SSP_50333-RevH.docx

DOCX document 2 MB Posted

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

About this file

Written by GovTribe AI ·

This document is a request for proposal for the Human Space Flight Technical Integration Contract. Key details include that 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. Responsible sources may submit offers which will be considered by the agency. NASA Clause 1852.215-84 regarding the Center Ombudsman is applicable. The solicitation and related documents will be available on the specified websites. Prospective offerors shall notify the office of their intent to submit an offer and are responsible for monitoring the sites and downloading required documents. All contractual technical questions must be submitted in writing.

From the source

SSP 50333-RevH

View the file

Other files for this federal contract opportunity

Other files attached to Human Space Flight Technical Integration Contract (HSFTIC), newest first.
File Type Posted
HSFTIC_J-4_Applicable_and_Reference_Document_List.xlsx XLSX spreadsheet
SSP_50035_Revision_C_Retired.docx DOCX document
SSP_50314-Rev_C.docx DOCX document
SSP41142P2_RD_CD_012045_2.pdf PDF
SSP-50803.doc DOC document
PPD_524_RB_FINAL_MRICB_Charter.docx DOCX document
GPO_Website_Ref.pptx PPTX presentation
SSP_50481-RevC.docx DOCX document
42124_P2_RC_.pdf PDF
SSP_50094-RevB.pdf PDF
SSP_50659_Rev_E.xlsx XLSX spreadsheet
IMPR_Package_Mar_Apr_18.pptx PPTX presentation
SSP_41167-RevJ.docx DOCX document
SSP_50835_Rev_E.doc DOC document
42097P1_RD.pdf PDF
SSP42003_P2_RevC.pdf PDF
Applicable_3.zip ZIP file
MD_101_RA_FINAL.docx DOCX document
SSP_50477-RevC.pdf PDF
SSP_50670-Rev_A-DCN001-Collated_Master.doc DOC document
SSP_50781-RevA-DCN_003.docx DOCX document
PPD_517.pdf PDF
SSP_41002-RevR.docx DOCX document
SSP_50901.docx DOCX document
SSP_54059_54060-Baseline.docx DOCX document
SSP5003.PDF PDF
SSP30559RD-Errata.pdf PDF
SSP_41000-RevCJ.pdf PDF
42137P1_RC_CD_012230.pdf PDF
SSP_41163-Rev_L.docx DOCX document
9.0.zip ZIP file
SSP_42001-RevW.docx DOCX document
SSP_50875.docx DOCX document
SSP41017p2rJ.pdf PDF
41143Pt2RD.pdf PDF
SSP_50489-Rev_G.docx DOCX document
41015P2RH.pdf PDF
SSP_42121_Part_2.pdf PDF
SSP_50309_Part_1.pdf PDF
SSP_50477-RevC_Joint_Crew_Provisioning_Catalog.pdf PDF
JSC_Form_1240.pdf PDF
SSP_41160-RevH.docx DOCX document
Increment_Utilization_Accomplishment_Report_Blank_Book_RevB(March_2019).docx DOCX document
SSP_50102.pdf PDF
SSP_50146-RevB-SSCD_15566.pdf PDF
SSP_50034_Revision_D.DOC DOC document
SSP_50227-RevC.docx DOCX document
SSP_50621-RevF-DCN001-Collated_Master.pdf PDF
SSP41004_P2_RJ.pdf PDF
DRAFT_HSFTIC_Work_Load_Indicators.xlsx XLSX spreadsheet
Show all 50

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

On GovTribe

Work with this file on GovTribe

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

Text version

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

SSP 50333

Revision H Cupola Segment Specification

International Space Station Program

Revision H

31 January 2015

Type 1 – NASA Approved

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

REVISION AND HISTORY

REVISION AND HISTORY - Continued

REVISION AND HISTORY - Continued

REVISION AND HISTORY - Continued

REVISION AND HISTORY - Continued

REVISION AND HISTORY - Continued

REV.
DESCRIPTION
PUB. DATE
G
Revision G released in accordance with SSCN 012319
07-09-10

Revision G incorporates SSCNs 009111, 009415, 009840, 009951, 009993, 010119, 010592, 010615, 010726, 010782, 011191, 011243, 011645, 012037, 012044, and 012319.

The following SCN numbers have been canceled. The content of the SSCNs has been incorporated into Revision H.

SCN 148 (SSCN 011671) (Administrative cancel) Overcome by Events SCN 153 (SSCN 011768) (Administrative cancel) SCN 155 (SSCN 012902) (Administrative cancel) SCN 156 (SSCN 012906) (Administrative cancel) SCN 157 (SSCN 012597) (Administrative cancel)

H
Revision H (Reference per SSCD 014310, EFF. 02-23-15)
02-24-15

Revision H incorporates SSCNs 011671 (OBE), 011768, 012028, 012447, 012597, 012662, 012902, 012906, 013564, 013573, 013845, and 014310

PREFACE

CUPOLA Segment specification SSP 50333, Cupola Segment Specification shall be implemented on all new Program contractual and internal activity and shall be included in any existing contracts through contract changes. 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 the respective International Partners.

