.3.1.3Materials and processes.69
3.3.1.3.1Control of water soluble volatile organic compounds.69
3.3.1.4Electrical, Electronic, and Electromechanical parts selection.69
3.3.1.5Deleted.69
3.3.1.5.1Deleted.69
3.3.1.5.2Deleted.69
3.3.2Electromagnetic radiation.69
3.3.2.1Electromagnetic compatibility requirements.69
3.3.2.2Electromagnetic emission.70
3.3.2.2.1Radiated emission.70
3.3.2.2.2Conducted emission.70
3.3.2.3Electromagnetic susceptibility.71
3.3.2.3.1Radiated Susceptibility.71
3.3.2.3.2Conducted susceptibility.72
3.3.2.4Bonding.73
3.3.3Nameplates and product marking.73
3.3.3.1Inventory labels.73
3.3.3.2Deleted.74
3.3.3.3On−orbit general labeling.74
3.3.3.4Unique and special labels.74
3.3.3.5Cable and hose labels.74
3.3.3.6Label attachment.74
3.3.3.7Caution and warning and emergency labels.74
3.3.3.8Label markings.75
3.3.3.9Location code labels.75
3.3.4Workmanship.75
3.3.4.1Cleanliness.75
3.3.5Interchangeability.75
3.3.6Safety.75
3.3.6.1Safety requirements during Integrated Operation.75
3.3.6.1.1Catastrophic hazards.75
3.3.6.1.2Critical hazards.75
3.3.6.1.3Design for minimum risk.75
3.3.6.1.4Control of functions resulting in critical hazards.76
3.3.6.1.4.1Inadvertent operation resulting in critical hazards.76
3.3.6.1.4.2Loss of function resulting in critical hazards.76
3.3.6.1.5Control of functions resulting in catastrophic hazards.76
3.3.6.1.5.1Inadvertent operation resulting in catastrophic hazards.76
3.3.6.1.5.2Loss of function resulting in catastrophic hazards.76
3.3.6.1.6Hazard detection and safing.76
3.3.6.1.6.1Monitors.76
3.3.6.1.6.1.1Status information.76
3.3.6.1.6.1.2Hazardous function operation prevention.77
3.3.6.1.6.1.3Loss of input or failure.77
3.3.6.1.6.1.4Flight crew availability.77
3.3.6.1.6.2Near−real−time monitoring.77
3.3.6.1.6.3Real−time monitoring.77
3.3.6.1.6.3.1Maintain status of hazard controls.77
3.3.6.1.6.3.2Crew response time and safing procedures.77
3.3.6.1.6.3.3Ground monitoring.77
3.3.6.1.7Computer control of hazardous functions.77
3.3.6.1.7.1General.77
3.3.6.1.7.1.1Safe initialization.77
3.3.6.1.7.1.2Safe termination.78
3.3.6.1.7.1.3Off−nominal power conditions.78
3.3.6.1.7.1.4Actions for override.78
3.3.6.1.7.1.5Commands out of sequence.78
3.3.6.1.7.1.6Inadvertent memory modification.78
3.3.6.1.7.1.7Recover for CBCS anomaly.78
3.3.6.1.7.1.8Input validation.78
3.3.6.1.7.1.9Flight software traceability.78
3.3.6.1.7.1.10Code documentation.78
3.3.6.1.7.1.11Integrity check.78
3.3.6.1.7.1.12Protection for uplinked commands.78
3.3.6.1.7.1.13Prerequisite checks.78
3.3.6.1.7.2Must work function.79
3.3.6.1.7.2.1Two unique commands (catastrophic).79
3.3.6.1.7.2.2Two unique commands (critical).79
3.3.6.1.7.2.3One operator action.79
3.3.6.1.7.2.4Must work assembly functions.79
3.3.6.1.7.2.5Separation/Protection of redundant paths.79
3.3.6.1.7.2.6Respond to loss of function.79
3.3.6.1.7.3Must not work function.79
3.3.6.1.7.3.1Fault containment approach (FCA).79
3.3.6.1.7.3.1.1prerequisite check.79
3.3.6.1.7.3.1.2Removal of inhibit.79
3.3.6.1.7.3.1.3Change of the state of inhibit.80
3.3.6.1.7.3.1.4Inhibit monitor.80
3.3.6.1.7.3.1.5Independent parameter for FCA.80
3.3.6.1.7.3.1.6Operator controllable parameter for FCA.80
3.3.6.1.7.3.1.7One operator action.80
3.3.6.1.7.3.1.8Software inhibit monitor.80
3.3.6.1.7.3.1.9Manual saving monitor.80
3.3.6.1.7.3.1.10Independent action for inhibit.80
3.3.6.1.7.3.2Control path separation approach.80
3.3.6.1.7.3.2.1Inhibit monitor.80
3.3.6.1.7.3.2.2Separate control paths.80
3.3.6.1.7.3.2.3Unique commands for inhibits.80
3.3.6.1.7.3.2.4Independent parameters for SCPs.81
3.3.6.1.7.3.2.5Operator controllable parameter.81
3.3.6.1.7.3.2.6Independent action for inhibits.81
3.3.6.1.7.3.2.7Functionally different SCPs.81
3.3.6.1.7.3.2.8Software inhibit monitor.81
3.3.6.1.7.3.2.9System status monitor.81
3.3.6.1.8Hazardous materials.81
3.3.6.1.8.1Hazardous fluid containment failure tolerance.81
3.3.6.1.9Deleted.81
3.3.6.1.9.1Deleted.81
3.3.6.1.10Radiation81
