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  • NASA JSC 29353 : 2014

    Current The latest, up-to-date edition.

    FLAMMABILITY CONFIGURATION ANALYSIS FOR SPACECRAFT APPLICATIONS

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    Published date:  01-01-2014

    Publisher:  National Aeronautics and Space Administration

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    Table of Contents - (Show below) - (Hide below)

    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

    Abstract - (Show below) - (Hide below)

    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.

    General Product Information - (Show below) - (Hide below)

    Document Type Standard
    Publisher National Aeronautics and Space Administration
    Status Current

    Standards Referenced By This Book - (Show below) - (Hide below)

    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

    Standards Referencing This Book - (Show below) - (Hide below)

    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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