SSP_50869-Rev_A.docx
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- Human Space Flight Technical Integration Contract (HSFTIC) Federal contract opportunity
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This document provides details for a solicitation for the Human Space Flight Technical Integration Contract (HSFTIC). Key information includes that NASA/JSC plans to issue a Request for Proposal (RFP) with an anticipated release date of November 1, 2019 and offer due date of December 11, 2019. The NAICS code is 541715 with a size standard of 1,250 employees. The procurement is a total small business set-aside. The RFP and any associated documents will be available at the listed websites. Prospective offerors must notify the agency of their intent to submit an offer and are responsible for downloading solicitation documents. All contractual technical questions must be submitted in writing. The Center Ombudsman information is also provided.
SSP 50869-Rev A
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Text version
Prime Item Development Specification for the Permanent Multipurpose Module (PMM)
International Space Station Program
Revision A
September 2010
National Aeronautics and Space Administration International Space Station Program Johnson Space Center Houston, Texas Contract No. NNJ09GA18B
SSP 50869
Revision A
REVISION AND HISTORY PAGE
| REV. |
| DESCRIPTION |
| PUB. DATE |
| - |
| Initial Release (Reference per SSCD 011801R2, EFF. 08/09/10) |
| 08-16-10 |
| A |
| Revision A (Reference per SSCD 012421, EFF. 09/22/10) |
| 10-05-10 |
SSP 50869
Revision A
PREFACE
Prime Item Development Specification for the Permanent Multipurpose Module (PMM) This document is developed and maintained by the NASA PMM Project Office. This document is under the control of the Space Station Control Board (SSCB).
The initial baseline release of this document is under the control of the SSCB. The SSCB delegates control and approval authority for future updates and/or revisions to the Multilateral Vehicle Control Board (MVCB).
INTERNATIONAL SPACE STATION PROGRAM
for the Permanent Multipurpose Module (PMM)
CONCURRENCE
august 2010 for the Permanent Multipurpose Module (PMM)
CONCURRENCE
august 2010
Prime item development specification for the permanent Multipurpose module (pMm)
LIST OF CHANGES
All changes to paragraphs, tables, and figures in this document are shown below:
Board Name
Entry Date
Change
Paragraph(s)
August 2010
Baseline
All
October 2010
Revision A
All v
TABLE OF CONTENTS
| PARAGRAPH | PAGE | |
| 1.0 | SCOPE | 1-1 |
| 1.1 | Identification | 1-1 |
| 1.2 | System overview | 1-1 |
| 2.0 | documents | 2-1 |
| 2.1 | applicable documents | 2-1 |
| 2.1.1 | specifications, standards, and handbooks | 2-1 |
| 2.1.2 | Other government documents, drawings, and publications | 2-2 |
| 2.2 | Meet or exceed | 2-9 |
| 3.0 | system requirements | 3-1 |
| 3.1 | system definition | 3-1 |
| 3.1.1 | System functional description | 3-1 |
| 3.1.2 | Mission Scenario | 3-1 |
| 3.1.2.1 | Ground Operations Scenario | 3-1 |
| 3.1.2.2 | Launch and On-Orbit Scenario | 3-1 |
| 3.1.2.3 | Contingency Scenarios | 3-2 |
| 3.1.3 | Integrated system functional diagram | 3-3 |
| 3.1.4 | Interface requirements | 3-4 |
| 3.1.4.1 | External interfaces | 3-4 |
| 3.1.4.1.1 | Orbiter external interface description | 3-4 |
| 3.1.4.1.2 | Launch/landing site support facilities external interface description | 3-4 |
| 3.1.4.1.3 | United States On-orbit Segment (USOS) external interface description | 3-4 |
| 3.1.4.1.3.1 | Portable Fire Extinguisher (PFE) external interface description | 3-4 |
| 3.1.4.1.3.2 | Portable Breathing Apparatus (PBA) external interface description | 3-4 |
| 3.1.4.1.3.3 | IntraVehicular Activity restraints and mobility aids interfaces | 3-5 |
| 3.1.4.1.3.4 | EXtraVehicular Activity translation aids and attachments Interfaces | 3-5 |
| 3.1.4.1.3.5 | CAUTION AND WARNING (C&W) DEVICE INTERFACES | 3-5 |
| 3.1.4.1.3.6 | PMM pcbm TO Node 1 acbm Thermal Conduction interface | 3-5 |
| 3.1.4.1.4 | Space Station Remote Manipulator System (SSRMS) external interface description | 3-11 |
| 3.1.4.1.5 | Rack external interface | 3-11 |
| 3.1.4.1.6 | Refrigerator/Freezer Rack external interface description | 3-11 |
| 3.1.4.1.7 | Re-supply stowage platform external interface | 3-11 |
| 3.1.4.1.8 | PMM to Ground Support Equipment interface description | 3-11 |
| 3.1.4.2 | Internal interfaces | 3-11 |
| 3.1.4.2.1 | PCBM interface | 3-11 |
| 3.1.4.2.2 | Hatch interface | 3-11 |
| 3.2 | Characteristics | 3-11 |
| 3.2.1 | Performance characteristics | 3-11 |
| 3.2.1.1 | State: Perform mission on-orbit | 3-11 |
| 3.2.1.1.1 | Capability | 3-12 |
| 3.2.1.1.1.1 | Relieve overpressure | 3-12 |
| 3.2.1.1.1.2 | Equalize pressure | 3-12 |
| 3.2.1.1.1.3 | Circulate atmosphere | 3-12 |
| 3.2.1.1.1.4 | Control internal lighting | 3-12 |
| 3.2.1.1.1.5 | Illuminate internal areas | 3-12 |
| 3.2.1.1.1.6 | Isolate to recovery level | 3-13 |
| 3.2.1.1.1.7 | Recover lost function | 3-13 |
| 3.2.1.1.1.8 | Isolate for safing | 3-13 |
| 3.2.1.1.1.9 | Safe | 3-13 |
| 3.2.1.1.1.9.1 | Re-attempt safing | 3-13 |
| 3.2.1.1.1.9.2 | Demand safing | 3-13 |
| 3.2.1.1.1.9.3 | Confirm successful safing | 3-13 |
| 3.2.1.1.1.10 | Maintain station mode | 3-13 |
| 3.2.1.1.1.11 | Transition station modes | 3-14 |
| 3.2.1.1.1.12 | Generate functional data | 3-14 |
| 3.2.1.1.1.13 | Assess functional status data | 3-14 |
| 3.2.1.1.1.14 | Acquire hazardous condition data | 3-14 |
| 3.2.1.1.1.15 | Identify hazardous condition | 3-14 |
| 3.2.1.1.1.16 | Respond to fire | 3-14 |
| 3.2.1.1.1.17 | Respond to hazardous atmosphere | 3-15 |
| 3.2.1.1.1.18 | Deleted | 3-15 |
| 3.2.1.1.1.19 | Deleted | 3-15 |
| 3.2.1.1.1.20 | Distribute power | 3-15 |
| 3.2.1.1.1.21 | Collect thermal energy | 3-19 |
| 3.2.1.1.1.22 | Distribute thermal energy | 3-19 |
| 3.2.1.1.1.23 | Distribute time | 3-19 |
| 3.2.1.1.1.24 | Support internal crew restraint and mobility | 3-19 |
| 3.2.1.1.1.25 | Provide direct visual access | 3-19 |
| 3.2.1.1.1.26 | Deleted | 3-19 |
| 3.2.1.1.1.27 | Provide data for downlink | 3-19 |
| 3.2.1.1.1.28 | Deleted | 3-19 |
| 3.2.1.1.1.29 | Deleted | 3-19 |
| 3.2.1.1.1.30 | Manage time | 3-19 |
| 3.2.1.1.1.30.1 | Maintain time | 3-19 |
| 3.2.1.1.1.30.2 | Control Time | 3-20 |
| 3.2.1.1.1.31 | Provide time interface | 3-20 |
| 3.2.1.1.1.31.1 | Receive time | 3-20 |
| 3.2.1.1.1.31.2 | Provide time services | 3-20 |
| 3.2.1.1.1.31.3 | Distribute time | 3-20 |
| 3.2.1.1.1.32 | Atmosphere sampling | 3-20 |
| 3.2.1.1.1.33 | Respond to rapid decompression | 3-20 |
| 3.2.1.1.1.34 | Annunciate alarms | 3-20 |
| 3.2.1.1.1.35 | Micro-gravity disturbances | 3-20 |
| 3.2.1.1.1.35.1 | Limit quasi−steady accelerations | 3-20 |
| 3.2.1.1.1.35.2 | Limit vibratory accelerations | 3-20 |
| 3.2.1.1.1.36 | Limit angular momentum disturbances | 3-21 |
| 3.2.1.1.1.36.1 | Limit disturbance induced ISS attitude rate Limit disturbance | 3-21 |
| 3.2.1.1.1.36.2 | Limit disturbance induced CMG MOMENTUM | 3-22 |
| 3.2.1.2 | DELETED | 3-23 |
| 3.2.1.3 | State: Support mission | 3-23 |
| 3.2.1.3.1 | Mode: Ground processing | 3-23 |
| 3.2.1.3.1.1 | Load and unload cargo items | 3-23 |