INTERNATIONAL SPACE STATION PROGRAM

CUPOLA Segment specification

CONCURRENCE

31 august 2014

TABLE OF CONTENTS

PARAGRAPHPAGE
1.0SCOPE1
1.1Identification.2
1.2Cupola Overview.3
2.0APPLICABLE DOCUMENTS4
2.1Government documents.5
2.1.1Specifications, standards, and handbooks.5
2.1.2Other Government documents, drawings, and publications.6
2.2Nongovernment documents.12
2.3Order of precedence.14
2.4Reference documents.15
3.0REQUIREMENTS16
3.1Cupola definition.17
3.1.1Cupola functional diagrams.17
3.1.2Interface definition.17
3.1.2.1External interfaces.17
3.1.2.1.1Interface with Node.17
3.1.2.1.2Interface with Space Lab Pallet.17
3.1.2.1.3Deleted.17
3.1.2.1.4Interface with Shuttle and Space Station Remote Manipulator Systems.17
3.1.2.1.5Interface with MSS Robotic Workstation portable console.17
3.1.2.1.6Interface with Station Management and Control.17
3.1.2.1.7Interface with crew.19
3.1.2.1.8Interface with Centerline Berthing Camera System.19
3.1.2.1.9Interface with internal task lighting.19
3.1.2.2Internal interfaces.19
3.1.2.2.1Interface with Audio Terminal Unit.19
3.1.2.2.2Interface with Utility Outlet Panels.19
3.1.3Major component list.19
3.1.4Government Furnished Material list.21
3.2Characteristics.22
3.2.1Performance characteristics.22
3.2.1.1Circulate atmosphere intermodule.22
3.2.1.2Circulate atmosphere intramodule.22
3.2.1.3Deleted.22
3.2.1.4Isolate for safing.22
3.2.1.5Determine safing procedures.22
3.2.1.6Demand safing.22
3.2.1.7Confirm successful safing.22
3.2.1.8Reattempt safing.22
3.2.1.9Provide visual data.22
3.2.1.10Annunciate alarms.23
3.2.1.11Validate commands.23
3.2.1.12Generate functional data.23
3.2.1.13Collect functional data.23
3.2.1.14Assess functional data.23
3.2.1.15Distribute power.23
3.2.1.15.1Power circuit conductor configurations.23
3.2.1.15.2Input power sources.23
3.2.1.15.3Utility outlets.24
3.2.1.15.4Isolation/ground referencing.24
3.2.1.15.5Launch-to-activation power.24
3.2.1.16Distribute thermal energy.24
3.2.1.17Support internal crew restraint and mobility.24
3.2.1.18Configure private point to point communication.24
3.2.1.19Configure public loop communication.25
3.2.1.20Configure public multiple loop listening communication.25
3.2.1.21Configure public broadcast and page communication.25
3.2.1.22Select push to talk.25
3.2.1.23Select voice activation.25
3.2.1.24Select voice activation and push to talk.25
3.2.1.25Transmit voice communications.25
3.2.1.26Annunciate hardwire.26
3.2.1.27Support internal equipment translation.26
3.2.1.28Support internal equipment removal and replacement.26
3.2.1.29Support internal equipment restraint.26
3.2.1.30Limit quasi-steady accelerations.26
3.2.1.31Limit vibratory accelerations.27
3.2.1.32Support direct viewing.28
3.2.1.33Support indirect viewing.28
3.2.1.34Accommodate Mobile Servicing System.29
3.2.2Physical characteristics.29
3.2.2.1Internal user payload volume.29
3.2.2.2External user payload accommodation.29
3.2.2.3External crew translation paths.29
3.2.2.4External crew worksites.29
3.2.2.5EVA handling aids.29
3.2.2.6Provide external stowage of tools and hardware.29
3.2.2.7Establish robotics translation corridor.29
3.2.2.8Envelope.30
3.2.2.8.1External envelope.30
3.2.2.8.2Internal envelope.30
3.2.2.8.3Jumper envelope.30
3.2.2.9Mass properties.31
3.2.2.10Crew access dimensions.31
3.2.2.11Node interface.31
3.2.2.12Space Lab Pallet interface.31
3.2.2.13Shuttle and Space Station Remote Manipulator System interface.31
3.2.2.14Mobile Servicing System Robotic Workstation portable console interface.31
3.2.2.15Station Management and Control interface.31
3.2.2.16Deleted.31
3.2.2.17Internal crew worksites.31
3.2.2.18Internal task lighting interface.31
3.2.2.19Distribute commands and data.32
3.2.2.19.1Provide MIL-STD-1553 data buses.32
3.2.2.19.2Sensor and Effector distribution.32
3.2.2.19.3RS-422A interface.32
3.2.3Reliability.32
3.2.3.1Failure tolerance.32
3.2.3.2Failure propagation.33
3.2.3.3Separation of redundant paths.33
3.2.3.4Redundancy status.33
3.2.4Maintainability.33
3.2.4.1Qualitative maintainability design.33
3.2.4.1.1Nonpressurized area equipment maintenance time.33
3.2.4.1.2Access item retention.34
3.2.4.1.3Installation/removal.34
3.2.4.1.3.1Equipment item interconnecting devices.34
3.2.4.1.3.2Incorrect equipment installation.34
3.2.4.1.3.3Lockwiring and staking.34
3.2.4.1.3.4Fluid capture and containment.34
3.2.4.1.4Standard EVA/EVR interfaces.34
3.2.4.2Cupola Mean Maintenance Crew Hours Per Year.34
3.2.4.3Failure Detection, Isolation, and Recovery (FDIR).34
3.2.4.3.1Manual FDIR.34
3.2.4.3.2Manual Control of FDIR.35
3.2.4.3.3Testing at operating location.35
3.2.4.3.4Ambiguity resolution.35
3.2.4.3.5Data availability.35
3.2.4.3.6False alarm mitigation.35
3.2.5Environmental conditions.35
3.2.5.1Thermal.38
3.2.5.1.1Transportation thermal environment.38
3.2.5.1.2Storage thermal environment.38
3.2.5.1.3Prelaunch thermal environment.38
3.2.5.1.4Ascent thermal environment.38
3.2.5.1.5On-orbit thermal environment.38
3.2.5.1.6Descent thermal environment.45
3.2.5.1.7Ferry-flight thermal environment.45
3.2.5.2Pressure.45
3.2.5.2.1Transportation pressure environment.45
3.2.5.2.2Storage pressure environment.45
3.2.5.2.3Prelaunch pressure environment.45
3.2.5.2.4Ascent pressure environment.45
3.2.5.2.5On-orbit pressure environment.45
3.2.5.2.6Descent pressure environment.45
3.2.5.2.7Ferry-flight pressure environment.46
3.2.5.3Humidity.46
3.2.5.3.1Transportation humidity environment.46
3.2.5.3.2Storage humidity environment.46
3.2.5.3.3Prelaunch humidity environment.46
3.2.5.3.4On-orbit humidity environment.46
3.2.5.3.5Descent humidity environment.46
3.2.5.3.6Ferry-flight humidity environment.46
3.2.5.4Atomic oxygen.47
3.2.5.5External contamination.47
3.2.5.5.1Transportation external contamination environment.47
3.2.5.5.2Storage external contamination environment.47
3.2.5.5.3Prelaunch external contamination environment.47
3.2.5.5.4On-orbit external contamination environment.47
3.2.5.6Electromagnetic.47
3.2.5.7Plasma.47
3.2.5.8Ionizing radiation.48
3.2.5.8.1Radiation dose environment.48
3.2.5.8.2Nominal single event effect environment.48
3.2.5.8.3Deleted.48
3.2.5.9Solar ultraviolet radiation.48
3.2.5.10Meteoroids and orbital debris.48
3.2.5.11Vibration.49
3.2.5.11.1Transportation vibration environment.49
3.2.5.11.2Ascent vibration environment.49
3.2.5.11.3General on-orbit vibration environment.50
3.2.5.11.3.1On-orbit shock environment.50
3.2.5.11.4Ferry-flight vibration environment.50
3.2.5.12Acoustic.50
3.2.5.12.1Transportation acoustic environment.50
3.2.5.12.2Ascent acoustic environment.51
3.2.5.13Acceleration.51
3.2.5.13.1Transportation acceleration environment.51
3.2.5.13.2Prelaunch acceleration environment.52
3.2.5.13.3Ascent acceleration environment.52
3.2.5.13.4On-orbit acceleration environment.53
