FLAMMABILITY CONFIGURATION ANALYSIS FOR SPACECRAFT APPLICATIONS

Published date

01-01-2014

Publisher

National Aeronautics and Space Administration

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
PublisherName	National Aeronautics and Space Administration
Status	Current

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

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