3.3.6.1.10.1Ionizing radiation.81
3.3.6.1.10.2Nonionizing radiation.81
3.3.6.1.11Optics and lasers.82
3.3.6.1.11.1Lasers.82
3.3.6.1.12Batteries.82
3.3.6.1.13Liquid propellant propulsion system.82
3.3.6.1.13.1Inadvertent firing of bi−propellant engines.82
3.3.6.1.13.2Reserved.82
3.3.6.1.13.3Absence of opening signal.82
3.3.6.1.13.4Isolation valves.82
3.3.6.1.13.5Opening the isolation valves.82
3.3.6.1.13.6Propellant overheating or freezing.83
3.3.6.1.13.7Propellant leakage.83
3.3.6.1.13.8Adiabatic or rapid compression detonation.83
3.3.6.1.13.9Hazardous venting.83
3.3.6.1.13.10Monitoring propulsion system status.83
3.3.6.1.14Subsequent induced loads.84
3.3.6.1.15Environmental capability.84
3.3.6.2Safety requirements during HTV attached phase.84
3.3.6.2.1Electrical safety.84
3.3.6.2.1.1Electrical power circuit overloads and short circuits.84
3.3.6.2.1.1.1Circuit over−load protection.84
3.3.6.2.1.1.2Protective device sizing.84
3.3.6.2.1.1.3Bent pin or conductive contamination84
3.3.6.2.1.1.4Load short to chassis wire sizing.84
3.3.6.2.1.1.5Load short to chassis safety.84
3.3.6.2.1.1.6Wire short to chassis safety.85
3.3.6.3Safety requirements for pressurized section.85
3.3.6.3.1Fire protection.85
3.3.6.3.1.1Fire detection.85
3.3.6.3.1.2Crew notification.85
3.3.6.3.1.3Fire isolation.89
3.3.6.3.1.4Fire consequences.89
3.3.6.3.1.5Fire extinguishment.89
3.3.6.3.1.6Fire suppressant.89
3.3.6.3.1.7Fire suppressant application.89
3.3.6.3.1.8Portable Breathing Apparatus and Portable Fire Extinguisher
locations.89
3.3.6.3.1.9Module depressurization.89
3.3.6.3.1.10Confirmation.89
3.3.6.3.1.11Manual activation.89
3.3.6.3.2Pressure volume depressurization and depressurization tolerance.90
3.3.6.3.2.1Pressure differential tolerance.90
3.3.6.3.2.2Operation during pressure changes.90
3.3.6.3.3Emergency intravehicular activity egress.90
3.3.6.3.4Verifiable seal leakage paths.90
3.3.6.3.5Hatch opening.91
3.3.6.3.6Hazardous gas accumulation.92
3.3.6.3.6.1Accumulation prevention. See section 3.2.1.4.5.92
3.3.6.3.6.2Detection and monitoring.92
3.3.6.3.7Equipment clearance for entrapment hazard.92
3.3.6.3.8Light fixture.92
3.3.6.3.9Crew protection from electrical shock.92
3.3.6.4Human engineering safety.92
3.3.6.4.1Internal volume touch temperature.92
3.3.6.4.2Internal corner and edge protection.92
3.3.6.4.2.1Equipment exposed to crew activity.92
3.3.6.4.2.2Equipment exposed only during planned maintenance activities.92
3.3.6.4.3External touch temperature.92
3.3.6.4.3.1Incidental contact.93
3.3.6.4.3.2Unlimited contact.93
3.3.6.4.4External corner and edge protection.94
3.3.6.4.4.1Sharp edges.94
3.3.6.4.4.2Thin materials.94
3.3.6.4.4.3Planned maintenance or storage.94
3.3.6.4.5Latches.94
3.3.6.4.6Screw and bolts.94
3.3.6.4.6.1Fasteners.94
3.3.6.4.7Safety−critical fastener.94
3.3.6.4.8Levers, cranks, hooks, and controls.94
3.3.6.4.9Burrs.95
3.3.6.4.10Holes.95
3.3.6.4.10.1Equipment located inside habitable volumes.95
3.3.6.4.10.2Equipment located outside habitable volumes.95
3.3.6.4.11Protrusions.95
3.3.6.4.12Pinch points.95
3.3.6.4.13Flexhoses.95
3.3.6.4.14Translation routes and established worksites.95
3.3.6.4.14.1EVA translation routes and established worksites.95
3.3.6.4.14.2Secondary translation routes and established worksites.95
3.3.6.4.14.3EVA crewmember contact isolation.97
3.3.6.4.15Moving or rotating equipment.97
3.3.6.5Rocket payload safety.97
3.3.6.6Range safety.97
3.3.6.7Reentry safety.97
3.3.7Human engineering.97
3.3.7.1Anthropometric requirements.97
3.3.7.1.1Strength requirements.97
3.3.7.1.1.1Normal operations.97
3.3.7.2HTV external hardware.97
3.3.7.2.1External task location requirements.97
3.3.7.2.2EVA crewmember field of view.98
3.3.7.2.3Working volume.98
3.3.7.2.4External limit loads.98
3.3.7.2.5Worksite crew−mobility aids.102
3.3.7.2.5.1Placement for worksite tasks.102
3.3.7.2.5.2Proximity to foot restraint.102
3.3.7.2.5.3Foot restraint ingress and egress aid.103
3.3.7.2.5.4Height considerations.103
3.3.7.2.5.5Centering.103