| 3.2.1.3.1.2 | Support system check-out and monitoring. | 3-23 |
| 3.2.1.3.2 | Mode: Space transport | 3-24 |
| 3.2.1.3.2.1 | Transport internal cargo | 3-24 |
| 3.2.2 | Physical characteristics | 3-24 |
| 3.2.2.1 | Tare weight | 3-24 |
| 3.2.2.2 | Launch envelope | 3-25 |
| 3.2.2.2.1 | External diameter | 3-25 |
| 3.2.2.2.2 | Axial length | 3-25 |
| 3.2.2.3 | Distribute commands and data | 3-25 |
| 3.2.2.4 | External NASA/ASI insignia emblem | 3-25 |
| 3.2.2.4.1 | External NASA insignia emblem | 3-25 |
| 3.2.2.4.2 | External ASI insignia emblem | 3-25 |
| 3.2.3 | Reliability | 3-25 |
| 3.2.3.1 | Flight system reliability | 3-25 |
| 3.2.3.1.1 | Failure tolerance | 3-25 |
| 3.2.3.1.2 | Failure propagation | 3-25 |
| 3.2.3.1.3 | Separation of redundant paths | 3-25 |
| 3.2.3.1.4 | Redundancy | 3-26 |
| 3.2.4 | Maintainability | 3-26 |
| 3.2.4.1 | Flight system maintainability | 3-26 |
| 3.2.4.1.1 | Qualitative maintainability design | 3-26 |
| 3.2.4.1.1.1 | Equipment item interconnecting devices | 3-26 |
| 3.2.4.1.1.2 | Incorrect equipment installation | 3-26 |
| 3.2.4.1.1.3 | Lockwiring and staking | 3-26 |
| 3.2.4.1.1.4 | PMM Mean Maintenance Crew Hours Per Year | 3-26 |
| 3.2.4.1.1.5 | Access item retention | 3-26 |
| 3.2.4.1.2 | Failure Detection, Isolation, and Recovery (FDIR) | 3-26 |
| 3.2.4.1.2.1 | Automatic hazard and hazardous condition detection | 3-26 |
| 3.2.4.1.2.2 | Automatic anomaly detection | 3-26 |
| 3.2.4.1.2.3 | Manual FDIR | 3-27 |
| 3.2.4.1.2.4 | Manual control of FDIR | 3-28 |
| 3.2.4.1.2.5 | Deleted | 3-28 |
| 3.2.4.1.2.6 | Automatic safing verification | 3-28 |
| 3.2.4.1.2.7 | Testing at operation location | 3-28 |
| 3.2.4.1.2.8 | Ambiguity resolution | 3-28 |
| 3.2.4.1.2.9 | Data availability | 3-28 |
| 3.2.4.1.2.10 | False alarm mitigation | 3-28 |
| 3.2.5 | Availability | 3-28 |
| 3.2.6 | Environmental conditions | 3-28 |
| 3.2.6.1 | Flight system environmental conditions | 3-28 |
| 3.2.6.1.1 | On-orbit environmental conditions | 3-28 |
| 3.2.6.1.1.1 | Thermal environment | 3-29 |
| 3.2.6.1.1.2 | Neutral atmosphere | 3-31 |
| 3.2.6.1.1.3 | External contamination | 3-31 |
| 3.2.6.1.1.4 | Electric and geomagnetic fields | 3-31 |
| 3.2.6.1.1.5 | Plasma | 3-32 |
| 3.2.6.1.1.6 | Ionizing radiation | 3-32 |
| 3.2.6.1.1.7 | Solar ultraviolet radiation | 3-32 |
| 3.2.6.1.1.8 | Micro Meteoroids and Orbital Debris (MMOD) | 3-33 |
| 3.2.6.1.1.9 | Deleted | 3-33 |
| 3.2.6.1.1.10 | Plume impingement pressures | 3-33 |
| 3.2.6.1.1.11 | Atomic oxygen | 3-33 |
| 3.2.6.1.2 | ascent/descent thermal environment | 3-33 |
| 3.2.7 | Transportability | 3-33 |
| 3.2.7.1 | PMM transportability | 3-33 |
| 3.2.8 | PLANAR REFLECTOR INTERFACE REQUIREMENTS | 3-34 |
| 3.2.8.1 | PLAnar reflector location | 3-34 |
| 3.2.8.2 | PLAnar reflector structural interface | 3-34 |
| 3.2.8.2.1 | Alignment tolerance | 3-34 |
| 3.2.8.2.2 | planar reflector flatness | 3-34 |
| 3.2.8.2.3 | planar reflector Structural Interface Temperature limits | 3-34 |
| 3.2.8.2.4 | planar reflector vibration limits | 3-34 |
| 3.3 | Design and construction | 3-35 |
| 3.3.1 | Materials, processes, and parts | 3-35 |
| 3.3.1.1 | PMM materials, processes, and parts | 3-35 |
| 3.3.1.1.1 | Materials and processes | 3-35 |
| 3.3.1.1.2 | Electrical, Electronic, and Electromechanical (EEE) parts | 3-35 |
| 3.3.1.1.2.1 | EEE parts selection | 3-35 |
| 3.3.1.1.3 | Static age life | 3-36 |
| 3.3.2 | Electromagnetic Radiation (EMR) | 3-36 |
| 3.3.2.1 | PMM Electromagnetic Compatibility (EMC) requirements | 3-36 |
| 3.3.2.1.1 | Grounding | 3-36 |
| 3.3.2.1.2 | Cabling and wire design | 3-36 |
| 3.3.2.1.3 | Electrical bonding | 3-36 |
| 3.3.2.1.4 | Power conducted disturbance | 3-36 |
| 3.3.2.1.5 | Equipment Electromagnetic Interference (EMI) requirements | 3-37 |
| 3.3.2.1.6 | Electromagnetic interference safety margins for critical circuits | 3-37 |
| 3.3.2.1.7 | Launch element transportation, storage, and launch environment | 3-37 |
| 3.3.2.1.8 | Static electricity | 3-37 |
| 3.3.2.1.9 | Corona | 3-37 |
| 3.3.2.1.10 | Selection and use of equipment | 3-37 |
| 3.3.3 | Nameplates and product markings | 3-37 |
| 3.3.3.1 | PMM nameplates and product markings | 3-37 |
| 3.3.3.1.1 | Labeling | 3-38 |
| 3.3.4 | Workmanship | 3-38 |
| 3.3.4.1 | PMM workmanship | 3-38 |
| 3.3.4.2 | PMM cleanliness | 3-38 |
| 3.3.5 | Interchangeability | 3-38 |
| 3.3.6 | Safety | 3-38 |
| 3.3.6.1 | General | 3-38 |
| 3.3.6.1.1 | Catastrophic hazards | 3-38 |
| 3.3.6.1.1.1 | Deleted | 3-39 |
| 3.3.6.1.1.2 | Deleted | 3-39 |
| 3.3.6.1.2 | Critical hazards | 3-39 |
| 3.3.6.1.3 | Design for minimum risk | 3-39 |
| 3.3.6.1.4 | Control of functions resulting in critical hazards | 3-39 |
| 3.3.6.1.4.1 | Inadvertent operation resulting in critical hazards | 3-39 |
| 3.3.6.1.4.2 | Loss of function resulting in critical hazards | 3-39 |
| 3.3.6.1.5 | Control of functions resulting in catastrophic hazards | 3-39 |
| 3.3.6.1.5.1 | Inadvertent operation resulting in catastrophic hazards | 3-39 |
| 3.3.6.1.5.2 | Loss of function resulting in catastrophic hazards | 3-40 |
| 3.3.6.1.6 | Subsequent induced loads | 3-40 |
| 3.3.6.1.6.1 | Deleted | 3-40 |
| 3.3.6.1.7 | Safety interlocks | 3-40 |
| 3.3.6.1.8 | Environmental compatibility | 3-40 |
| 3.3.6.2 | Hazard detection and safing | 3-40 |
| 3.3.6.2.1 | Reserved | 3-40 |
| 3.3.6.2.2 | Monitors | 3-40 |
| 3.3.6.2.2.1 | Status information | 3-40 |
| 3.3.6.2.2.2 | Hazardous function operation prevention | 3-41 |
| 3.3.6.2.2.3 | Loss of input or failure | 3-41 |
| 3.3.6.2.2.4 | Launch site availability | 3-41 |
| 3.3.6.2.2.5 | Flight crew availability | 3-41 |
| 3.3.6.2.3 | Near-real-time monitoring | 3-41 |
| 3.3.6.2.4 | Real-time monitoring | 3-41 |
| 3.3.6.2.4.1 | Maintain status of hazard controls | 3-41 |
| 3.3.6.2.4.2 | Crew response time and safing procedures | 3-41 |
| 3.3.6.2.4.3 | Deleted | 3-41 |
| 3.3.6.3 | Command and computer control of hazardous functions | 3-41 |
| 3.3.6.3.1 | Computer control of hazardous functions | 3-41 |
| 3.3.6.4 | Hazardous materials | 3-47 |
| 3.3.6.4.1 | Hazardous fluid containment | 3-47 |
| 3.3.6.5 | Pyrotechnics | 3-47 |
| 3.3.6.6 | Radiation | 3-47 |
| 3.3.6.6.1 | Non-ionizing radiation | 3-47 |
| 3.3.6.6.2 | Ionizing radiation crew limits | 3-47 |
| 3.3.6.6.3 | PMM transmitters | 3-47 |
| 3.3.6.7 | optics and lasers | 3-47 |
| 3.3.6.8 | electical safety | 3-47 |
| 3.3.6.8.1 | electrical power circuit overloads | 3-47 |
| 3.3.6.8.1.1 | circuit overload protection | 3-47 |
| 3.3.6.8.1.2 | protective device sizing | 3-47 |
| 3.3.6.8.1.3 | bent pin or conductive contamination | 3-47 |
| 3.3.6.8.2 | crew protection for electrical shock | 3-47 |
| 3.3.6.8.3 | reapplication of power | 3-48 |
| 3.3.6.8.4 | batteries | 3-48 |
| 3.3.6.9 | cryogenics | 3-48 |
| 3.3.6.10 | fire protection | 3-48 |
| 3.3.6.10.1 | reserved | 3-48 |
| 3.3.6.10.2 | isolation | 3-48 |
| 3.3.6.10.3 | suppression | 3-48 |
| 3.3.6.10.4 | suppressant | 3-48 |
| 3.3.6.10.5 | restorable suppression | 3-48 |
| 3.3.6.10.6 | power removal | 3-48 |
| 3.3.6.10.7 | portable equipment | 3-48 |
| 3.3.6.10.7.1 | set co-location | 3-48 |
| 3.3.6.10.8 | confirmation | 3-50 |
| 3.3.6.11 | constraints | 3-50 |
