NASA JSC 29353 : 2014
Current
The latest, up-to-date edition.
FLAMMABILITY CONFIGURATION ANALYSIS FOR SPACECRAFT APPLICATIONS
Hardcopy , PDF
English
01-07-2014
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1.0 INTRODUCTION
2.0 TECHNICAL REQUIREMENTS
3.0 ENVIRONMENTS
4.0 FLAMMABILITY ASSESSMENT GUIDELINES
5.0 CONTAINERS
6.0 STOWED HARDWARE
7.0 FLAMMABILITY REDUCTION METHODS
8.0 TEST EXAMPLES
Appendices
Appendix A - Test References
Appendix B - Specification References
Appendix C - Definitions
Appendix D - Acronyms and Abbreviations
Appendix E - Flammability Rationale Codes
Helps International Space Station, and other program hardware customers with the flammability configuration analyses required to justify the use of flammable materials in flight hardware.
| DocumentType |
Standard
|
| Pages |
54
|
| PublisherName |
National Aeronautics and Space Administration
|
| Status |
Current
|
| Supersedes |
| NASA KSC DE 512-SM : 2012 | FACILITY SYSTEMS, GROUND SUPPORT SYSTEMS, AND GROUND SUPPORT EQUIPMENT GENERAL DESIGN REQUIREMENTS |
| NASA STD 6016 : 2016 | STANDARD MATERIALS AND PROCESSES REQUIREMENTS FOR SPACECRAFT |
| NASA STD 6001 : 2011 | FLAMMABILITY, OFFGASSING, AND COMPATIBILITY REQUIREMENTS AND TEST PROCEDURES |
| NASA JSC 27301 : 2009 | MATERIALS AND PROCESSES SELECTION, CONTROL, AND IMPLEMENTATION PLAN FOR JSC FLIGHT HARDWARE |
| NEMA WC 27500 : 2015 | STANDARD FOR AEROSPACE AND INDUSTRIAL ELECTRICAL CABLE |
| SAE AS22759C | Wire, Electrical, Fluoropolymer-Insulated, Copper or Copper Alloy |
| SAE AS81044A | Wire, Electrical, Crosslinked Polyalkene, Crosslinked Alkane-Imide Polymer, or Polyarlyene Insulated, Copper or Copper Alloy |
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