3.3.7.2.5.6Gloved operation.103
3.3.7.2.5.6.1Clearance.103
3.3.7.3Location coding.103
3.3.7.4Internal crew and equipment translation.104
3.3.7.5Support housekeeping.104
3.3.7.6Operational uniformity.104
3.3.7.7Annunciator commonality.104
3.3.7.8Pressure−suited operation.104
3.3.7.9Incorrect equipment installation.104
3.3.7.10Connectors.104
3.3.7.11Controls and displays.104
3.3.7.12Cable management.104
3.3.7.13IVA closures and covers and item retention.105
3.3.7.14Removal, replacement, and modularity of design.105
3.3.7.15Tool access.105
3.3.7.16Alignment devices.105
3.3.7.17Reserved.105
3.3.7.18Emergency controls strength.105
3.3.7.19Fluid/gas capture and containment.105
3.3.7.20General mounting.105
3.3.7.21Contingency EVA operations.105
3.3.7.21.1Unpressurized access for on−orbit contingency EVA operations.105
3.3.7.21.1.1Access for on−orbit inspection.106
3.3.7.21.1.2Visual access.106
3.3.7.21.1.3EVA access to fasteners.106
3.3.7.21.2Standard on−orbit tools.107
3.3.7.22Hatch design.107
3.3.8Nuclear control.107
3.3.9System security.107
3.3.10Environmental constraints.107
3.3.10.1Reserved.107
3.3.10.2Acoustic emission limits.107
3.3.10.3External contamination releases.107
3.3.10.3.1Material outgassing induced contamination during the Integrated Operations.107
3.3.10.3.2Thruster plume induced contamination during the Integrated
Operations.108
3.3.10.4Ionizing radiation emission limits.108
3.3.10.5Plume impingement.108
3.3.10.5.1Pressures.108
3.3.10.5.2HTV plume heating and induced thermal environment on ISS.108
3.3.11Design for remote controlled external operations.109
3.3.11.1Equipment requiring Shuttle robotic support.109
3.3.11.2External equipment requiring robotic hand−off.109
3.3.11.3External equipment requiring SSRMS support.109
3.3.11.3.1Equipment requiring SSRMS support using an NSTS GF.112
3.3.11.3.2Equipment requiring SSRMS support using a PDGF.113
3.3.11.3.3Equipment requiring SSRMS support using a PVGF.113
3.3.11.4External equipment requiring dexterous robotic support.113
3.3.11.5Equipment requiring robotic translation.116
3.3.12Structures and mechanisms.117
3.3.12.1Structural Design.117
3.3.12.2Structure Penetrations.118
3.3.12.3Microgravity Disturbances.118
3.3.12.3.1Limit accelerations.118
3.3.12.3.1.1Limit quasi−steady acceleration.118
3.3.12.3.1.2Limit vibratory accelerations.118
3.3.12.3.2Limit angular momentum disturbance.118
3.3.12.3.2.1Limit disturbance induced ISS attitude rate.118
3.3.12.3.2.2Limit disturbance induced CMG momentum usage.120
3.3.12.4EVA induced loads.121
3.3.12.5IVA induced loads.123
3.3.12.6Window, glass, and ceramic structural design.124
3.3.13Fluid standards.124
3.3.14Atmosphere leakage.124
3.3.15Preclude condensation.124
3.3.15.1condensation.124
3.3.16MIL−STD−1553 data bus constraints.124
3.3.16.1SSQ components.124
3.3.16.1.1Bus coupler type.125
3.3.16.2Bus stub length.125
3.3.16.3Bus coupling.125
3.3.16.4HTV not−to−exceed bus length.126
3.3.16.5Deleted.127
3.3.16.6Output amplitude.127
3.3.17Terminal Interface Units.127
3.3.17.1Deleted.127
3.3.17.2TIU Multiple Bus Isolation.127
3.3.17.3Deleted.127
3.3.17.4HTV addresses.127
3.3.17.5PROX addresses.127
3.3.17.6Input impedance.127
3.3.18Deleted.127
3.3.18.1Deleted.127
3.3.18.2Deleted.127
3.3.18.3Deleted.127
3.3.18.4Deleted.127
3.3.18.5Deleted.128
3.3.18.6Deleted.128
3.3.19Resource management.128
3.3.19.1Power resource.128
3.3.19.1.1Housekeeping power allocations.128
3.3.19.1.2Manage random cyclic loads.129
3.3.20Optical interference.129
3.3.21Hatch.129
3.4Computer resource requirements.129
3.5Logistics.129
3.6Personnel.129
3.7Characteristics.129
3.8Precedence.129
4.0VERIFICATION.130
4.1General.130
4.1.1Responsibility for verifications.131
4.1.2Special tests and examinations.131
4.2Requirement/Verification cross reference matrix.131
4.3System requirements.131
4.3.1System definition.131
4.3.2Characteristics.131
4.3.2.1Performance characteristics.131
4.3.2.1.1Launch phase capability.131
4.3.2.1.2Mode: Rendezvous phase capability.131