| 3.3.6.11.1 | reserved | 3-50 |
| 3.3.6.11.2 | pressurized volume depressurization and re-pressurization tolerance | 3-50 |
| 3.3.6.11.2.1 | pressure differential tolerance | 3-50 |
| 3.3.6.11.2.2 | operation during pressure changes | 3-50 |
| 3.3.6.11.3 | emergency egress | 3-50 |
| 3.3.6.11.4 | reserved | 3-51 |
| 3.3.6.11.5 | reserved | 3-51 |
| 3.3.6.11.6 | component hazardous energy provision | 3-51 |
| 3.3.6.11.7 | hatch opening | 3-51 |
| 3.3.6.11.8 | reserved | 3-51 |
| 3.3.6.11.9 | reserved | 3-51 |
| 3.3.6.11.10 | reserved | 3-51 |
| 3.3.6.11.11 | reserved | 3-51 |
| 3.3.6.11.12 | hazardous Gas accumulation | 3-51 |
| 3.3.6.11.12.1 | accumulation prevention | 3-51 |
| 3.3.6.11.13 | equipment clearance for entrapment hazard | 3-51 |
| 3.3.6.11.14 | light fixture | 3-51 |
| 3.3.6.12 | human engineering safety | 3-51 |
| 3.3.6.12.1 | internal volume touch temperature | 3-51 |
| 3.3.6.12.1.1 | continuous contact - high temperature | 3-51 |
| 3.3.6.12.1.2 | incidental or momentary contact - high temperature | 3-51 |
| 3.3.6.12.1.3 | internal volume low touch temperature | 3-52 |
| 3.3.6.12.2 | external touch temperature | 3-52 |
| 3.3.6.12.2.1 | incidental contact | 3-52 |
| 3.3.6.12.2.2 | unlimited contacT | 3-52 |
| 3.3.6.12.3 | external corner and edge protection | 3-52 |
| 3.3.6.12.3.1 | sharp edges | 3-52 |
| 3.3.6.12.3.2 | thin materials | 3-53 |
| 3.3.6.12.4 | internal corner and edge protection | 3-53 |
| 3.3.6.12.4.1 | equipment exposed to crew activity | 3-53 |
| 3.3.6.12.5 | reserved | 3-53 |
| 3.3.6.12.6 | latches | 3-53 |
| 3.3.6.12.7 | screws and bolts | 3-53 |
| 3.3.6.12.8 | safety critical fasteners | 3-53 |
| 3.3.6.12.9 | levers, cranks, hooks and controls | 3-53 |
| 3.3.6.12.10 | burrs | 3-53 |
| 3.3.6.12.11 | holes | 3-54 |
| 3.3.6.12.11.1 | equipment located inside habitable volumes | 3-54 |
| 3.3.6.12.11.2 | equipment located outside habitable volumes | 3-54 |
| 3.3.6.12.12 | protrusions | 3-54 |
| 3.3.6.12.13 | pinch points | 3-54 |
| 3.3.6.12.14 | reserved | 3-54 |
| 3.3.6.12.15 | reserved | 3-54 |
| 3.3.6.12.16 | flexhoses | 3-54 |
| 3.3.6.12.17 | translation routes and established worksites | 3-54 |
| 3.3.6.12.17.1 | Primary translation routes and established worksites | 3-54 |
| 3.3.6.12.17.2 | secondary translation routes and eStablished worksites | 3-54 |
| 3.3.6.12.17.3 | eva crewmember contact isolation | 3-54 |
| 3.3.6.12.18 | moving or rotating equipment | 3-55 |
| 3.3.6.13 | launch vehicle interfaces and services | 3-56 |
| 3.3.6.13.1 | safe without space shuttle program services | 3-56 |
| 3.3.6.13.1.1 | fault tolerance/safety margins | 3-56 |
| 3.3.6.13.1.2 | termination of services due to orbiter emergency conditions | 3-56 |
| 3.3.6.13.2 | critical orbiter services | 3-56 |
| 3.3.6.13.3 | inadvertent deployment, separation, and jettison functions | 3-56 |
| 3.3.6.13.4 | planned deployment/extension functions | 3-56 |
| 3.3.6.13.4.1 | violation of orbiter payload door envelope | 3-56 |
| 3.3.6.13.4.2 | method of fault tolerance | 3-56 |
| 3.3.6.13.5 | contingency return and rapid safing | 3-56 |
| 3.3.6.13.5.1 | deleted | 3-56 |
| 3.3.6.13.5.2 | deleted | 3-56 |
| 3.3.6.14 | flammable atmosphere | 3-56 |
| 3.3.6.14.1 | normal functions | 3-56 |
| 3.3.6.14.2 | electrical ignition sources | 3-57 |
| 3.3.6.14.3 | surface temperatures | 3-57 |
| 3.3.6.14.4 | conductive surfaces | 3-57 |
| 3.3.6.15 | reserved | 3-57 |
| 3.3.6.16 | lightning protection | 3-57 |
| 3.3.6.17 | orbiter vent/dump provisions | 3-57 |
| 3.3.6.17.1 | release or ejection of hazardous materials | 3-57 |
| 3.3.6.17.2 | fluid system containment | 3-57 |
| 3.3.6.18 | sealed compartments | 3-57 |
| 3.3.6.19 | ground safety requirements for space shuttle launch of PMM hardware | 3-57 |
| 3.3.6.20 | Indicate emergency egress hatches | 3-57 |
| 3.3.7 | human engineering | 3-57 |
| 3.3.7.1 | internal hardware | 3-57 |
| 3.3.7.1.1 | anthropometric requirements | 3-57 |
| 3.3.7.1.2 | strength requirements | 3-58 |
| 3.3.7.1.2.1 | normal and maintenance operations | 3-58 |
| 3.3.7.1.2.2 | emergency controls | 3-58 |
| 3.3.7.1.3 | gloved operation | 3-58 |
| 3.3.7.1.4 | location coding | 3-58 |
| 3.3.7.1.4.1 | alphanumeric coding | 3-58 |
| 3.3.7.1.4.2 | reference configuration coordinate system | 3-58 |
| 3.3.7.1.4.3 | deleted | 3-58 |
| 3.3.7.1.4.4 | deleted | 3-58 |
| 3.3.7.1.4.5 | deleted | 3-58 |
| 3.3.7.1.4.6 | deleted | 3-58 |
| 3.3.7.1.4.7 | deleted | 3-58 |
| 3.3.7.1.4.8 | utility accessibility | 3-58 |
| 3.3.7.1.5 | iva closures and design requirements | 3-58 |
| 3.3.7.1.6 | iva housekeeping | 3-58 |
| 3.3.7.1.7 | controls and displays | 3-59 |
| 3.3.7.1.8 | interior colors | 3-59 |
| 3.3.7.1.9 | Hand Holds and Hand Rails | 3-59 |
| 3.3.7.1.10 | Maintenance of Crew Position | 3-59 |
| 3.3.7.2 | external eva hardware | 3-59 |
| 3.3.7.2.1 | external task location requirements | 3-59 |
| 3.3.7.2.2 | eva crewmember field of view | 3-59 |
| 3.3.7.2.3 | working volume | 3-59 |
| 3.3.7.2.4 | eva induced loads | 3-59 |
| 3.3.7.2.5 | repetitive actuation forces | 3-61 |
| 3.3.7.2.6 | crew aids for worksite stability | 3-61 |
| 3.3.7.2.6.1 | placement for worksite tasks | 3-61 |
| 3.3.7.2.6.2 | proximity to foot restraint | 3-61 |
| 3.3.7.2.6.3 | foot restraing ingress and egress aid | 3-61 |
| 3.3.7.2.6.4 | height considerations | 3-61 |
| 3.3.7.2.6.5 | centering | 3-61 |
| 3.3.7.2.7 | glove clearance | 3-61 |
| 3.3.7.2.8 | primary translation path marking | 3-61 |
| 3.3.7.2.9 | translation path | 3-61 |
| 3.3.7.2.10 | handrail spacing | 3-61 |
| 3.3.8 | nuclear control | 3-62 |
| 3.3.9 | system security | 3-62 |
| 3.3.10 | environmental constraints | 3-62 |
| 3.3.10.1 | flight system environmental constaints | 3-62 |
| 3.3.10.1.1 | acoustic emission limits | 3-62 |
| 3.3.10.1.2 | external contamination releases | 3-62 |
| 3.3.10.1.3 | ionizing radiation emission limits | 3-62 |
| 3.3.10.1.4 | internal temperature limits during transfer of PMM | 3-63 |
| 3.3.10.1.5 | internal temperature limits edward afb operations and ferry flight of PMM | 3-63 |
| 3.3.11 | design for remote controlled external operations | 3-63 |
| 3.3.11.1 | equipment requiring shuttle robotic support | 3-63 |
| 3.3.11.2 | external equipment requiring robotic hand-off | 3-63 |
| 3.3.11.3 | External equipment requiring ssrms support | 3-63 |
| 3.3.11.3.1 | equipment requiring ssrms support using an nsts gf | 3-65 |
| 3.3.12 | design requirements | 3-65 |
| 3.3.12.1 | PMM design requirements | 3-65 |
| 3.3.12.1.1 | structural design requirements | 3-65 |
| 3.3.12.1.1.1 | structure penetrations | 3-65 |
| 3.3.12.1.1.2 | window, glass, and ceramic structural design | 3-65 |
| 3.3.12.1.1.3 | fracture control | 3-66 |
| 3.3.12.1.1.4 | allowabLE mechanical properties | 3-66 |
| 3.3.12.1.1.5 | on-orbit loads | 3-66 |
| 3.3.12.1.1.5.1 | on-orbit pressure spectra | 3-66 |
| 3.3.12.1.1.5.2 | on-orbit transient loads | 3-66 |
| 3.3.12.1.1.5.3 | on-orbit thermally induced loads | 3-68 |
| 3.3.12.1.2 | fluid handling requirements | 3-68 |
| 3.3.12.1.2.1 | fluid standards | 3-68 |
| 3.3.12.1.2.2 | fluid quantity | 3-68 |
| 3.3.12.1.2.3 | interface hardware | 3-69 |
| 3.3.12.1.2.4 | flexible lines and bellows design | 3-69 |