3.2.5.13.5Descent acceleration environment.53
3.2.5.14Plume impingement pressures.53
3.2.6Transportability.53
3.3Design and construction.55
3.3.1Materials, processes, and parts.55
3.3.1.1Materials and processes.55
3.3.1.1.1Control of water soluble volatile organic compounds.55
3.3.1.2Electrical, Electronic, and Electromechanical parts.55
3.3.1.3Fluid Standards.55
3.3.1.4Seal life.55
3.3.2Electromagnetic radiation.55
3.3.2.1Electromagnetic compatibility.55
3.3.2.2Electromagnetic interference.55
3.3.2.3Electrical grounding.56
3.3.2.4Electrical bonding.56
3.3.2.5Cable and wire design.56
3.3.2.6Electrostatic discharge.56
3.3.2.7Corona.56
3.3.3Nameplates and product marking.56
3.3.4Workmanship.57
3.3.4.1Cleanliness.57
3.3.4.2Cleanliness of surfaces in contact with fluids.57
3.3.4.2.1Internal surfaces.57
3.3.4.2.2Packaging design.57
3.3.5Interchangeability.57
3.3.5.1On-orbit assembly interface durability.57
3.3.5.2Common mate/demate device.57
3.3.6Safety.57
3.3.6.1General.57
3.3.6.1.1Catastrophic hazards.57
3.3.6.1.2Critical hazards.58
3.3.6.1.3Design for minimum risk.58
3.3.6.1.4Control of hazardous functions.58
3.3.6.1.4.1Functions resulting in critical hazard.58
3.3.6.1.4.2Functions resulting in catastrophic hazard.58
3.3.6.1.5Deleted.58
3.3.6.1.6Subsequent induced loads.58
3.3.6.1.7Safety interlocks.59
3.3.6.1.8Environmental compatibility.59
3.3.6.2Hazard detection and safing.59
3.3.6.3Computer-based control of hazardous functions.59
3.3.6.4Hazardous materials.59
3.3.6.5Pyrotechnics.59
3.3.6.6Radiation.59
3.3.6.6.1Ionizing radiation.59
3.3.6.6.2Nonionizing radiation.59
3.3.6.7Optics and lasers.59
3.3.6.8Electrical safety.60
3.3.6.8.1Electrical power circuit overloads.60
3.3.6.8.1.1Circuit overload protection.60
3.3.6.8.1.2Protective device sizing.60
3.3.6.8.1.3Bent pin or conductive contamination.60
3.3.6.8.2Crew protection for electrical shock.60
3.3.6.8.3Reapplication of power.60
3.3.6.8.4Batteries.60
3.3.6.9Cryogenics.60
3.3.6.10Fire protection.60
3.3.6.11Constraints.61
3.3.6.11.1Reserved.61
3.3.6.11.2Pressurized volume depressurization and repressurization tolerance.61
3.3.6.11.2.1Pressure differential tolerance.61
3.3.6.11.3Emergency egress.61
3.3.6.11.4Reserved.61
3.3.6.11.5Component hazardous energy provision.61
3.3.6.11.6Reserved.61
3.3.6.11.7Pressure integrity.61
3.3.6.11.8Reserved.61
3.3.6.11.9Reserved.61
3.3.6.11.10Reserved.61
3.3.6.11.11Hazardous gas accumulation.61
3.3.6.11.11.1Accumulation prevention.61
3.3.6.11.11.2Detection, monitoring, and control.61
3.3.6.11.12Equipment clearance for entrapment hazard.62
3.3.6.11.13Light fixture.62
3.3.6.12Human engineering safety.62
3.3.6.12.1Internal volume touch temperature.62
3.3.6.12.1.1Continuous contact - high temperature.62
3.3.6.12.1.2Incidental or momentary contact - high temperature.62
3.3.6.12.1.3Internal volume low touch temperature.62
3.3.6.12.2External touch temperature.62
3.3.6.12.2.1Incidental contact.62
3.3.6.12.2.2Unlimited contact.63
3.3.6.12.3External corner and edge protection.63
3.3.6.12.3.1Sharp edges.63
3.3.6.12.3.2Thin materials.64
3.3.6.12.3.3Planned maintenance or storage.64
3.3.6.12.4Internal corner and edge protection.64
3.3.6.12.4.1Equipment exposed to crew activity.64
3.3.6.12.4.2Equipment exposed only during planned maintenance activities.64
3.3.6.12.5Contingency repressurization.64
3.3.6.12.6Holes.64
3.3.6.12.6.1Equipment located inside habitable volumes.64
3.3.6.12.6.2Equipment located outside habitable volumes.64
3.3.6.12.7Protrusions.65
3.3.6.12.8Pinch points.65
3.3.6.12.9Emergency ingress.65
3.3.6.12.10Flexhoses.65
3.3.6.12.11Translation routes and established worksites.65
3.3.6.12.12Latches.66
3.3.6.12.13Screws and bolts.66
3.3.6.12.14Moving or rotating equipment.66
3.3.6.12.15Reserved.66
3.3.6.12.16Safety critical fasteners.66
3.3.6.12.17Levers, cranks, hooks, and controls.66
3.3.6.12.18Burrs.66
3.3.6.13Launch vehicle interfaces and services.67
3.3.6.13.1Safe without Space Shuttle Program services.67
3.3.6.13.2Critical Orbiter services.67
3.3.6.13.3Inadvertent deployment, separation, and jettison functions.67
3.3.6.13.4Planned deployment/extension functions.67
3.3.6.13.5Contingency return and rapid safing.67
3.3.6.13.6Flammable atmosphere.67
3.3.6.13.6.1Normal functions.67
3.3.6.13.6.2Electrical ignition sources.67
3.3.6.13.6.3Surface temperatures.67
3.3.6.13.6.4Conductive surfaces.67
3.3.6.13.7Allowable Radio Frequency radiation levels.67
3.3.6.13.8Lightning protection.67
3.3.6.13.9Orbiter vent/dump provisions.68
3.3.6.13.10Sealed compartments.68
3.3.6.14Ground interfaces and services - Space Shuttle launch.68
3.3.6.14.1Moving parts.68
3.3.6.14.2Equipment requiring adjustment.68
3.3.6.14.3Ignition of adjacent materials.68
3.3.6.14.4Accidental contact with electrical equipment.68
3.3.6.15Ground handling and processing.68
3.3.7Human engineering.68
3.3.7.1Internal hardware.68
3.3.7.1.1Internal anthropometric requirements.68
3.3.7.1.2Strength requirements.69
3.3.7.1.3Maintenance.69
3.3.7.1.4Emergency controls.69
3.3.7.1.5IVA crew load requirements.69
3.3.7.1.5.1IVA translation path obstructions.69
3.3.7.1.5.2IVA closure and cover design requirements.69
3.3.7.1.6Housekeeping.69
3.3.7.1.7Controls and displays.69
3.3.7.1.8Interior colors.69
3.3.7.2External hardware.69
3.3.7.2.1External task location requirements.69
3.3.7.2.2EVA crewmember field of view.71
3.3.7.2.3Working volume.71
3.3.7.2.4External limit loads.72
3.3.7.3Gloved operation.73
3.3.7.3.1Clearance.73
3.3.7.4Location coding.74
3.3.8Nuclear control.74
3.3.9Cupola security.74
3.3.10Environmental constraints.74
3.3.10.1Acoustic emission limits.74
3.3.10.2External contamination releases.74
3.3.10.3Ionizing radiation emission limits.74
3.3.11Design for remote controlled external operations.74
3.3.11.1Equipment requiring Shuttle robotic support.74
3.3.11.2External equipment requiring robotic hand-off.75
3.3.11.3External equipment requiring SSRMS support.75
3.3.11.3.1Equipment requiring SSRMS support using an FRGF.78
3.3.12Design requirements.79
3.3.12.1Structural design requirements.79
3.3.12.1.1Strength, stiffness, and resonant frequency.79
3.3.12.1.2Thermal effects.79
3.3.12.1.3Damage tolerance.79
3.3.12.1.3.1M/OD damage tolerance.79
3.3.12.1.3.2IVA induced loads.79
3.3.12.1.4Fracture control.79
3.3.12.1.5Glass, window, and ceramic design criteria.80
3.3.12.1.5.1Window pane stresses.80
3.3.12.1.5.1.1Factor of safety for glass panes.80
3.3.12.1.5.1.2Lift-off, ascent, descent and landing loading condition.80
3.3.12.1.5.1.3On-orbit loading condition.80
3.3.12.1.5.1.4Glass pane margin of safety.81
3.3.12.1.5.1.5Stresses for life verification.81
3.3.12.1.5.1.6Life verification.81
3.3.12.1.6Design requirements for Orbiter payloads.81
3.3.12.1.7Pressurized storage containers.81
3.3.12.1.8Structural degradation from material erosion.81