4.3.2.1.2.1Capability: Trajectory.132
4.3.2.1.2.2Capability: Communication.132
4.3.2.1.2.2.1Capability: Communication with HTVCC via TDRSS.132
4.3.2.1.2.2.2Capability: Ranging support via TDRSS.132
4.3.2.1.2.2.3Capability: RF Communication interface.132
4.3.2.1.3Proximity operation phase and departure phase capability.133
4.3.2.1.3.1Trajectory.133
4.3.2.1.3.1.1Capability: Predefined trajectory.133
4.3.2.1.3.1.2Capability: Trajectory prior to AI.134
4.3.2.1.3.1.3Capability: Time adjustment prior to Integrated Operation.134
4.3.2.1.3.1.4Capability: Proximity operation time capability.135
4.3.2.1.3.1.5Capability: Nominal proximity operation phase duration.135
4.3.2.1.3.1.6Capability: Approach Trajectory after AI.135
4.3.2.1.3.1.7Capability: Hold point inside AE.136
4.3.2.1.3.1.8Capability: Visibility to ISS.137
4.3.2.1.3.1.9Capability: Keep out sphere penetration and approach corridor.137
4.3.2.1.3.1.10Capability: Range rate and braking.138
4.3.2.1.3.1.11Capability: Safe free drift trajectory after AI.138
4.3.2.1.3.1.12Capability: Abort.139
4.3.2.1.3.1.13Capability: Safe retreat to hold point.140
4.3.2.1.3.1.14Capability: Condition for SSRMS capture.140
4.3.2.1.3.1.15Capability: Maximum free drift time for capture.140
4.3.2.1.3.1.16Capability: Capture abort.141
4.3.2.1.3.1.17Capability: Backup separation.142
4.3.2.1.3.1.18Capability: Condition for SSRMS release.143
4.3.2.1.3.1.19Capability: Departure from ISS and departure corridor.143
4.3.2.1.3.1.20Capability: Maintain positive opening rate during departure.144
4.3.2.1.3.1.21Capability: Time for exiting AE.144
4.3.2.1.3.1.22Capability: Reintersection with AE after departure.144
4.3.2.1.3.1.23Capability: Deorbit and reentry maneuver.144
4.3.2.1.3.1.24Capability: HTV motions in Berthing Box.145
4.3.2.1.3.1.25Disturbance induced by SSRMS.145
4.3.2.1.3.1.26Minimum clearance with ISS during capturing and release
operations.146
4.3.2.1.3.2Communication.146
4.3.2.1.3.2.1Capability: Communication with ISS.146
4.3.2.1.3.2.2Capability: Communication with HTVCC via data relay satellites.147
4.3.2.1.3.2.3Capability: Communication with HTVCC via SSCC.147
4.3.2.1.3.2.4Capability: Loss of communication.147
4.3.2.1.3.2.5Capability: Command protection.148
4.3.2.1.3.2.6Capability: Omni−Communication coverage.148
4.3.2.1.3.2.7Capability: Independent means of range and range rate.148
4.3.2.1.3.2.8RF Communication interference.149
4.3.2.1.3.3Telemetry and command.149
4.3.2.1.3.3.1Capability: Telemetry.150
4.3.2.1.3.3.2Capability: Command.151
4.3.2.1.3.3.3Capability: GPS data and ISS attitude data.151
4.3.2.1.3.3.4Capability: Space Station crew command capability.151
4.3.2.1.3.3.5Capability: Abort command execution.152
4.3.2.1.3.3.6Capability: Command verification.152
4.3.2.1.3.3.7Crew display of telemetry.152
4.3.2.1.3.3.8Capability: Hazard identification.152
4.3.2.1.3.4Capability: Guidance, Navigation, and Control.153
4.3.2.1.3.4.1Capability: General design.153
4.3.2.1.3.4.2Capability: GPS absolute navigation.153
4.3.2.1.3.4.3Capability: GPS Relative navigation.153
4.3.2.1.3.4.4Capability: Rendezvous sensor relative navigation.154
4.3.2.1.3.4.5Capability: Proximity rendezvous maneuver plan.154
4.3.2.1.3.4.6Capability: Departure and reentry maneuver plan.155
4.3.2.1.3.4.7Capability: Initiation of AI maneuver.155
4.3.2.1.3.4.8Capability: Approach maneuver.155
4.3.2.1.3.4.9Capability: Departure maneuver.156
4.3.2.1.3.4.10Capability: Automatic abort.156
4.3.2.1.3.4.11Capability: Motion actuator inhibit and enable.156
4.3.2.1.3.4.12Capability: Rerendezvous.157
4.3.2.1.4Mode: Functional capability for pressurized section of HTV LC.158
4.3.2.1.4.1Capability: Relieve overpressure.158
4.3.2.1.4.2Capability: Equalize pressure.158
4.3.2.1.4.3Capability: Monitor atmosphere temperature.158
4.3.2.1.4.4Reserved.158
4.3.2.1.4.5Capability: Circulate atmosphere.158
4.3.2.1.4.6Capability: Illuminate internal area.159
4.3.2.1.4.7Capability: Monitor total pressure.159
4.3.2.1.4.8Capability: Support internal crew restraint and mobility.160