| 3.3.12.1.3 | fasteners | 3-69 |
| 3.3.12.1.4 | internal atmosphere | 3-69 |
| 3.3.12.1.4.1 | maximum design pressure | 3-69 |
| 3.3.12.1.4.2 | atmospheric leakage | 3-69 |
| 3.3.12.1.5 | operational life | 3-69 |
| 3.3.12.1.6 | carrier mating/de-mating | 3-69 |
| 3.3.12.1.6.1 | bertHing stay - out zones | 3-69 |
| 3.3.12.1.7 | element access | 3-69 |
| 3.3.12.1.8 | preclude condensation | 3-70 |
| 3.3.12.1.9 | support internal equipment removal and replacement | 3-70 |
| 3.3.12.1.10 | iva translation path obstructions | 3-70 |
| 3.3.12.1.11 | iva restrainT for non - permanent equipment | 3-70 |
| 3.3.12.1.12 | GENERAL MOUNTING | 3-70 |
| 3.3.12.2 | iva connectors | 3-70 |
| 3.3.12.3 | external hardware | 3-70 |
| 3.3.12.3.1 | eva equipment handling capabilities | 3-70 |
| 3.3.12.4 | alignment devices | 3-70 |
| 3.3.12.5 | cable management | 3-71 |
| 3.3.13 | mil-std-1553 data bus addresses | 3-71 |
| 3.3.14 | mil-std-1553 data bus constraints | 3-71 |
| 3.3.14.1 | ssq components | 3-71 |
| 3.3.14.1.1 | bus coupler type | 3-71 |
| 3.3.14.2 | bus stub length | 3-71 |
| 3.3.14.3 | bus coupling | 3-72 |
| 3.3.15 | terminal interface units | 3-72 |
| 3.3.15.1 | input impedance | 3-72 |
| 3.3.15.2 | tiu multiple bus isolation | 3-73 |
| 3.3.16 | PMM not-to exceed bus length | 3-73 |
| 3.4 | computer resource requirements | 3-73 |
| 3.4.1 | flexibility and expansion | 3-73 |
| 3.5 | logistics | 3-73 |
| 3.5.1 | maintenance | 3-73 |
| 3.5.1.1 | on-orbit maintenance | 3-73 |
| 3.5.1.1.1 | corrective maintenance | 3-74 |
| 3.5.1.1.2 | in situ maintenance | 3-74 |
| 3.5.1.1.3 | oru intermediate maintenance | 3-74 |
| 3.5.1.1.4 | preventive maintenance | 3-74 |
| 3.5.1.1.5 | pressurized volume rack rotation | 3-74 |
| 3.5.1.2 | on-orbit maintenance backup | 3-74 |
| 3.5.1.3 | access for on-orbit maintenance | 3-74 |
| 3.5.1.3.1 | access for on-orbit inspection | 3-74 |
| 3.5.1.3.2 | visual access | 3-74 |
| 3.5.1.3.3 | eva access to fasteners | 3-74 |
| 3.5.1.3.4 | physical access | 3-74 |
| 3.5.1.3.4.1 | deleted | 3-74 |
| 3.5.1.3.5 | removal, replacement, and modularity design | 3-74 |
| 3.5.1.4 | standard on-orbit tools | 3-75 |
| 3.5.1.5 | standard on-orbit diagnostic equipment | 3-76 |
| 3.5.1.6 | ground maintenance | 3-76 |
| 3.6 | personnel and training | 3-76 |
| 3.7 | chAracteristics | 3-76 |
| 3.8 | precedence | 3-77 |
| 4.0 | quality assurance provisions | 4-1 |
| 4.1 | general | 4-2 |
| 4.1.1 | responsibility for verifications | 4-3 |
| 4.1.2 | particular instructions applicable to PMM verification | 4-3 |
| 4.2 | PMM quality conformance inspections | 4-3 |
| 4.3 | system requirements | 4-4 |
| 4.3.1 | system definition | 4-4 |
| 4.3.1.1 | system functional description | 4-4 |
| 4.3.1.2 | mission sCENARIO | 4-4 |
| 4.3.1.2.1 | GROUND OPERATIONS sCENARIO | 4-4 |
| 4.3.1.2.2 | LAUNCH AND ON-ORBIT sCENARIO | 4-4 |
| 4.3.1.2.3 | CONTINGENCY sCENARIO | 4-4 |
| 4.3.1.3 | integrated system functional diagram | 4-4 |
| 4.3.1.4 | interface requirements | 4-4 |
| 4.3.1.4.1 | external interfaces | 4-4 |
| 4.3.1.4.1.1 | orbiter external interface description | 4-4 |
| 4.3.1.4.1.2 | launch/landing site support facilities external interface description | 4-4 |
| 4.3.1.4.1.3 | united states on-orbit segment (usos) external interface description | 4-4 |
| 4.3.1.4.1.3.1 | portable fire extinguisher (pfe) external interface description | 4-4 |
| 4.3.1.4.1.3.2 | portable breathing apparatus (pba) external interface description | 4-4 |
| 4.3.1.4.1.3.3 | intravehicular activity restraints and mobility aids interface | 4-5 |
| 4.3.1.4.1.3.4 | extravehicular activity translation aids and attachments interfaces | 4-5 |
| 4.3.1.4.1.3.5 | CAUTION & WARNING (C&w) DEVICE interfaces | 4-5 |
| 4.3.1.4.1.3.6 | PMM pcbm TO Node 1 acbm interface | 4-5 |
| 4.3.1.4.1.4 | space station remote manipulator system (ssrms) external interface description | 4-5 |
| 4.3.1.4.1.5 | rack external interface | 4-5 |
| 4.3.1.4.1.6 | refrigerator/freezer rack external interface description | 4-5 |
| 4.3.1.4.1.7 | re-supply stowage platform external interface | 4-5 |
| 4.3.1.4.1.8 | PMM to ground support equipment interface description | 4-5 |
| 4.3.1.4.1.9 | K-BAR/PIVOT PIN INTERFACES | 4-5 |
| 4.3.1.4.2 | INTERNAL INTERFACES | 4-5 |
| 4.3.1.4.2.1 | PCBM INTERFACE | 4-5 |
| 4.3.1.4.2.2 | hatch interface | 4-5 |
| 4.3.2 | characteristics | 4-6 |
| 4.3.2.1 | performance characteristics | 4-6 |
| 4.3.2.1.1 | state: perform mission on-orbit | 4-6 |
| 4.3.2.1.1.1 | capability | 4-6 |
| 4.3.2.1.1.1.1 | relieve overpressure | 4-6 |
| 4.3.2.1.1.1.2 | equalize pressure | 4-6 |
| 4.3.2.1.1.1.3 | circulate atmosphere | 4-6 |
| 4.3.2.1.1.1.4 | control internal lighting | 4-7 |
| 4.3.2.1.1.1.5 | illumination internal areas | 4-7 |
| 4.3.2.1.1.1.6 | isolate to recovery level | 4-8 |
| 4.3.2.1.1.1.7 | recover lost function | 4-8 |
| 4.3.2.1.1.1.8 | isolate for safing | 4-8 |
| 4.3.2.1.1.1.9 | safe | 4-8 |
| 4.3.2.1.1.1.9.1 | re-attempt safing | 4-8 |
| 4.3.2.1.1.1.9.2 | demand safing | 4-9 |
| 4.3.2.1.1.1.9.3 | confirm successful safing | 4-9 |
| 4.3.2.1.1.1.10 | maintain station mode | 4-9 |
| 4.3.2.1.1.1.11 | transition station modes | 4-9 |
| 4.3.2.1.1.1.12 | generate functional data | 4-9 |
| 4.3.2.1.1.1.13 | assess functional status data | 4-9 |
| 4.3.2.1.1.1.14 | acquire hazardous condition data | 4-10 |
| 4.3.2.1.1.1.15 | identify hazardous condition | 4-10 |
| 4.3.2.1.1.1.16 | respond to fire | 4-10 |
| 4.3.2.1.1.1.17 | respond to hazardous atmosphere | 4-11 |
| 4.3.2.1.1.1.18 | deleted | 4-11 |
| 4.3.2.1.1.1.19 | deleted | 4-11 |
| 4.3.2.1.1.1.20 | distribute power | 4-11 |
| 4.3.2.1.1.1.21 | collect thermal energy | 4-11 |
| 4.3.2.1.1.1.22 | distribute thermal energy | 4-12 |
| 4.3.2.1.1.1.23 | distribute time | 4-12 |
| 4.3.2.1.1.1.24 | Support internal crew restraint and mobility | 4-12 |
| 4.3.2.1.1.1.25 | provide direct visual access | 4-13 |
| 4.3.2.1.1.1.26 | deleted | 4-13 |
| 4.3.2.1.1.1.27 | provide data for downlink | 4-13 |
| 4.3.2.1.1.1.28 | deleted | 4-13 |
| 4.3.2.1.1.1.29 | deleted | 4-13 |
| 4.3.2.1.1.1.30 | manage time | 4-13 |
| 4.3.2.1.1.1.30.1 | maintain time | 4-13 |
| 4.3.2.1.1.1.30.2 | control time | 4-13 |
| 4.3.2.1.1.1.31 | provide time interface | 4-14 |
| 4.3.2.1.1.1.31.1 | receive time | 4-14 |
| 4.3.2.1.1.1.31.2 | provide time services | 4-14 |
| 4.3.2.1.1.1.31.3 | distribute time | 4-14 |
| 4.3.2.1.1.1.32 | ATMOSPHERE SAMPLING | 4-14 |
| 4.3.2.1.1.1.33 | respond to rapid decompression | 4-15 |
| 4.3.2.1.1.1.34 | annunciate alarms | 4-15 |
| 4.3.2.1.1.1.35 | micro-gravity distrubances | 4-15 |
| 4.3.2.1.1.1.35.1 | limit quasi-steady accelerations | 4-15 |
| 4.3.2.1.1.1.35.2 | Limit vibratory accelerations | 4-15 |
| 4.3.2.1.1.1.36 | limit angular momentum disturbances | 4-15 |
| 4.3.2.1.1.1.36.1 | limit disturbance induced iss attitude rate | 4-15 |
| 4.3.2.1.1.1.36.2 | limit disturbance induced cmg momentum usage | 4-16 |
| 4.3.2.1.2 | deleted | 4-16 |
| 4.3.2.1.3 | state: support mission | 4-16 |
| 4.3.2.1.3.1 | mode: ground processing | 4-17 |
| 4.3.2.1.3.1.1 | load and unload cargo items | 4-17 |
| 4.3.2.1.3.1.2 | support system checkout and monitoring | 4-17 |
| 4.3.2.1.3.2 | mode: space transport | 4-17 |