3.3.12.1.9Design loads.82
3.3.12.1.10Factor(s) of safety.82
3.3.12.1.11Margins of safety.82
3.3.12.1.12General design requirements.82
3.3.12.1.12.1Bolts.82
3.3.12.1.12.2Design service life.82
3.3.12.1.13Structural materials criteria.83
3.3.12.1.13.1Materials properties.83
3.3.12.1.14Secondary structure accommodations for human interface.83
3.3.12.1.15Nonstandard fasteners.83
3.3.12.1.16M/OD structural protection.83
3.3.12.1.16.1Probability of no penetration.83
3.3.12.1.16.2M/OD augmentation.83
3.3.12.1.17EVA on-orbit induced loads.83
3.3.12.2Fluid handling requirements.85
3.3.12.2.1Interface hardware.85
3.3.12.2.2Fluid leakage.86
3.3.12.2.2.1Heat transfer fluid leakage.86
3.3.12.3Fasteners.86
3.3.12.4Internal atmosphere.86
3.3.12.4.1Maximum design pressure.86
3.3.12.4.2Atmospheric leakage.86
3.3.12.5Connectors.86
3.3.12.6Fluid connectors.86
3.3.12.6.1Fluid system connectors.86
3.3.12.6.2Connectors used for hazardous fluids.87
3.3.12.6.3Connectors used for contamination sensitive components.87
3.3.12.7Flexible lines and bellows design.87
3.3.12.8Operational lifetime.87
3.3.12.8.1Longevity.87
3.3.12.9Power resource.87
3.3.12.10Housekeeping power allocations.87
3.3.12.10.1Manage random cyclic loads.88
3.3.12.11Alignment devices.88
3.3.12.12Handles.88
3.3.12.13Cable management.89
3.3.12.14Electrical Power Consuming Equipment design.89
3.3.13EVA equipment handling capabilities.89
3.3.14Preclude condensation.89
3.3.15MIL-STD-1553 data bus constraints.90
3.3.15.1Space Station Quality components.90
3.3.15.1.1Bus coupler type.90
3.3.15.2Bus stub length.90
3.3.15.3Bus coupling.91
3.3.15.4Cupola not-to-exceed bus length.91
3.3.16Cupola not-to exceed Sensor and Effector wire harness length.92
3.4Computer resource requirements.93
3.5Logistics.94
3.5.1Maintenance.94
3.5.1.1On-orbit maintenance.94
3.5.1.1.1Corrective maintenance.94
3.5.1.1.2In situ maintenance.94
3.5.1.1.3ORU intermediate maintenance.94
3.5.1.1.4Preventive maintenance.94
3.5.1.2On-orbit maintenance backup.94
3.5.1.3Access for on-orbit maintenance.94
3.5.1.3.1Access for on-orbit inspection.94
3.5.1.3.2Visual access.95
3.5.1.3.3EVA access to fasteners.95
3.5.1.3.4Physical access.95
3.5.1.3.5Removal, replacement, and modularity design.95
3.5.1.4Standard on-orbit tools.95
3.5.1.5Standard on-orbit diagnostic equipment.97
3.5.1.6Ground maintenance.98
3.5.2Supply.99
3.5.2.1Multiple launch capability.99
3.5.2.2Additional launches.99
3.5.3Facilities and facility equipment.99
3.6Personnel and training.100
3.7Configuration and operations constraints.101
3.7.1Seat track interface.101
3.7.2Internal handrails.101
3.7.3Audio Terminal Unit interface.101
3.7.4Utility Outlet Panel interface.101
3.7.5Robotic Workstation harness bracket.101
3.7.6Intermodule ventilation temperature controller location.101
3.7.7Cupola Foot Restraint Device.101
3.7.8Operational constraints.101
3.7.9CBCS target accommodation.105
3.7.9.1CBCS physical characteristics.105
3.7.9.2Target accommodation location and orientation.105
3.7.9.3On-orbit stowage.106
3.7.9.4Bonding.106
3.7.9.5Environments.106
3.8Precedence.107
4.0QUALITY ASSURANCE PROVISIONS108
4.1General.109
4.1.1Responsibility for verifications.109
4.2Cupola quality conformance inspections.111
4.3Quality conformance verifications.112
4.3.1General.112
4.3.2Characteristics.112
4.3.2.1Performance characteristics.112
4.3.2.1.1Circulate atmosphere intermodule.112
4.3.2.1.2Circulate atmosphere intramodule.112
4.3.2.1.3Deleted.112
4.3.2.1.4Isolate for safing.112
4.3.2.1.5Determine safing procedures.112
4.3.2.1.6Demand safing.112
4.3.2.1.7Confirm successful safing.112
4.3.2.1.8Reattempt safing.112
4.3.2.1.9Provide visual data.113
4.3.2.1.10Annunciate alarms.113
4.3.2.1.11Validate commands.113
4.3.2.1.12Generate functional data.113
4.3.2.1.13Collect functional data.113
4.3.2.1.14Assess functional data.113
4.3.2.1.15Distribute power.113
4.3.2.1.15.1Power circuit conductor configurations.114
4.3.2.1.15.2Input power sources.114
4.3.2.1.15.3Utility outlets.114
4.3.2.1.15.4Isolation/ground referencing.114
4.3.2.1.15.5Launch-to-activation power.115
4.3.2.1.16Distribute thermal energy.115
4.3.2.1.17Support internal crew restraint and mobility.115
4.3.2.1.18Configure private point to point communication.115
4.3.2.1.19Configure public loop communication.115
4.3.2.1.20Configure public multiple loop listening communication.115
4.3.2.1.21Configure public broadcast and page communication.116
4.3.2.1.22Select push to talk.116
4.3.2.1.23Select voice activation.116
4.3.2.1.24Select voice activation and push to talk.116
4.3.2.1.25Transmit voice communications.116
4.3.2.1.26Annunciate hardwire.116
4.3.2.1.27Support internal equipment translation.117
4.3.2.1.28Support internal equipment removal and replacement.117
4.3.2.1.29Support internal equipment restraint.117
4.3.2.1.30Limit quasi-steady accelerations.117
4.3.2.1.31Limit vibratory accelerations.117
4.3.2.1.32Support direct viewing.118
4.3.2.1.33Support indirect viewing.118
4.3.2.1.34Accommodate Mobile Servicing System.118
4.3.2.2Physical characteristics.118
4.3.2.2.1Internal user payload volume.118
4.3.2.2.2External user payload accommodation.118
4.3.2.2.3External crew translation paths.118
4.3.2.2.4External crew worksites.118
4.3.2.2.5EVA handling aids.119
4.3.2.2.6Provide external stowage of tools and hardware.119
4.3.2.2.7Establish robotics translation corridor.119
4.3.2.2.8Envelope.119
4.3.2.2.8.1External envelope.119
4.3.2.2.8.2Internal envelope.119
4.3.2.2.8.3Jumper envelope.119
4.3.2.2.9Mass properties.119
4.3.2.2.10Crew access dimensions.120
4.3.2.2.11Node interface.120
4.3.2.2.12Space Lab Pallet interface.120
4.3.2.2.13Shuttle and Space Station Remote Manipulator System interface.120
4.3.2.2.14Mobile Servicing System Robotic Workstation portable console interface.120
4.3.2.2.15Station Management and Control interface.120
4.3.2.2.16Deleted.120
4.3.2.2.17Internal crew worksite.120
4.3.2.2.18Internal task lighting interface.121
4.3.2.2.19Distribute commands and data.121
4.3.2.2.19.1Provide MIL-STD-1553 data buses.121
4.3.2.2.19.2Sensor and Effector distribution.122
4.3.2.2.19.3RS-422A interface.122
4.3.2.3Reliability.122
4.3.2.3.1Failure tolerance.122
4.3.2.3.2Failure propagation.122
4.3.2.3.3Separation of redundant paths.122
4.3.2.3.4Redundancy status.122
4.3.2.4Maintainability.122
4.3.2.4.1Qualitative maintainability design.122
4.3.2.4.1.1Nonpressurized area equipment maintenance time.122
4.3.2.4.1.2Access item retention.123
4.3.2.4.1.3Installation/removal.123
4.3.2.4.1.3.1Equipment item interconnecting devices.123
4.3.2.4.1.3.2Incorrect equipment installation.123
4.3.2.4.1.3.3Lockwiring and staking.123
4.3.2.4.1.3.4Fluid capture and containment.123
4.3.2.4.1.4Standard EVA/EVR interfaces.123
4.3.2.4.2Cupola Mean Maintenance Crew Hours Per Year.124
4.3.2.4.3Failure Detection, Isolation, and Recovery.124