4.3.2.1.4.9Capability: Support internal items translations.160
4.3.2.1.4.10Capability: Hazardous atmosphere.161
4.3.2.1.4.11Capability: Respond to fire.161
4.3.2.1.4.12Capability: Internal user payload volume.161
4.3.2.1.4.13Capability: Sample atmosphere.161
4.3.2.1.5Mode: FDIR functional capability during integrated operation.162
4.3.2.1.5.1Capability: Isolate for safing.162
4.3.2.1.5.2Capability: Safe.162
4.3.2.1.5.3Capability: Annunciate alarms.162
4.3.2.1.5.4Capability: Acquire function status data.162
4.3.2.1.5.5Capability: Assess functional status data.163
4.3.2.1.5.6Capability: Manual control of failure, detection, isolation and
recovery.163
4.3.2.1.6Mode: Functional capability during attached phase.163
4.3.2.1.6.1Capability: Distribute power from ISS.163
4.3.2.1.6.2Communication.164
4.3.2.1.6.2.1Capability: Command and data handling interface with ISS.164
4.3.2.1.6.2.2Deleted.165
4.3.2.1.6.2.3Deleted.165
4.3.2.1.6.2.4Deleted.165
4.3.2.1.6.3Deleted.165
4.3.2.1.6.4Deleted.165
4.3.2.1.7Functional capability during reentry phase.165
4.3.2.1.7.1Communication.165
4.3.2.1.7.1.1Capability: Communication with HTVCC via TDRSS.165
4.3.2.1.7.1.2RF communication interference.165
4.3.2.1.8Mode: Functional capability of HTV PROX and reflector.165
4.3.2.1.8.1Capability: Command and data handling interface with ISS.166
4.3.2.1.8.2Deleted.166
4.3.2.1.8.3Capability: Reflection of Laser Radar Reflectors.166
4.3.2.1.8.4Capability: Range and range rate measurement.167
4.3.2.1.8.5Capability: GPS navigation.167
4.3.2.1.8.6Crew commanding device HCP and command generation.168
4.3.2.1.8.6.1Capability: General.168
4.3.2.1.8.6.2Capability: Command from HCP to HTV.168
4.3.2.1.8.6.3Capability: Indication of PROX command receipt status.169
4.3.2.1.8.6.4Capability: Indication of HTV information.170
4.3.2.1.8.6.5Capability: Indication of communication link status.170
4.3.2.1.8.6.6Capability: HCP test.171
4.3.2.1.9System performance.171
4.3.2.1.9.1Capability: Cargo transportation.171
4.3.2.1.9.2Capability: Cargo disposal.171
4.3.2.1.9.3Capability: Rendezvous station altitude.172
4.3.2.1.9.4Capability: On−orbit life time.172
4.3.2.1.9.5Capability: Phase adjustment.172
4.3.2.1.9.6Capability: Launch window.172
4.3.2.1.9.7Deleted.172
4.3.2.1.9.8Deleted.172
4.3.2.1.9.9Late access.172
4.3.2.1.9.10Keep alive power capability.173
4.3.2.1.9.11resource margin.173
4.3.2.1.9.12Deberthing time.173
4.3.2.1.10Exposed Pallet.173
4.3.2.1.10.1Exposed Pallet Type I.173
4.3.2.1.10.1.1Unpressurized cargo transportation capability.174
4.3.2.1.10.1.2Berthing capability of Exposed Pallet Type I.174
4.3.2.1.10.1.2.1Resupply and reload of unpressurized cargo.175
4.3.2.1.10.1.2.2Power.175
4.3.2.1.10.1.2.3Communication.175
4.3.2.1.10.1.3Reserved.176
4.3.2.1.10.1.4Reserved.176
4.3.2.1.10.1.5Reserved.176
4.3.2.1.10.1.6Reserved.176
4.3.2.1.10.1.7Stay time.176
4.3.2.1.10.1.8Thermal protection.176
4.3.2.1.10.1.9Reserved.177
4.3.2.1.10.1.10EVA worksite.177
4.3.2.1.10.1.11EVR worksite.177
4.3.2.1.10.2Deleted.177
4.3.2.1.10.3Deleted.177
4.3.2.1.10.4Deleted.177
4.3.2.1.10.5Deleted.177
4.3.2.1.10.6Deleted.177
4.3.2.1.10.7Deleted.177
4.3.2.1.10.8EP−MP177
4.3.2.1.10.8.1Unpressurized cargo transportation capability.177
4.3.2.1.10.8.2Berthing capability of EP−MP.178
4.3.2.1.10.8.2.1Resupply and reload of unpressurized cargo.179
4.3.2.1.10.8.2.2Power.179
4.3.2.1.10.8.2.2.1ISS provided power.179
4.3.2.1.10.8.2.2.2HTV provided power.180
4.3.2.1.10.8.2.2.3EP−MP power physical interface.180
4.3.2.1.10.8.2.2.4Over−current protection.180
4.3.2.1.10.8.2.3Communication.180
4.3.2.1.10.8.3Structural compatibility.180
4.3.2.1.10.8.3.1Passive FRAM adapter plate.181
4.3.2.1.10.8.3.2Reserved.181
4.3.2.1.10.8.3.3FRAM accommodation.181
4.3.2.1.10.8.3.4DRC accommodation.181
4.3.2.1.10.8.4Reserved.181
4.3.2.1.10.8.5Reserved.181
4.3.2.1.10.8.6Reserved.181
4.3.2.1.10.8.7Stay time.181
4.3.2.1.10.8.8Thermal protection.182
4.3.2.1.10.8.9EP−MP EVA and EVR accommodation.182
4.3.2.1.10.8.9.1EVA worksite.182