| 4.3.2.1.3.2.1 | transport internal cargo | 4-17 |
| 4.3.2.2 | physical characteristics | 4-18 |
| 4.3.2.2.1 | tare weight | 4-18 |
| 4.3.2.2.2 | launch envelope | 4-18 |
| 4.3.2.2.2.1 | external diameter | 4-18 |
| 4.3.2.2.2.2 | axial length | 4-18 |
| 4.3.2.2.3 | distribute commands and data | 4-18 |
| 4.3.2.2.4 | external nasa/ASI insignia emblem | 4-18 |
| 4.3.2.2.4.1 | external nasa insignia emblem | 4-18 |
| 4.3.2.2.4.2 | No verification required. external ASI insignia emblem | 4-18 |
| 4.3.2.3 | reliability | 4-19 |
| 4.3.2.3.1 | flight system reliability | 4-19 |
| 4.3.2.3.1.1 | failure tolerance | 4-19 |
| 4.3.2.3.1.2 | failure propagation | 4-19 |
| 4.3.2.3.1.3 | separation of redundant path | 4-19 |
| 4.3.2.3.1.4 | redundancy | 4-19 |
| 4.3.2.4 | maintainability | 4-19 |
| 4.3.2.4.1 | flight system maintainability | 4-19 |
| 4.3.2.4.1.1 | qualitative maintainability design | 4-19 |
| 4.3.2.4.1.1.1 | equipment item interconnecting devices | 4-19 |
| 4.3.2.4.1.1.2 | incorrect equipment installation | 4-20 |
| 4.3.2.4.1.1.3 | lockwiring and staking | 4-20 |
| 4.3.2.4.1.1.4 | PMM mean maintenance crew hours per year | 4-20 |
| 4.3.2.4.1.1.5 | ACCESS ITEM RETENTION | 4-20 |
| 4.3.2.4.1.2 | failure detection, isolation, and recovery (fdir) | 4-20 |
| 4.3.2.4.1.2.1 | automatic hazard and hazardous condition detection | 4-20 |
| 4.3.2.4.1.2.2 | automatic anomaly detection | 4-20 |
| 4.3.2.4.1.2.3 | manual fdir | 4-20 |
| 4.3.2.4.1.2.4 | manual control of fdir | 4-20 |
| 4.3.2.4.1.2.5 | deleted | 4-21 |
| 4.3.2.4.1.2.6 | automatic safing verification | 4-21 |
| 4.3.2.4.1.2.7 | testing at operation location | 4-21 |
| 4.3.2.4.1.2.8 | ambiguity resolution | 4-22 |
| 4.3.2.4.1.2.9 | data availability | 4-22 |
| 4.3.2.4.1.2.10 | false alarm mitigation | 4-22 |
| 4.3.2.5 | availability | 4-22 |
| 4.3.2.6 | environmental conditions | 4-23 |
| 4.3.2.6.1 | flight system environmental conditions | 4-23 |
| 4.3.2.6.1.1 | on-orbit environmental conditions | 4-23 |
| 4.3.2.6.1.1.1 | thermal environment | 4-23 |
| 4.3.2.6.1.1.2 | neutral atmosphere | 4-28 |
| 4.3.2.6.1.1.3 | external contamination | 4-28 |
| 4.3.2.6.1.1.4 | electromagnetic and geomagnetic fields | 4-28 |
| 4.3.2.6.1.1.5 | plasma | 4-28 |
| 4.3.2.6.1.1.6 | ionizing radiation | 4-28 |
| 4.3.2.6.1.1.7 | solar ultraviolet radiation | 4-29 |
| 4.3.2.6.1.1.8 | micro meteoroids and orbital debris (mmod) | 4-29 |
| 4.3.2.6.1.1.9 | deleted | 4-29 |
| 4.3.2.6.1.1.10 | plume impingement pressures | 4-29 |
| 4.3.2.6.1.1.11 | atomic oxygen | 4-29 |
| 4.3.2.6.1.2 | ascent/descent thermal environment | 4-29 |
| 4.3.2.7 | transportability | 4-29 |
| 4.3.2.7.1 | PMM transportability | 4-29 |
| 4.3.3 | design and construction | 4-30 |
| 4.3.3.1 | materials, processes, and parts | 4-30 |
| 4.3.3.1.1 | PMM materials, processes, and parts | 4-30 |
| 4.3.3.1.1.1 | materials and processes | 4-30 |
| 4.3.3.1.1.2 | electrical, electronic, and electromechanical (eee) parts | 4-31 |
| 4.3.3.1.1.2.1 | eee parts seLEction | 4-31 |
| 4.3.3.1.1.3 | static age life | 4-31 |
| 4.3.3.2 | electromagnetic radiation (emr) | 4-31 |
| 4.3.3.2.1 | PMM electromagnetic compatibility (emc) requirements | 4-31 |
| 4.3.3.2.1.1 | grounding | 4-31 |
| 4.3.3.2.1.2 | cabling and wire design | 4-32 |
| 4.3.3.2.1.3 | electrical bonding | 4-32 |
| 4.3.3.2.1.4 | power conducted disturbances | 4-32 |
| 4.3.3.2.1.5 | equipment electromagnetic interference (emi) requirements | 4-32 |
| 4.3.3.2.1.6 | electromagnetic interference safety margins for critical circuits | 4-32 |
| 4.3.3.2.1.7 | launch element transportation, storage, and launch environment | 4-32 |
| 4.3.3.2.1.8 | static electricity | 4-32 |
| 4.3.3.2.1.9 | corona | 4-33 |
| 4.3.3.2.1.10 | selection and use of equipment | 4-33 |
| 4.3.3.3 | nameplates and product markings | 4-33 |
| 4.3.3.3.1 | PMM nameplates and product markings | 4-33 |
| 4.3.3.3.1.1 | labeling | 4-33 |
| 4.3.3.4 | workmanship | 4-34 |
| 4.3.3.4.1 | PMM workmanship | 4-34 |
| 4.3.3.4.2 | PMM cleanliness | 4-34 |
| 4.3.3.5 | interchangeability | 4-35 |
| 4.3.3.6 | safety | 4-35 |
| 4.3.3.6.1 | general | 4-35 |
| 4.3.3.6.1.1 | catastrophic hazards | 4-35 |
| 4.3.3.6.1.1.1 | deleted | 4-35 |
| 4.3.3.6.1.1.2 | deleted | 4-35 |
| 4.3.3.6.1.2 | critical hazards | 4-35 |
| 4.3.3.6.1.3 | design for minimum risk | 4-35 |
| 4.3.3.6.1.4 | control of functions of resulting in critical hazards | 4-35 |
| 4.3.3.6.1.4.1 | inadvertent operations resulting in a critical hazard | 4-35 |
| 4.3.3.6.1.4.2 | loss of a function resulting in a critical hazard | 4-36 |
| 4.3.3.6.1.5 | control of functions resulting in a catastrophic hazards | 4-36 |
| 4.3.3.6.1.5.1 | inadvertent operation resulting in caTastrophic hazards | 4-36 |
| 4.3.3.6.1.5.2 | loss of function resulting in carastrophic hazards | 4-36 |
| 4.3.3.6.1.6 | subsequent induced loads | 4-36 |
| 4.3.3.6.1.6.1 | deleted | 4-36 |
| 4.3.3.6.1.7 | safety interlocks | 4-36 |
| 4.3.3.6.1.8 | environmental compatibility | 4-37 |
| 4.3.3.6.2 | hazard detection and safing | 4-37 |
| 4.3.3.6.2.1 | reserved | 4-37 |
| 4.3.3.6.2.2 | monitors | 4-37 |
| 4.3.3.6.2.2.1 | status information | 4-37 |
| 4.3.3.6.2.2.2 | hazardous function operation prevention | 4-37 |
| 4.3.3.6.2.2.3 | loss of input or failure | 4-37 |
| 4.3.3.6.2.2.4 | launch site availability | 4-38 |
| 4.3.3.6.2.2.5 | flight crew availability | 4-38 |
| 4.3.3.6.2.3 | near real - time monitoring | 4-38 |
| 4.3.3.6.2.4 | real - time monitoring | 4-38 |
| 4.3.3.6.2.4.1 | maintain status of hazard condtrols | 4-38 |
| 4.3.3.6.2.4.2 | crew response time and safing procedures | 4-38 |
| 4.3.3.6.2.4.3 | deleted | 4-39 |
| 4.3.3.6.3 | command and computer control of hazardous functions | 4-39 |
| 4.3.3.6.3.1 | computer control of hazardous functions | 4-39 |
| 4.3.3.6.4 | hazardous materials | 4-39 |
| 4.3.3.6.4.1 | hazardous fluid containment | 4-39 |
| 4.3.3.6.5 | pyrotechnics | 4-39 |
| 4.3.3.6.6 | radiation | 4-39 |
| 4.3.3.6.6.1 | non - ionizing radiation | 4-39 |
| 4.3.3.6.6.2 | ionizing radiation crew limits | 4-39 |
| 4.3.3.6.6.3 | PMM transmitters | 4-39 |
| 4.3.3.6.7 | optics and lasers | 4-39 |
| 4.3.3.6.8 | electrical safety | 4-40 |
| 4.3.3.6.8.1 | electrical power circuit overloads | 4-40 |
| 4.3.3.6.8.1.1 | circuit overload protection | 4-40 |
| 4.3.3.6.8.1.2 | protective device sizing | 4-40 |
| 4.3.3.6.8.1.3 | bent pin or conductive contamination | 4-40 |
| 4.3.3.6.8.2 | crew protection for electrical shock | 4-40 |
| 4.3.3.6.8.3 | reapplication of power | 4-40 |
| 4.3.3.6.8.4 | batteries | 4-40 |
| 4.3.3.6.9 | cryogenics | 4-41 |
| 4.3.3.6.10 | fire protection | 4-41 |
| 4.3.3.6.10.1 | reserved | 4-41 |
| 4.3.3.6.10.2 | isolation | 4-41 |
| 4.3.3.6.10.3 | suppression | 4-41 |
| 4.3.3.6.10.4 | suppressant | 4-41 |
| 4.3.3.6.10.5 | restorable suppression | 4-41 |
| 4.3.3.6.10.6 | power removal | 4-41 |
| 4.3.3.6.10.7 | portable equipment | 4-41 |
| 4.3.3.6.10.7.1 | set co - location | 4-41 |
| 4.3.3.6.10.8 | confirmation | 4-42 |
| 4.3.3.6.11 | constraints | 4-42 |
| 4.3.3.6.11.1 | reserved | 4-42 |
| 4.3.3.6.11.2 | pressurized volume depressurization and re - pressurization tolerance | 4-42 |
| 4.3.3.6.11.2.1 | pressure differential tolerance | 4-42 |