4.3.2.4.3.1Manual FDIR.124
4.3.2.4.3.2Manual Control of FDIR.124
4.3.2.4.3.3Testing at operating location.124
4.3.2.4.3.4Ambiguity resolution.124
4.3.2.4.3.5Data availability.125
4.3.2.4.3.6False alarm mitigation.125
4.3.2.5Environmental conditions.125
4.3.2.5.1Thermal.125
4.3.2.5.1.1Transportation thermal environment.125
4.3.2.5.1.2Storage thermal environment.125
4.3.2.5.1.3Prelaunch thermal environment.125
4.3.2.5.1.4Ascent thermal environment.126
4.3.2.5.1.5On-orbit thermal environment.126
4.3.2.5.1.6Descent thermal environment.126
4.3.2.5.1.7Ferry-flight thermal environment.126
4.3.2.5.2Pressure.127
4.3.2.5.2.1Transportation pressure environment.127
4.3.2.5.2.2Storage pressure environment.127
4.3.2.5.2.3Prelaunch pressure environment.127
4.3.2.5.2.4Ascent pressure environment.127
4.3.2.5.2.5On-orbit pressure environment.127
4.3.2.5.2.6Descent pressure environment.128
4.3.2.5.2.7Ferry-flight pressure environment.128
4.3.2.5.3Humidity.128
4.3.2.5.3.1Transportation humidity environment.128
4.3.2.5.3.2Storage humidity environment.128
4.3.2.5.3.3Prelaunch humidity environment.128
4.3.2.5.3.4On-orbit humidity environment.128
4.3.2.5.3.5Descent humidity environment.128
4.3.2.5.3.6Ferry-flight humidity environment.129
4.3.2.5.4Atomic oxygen.129
4.3.2.5.5External contamination.129
4.3.2.5.5.1Transportation external contamination environment.129
4.3.2.5.5.2Storage external contamination environment.129
4.3.2.5.5.3Prelaunch external contamination environment.129
4.3.2.5.5.4On-orbit external contamination environment.129
4.3.2.5.6Electromagnetic.129
4.3.2.5.7Plasma.129
4.3.2.5.8Ionizing radiation.130
4.3.2.5.8.1Radiation dose environment.130
4.3.2.5.8.2Nominal single event effect environment.130
4.3.2.5.8.3Deleted.130
4.3.2.5.9Solar ultraviolet radiation.130
4.3.2.5.10Meteoroids and orbital debris.130
4.3.2.5.11Vibration.130
4.3.2.5.11.1Transportation vibration environment.130
4.3.2.5.11.2Ascent vibration environment.130
4.3.2.5.11.3General on-orbit vibration environment.131
4.3.2.5.11.3.1On orbit shock environment.131
4.3.2.5.11.4Ferry-flight vibration environment.131
4.3.2.5.12Acoustic.131
4.3.2.5.12.1Transportation acoustic environment.131
4.3.2.5.12.2Ascent acoustic environment.131
4.3.2.5.13Acceleration.131
4.3.2.5.13.1Transportation acceleration environment.131
4.3.2.5.13.2Prelaunch acceleration environment.132
4.3.2.5.13.3Ascent acceleration environment.132
4.3.2.5.13.4On-orbit acceleration environment.132
4.3.2.5.13.5Descent acceleration environment.132
4.3.2.5.14Plume impingement pressures.132
4.3.2.6Transportability.132
4.3.3Design and construction.133
4.3.3.1Materials, processes, and parts.133
4.3.3.1.1Materials and processes.133
4.3.3.1.1.1Control of water soluble volatile organic compounds.133
4.3.3.1.2Electrical, Electronic, and Electromechanical parts.133
4.3.3.1.3Fluid standards.133
4.3.3.1.4Seal life.133
4.3.3.2Electromagnetic radiation.134
4.3.3.2.1Electromagnetic compatibility.134
4.3.3.2.2Electromagnetic interference.134
4.3.3.2.3Electrical grounding.134
4.3.3.2.4Electrical bonding.134
4.3.3.2.5Cable and wire design.134
4.3.3.2.6Electrostatic discharge.135
4.3.3.2.7Corona.135
4.3.3.3Nameplates and product marking.135
4.3.3.4Workmanship.135
4.3.3.4.1Cleanliness.135
4.3.3.4.2Cleanliness of surfaces in contact with fluids.135
4.3.3.4.2.1Internal surfaces.135
4.3.3.4.2.2Packaging designs.136
4.3.3.5Interchangeability.136
4.3.3.5.1On-orbit assembly interface durability.136
4.3.3.5.2Common mate/demate device136
4.3.3.6Safety.136
4.3.3.6.1General.136
4.3.3.6.1.1Catastrophic hazards.136
4.3.3.6.1.2Critical hazards.136
4.3.3.6.1.3Design for minimum risk.136
4.3.3.6.1.4Control of hazardous functions.137
4.3.3.6.1.4.1Functions resulting in critical hazard.137
4.3.3.6.1.4.2Function resulting in catastrophic hazard.137
4.3.3.6.1.5Deleted.137
4.3.3.6.1.6Subsequent induced loads.137
4.3.3.6.1.7Safety interlocks.137
4.3.3.6.1.8Environmental compatibility.138
4.3.3.6.2Hazard detection and safing.138
4.3.3.6.3Computer-based control of hazardous functions.138
4.3.3.6.4Hazardous materials.138
4.3.3.6.5Pyrotechnics.138
4.3.3.6.6Radiation.138
4.3.3.6.6.1Ionizing radiation138
4.3.3.6.6.2Nonionizing radiation.138
4.3.3.6.7Optics and lasers.138
4.3.3.6.8Electrical safety.139
4.3.3.6.8.1Electrical power circuit overloads.139
4.3.3.6.8.1.1Circuit overload protection.139
4.3.3.6.8.1.2Protective device sizing.139
4.3.3.6.8.1.3Bent pin or conductive contamination.139
4.3.3.6.8.2Crew protection for electrical shock.139
4.3.3.6.8.3Reapplication of power.139
4.3.3.6.8.4Batteries.139
4.3.3.6.9Cryogenics.139
4.3.3.6.10Fire protection.139
4.3.3.6.11Constraints.140
4.3.3.6.11.1Reserved.140
4.3.3.6.11.2Pressurized volume depressurization and repressurization tolerance.140
4.3.3.6.11.2.1Pressure differential tolerance.140
4.3.3.6.11.3Emergency egress.140
4.3.3.6.11.4Reserved.140
4.3.3.6.11.5Component hazardous energy provision.140
4.3.3.6.11.6Reserved.140
4.3.3.6.11.7Pressure integrity.140
4.3.3.6.11.8Reserved.141
4.3.3.6.11.9Reserved.141
4.3.3.6.11.10Reserved.141
4.3.3.6.11.11Hazardous gas accumulation.141
4.3.3.6.11.11.1Accumulation prevention.141
4.3.3.6.11.11.2Detection, monitoring, and control.141
4.3.3.6.11.12Equipment clearance for entrapment hazard.141
4.3.3.6.11.13Light fixture.141
4.3.3.6.12Human engineering safety.141
4.3.3.6.12.1Internal volume touch temperature.141
4.3.3.6.12.1.1Continuous contact - high temperature.141
4.3.3.6.12.1.2Incidental or momentary contact - high temperature.141
4.3.3.6.12.1.3Internal volume low touch temperature.142
4.3.3.6.12.2External touch temperature.142
4.3.3.6.12.2.1Incidental contact.142
4.3.3.6.12.2.2Unlimited contact.142
4.3.3.6.12.3External corner and edge protection.143
4.3.3.6.12.3.1Sharp edges.143
4.3.3.6.12.3.2Thin materials.143
4.3.3.6.12.3.3Planned maintenance or storage.143
4.3.3.6.12.4Internal corner and edge protection.144
4.3.3.6.12.4.1Equipment exposed to crew activity.144
4.3.3.6.12.4.2Equipment exposed only during planned maintenance activities.144
4.3.3.6.12.5Contingency repressurization.144
4.3.3.6.12.6Holes.144
4.3.3.6.12.6.1Equipment located inside habitable volumes.144
4.3.3.6.12.6.2Equipment located outside habitable volumes.144
4.3.3.6.12.7Protrusions.144
4.3.3.6.12.8Pinch points.145
4.3.3.6.12.9Emergency ingress.145
4.3.3.6.12.10Flexhoses.145
4.3.3.6.12.11Translation routes and established worksites.145
4.3.3.6.12.12Latches.145
4.3.3.6.12.13Screws and bolts.146
4.3.3.6.12.14Moving or rotating equipment.146
4.3.3.6.12.15Reserved.146
4.3.3.6.12.16Safety critical fasteners.146
4.3.3.6.12.17Levers, cranks, hooks, and controls.146
4.3.3.6.12.18Burrs.146
4.3.3.6.13Launch vehicle interfaces and services.147
4.3.3.6.13.1Safe without Space Shuttle Program services.147
4.3.3.6.13.2Critical Orbiter services.147