4.3.2.1.10.8.9.2EVR worksite.182
4.3.2.1.10.8.9.3DELETED183
4.3.2.1.10.9exposed pallet type li-ion battery oru plus183
4.3.2.1.10.9.1unpressurized cargo transportaion capability183
4.3.2.1.10.9.2berthing capability of ep-6b+183
4.3.2.1.10.9.2.1resupply and reload of unpressurized cargo184
4.3.2.1.10.9.2.2power185
4.3.2.1.10.9.2.2.1iss provided power185
4.3.2.1.10.9.2.2.2reserved185
4.3.2.1.10.9.2.2.3EP-6B+ power physical interface185
4.3.2.1.10.9.2.2.4CONNECTION resposibility185
4.3.2.1.10.9.2.2.5over-current protection185
4.3.2.1.10.9.2.3communication186
4.3.2.1.10.9.3reserved186
4.3.2.1.10.9.4reserved186
4.3.2.1.10.9.5reserved186
4.3.2.1.10.9.6reserved186
4.3.2.1.10.9.7stay time186
4.3.2.1.10.9.8thermal protection186
4.3.2.1.10.9.9ep-6b+ Eva and evr accomodation187
4.3.2.1.10.9.9.1eva worksite187
4.3.2.1.10.9.9.2evr worksite187
4.3.2.1.11Mode: Functional capability for unpressurized section of HTV LC.187
4.3.2.1.11.1Capability: Holding the Exposed Pallet.187
4.3.2.1.11.2Capability: Removal and capture of the Exposed Pallet.187
4.3.2.1.11.3Capability: Guide for the Exposed Pallet operations.188
4.3.2.2Physical and mechanical characteristics.188
4.3.2.2.1Coordinate systems.188
4.3.2.2.2Mass property.188
4.3.2.2.2.1Berthing configuration including cargo.188
4.3.2.2.2.2Deleted.188
4.3.2.2.2.3Unberthing configuration including cargo.188
4.3.2.2.2.4Deleted.189
4.3.2.2.3HTV grappling by SSRMS.189
4.3.2.2.4HTV berthing to ISS.189
4.3.2.2.4.1Alternate ISS berthing port.189
4.3.2.2.5External crew translation path.189
4.3.2.2.5.1External translation path interfaces.189
4.3.2.2.5.2Translation path aids and attachments.190
4.3.2.2.6Establish Extravehicular Activity translation paths.190
4.3.2.2.7Establish worksites.190
4.3.2.2.8Provide MIL−STD−1553B data buses.191
4.3.2.2.9Physical and Mechanical Characteristics of Exposed Pallet.191
4.3.2.2.9.1Deleted.191
4.3.2.2.9.2Size.191
4.3.2.2.10Structural envelope.192
4.3.2.3Reliability.192
4.3.2.3.1Failure tolerance.192
4.3.2.3.1.1Redundancy verification.192
4.3.2.3.1.2Illumination failure tolerance.193
4.3.2.3.2Reserved.193
4.3.2.3.3Failure propagation.193
4.3.2.3.4Separation of redundant paths.193
4.3.2.3.5Deleted.193
4.3.2.4Maintainability.193
4.3.2.4.1Maintenance.193
4.3.2.4.2Nonpressurized area equipment maintenance time.194
4.3.2.4.3Access item retainment.194
4.3.2.4.4Equipment item interconnecting devices.194
4.3.2.4.5Incorrect equipment installation.194
4.3.2.4.6Lockwiring and staking.195
4.3.2.4.7Restraining and handling devices for temporary storage.195
4.3.2.4.8Fluid Capture and Containment.195
4.3.2.5Reserved.195
4.3.2.6Environmental conditions.195
4.3.2.6.1On−orbit environmental conditions.195
4.3.2.6.1.1Thermal environment.196
4.3.2.6.1.2Neutral atmosphere.196
4.3.2.6.1.3External contamination.196
4.3.2.6.1.4Electromagnetic and geomagnetic fields.197
4.3.2.6.1.5Plasma.197
4.3.2.6.1.6Ionizing radiation.197
4.3.2.6.1.7Solar ultraviolet radiation.198
4.3.2.6.1.8Meteoroids and Orbital Debris.198
4.3.2.6.1.9Gravitational field.198
4.3.2.6.1.10Plume impingement pressures.198
4.3.2.6.2Launch environmental conditions.199
4.3.2.6.3Storage and transportation conditions.199
4.3.2.6.4Deleted.199
4.3.2.7ISS flight configuration and performance.199
4.3.2.7.1ISS flight attitude.199
4.3.2.7.2ISS orbit.200
4.3.2.7.3Air drag.200
4.3.2.7.4Solar array orientation.200
4.3.2.7.5ISS CG envelope.200
4.3.2.7.6Deleted.201
4.3.2.7.7Deleted.201
4.3.2.7.8Deleted.201
4.3.3Design and construction.201
4.3.3.1Material, process and parts.201
4.3.3.1.1Toxic products and formulations.201
4.3.3.1.2Protective coating.201
4.3.3.1.3Materials and processes.201
4.3.3.1.3.1Control of water soluble volatile organic compounds.201
4.3.3.1.4Electrical, Electronic, and Electromechanical parts selection.201
4.3.3.1.5Deleted.202
4.3.3.1.5.1Deleted.202
4.3.3.1.5.2Deleted.202
4.3.3.2Electromagnetic radiation.202
4.3.3.2.1Electromagnetic compatibility requirements.202
4.3.3.2.2Electromagnetic emission.202