| 4.3.3.6.11.2.2 | operation during pressure changes | 4-42 |
| 4.3.3.6.11.3 | emergency egress | 4-42 |
| 4.3.3.6.11.4 | reserved | 4-43 |
| 4.3.3.6.11.5 | reserved | 4-43 |
| 4.3.3.6.11.6 | component hazardous energy provision | 4-43 |
| 4.3.3.6.11.7 | hatch opening | 4-43 |
| 4.3.3.6.11.8 | reserved | 4-43 |
| 4.3.3.6.11.9 | reserved | 4-43 |
| 4.3.3.6.11.10 | reserved | 4-43 |
| 4.3.3.6.11.11 | reserved | 4-43 |
| 4.3.3.6.11.12 | hazardous gas accumulation | 4-43 |
| 4.3.3.6.11.12.1 | accumulation prevention | 4-43 |
| 4.3.3.6.11.12.2 | reserved | 4-43 |
| 4.3.3.6.11.13 | equipment clearance for entrapment hazard | 4-43 |
| 4.3.3.6.11.14 | light fixture | 4-44 |
| 4.3.3.6.12 | human engineering safety | 4-44 |
| 4.3.3.6.12.1 | internal volume touch temperature | 4-44 |
| 4.3.3.6.12.1.1 | continuous contact - high temperature | 4-44 |
| 4.3.3.6.12.1.2 | incidental or momentary contact - high temperature | 4-44 |
| 4.3.3.6.12.1.3 | internal volume low touch temperature | 4-44 |
| 4.3.3.6.12.2 | external touch temperature | 4-45 |
| 4.3.3.6.12.2.1 | incidental contact | 4-45 |
| 4.3.3.6.12.2.2 | unlimited contact | 4-45 |
| 4.3.3.6.12.3 | external corner and edge protection | 4-45 |
| 4.3.3.6.12.3.1 | sharp edges | 4-45 |
| 4.3.3.6.12.3.2 | thin materials | 4-45 |
| 4.3.3.6.12.4 | internal corner and edge protection | 4-46 |
| 4.3.3.6.12.4.1 | equipment exposed to crew activity | 4-46 |
| 4.3.3.6.12.5 | reserved | 4-46 |
| 4.3.3.6.12.6 | latches | 4-46 |
| 4.3.3.6.12.7 | screws and bolts | 4-46 |
| 4.3.3.6.12.8 | safety critical fasteners | 4-46 |
| 4.3.3.6.12.9 | levers, cranks, hooks, and controls | 4-46 |
| 4.3.3.6.12.10 | burrs | 4-47 |
| 4.3.3.6.12.11 | holes | 4-47 |
| 4.3.3.6.12.11.1 | equpment located inside habitable volumes | 4-47 |
| 4.3.3.6.12.11.2 | equipment located outside habitable volumes | 4-47 |
| 4.3.3.6.12.12 | protrusions | 4-47 |
| 4.3.3.6.12.13 | pinch points | 4-47 |
| 4.3.3.6.12.14 | reserved | 4-48 |
| 4.3.3.6.12.15 | reserved | 4-48 |
| 4.3.3.6.12.16 | flexhoses | 4-48 |
| 4.3.3.6.12.17 | translation routes and established worksites | 4-48 |
| 4.3.3.6.12.17.1 | primary translation routes and established worksites | 4-48 |
| 4.3.3.6.12.17.2 | secondary translation routes and established worksited | 4-48 |
| 4.3.3.6.12.17.3 | eva crewmember contact isolation | 4-48 |
| 4.3.3.6.12.18 | moving or rotating equipment | 4-48 |
| 4.3.3.6.13 | launch vehicle interfaces and services | 4-49 |
| 4.3.3.6.13.1 | safe without space shuttle program services | 4-49 |
| 4.3.3.6.13.1.1 | fault tolerance/safety margins | 4-49 |
| 4.3.3.6.13.1.2 | termination of services due to orbiter emergency conditions | 4-49 |
| 4.3.3.6.13.2 | critical orbiter services | 4-49 |
| 4.3.3.6.13.3 | inadvertent deployment, separation, and jettison functions | 4-49 |
| 4.3.3.6.13.4 | planned deployment/extension functions | 4-49 |
| 4.3.3.6.13.4.1 | violation of orbiter payload door envelope | 4-49 |
| 4.3.3.6.13.4.2 | method of fault tolerance | 4-50 |
| 4.3.3.6.13.5 | contingency return and rapid safing | 4-50 |
| 4.3.3.6.13.5.1 | deleted | 4-50 |
| 4.3.3.6.13.5.2 | deleted | 4-50 |
| 4.3.3.6.14 | flammable atmosphere | 4-50 |
| 4.3.3.6.14.1 | normal functions | 4-50 |
| 4.3.3.6.14.2 | electrical ignition sources | 4-50 |
| 4.3.3.6.14.3 | surface temperatures | 4-51 |
| 4.3.3.6.14.4 | conductive surfaces | 4-51 |
| 4.3.3.6.15 | reserved | 4-51 |
| 4.3.3.6.16 | lightning protection | 4-51 |
| 4.3.3.6.17 | orbiter vent/dump provisions | 4-51 |
| 4.3.3.6.17.1 | release or ejection of hazardous material | 4-51 |
| 4.3.3.6.17.2 | fluid system containment | 4-51 |
| 4.3.3.6.18 | sealed compartments | 4-51 |
| 4.3.3.6.19 | ground safety requirements for space shuttle launch of PMM hardware | 4-52 |
| 4.3.3.6.20 | Indicate emergency egress hatches | 4-52 |
| 4.3.3.7 | human engineering | 4-52 |
| 4.3.3.7.1 | internal hardware | 4-52 |
| 4.3.3.7.1.1 | anthropometric requirements | 4-52 |
| 4.3.3.7.1.2 | strength requirements | 4-52 |
| 4.3.3.7.1.2.1 | normal and maintenance operations | 4-52 |
| 4.3.3.7.1.2.2 | emergency controls | 4-53 |
| 4.3.3.7.1.3 | gloved operation | 4-53 |
| 4.3.3.7.1.4 | location coding | 4-53 |
| 4.3.3.7.1.4.1 | alphanumeric coding | 4-53 |
| 4.3.3.7.1.4.2 | reference configuration coordinate system | 4-53 |
| 4.3.3.7.1.4.3 | deleted | 4-54 |
| 4.3.3.7.1.4.4 | deleted | 4-54 |
| 4.3.3.7.1.4.5 | deleted | 4-54 |
| 4.3.3.7.1.4.6 | deleted | 4-54 |
| 4.3.3.7.1.4.7 | deleted | 4-54 |
| 4.3.3.7.1.4.8 | utility accessibility | 4-54 |
| 4.3.3.7.1.5 | iva closures and design requirements | 4-54 |
| 4.3.3.7.1.6 | iva housekeeping | 4-54 |
| 4.3.3.7.1.7 | colors and displays | 4-54 |
| 4.3.3.7.1.8 | interior colors | 4-55 |
| 4.3.3.7.1.9 | Hand Holds and Hand Rails | 4-55 |
| 4.3.3.7.1.10 | MAINTENANCE OF CREW POSITION | 4-55 |
| 4.3.3.7.2 | external eva hardware | 4-55 |
| 4.3.3.7.2.1 | external task location requirements | 4-55 |
| 4.3.3.7.2.2 | eva crewmember field of view | 4-55 |
| 4.3.3.7.2.3 | working volume | 4-55 |
| 4.3.3.7.2.4 | eva induced loads | 4-55 |
| 4.3.3.7.2.5 | repetitive actuation forces | 4-55 |
| 4.3.3.7.2.6 | crew aids for worksite stability | 4-55 |
| 4.3.3.7.2.6.1 | placement of worksite tasks | 4-55 |
| 4.3.3.7.2.6.2 | proximity of foot restraint | 4-56 |
| 4.3.3.7.2.6.3 | foot restraing ingress and egress aid | 4-56 |
| 4.3.3.7.2.6.4 | height considerations | 4-56 |
| 4.3.3.7.2.6.5 | centering | 4-56 |
| 4.3.3.7.2.7 | glove clearance | 4-56 |
| 4.3.3.7.2.8 | primary translation path marking | 4-56 |
| 4.3.3.7.2.9 | tranSlation path | 4-56 |
| 4.3.3.7.2.10 | hand rail spacing | 4-56 |
| 4.3.3.8 | Nuclear control | 4-56 |
| 4.3.3.9 | System security | 4-56 |
| 4.3.3.10 | Environmental constraints | 4-56 |
| 4.3.3.10.1 | Flight system environmental constraints | 4-56 |
| 4.3.3.10.1.1 | Acoustic emission limits | 4-56 |
| 4.3.3.10.1.2 | External contamination releases | 4-56 |
| 4.3.3.10.1.3 | Ionizing radiation emission limits | 4-57 |
| 4.3.3.10.1.4 | Internal temperature limits during transfer of PMM | 4-57 |
| 4.3.3.10.1.5 | Internal temperature limits during Edwards AFB operations and ferry flight of PMM | 4-57 |
| 4.3.3.11 | Design for remote controlled external operations | 4-57 |
| 4.3.3.11.1 | equipment requiring shuttle robotic support | 4-57 |
| 4.3.3.11.2 | External equipment requiring robotic hand-off | 4-57 |
| 4.3.3.11.3 | External equipment requiring SSRMS support | 4-57 |
| 4.3.3.11.3.1 | Equipment requiring SSRMS support using an NSTS GF | 4-58 |
| 4.3.3.12 | Design requirements | 4-59 |
| 4.3.3.12.1 | PMM design requirements | 4-59 |
| 4.3.3.12.1.1 | Structural design requirements | 4-59 |
| 4.3.3.12.1.1.1 | Structure penetrations | 4-59 |
| 4.3.3.12.1.1.2 | Window, glass, and ceramic structural design | 4-59 |
| 4.3.3.12.1.1.3 | Fracture control | 4-59 |
| 4.3.3.12.1.1.4 | Allowable mechanical properties | 4-59 |
| 4.3.3.12.1.1.5 | On-orbit loads | 4-60 |
| 4.3.3.12.1.1.5.1 | On-orbit pressure spectra | 4-60 |
| 4.3.3.12.1.1.5.2 | On-orbit transient loads | 4-60 |
| 4.3.3.12.1.1.5.3 | On-orbit thermally induced loads | 4-60 |
| 4.3.3.12.1.2 | Fluid handling requirements | 4-60 |
| 4.3.3.12.1.2.1 | Fluid standards | 4-60 |