4.3.3.6.13.3Inadvertent deployment, separation, and jettison functions.147
4.3.3.6.13.4Planned deployment/extension functions.147
4.3.3.6.13.5Contingency return and rapid safing.147
4.3.3.6.13.6Flammable atmosphere.147
4.3.3.6.13.6.1Normal functions.147
4.3.3.6.13.6.2Electrical ignition sources.147
4.3.3.6.13.6.3Surface temperatures.147
4.3.3.6.13.6.4Conductive surfaces.148
4.3.3.6.13.7Allowable RF radiation levels.148
4.3.3.6.13.8Lightning protection.148
4.3.3.6.13.9Orbiter vent/dump provisions.148
4.3.3.6.13.10Sealed compartments.148
4.3.3.6.14Ground interfaces and services - Space Shuttle launch.148
4.3.3.6.14.1Moving parts.148
4.3.3.6.14.2Equipment requiring adjustment.148
4.3.3.6.14.3Ignition of adjacent materials.148
4.3.3.6.14.4Accidental contact with electrical equipment.149
4.3.3.6.15Ground handling and processing.149
4.3.3.7Human engineering.149
4.3.3.7.1Internal hardware.149
4.3.3.7.1.1Internal anthropometric requirements.149
4.3.3.7.1.2Strength requirements.149
4.3.3.7.1.3Maintenance.149
4.3.3.7.1.4Emergency controls.149
4.3.3.7.1.5IVA crew load requirements.149
4.3.3.7.1.5.1IVA translation path obstructions.149
4.3.3.7.1.5.2IVA closure and cover design requirements.150
4.3.3.7.1.6Housekeeping.150
4.3.3.7.1.7Controls and displays.150
4.3.3.7.1.8Interior colors.150
4.3.3.7.2External hardware.150
4.3.3.7.2.1External task location requirements.150
4.3.3.7.2.2EVA crewmember field of view.150
4.3.3.7.2.3Working volume.150
4.3.3.7.2.4External limit loads.151
4.3.3.7.3Gloved operation.151
4.3.3.7.3.1Clearance.151
4.3.3.7.3.2Location coding.151
4.3.3.8Nuclear control.151
4.3.3.9Cupola security.151
4.3.3.10Environmental constraints.151
4.3.3.10.1Acoustic emission limits.151
4.3.3.10.2External contamination releases.152
4.3.3.10.3Ionizing radiation emission limits.152
4.3.3.11Design for remote controlled external operations.152
4.3.3.11.1Equipment requiring Shuttle robotic support.152
4.3.3.11.2External equipment requiring robotic hand-off.153
4.3.3.11.3External equipment requiring SSRMS support.153
4.3.3.11.3.1Equipment requiring SSRMS support using and FRGF.154
4.3.3.12Design requirements.154
4.3.3.12.1Structural design requirements.154
4.3.3.12.1.1Strength, stiffness, and resonant frequency.154
4.3.3.12.1.2Thermal effects.154
4.3.3.12.1.3Damage tolerance.155
4.3.3.12.1.3.1M/OD damage tolerance.155
4.3.3.12.1.3.2IVA induced loads.155
4.3.3.12.1.4Fracture control.155
4.3.3.12.1.5Glass, window, and ceramic design criteria.155
4.3.3.12.1.5.1Window pane stresses.156
4.3.3.12.1.5.1.1Factor of safety for glass panes.156
4.3.3.12.1.5.1.2Lift-off, ascent, descent and landing loading condition.156
4.3.3.12.1.5.1.3On-orbit loading condition.156
4.3.3.12.1.5.1.4Glass panes margin of safety.156
4.3.3.12.1.5.1.5Stresses for life verification.156
4.3.3.12.1.5.1.6Life verification.157
4.3.3.12.1.6Design requirements for Orbiter payloads.157
4.3.3.12.1.7Pressurized storage containers.157
4.3.3.12.1.8Structural degradation from material erosion.157
4.3.3.12.1.9Design loads.157
4.3.3.12.1.10Factor(s) of safety.157
4.3.3.12.1.11Margins of safety.158
4.3.3.12.1.12General design requirements.158
4.3.3.12.1.12.1Bolts.158
4.3.3.12.1.12.2Design service life.158
4.3.3.12.1.13Structural materials criteria.158
4.3.3.12.1.13.1Materials properties.159
4.3.3.12.1.14Secondary structure accommodations for human interface.159
4.3.3.12.1.15Nonstandard fasteners.159
4.3.3.12.1.16M/OD structural protection.159
4.3.3.12.1.16.1Probability of no penetration.159
4.3.3.12.1.16.2M/OD augmentation.159
4.3.3.12.1.17EVA on-orbit induced loads.159
4.3.3.12.2Fluid handling requirements.159
4.3.3.12.2.1Interface hardware.159
4.3.3.12.2.2Fluid leakage.160
4.3.3.12.2.2.1Heat transport fluid leakage.160
4.3.3.12.3Fasteners.160
4.3.3.12.4Internal atmosphere.160
4.3.3.12.4.1Maximum design pressure.160
4.3.3.12.4.2Atmospheric leakage.160
4.3.3.12.5Connectors.160
4.3.3.12.6Fluid connectors.161
4.3.3.12.6.1Fluid system connectors.161
4.3.3.12.6.2Connectors used for hazardous fluids.161
4.3.3.12.6.3Connectors used for contamination sensitive components.161
4.3.3.12.7Flexible lines and bellows design.161
4.3.3.12.8Operational lifetime.161
4.3.3.12.8.1Longevity.161
4.3.3.12.9Power resource.162
4.3.3.12.9.1Housekeeping power allocations.162
4.3.3.12.9.2Manage random cyclic loads.163
4.3.3.12.10Alignment devices.163
4.3.3.12.11Handles.163
4.3.3.12.12Cable management.164
4.3.3.12.13Electrical Power Consuming Equipment design.164
4.3.3.13EVA equipment handling capabilities.164
4.3.3.14Preclude condensation.164
4.3.3.15MIL-STD-1553 data bus constraints.164
4.3.3.15.1Space Station Quality components.164
4.3.3.15.1.1Bus coupler type.164
4.3.3.15.2Bus stub length.165
4.3.3.15.3Bus coupling.165
4.3.3.15.4Cupola not-to-exceed bus length.165
4.3.3.16Cupola not-to-exceed Sensor and Effector wire harness length.165
4.3.4Computer resource requirements.165
4.3.5Logistics.165
4.3.5.1Maintenance.165
4.3.5.1.1On-orbit maintenance.165
4.3.5.1.1.1Corrective maintenance.165
4.3.5.1.1.2In situ maintenance.166
4.3.5.1.1.3ORU intermediate maintenance.166
4.3.5.1.1.4Preventive maintenance.166
4.3.5.1.2On-orbit maintenance backup.166
4.3.5.1.3Access for on-orbit maintenance.166
4.3.5.1.3.1Access for on-orbit inspection.167
4.3.5.1.3.2Visual access.167
4.3.5.1.3.3EVA access to fasteners.167
4.3.5.1.3.4Physical access.167
4.3.5.1.3.5Removal, replacement, and modularity design.167
4.3.5.1.4Standard on-orbit tools.167
4.3.5.1.5Standard on-orbit diagnostic equipment.168
4.3.5.1.6Ground maintenance.168
4.3.5.2Supply.168
4.3.5.2.1Multiple launch capability.168
4.3.5.2.2Additional launches.168
4.3.5.3Facilities and facility equipment.168
4.3.6Personnel and training.168
4.3.7Configuration and operations constraints.168
4.3.7.1Seat track interface.168
4.3.7.2Internal handrails.168
4.3.7.3Audio Terminal Unit interface.169
4.3.7.4Utility Outlet Panel interface.169
4.3.7.5Robotic Workstation harness bracket.169
4.3.7.6Intermodule temperature controller location.169
4.3.7.7Crew Foot Restraint Device.169
4.3.7.8Operational constraints.169
4.3.7.9CBCS target accommodation.169
4.3.7.9.1CBCS physical characteristics.170
4.3.7.9.2Target accommodations, location, and orientation.170
4.3.7.9.3On-orbit stowage.170
4.3.7.9.4Bonding.170
4.3.7.9.5Environments.170
5.0PREPARATION FOR DELIVERY172
5.1Preservation.173
5.1.1General preservation requirements.173
5.1.2Detailed preservation requirements.173
5.2Packing.174
5.2.1General packing requirements.174
5.2.2Detailed packing requirements.174
5.3Marking and labeling.175
5.3.1General marking and labeling requirements.175
5.3.1.1Unit packages, intermediate packages, and exterior shipping containers.175
5.3.1.2Hazardous materials.175
5.3.2Detailed marking requirements.175
6.0NOTES176
6.1Definitions.177
6.2Abbreviations and acronyms.189