4.3.3.2.2.1Radiated emission.202
4.3.3.2.2.2Conducted emission.202
4.3.3.2.3Electromagnetic susceptibility.203
4.3.3.2.3.1Radiated susceptibility.203
4.3.3.2.3.2Conducted susceptibility.203
4.3.3.2.4Bonding.203
4.3.3.3Nameplates and product marking.203
4.3.3.3.1Inventory labels.203
4.3.3.3.2Deleted.204
4.3.3.3.3On−orbit general labeling.204
4.3.3.3.4Unique and special labels.204
4.3.3.3.5Cable and hose labels.205
4.3.3.3.6Label attachment.205
4.3.3.3.7Caution and warning and emergency labels.205
4.3.3.3.8Label markings.206
4.3.3.3.9Location code labels.206
4.3.3.4Workmanship.206
4.3.3.4.1Cleanliness.206
4.3.3.5Interchangeability.206
4.3.3.6Safety.206
4.3.3.6.1Safety requirements during Integrated Operation.207
4.3.3.6.1.1Catastrophic hazards.207
4.3.3.6.1.2Critical hazards.207
4.3.3.6.1.3Design for minimum risk.207
4.3.3.6.1.4Control of functions resulting in critical hazards.207
4.3.3.6.1.4.1Inadvertent operation resulting in critical hazards.207
4.3.3.6.1.4.2Loss of Function resulting in critical hazards.207
4.3.3.6.1.5Control of functions resulting in catastrophic hazards.208
4.3.3.6.1.5.1Inadvertent operation resulting in catastrophic hazards.208
4.3.3.6.1.5.2Loss of function resulting in catastrophic hazards.208
4.3.3.6.1.6Hazard detection and safing.209
4.3.3.6.1.6.1monitors.209
4.3.3.6.1.6.1.1Status information.209
4.3.3.6.1.6.1.2Hazardous function operation prevention.209
4.3.3.6.1.6.1.3Loss of input or failure.209
4.3.3.6.1.6.1.4Flight crew availability.209
4.3.3.6.1.6.2Near−real−time monitoring.210
4.3.3.6.1.6.3Real−time monitoring.210
4.3.3.6.1.6.3.1Maintain status of hazard controls.210
4.3.3.6.1.6.3.2Crew response time and safing procedures.210
4.3.3.6.1.6.3.3Ground monitoring.210
4.3.3.6.1.7Computer control of hazardous functions.210
4.3.3.6.1.7.1General.211
4.3.3.6.1.7.1.1Safe initialization.211
4.3.3.6.1.7.1.2Safe termination.211
4.3.3.6.1.7.1.3Off−nominal power conditions.211
4.3.3.6.1.7.1.4Actions for override.211
4.3.3.6.1.7.1.5Commands out of sequence.212
4.3.3.6.1.7.1.6Inadvertent memory modification.212
4.3.3.6.1.7.1.7Recover for CBCS anomaly.212
4.3.3.6.1.7.1.8Input validation.212
4.3.3.6.1.7.1.9Flight software traceability.212
4.3.3.6.1.7.1.10Code documentation.212
4.3.3.6.1.7.1.11Integrity check.212
4.3.3.6.1.7.1.12Protection for uplinked commands.213
4.3.3.6.1.7.1.13Prerequisite checks.213
4.3.3.6.1.7.2Must work function.213
4.3.3.6.1.7.2.1Two unique commands (catastrophic).213
4.3.3.6.1.7.2.2Two unique commands (critical).213
4.3.3.6.1.7.2.3One operator action.214
4.3.3.6.1.7.2.4Must work assembly functions.214
4.3.3.6.1.7.2.5Separation/Protection of redundant paths.214
4.3.3.6.1.7.2.6Respond to loss of function.214
4.3.3.6.1.7.3Must not work function.214
4.3.3.6.1.7.3.1Fault containment approach.214
4.3.3.6.1.7.3.1.1Prerequisite check.214
4.3.3.6.1.7.3.1.2Removal of inhibit.215
4.3.3.6.1.7.3.1.3Change of the state of inhibit.215
4.3.3.6.1.7.3.1.4Inhibit monitor.215
4.3.3.6.1.7.3.1.5Independent parameter for FCA.215
4.3.3.6.1.7.3.1.6Operator controllable parameter for FCA.215
4.3.3.6.1.7.3.1.7One operator action.216
4.3.3.6.1.7.3.1.8Software inhibit monitor.216
4.3.3.6.1.7.3.1.9Manual saving monitor.216
4.3.3.6.1.7.3.1.10Independent action for inhibit.216
4.3.3.6.1.7.3.2Control path separation approach.216
4.3.3.6.1.7.3.2.1Inhibit monitor.216
4.3.3.6.1.7.3.2.2Separate control paths.216
4.3.3.6.1.7.3.2.3Unique commands for inhibits.217
4.3.3.6.1.7.3.2.4Independent parameters for SCPs.217
4.3.3.6.1.7.3.2.5Operator controllable parameter.217
4.3.3.6.1.7.3.2.6Independent action for inhibits.217
4.3.3.6.1.7.3.2.7Functionally different SCPs.217
4.3.3.6.1.7.3.2.8Software inhibit monitor.218
4.3.3.6.1.7.3.2.9System status monitor.218
4.3.3.6.1.8Hazardous materials.218
4.3.3.6.1.8.1Hazardous fluid containment failure tolerance.218
4.3.3.6.1.9Deleted.218
4.3.3.6.1.9.1Deleted.218
4.3.3.6.1.10Radiation.218
4.3.3.6.1.10.1Ionizing radiation.218
4.3.3.6.1.10.2Nonionizing radiation.218
4.3.3.6.1.11Optics and lasers.219