| 4.3.3.12.1.2.2 | Fluid quantity determination | 4-60 |
| 4.3.3.12.1.2.3 | Interface hardware | 4-60 |
| 4.3.3.12.1.2.4 | Flexible lines and bellows design | 4-60 |
| 4.3.3.12.1.3 | Fasteners | 4-60 |
| 4.3.3.12.1.4 | Internal atmosphere | 4-61 |
| 4.3.3.12.1.4.1 | Maximum design pressure | 4-61 |
| 4.3.3.12.1.4.2 | Atmospheric leakage | 4-61 |
| 4.3.3.12.1.5 | Operational life | 4-61 |
| 4.3.3.12.1.6 | Carrier mating/de-mating | 4-61 |
| 4.3.3.12.1.6.1 | Berthing stay-out zones | 4-62 |
| 4.3.3.12.1.7 | Element access | 4-62 |
| 4.3.3.12.1.8 | Preclude condensation | 4-62 |
| 4.3.3.12.1.9 | Support internal equipment removal and replacement | 4-62 |
| 4.3.3.12.1.10 | IVA translation path obstructions | 4-62 |
| 4.3.3.12.1.11 | IVA restraint for non-permanent equipment | 4-63 |
| 4.3.3.12.1.12 | General Mounting | 4-63 |
| 4.3.3.12.2 | IVA Connectors | 4-63 |
| 4.3.3.12.3 | External Hardware | 4-63 |
| 4.3.3.12.3.1 | EVA equipment handling capabilities | 4-63 |
| 4.3.3.12.4 | Alignment devices | 4-63 |
| 4.3.3.12.5 | Cable management | 4-63 |
| 4.3.3.13 | MIL-STD-1553 data bus addresses | 4-63 |
| 4.3.3.14 | MIL-STD-1553 data bus constraints | 4-64 |
| 4.3.3.14.1 | SSQ components | 4-64 |
| 4.3.3.14.1.1 | Bus coupler type | 4-64 |
| 4.3.3.14.2 | Bus stub length | 4-64 |
| 4.3.3.14.3 | Bus coupling | 4-64 |
| 4.3.3.15 | Terminal interface units | 4-64 |
| 4.3.3.15.1 | Input impedance | 4-64 |
| 4.3.3.15.2 | TIU multiple bus isolation | 4-65 |
| 4.3.3.16 | PMM not-to-exceed bus length | 4-65 |
| 4.3.4 | Computer resource requirements | 4-65 |
| 4.3.4.1 | Flexibility and expansion | 4-65 |
| 4.3.5 | Logistics | 4-65 |
| 4.3.5.1 | Maintenance | 4-65 |
| 4.3.5.1.1 | On-orbit maintenance | 4-65 |
| 4.3.5.1.1.1 | Corrective maintenance | 4-65 |
| 4.3.5.1.1.2 | In situ maintenance | 4-65 |
| 4.3.5.1.1.3 | ORU intermediate maintenance | 4-66 |
| 4.3.5.1.1.4 | Preventive maintenance | 4-66 |
| 4.3.5.1.1.5 | Pressurized volume rack rotation | 4-66 |
| 4.3.5.1.2 | On-orbit maintenance back-up | 4-66 |
| 4.3.5.1.3 | Access for on-orbit maintenance | 4-66 |
| 4.3.5.1.3.1 | Access for on-orbit inspection | 4-66 |
| 4.3.5.1.3.2 | Visual access | 4-67 |
| 4.3.5.1.3.3 | EVA access to fasteners | 4-67 |
| 4.3.5.1.3.4 | Physical access | 4-67 |
| 4.3.5.1.3.4.1 | Deleted | 4-67 |
| 4.3.5.1.3.5 | Removal, replacement, and modularity design | 4-67 |
| 4.3.5.1.4 | Standard on-orbit tools | 4-67 |
| 4.3.5.1.5 | Standard on-orbit diagnostic equipment | 4-67 |
| 4.3.5.1.6 | Ground maintenance | 4-68 |
| 4.3.6 | Personnel and training | 4-68 |
| 4.3.7 | Characteristics | 4-68 |
| 4.3.8 | Precedence | 4-68 |
| 5.0 | preparation for delivery | 5-1 |
| 5.1 | general | 5-1 |
| 5.2 | detailed preparation | 5-1 |
| 5.2.1 | preservation and packaging | 5-1 |
| 6.0 | notes | 6-1 |
| 6.1 | definitions | 6-1 |
| 6.2 | acronyms and abbreviations | 6-8 |
APPENDIX
| a | requirement exceptions | A-1 |
| B | open work | B-1 |
| C | PMM Bilateral Integrated Verification Plan (BIVP) | C-1 |
TABLE
| 1 | PMM flight system power allocations | 3-15 |
| 2 | Maximum angular momentum impulse | 3-22 |
| 3 | CMG Momentum usage calculation | 3-23 |
| 4 | Functions required for 24-hour autonomous operation | 3-27 |
| 5 | FLIGHT ATTITUDE ENVELOPES FOR VEHICLE DESIGN – ORBITER ATTACHED OPERATIONS | 3-29 |
| 6 | FLIGHT ATTITUDE ENVELOPES FOR VEHICLE DESIGN – STAGE (ORBITER NOT ATTACHED) OPERATIONS | 3-29 |
| 7 | Hot and cold natural thermal environment | 3-30 |
| 8 | Extreme hot and cold natural thermal environment | 3-31 |
| 9 | Parameters for MMOD environment definition | 3-33 |
| 9.1 | pmm planar reflector vibration environment | 3-35 |
| 10 | Equivalent ESA/SCC parts | 3-36 |
| 11 | SSP 50038 applicability matrix | 3-42 |
| 12 | iva crew induced loads at the interface | 3-49 |
| 13 | fluid interfaces portable fire extinguisher | 3-49 |
| 14 | heat transfer rate | 3-52 |
| 15 | PMM interior colors | 3-59 |
| 16 | eva induced loads | 3-60 |
| 17 | moBile servicing centre robotic payload properties | 3-63 |
| 18 | berthing contact conditions | 3-64 |
| 19 | ssrms backdrive threshold | 3-64 |
| 20 | force/moment accommodation | 3-65 |
| 21 | on-orbit pressure spectra | 3-66 |
| 22 | limit load conditions | 3-66 |
| 23 | on-orbit transient load spectra | 3-67 |
| 24 | resultant berthing contact forces (limit) | 3-67 |
| 25 | constrainTs for single eva crewmember transport of objects | 3-70 |
| 26 | standard iva tool list | 3-75 |
| 26 | standard iva tool list - continued | 3-76 |
| B-1 | to be determined items | B-1 |
| B-2 | TO BE RESOLVED ISSUES | B-1 |
FIGURE
| 1 | Integrated system functional block diagram | 3-3 |
| 2 | PMM to PFE interface | 3-6 |
| 3 | PFE envelope | 3-7 |
| 4 | PMM side of R&MA structural interface | 3-8 |
| 5 | R&MA entry/exit envelope to PMM (Configuration 1) | 3-9 |
| 6 | R&MA entry/exit envelope to PMM (Configuration 2) | 3-10 |
| 7 | Fire protection selection criteria | 3-16 |
| 8 | PMM vibro−acoustic microgravity acceleration limits | 3-21 |
| 9 | PMM rack load envelope | 3-24 |
| 10 | On-orbit electric field environment | 3-32 |
| 11 | center of gravity (pfe) | 3-50 |
| 12 | eva zones - top view looking down into cargo bay | 3-55 |
| 13 | eva zones - end view looking at the PMM aft end cone in the cargo bay | 3-55 |
| 14 | Deleted | 3-55 |
| 15 | crewmember optimum work envelope | 3-59 |
| 16 | crewmember field of view | 3-59 |
| 17 | eva work volume and incidental contact volume | 3-60 |
| 18 | crew aids for stability | 3-61 |
| 19 | foot restraint ingress and egress aid | 3-61 |
| 20 | minimum clearance for gloved hand access | 3-62 |
| 21 | envelope for Handrail-assisted translation | 3-62 |
| 22 | load application diagram | 3-68 |
| 23 | typical bus | 3-72 |
| 24 | tiu minimum input impedance | 3-73 |
| 24 | design cold thermal environment profile | 4-24 |
| 25 | Design hot thermal environment profile | 4-25 |
| 26 | extreme cold thermal environment profile | 4-26 |
| 27 | EXTREME HOT THERMAL ENVIRONMENT PROFILE | 4-27 |
xxvii
SCOPE
This specification establishes the performance, design, development, and qualification requirements for the Permanent Multipurpose Module (PMM).
Identification This specification is for the PMM that will be a modification of the MPLM Flight Unit FM-1 (Leonardo) developed by ASI and delivered to NASA. The PMM Part Number: is 0000P001-805, the Serial Number is 00001 and the NASA ISS Configuration Item (CI) number of the upgraded MPLM is ISSA15A.
System overview The purpose of the PMM is to provide:
a. Logistics re-supply and transportation of user passive cargo and payloads for use by the on-orbit Space Station, as per the Flight ULF5 upload manifest;
b. Additional pressurized volume for stowage of cargo at the ISS, when docked to Node 1 Nadir.
1-1 documents applicable documents specifications, standards, and handbooks The following specifications, standards, and handbooks of the exact issue shown, form a part of this specification to the extent specified herein. In the event of a conflict between the documents referenced herein and the contents of this specification, the contents of this specification shall be considered a superseding requirement.