APPENDIX

AAPPROVED LIMITED APPLICABILITY REQUIREMENTS193
BAPPROVED REQUIREMENT EXCEPTIONS194

TABLE

I.Cupola input power sources23
II.Transmission characteristics28
III.Deleted32
IV.Cupola failure tolerance requirements32
V.Flight Attitudes for Vehicle Design36
VI.Hot and cold natural thermal environments38
VII.Extreme hot and cold natural thermal environments (1)42
VIII.Parameters for M/OD environments definition48
IX.Common carrier transport random vibration environments49
X.On-orbit vibration environment50
XI.Orbiter cargo bay ferry-flight vibration environment50
XII.Ground transportation and ferry-flight acoustic environment50
XIII.Transportation and handling limit load factors52
XIV.Launch and landing accelerations53
XV.Heat transfer rates63
XVI.Designated EVA interfaces63
XVII.Control for exposed risks to EVA crew65
XVIII.Miscellaneous crew actuation load limits72
XIX.Mobile Servicing Center robotic payload properties76
XX.Berthing contact conditions76
XXI.SSRMS backdrive threshold77
XXII.Force/moment accommodation78
XXIII.SRMS and SSRMS placement accuracy78
XXIV.Cupola stiffness and resonant frequency requirements79
XXV.Structural design loads82
XXVI.EVA induced loads84
XXVII.Constraints for single EVA crewmember transport of objects89
XXVIII.Cupola not-to-exceed bus length92
XXIX.Standard IVA tool list95
XXX.Diagnostic equipment list98
XXXI.Cupola configuration162
XXXII.Cupola GFE power162
XXXIII.EPCE Equipment with Applicable Power Quality Specification
SSP 30482 Vol. 1200

FIGURE

1.Cupola on-orbit functionality and interfaces18
2.Seat track interface20
3.Combined cold thermal environmental profile.28
4.Cupola external envelope30
5.Design cold thermal environmental profile40
6.Design hot thermal environmental profile41
7.Extreme cold thermal environment profile43
8.Extreme hot thermal environment profile44
9.Crewmember optimum work envelope70
10.Crewmember field of view71
11.Working volume for manipulative EVA tasks72
12.Work envelope for gloved hand73
13.Typical bus91
14.Cupola FRGF locations103
15.Side shutter FRGF release mechanism encroachment envelope198

SSP 50333

Revision H xiv

SCOPE

This specification establishes the performance, design, development, and verification requirements for the International Space Station (ISS) Cupola. This specification has been developed using SSP 41171, Revision A as a guide for a Type B1 Prime Item Development Specification. Sections 1 and 3.1 are for informational purposes only and are not binding between National Aeronautics and Space Administration (NASA) and European Space Agency (ESA). Documents listed in section 2 are applicable to NASA and ESA to the extent that they are referenced in sections 3 and 4.

Section 3.2.1 performance requirements are derived from the functional decomposition, a hierarchical breakdown of capabilities and subtiered functions which the Space Station will perform. Requirements in section 3.2.1 define the performance level of the Cupola and are based on the third level of the functional decomposition. Requirements in section 3.7 define the the agreements between ESA and NASA for design implementation.

Requirements in sections 3.2.2 through 3.7 are constraints with which the Cupola must comply. Section 3.2.1 performance requirements herein are applicable during nominal operation and do not account for maintenance or contingency events.

The Cupola is supplied by ESA with Audio Terminal Unit (ATU) and two Utility Outlet Panels provided and installed on-orbit by NASA. ESA has the responsibility for the Cupola integration, configuration control, and functionality, including functionality required for on-orbit installation of the functional units, to the extent specified in this specification and NASA-ESA implementation arrangement. NASA has an overall responsibility for station-level integration of the Cupola.

For the purposes of this specification Portable Computer System (PCS), Robotic Workstation (RWS) and portable light are external to the Cupola. They are provided and installed on orbit by NASA.

Identification.

This specification is for the Cupola, Configuration Item 684EA2A Cupola Overview.

The purpose of the Cupola is to provide an observation and worksite for the crewmembers.

APPLICABLE DOCUMENTS

The following specifications, standards, and handbooks of the exact issue shown form a part of this specification to the extent specified herein. Documents or portions thereof cited within referenced Part 1 Interface Control Documents (ICDs) are considered part of this specification.

Government documents.

Specifications, standards, and handbooks.

SPECIFICATIONS

FEDERAL

None

MILITARY

None

STANDARDS

FEDERAL

CFR, Title 49 November 1, 1994 CFR Department of Transportation, Hazardous Materials Registration Board

MILITARY

MIL-STD-129

Rev. M July 15, 1993 Marking for Shipping and Storage

MIL-STD-130

Rev. G October 11, 1988 Identification Marking of U.S. Military Property

MIL-STD-1522

Rev. A, CN-03 September 4, 1992 Safe Design and Operation of Pressurized Missile and Space Systems, Standard Requirements

MIL-STD-1553

Rev. B, CN-02 September 8, 1986 Digital Time Division Command/Response Multiplex Data Bus

MIL-STD-2073-01

Rev. B June 21, 1991 Packaging Requirements

MIL-STD-2073-02

Rev. B June 21, 1991 Packaging Requirements Codes

HANDBOOKS

FEDERAL

None

MILITARY

MIL-HDBK-5

Rev. G November 1, 1994 Metallic Materials and Elements for Aerospace Vehicle Structures

MIL-HDBK-17, Part II Rev. B, CN-01 February 29, 1988 Plastics for Aerospace Vehicles Transparent Glazing Materials, Part II

(Unless otherwise indicated, copies of U.S. federal and military specifications, standards, and handbooks are available from the Standardization Documents Order Desk, Building 4D, 700 Robbins Avenue, Philadelphia, PA 19111-5094.)

Other Government documents, drawings, and publications.