4.3.3.6.1.11.1Lasers.219
4.3.3.6.1.12Batteries.219
4.3.3.6.1.13Liquid propellant propulsion system.219
4.3.3.6.1.13.1Inadvertent firing of bi−propellant engines.219
4.3.3.6.1.13.2Reserved.220
4.3.3.6.1.13.3Absence of opening signal.220
4.3.3.6.1.13.4Isolation valves.220
4.3.3.6.1.13.5Opening the isolation valves.220
4.3.3.6.1.13.6Propellant overheating or freezing.221
4.3.3.6.1.13.7Propellant leakage.221
4.3.3.6.1.13.8Adiabatic or rapid compression detonation.222
4.3.3.6.1.13.9Hazardous venting.222
4.3.3.6.1.13.10Monitoring propulsion system status.222
4.3.3.6.1.14Subsequent induced loads.223
4.3.3.6.1.15Environmental capability.223
4.3.3.6.2Safety requirements during HTV attached phase.223
4.3.3.6.2.1Electrical safety.223
4.3.3.6.2.1.1Electrical power circuit overloads and short circuits.223
4.3.3.6.2.1.1.1Circuit over−load protection.223
4.3.3.6.2.1.1.2Protective device sizing.223
4.3.3.6.2.1.1.3Bent pin or conductive contamination.224
4.3.3.6.2.1.1.4Load short to chassis wire sizing.224
4.3.3.6.2.1.1.5Load short to chassis safety.224
4.3.3.6.2.1.1.6Wire short to chassis safety.225
4.3.3.6.3Safety requirements for pressurized section.225
4.3.3.6.3.1Fire protection.225
4.3.3.6.3.1.1Fire detection.225
4.3.3.6.3.1.2Crew notification.226
4.3.3.6.3.1.3Fire isolation.226
4.3.3.6.3.1.4Fire consequences.226
4.3.3.6.3.1.5Fire extinguishment.226
4.3.3.6.3.1.6Fire suppressant.227
4.3.3.6.3.1.7Fire suppressant application.227
4.3.3.6.3.1.8Portable Breathing Apparatus and Portable Fire Extinguisher
locations.227
4.3.3.6.3.1.9Module depressurization.227
4.3.3.6.3.1.10Confirmation.227
4.3.3.6.3.1.11Manual activation.228
4.3.3.6.3.2Pressure volume depressurization and depressurization tolerance.228
4.3.3.6.3.2.1Pressure differential tolerance.228
4.3.3.6.3.2.2Operation during pressure changes.228
4.3.3.6.3.3Emergency intravehicular activity egress.228
4.3.3.6.3.4Verifiable seal leakage paths.229
4.3.3.6.3.5Hatch opening.229
4.3.3.6.3.6Hazardous gas accumulation.229
4.3.3.6.3.6.1Accumulation prevention.230
4.3.3.6.3.6.2Detection and monitoring.230
4.3.3.6.3.7Equipment clearance for entrapment hazard.230
4.3.3.6.3.8Light fixture.230
4.3.3.6.3.9Crew protection from electrical shock.230
4.3.3.6.4Human engineering safety.230
4.3.3.6.4.1Internal volume touch temperature.231
4.3.3.6.4.2Internal corner and edge protection.231
4.3.3.6.4.2.1Equipment exposed to crew activity.231
4.3.3.6.4.2.2Equipment exposed only during planned maintenance activities.231
4.3.3.6.4.3External touch temperature.231
4.3.3.6.4.3.1Incidental contact.231
4.3.3.6.4.3.2Unlimited contact.231
4.3.3.6.4.4External corner and edge protection.232
4.3.3.6.4.4.1Sharp edges.232
4.3.3.6.4.4.2Thin materials.232
4.3.3.6.4.4.3Planned maintenance or storage.232
4.3.3.6.4.5Latches.232
4.3.3.6.4.6Screw and bolts.232
4.3.3.6.4.6.1Fasteners.233
4.3.3.6.4.7Safety−critical fastener.233
4.3.3.6.4.8Levers, cranks, hooks, and controls.233
4.3.3.6.4.9Burrs.233
4.3.3.6.4.10Holes.233
4.3.3.6.4.10.1Equipment located inside habitable volumes.234
4.3.3.6.4.10.2Equipment located outside habitable volumes.234
4.3.3.6.4.11Protrusions.234
4.3.3.6.4.12Pinch points.234
4.3.3.6.4.13Flexhoses.234
4.3.3.6.4.14Translation routes and established worksites.235
4.3.3.6.4.14.1EVA translation routes and established worksites.235
4.3.3.6.4.14.2Secondary translation routes and established worksites.235
4.3.3.6.4.14.3EVA crewmember contact isolation.235
4.3.3.6.4.15Moving or rotating equipment.235
4.3.3.6.5Rocket payload safety.236
4.3.3.6.6Range safety.236
4.3.3.6.7Reentry safety.236
4.3.3.7Human engineering.236
4.3.3.7.1Anthropometric requirements.236
4.3.3.7.1.1Strength requirements.236
4.3.3.7.1.1.1Normal operations.236
4.3.3.7.2HTV external hardware.236
4.3.3.7.2.1External task location requirements.237
4.3.3.7.2.2EVA crewmember field of view.237
4.3.3.7.2.3Working volume.237
4.3.3.7.2.4External limit loads.237
4.3.3.7.2.5Worksite crew−mobility aids.239

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