MILITARY STANDARDS
MIL-D-3464 Rev. E April 21, 1987 Desiccants, Activated, Bagged, Packaging Use and Static Dehumidification
MIL-STD-130 Rev. G October 11, 1988 Identification Marking of US Military Property
MIL-STD-1553 Rev. B, Notice 2 September 8, 1986 Digital Time Division Command/Response Multiplex Data Bus
MILITARY HANDBOOKS
MIL-HDBK-5, Rev. E June 1, 1987 Metallic Materials and Elements for Aerospace Vehicle Structures
MIL-HDBK-17 Rev. B, Notice 1 February 29, 1988 Polymer Matrix Composites Volume 1:Guidelines
MIL-HDBK-1553A plus Notice 1, 2, and 3 1 November 1998Multiplex Application Handbook
Other government documents, drawings, and publications The following other government documents, drawings, and publications of the exact issue shown, form a part of this specification to the extent specified herein.
SPECIFICATIONS
JSC-SN-C-0005 Rev. C February 15, 1989 NSTS Contamination Control Requirement Manual
JSC 27260, Rev. E Date: January, 2006 Decal Process Document and Catalog
KHB 1700.7, Rev. C August 19, 1999 STS Payload Ground Safety Handbook
NHB 6000.1, Rev. D September 30, 1990 Requirements for Packaging, Handling, and Transportation for Aeronautical and Space Systems, Equipment and Associated Components
NHB 8060.1, Rev. C April 2, 1991 Flammability, Odor, and Offgassing Requirements and Test Procedures for Materials in Environments that Support Combustion
NP 212 Current Issue NASA Graphics Standard, NASA Insignia
NSTS 1700.7 Rev. B, PCN 1 February 24, 1993 Safety Policy and Requirements for Payloads using the Space Transportation System
ICD-A-21499-MPLM-A ,
June 15, 2009 Shuttle Orbiter/MPLM-A Cargo Element Interfaces
NSTS 07700, Volume XIV June 1989 Space Shuttle System Payload Accommodations
NSTS 07700, Appendix 1 Rev. J, Change 1 June 1989 Contamination Environment
NSTS 07700, Appendix 2 Rev. J, Change 1 June 1989 System Description and Design Data-Thermal
NSTS 07700, Appendix 3 Rev. J, Change 2 June 1989 Electrical Power and Avionics
NSTS 07700, Appendix 4 Rev. J, Change 1 June 1989 Structures and Mechanisms
NSTS 07700, Appendix 5 Rev. K, Change 1 July 31, 1991 Ground Operations
NSTS 07700, Appendix 6 Rev. J October 4, 1988 Mission Planning and Flight Design
NSTS 07700, Appendix 7 Rev. J, Change 1 June 1989 Extravehicular Activities
NSTS 07700, Appendix 8 Rev. J, Change 1 June 1989 Payload Deployment and Retrieval System
NSTS 07700, Appendix 9 Rev. K December 16, 1992 Intravehicular Activities
NSTS 07700, Appendix 10 Rev. J, Change 1 June 1989 Integration Hardware
NSTS 08123 Rev. B March 28, 1991 Certification of Flex Hoses and Bellows for Flow Induced Vibration
NSTS 14046 Rev. C Including Numbered Updates 1 and 2 April 1994 Payload Verification Requirements
NSTS 20793
September 28, 1985 Manned Space Vehicle Battery Safety Handbook
SSP 30219, Rev. J Space Station Reference Coordinate Systems
SSP 30233, Rev. F March 6, 1998 Space Station Requirements for Materials and Processes
SSP 30234, Rev. D August 5, 1994 Instructions for Preparation of Failure Modes and Effects Analysis and Critical Items List for Space Station
SSP 30237, Rev. J Space Station Electromagnetic Emission and Susceptibility Requirements (except paragraph 3.2.1.3.2 for which Rev. B shall apply)
SSP 30238, Rev. C May 31, 1996 Space Station Electromagnetic Techniques (except paragraphs 3.2.4.1.3, 3.2.4.1.4.2, 3.2.4.1.5, Figures 3-1 and 3-6 for which Rev. B shall apply)
SSP 30240, Rev. F Space Station Grounding Requirements
SSP 30242, Rev. D, DCN 001, 002 May 31, 1996 Space Station Cable/Wire Design and Control Requirements for Electromagnetic Compatibility
SSP 30243, Rev. H Space Station Requirements for Electromagnetic Compatibility (except paragraphs 2.0, 3.2.2, 3.2.5, 3.2.10, 3.2.11, 3.5.3, 3.6.2.1, 3.6.2.1.1, 3.6.2.1.5, Appendix D, and Appendix E for which Rev. B shall apply)
SSP 30245, Rev. J Space Station Electrical Bonding Requirements (except paragraph 3.3.7 for which Rev. B shall apply)
SSP 30245
EMECB Tailoring Interpretation Agreement (TIA) 0031
SSP 30309 F
Safety Analysis and Risk Assessment Requirement Document
SSP 30312, Rev. J Electrical, Electronic, and Electromechanical and Mechanical Parts Management and Implementation Plan for Space Station Program
SSP 30420, Rev. B June 18, 1993 Space Station Electromagnetic, Ionizing Radiation and Plasma Environment Definition and Design Requirements
SSP 30423, Rev. F March 31, 1995 Space Station Approved Electrical, Electronic, and Electromechanical Parts List
SSP 30425, Rev. B February 8, 1994 Space Station Program Natural Environment Definition for Design
SSP 30426, Rev. D, DCN 001 January 21, 1994 Space Station External Contamination Control Requirements
SSP 30482, Vol. I Rev. A, DCN 001 January 2, 1994 Electrical Power Specifications and Standards: Vol. I, EPS Electrical Power Specifications
SSP 30482, Vol. II Rev. A, DCN 001, 002 January 1, 1994 Electrical Power Specifications and Standards: Vol. II, Consumer Constraints
SSP 30512, Rev. C June 3, 1994 Space Station Ionizing Radiation Design Environment
SSP 30558, Rev. B June 30, 1994 Fracture Control Requirements for Space Station
SSP 30559, D
Structural Design and Verification Requirements
SSP 30560, Rev. Basic June 1, 1991 Glass, Window and Ceramic Structural Design and Verification Requirements
SSP 30575, Rev. E April, 2007 Space Station Interior and Exterior Operational Location Coding System
SSP 30599, Rev. D September 2006 Safety Review Process
SSP 41004, Revision H, Part 1 October 25, 2005 Common Berthing Mechanism to Pressurized Elements Interface Control Document, Part 1
SSP 41004, Revision G, Part 2 Date: April 30, 1998 Common Berthing Mechanism to Pressurized Elements Interface Control Document, Part 2
SSP 41015, Rev. G, Part 1 Common Hatch and Mechanisms to Pressurized Elements Interface Control Document (Part 1)
SSP 41015, Rev. F Part 2 Date: July 29,1999 Common Hatch and Mechanisms to Pressurized Elements Interface Control Document (Part 2)
SSP 41017, Rev. G, Part 1 Rack To Mini-Pressurized Logistics Module Interface Control Document (Part 1)
SSP 41017, Rev. F, Part 2 November 13, 1998 Rack To Mini-Pressurized Logistics Module Interface Control Document (Part 2)
SSP 41172, Rev. J March 30, 2001 Qualification and Acceptance Environment Test Requirement
SSP 42004, Rev. H, Part 1 Mobile Servicing System (MSS) to User (Generic) Interface Control Document Part 1
SSP 42004, Rev. A, Part 2 Date: May 22, 1997 Mobile Servicing System (MSS) to User (Generic) Interface Control Document Part 2
SSP 42007, Rev. H, Part 1 December 31, 2002 United States On-orbit Segment to Italian to Mini-Pressurized Logistics Module Interface Control Document Part 1
SSP 42007, Rev. H, Part 2 Date:June 29, 1999 United States On-orbit Segment to Italian to Mini-Pressurized Logistics Module Interface Control Document Part 2
SSP 50004, Rev. Basic, DCN 001, 002 February 1, 1994 Ground Support Equipment Design Requirements (except paragraph 3.6.7.1 where Revision Basic plus CN001 shall apply)
SSP 50005, Rev. E June 30, 2006 International Space Station Flight Crew Integration Standard (NASA-STD-3000/T)
SSP 50007, Rev. D February, 2006 Space Station Inventory Management System Label Specification
SSP 50014, Rev. B September 3, 1997 International Space Station Utility Coding Specification
SSP 50023, Rev. Basic April 15, 1994 Thermal Control Plan
SSP 50038, Rev. B November 17, 1995 Computer Based Control System Safety Requirements
SSP 50104, Rev. A.
November 1996 Portable Breathing Apparatus Standard Interface Control Document Part 1
SSP 50110, Rev. J Multi-Increment Manifest Document
SSP 50228-6, Rev. Basic September, 1997 Space Station Program Configuration and Assembly Standard Interface Control Document, Volume 6: Advanced Vision Function To Multi Purpose Logistics Module
SSP 50699, Rev. B December, 2008 ISS Certification Baseline Volume 3: Flight Attitudes
SSQ 26000, Rev. Basic, October 16, 1996 Space Station Program Office Standard Repair for Sharp Edges on SSQ 21635 NZGL Type Connector Assemblies and Components
SSP 50342, Rev. Initial Release May 1998 MIL-STD-1553 Remote Terminal Test Exceptions Report
SSP 30256:001, Rev. H July 17, 2006 Extravehicular Activity (EVA) Standard Interface Control Document
| SSP 30256:010 Basic |
| Portable Fire Extinguisher Interface Control Document |
SSP 30257:004, Rev. E Space Station Program Intravehicular Activity Restraints and Mobility Aids Interface Control Document
SSP 41148, Rev. D September 30, 1998 Active Common Berthing Mechanism to Passive Common Berthing Mechanism Interface Control Document, Part 1
STANDARDS
OTHER PUBLICATIONS
SID 82K00760, Rev. D April 15, 1993 Standard Interface Document Space Station Processing Facility
D684-10058-2 Rev. A May 15, 1997 Plume Impingement Heat Rate Report, Volume 2
D684-10058-03-01 Rev. Basic December 1997 Integrated ISS Thermal Math Models, Volume 3, Book 1
D684-10058-03-02 Rev. Basic October 1997 Integrated ISS Thermal Math Models, Volume 3, Book 2
D684-10058-03-03 Rev. Basic March 2005 Integrated ISS Thermal Math Models, Volume 3, Book 3
Meet or exceed All the documents identified below have undergone…
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