NASA JSC 29353 : 2014
Current
The latest, up-to-date edition.
FLAMMABILITY CONFIGURATION ANALYSIS FOR SPACECRAFT APPLICATIONS
Hardcopy , PDF
English
01-07-2014
Important note : Users cannot be edited or removed once added to your Multi user PDF.
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 AS 22759 : 2014 | WIRE, ELECTRICAL, FLUOROPOLYMER-INSULATED, COPPER OR COPPER ALLOY |
| SAE AS 81044 : 2011 | WIRE, ELECTRICAL, CROSSLINKED POLYALKENE, CROSSLINKED ALKANE-IMIDE POLYMER, OR POLYARLYENE INSULATED, COPPER OR COPPER ALLOY |
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