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

OTHER GOVERNMENT DOCUMENTS

NASA

JSC 26895

Rev. Baseline 28 October 1997 Guidelines for Assessing the Toxic Hazard of Spacecraft Chemicals and Test Materials

JSC 63828

Rev. C October 2010 Biosafety Review Board Operations and Requirements Document

JSC 64825

Rev. Baseline 9 July 09 Guidelines for Assessing the Flammability Hazard of Spacecraft Chemicals and Test Materials

K-STSM-14.2.1

Rev. C July 1, 1995 KSC Payload Facility Contamination Control Requirements/Plan

NASA SP-8007

August 1, 1968 Buckling of Thin-Walled Circular Cylinders

NHB 6000.1

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

NSTS 07700 Volume XIV Rev. K March 23, 1993 Space Shuttle System Payload Accommodations

NSTS 07700 Volume XIV Appendix 7 Rev. J, Change 1 June 14, 1989 System Description and Design Data - Extravehicular Activities

NSTS 07700 Volume XIV Appendix 8 Rev. J, Change 1 June 14, 1989 System Description and Design Data - Payload Deployment and Retrieval System

NSTS 08307

Rev. Basic October 13, 1989 Criteria for Preloaded Bolts

NSTS 14046

Rev. E March, 2000 Payload Verification Requirements

NSTS 21000-IDD-ISS

Rev. A, plus Change Packages 9 through 49 February 18, 1998 International Space Station Interface Definition Document (except paragraphs 3.1.3.3, 3.1.3.4, 3.3.1.1.2.2, 3.3.4.1, 3.3.5.1.1, 4.1.1.6.2, 4.3.1, 6.1.5.2, 6.4.1, 6.4.3, 8.1.1.1, 8.1.1.2, 8.1.4.2.1.1, 10.7.3.2.2.2, 11.2, 14, 14.3.4, 14.5.1, 14.5.2, S.6.3.2.1.1, S.6.3.2.1.2, S.6.4, Figures 13.2.1.3-1, 14.4.6-1, S.4.3.1-1, Tables 4.1.1.3.2.1-1, 4.1.1.5-1, 6.4.3-1, 8.1.1.1-2, 8.1.1.2-2, and S6.3.2-1)

NSTS-21000-IDD-MDK

Rev. B, CN 001, 002, 017, 018 January 6, 1997 Middeck Interface Definition Document

NSTS 37329

Rev. B, Change 3 October 18, 2004 Structural Integration Analyses Responsibility Definition for Space Shuttle Vehicle and Cargo Element Developers

SLP-2104

Rev. 3 Date July 8, 1993 Spacelab Payload Accommodation Handbook

SN-C-0005

Rev. C February 15, 1989 National Space Transportation System Contamination Control Requirements for the Space Shuttle Program

SSP 30219

Rev. H June 1, 2005 Space Station Reference Coordinate Systems

SSP 30233

Rev. F plus SSCN 5144, 7292, 9111 March 6, 1998 Space Station Requirements for Materials and Processes

SSP 30237

Rev. G, DCN 036 May 3, 2002 Space Station Electromagnetic Emission and Susceptibility Requirements

SSP 30238

Rev. E July 31, 2002 Space Station Electromagnetic Techniques

SSP 30240

Rev. D July 31, 2002 Space Station Grounding Requirements

SSP 30242

Rev. G, DCN 008 July 25, 2003 Space Station Cable/Wire Design and Control Requirements for Electromagnetic Compatibility

SSP 30243

Rev. G, DCN 013, 014 July 31, 2002 Space Station Systems Requirements for Electromagnetic Compatibility

SSP 30245

Rev. F, DCN 027, 029 May 3, 2002 Space Station Electrical Bonding Requirements

SSP 30256:001

Rev. J October 17, 2012 Space Station Program Extravehicular Activity (EVA) Standard Interface Control Document

SSP 30257:002

Current Issue Space Station Program Utility Outlet Panel Interface Control Document

SSP 30260:019

Current Issue Space Station Program Audio Terminal Unit Standard Interface Control Document

SSP 30312

Rev. H, DCN 001, 002, SSCN (7485) November 22, 1999 Electrical, Electronic, and Electromechanical (EEE) and Mechanical Parts Management and Implementation Plan for Space Station Program Document

SSP 30420

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

SSP 30423

Rev. H January 15, 2000 Space Station Approved Electrical, Electronic, and Electromechanical Parts List

SSP 30425

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

SSP 30426

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

SSP 30482 Volume 1 Rev. C, DCN 003 July 7, 1997 Electrical Power Specifications and Standards Volume 1: EPS Electrical Performance Specifications

SSP 30482 Volume 2 Rev. A, DCN 001, 02, 03, 04, 05, 06, plus SSCN 2191, 2130, 2135, 2915 January 1994 Electrical Power Specifications and Standards Volume 2: Consumer Constraints

SSP 30512

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

SSP 30558

Rev. B, DCN 002 (256) June 30, 1994 Fracture Control Requirements for Space Station

SSP 30559

Rev. C, DCN 009, 010, 011, 012, SSCN 9111 September 29, 2000 Structural Design and Verification Requirements

SSP 30560

Rev. A May 5, 2003 Glass, Window, and Ceramic Structural Design and Verification Requirements

SSP 30573

Rev. E, SSCN 256 December 2, 2009 Space Station Fluid Procurement and Use Control Specification

SSP 30575

Rev. E April 2007 Space Station Interior & Exterior Operational Location Coding System

SSP 30599

Rev. E June, 2008 Safety Review Process

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

SSP 41142, Part 1 Rev. F October 19, 2009 Node Elements to Cupola Element Interface Control Document, Part 1

SSP 41172

Rev. N, DCNs 200, 206, 219 March 29, 2002 Qualification and Acceptance Environmental Test Requirements

SSP 41175-01

Rev. M September 30, 2010 Software Interface Control Document Station Management and Control to International Space Station Book 01, Hardware Architecture

SSP 41175-03

Rev. L September 1, 2004 Software Interface Control Document Payload Executive Processor and Station Management and Control to International Space Station Book 3, Portable Computer System Interface

SSP 42003, Part 1 Rev. H, SSCN 9993 March 6, 2007 Space Station Manned Base (SSMB) to Mobile Servicing System (MSS) Interface Control Document Part I

SSP 42004, Part 1 Rev. K June 3, 2013 Mobile Servicing System (MSS) to User (Generic) Interface Control Document Part 1

SSP 50004

Rev. Initial, SCN 001, 002, SSCN (3214), (8563) February 1, 1994 Ground Support Equipment Design Requirements

SSP 50005

Rev. E, DCN TBD (SSCN 010331 and SSCN 012447) June 30, 2006 International Space Station Flight Crew Integration Standard (NASA-STD-3000/T)

SSP 50007

Rev. D November, 2005 Space Station Inventory Management System Label Specification

SSP 50008

Rev. C February 7, 2001 International Space Station Interior Color Scheme

SSP 50014

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

SSP 50023

Initial April 15, 1994 Thermal Control Plan

SSP 50036

Rev. C April 15, 2003 Microgravity Control Plan

SSP 50098, Part 1 Rev. B, IRNs 50098-01-0600, SSCNs 3219, 9744, 9055, 10726 April 5, 2006 Robotic Workstation to Space Station Manned Base (SSMB) Interface Control Document, Part 1

SSP 50110

Rev. K January 2010 Multi Increment Manifest Document

SSP 50214

Rev. A July 4, 1997 Space Station Freedom Hardware/Software Usage for International Space Station

SSP 50496

Rev. Basic September. 26, 2000 Cupola Element to Manual Berthing Mechanism for Space Lab Logistics Pallet Interface Control Document

SSQ 21676

Rev. C May 16, 1997 Coupler Data Bus, MIL-1553B, Space Quality General Specification

ICD-B-21479-Cupola

CN01

September 27, 2002 2JA SLP Cargo Element Integration Control Document

DRAWINGS

20M02540 Rev. D February 28, 1990 Assessment of Flexible Lines for Flow Induced Vibrations

Nongovernment documents.

In the event of a conflict between the documents referenced herein and the contents of this specification, the contents of this specification shall be…

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

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