• NASA HDBK 6024 : 2014

    Current The latest, up-to-date edition.

    SPACECRAFT POLYMERS ATOMIC OXYGEN DURABILITY HANDBOOK

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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)

    DOCUMENT HISTORY LOG
    FOREWORD
    1. SCOPE
    2. APPLICABLE DOCUMENTS
    3. ACRONYMS AND DEFINITIONS
    4. INTRODUCTION
    5. THE LEO ATOMIC OXYGEN ENVIRONMENT
    6. ATOMIC OXYGEN INTERACTION WITH MATERIALS
    7. ATOMIC OXYGEN EROSION YIELD
    8. MATERIALS INTERNATIONAL SPACE STATION
        EXPERIMENT
    9. MISSE 2 POLYMER EROSION AND CONTAMINATION
        EXPERIMENT POLYMERS
    10. CORRELATION OF GROUND-LABORATORY DATA TO
        IN-SPACE DATA
    11. ATOMIC OXYGEN EROSION YIELD PREDICTIVE TOOL
    12. ATOMIC OXYGEN EROSION YIELD VALUES FOR SIMPLE
        AND COMPOSITE MATERIALS
    13. SUMMARY AND CONCLUSIONS
    14. REFERENCES
    APPENDICES
    A - Authors and Acknowledgements
    B - MISSE 2 PEACE Polymers Experiment Atomic Oxygen Erosion
        Yield Error Analysis
    C - MISSE 2 PEACE Polymers Optical and Thermal Data
    D - Summary Pages for Individual MISSE 2 PEACE Polymers Flight
        Samples
    E - Lessons Learned from Atomic Oxygen Interaction with Spacecraft
        Materials in Low Earth Orbit
    F - Additional Reference Documents

    Abstract - (Show below) - (Hide below)

    Describes spacecraft designers with materials durability data for long-duration exposure to the low Earth orbit (LEO) atomic oxygen environment.

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    Document Type Standard
    Publisher National Aeronautics and Space Administration
    Status Current

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

    MIL-STD-1809 Base Document:1991 SPACE ENVIRONMENT FOR USAF SPACE VEHICLES
    ASTM E 595 : 2015 : REDLINE Standard Test Method for Total Mass Loss and Collected Volatile Condensable Materials from Outgassing in a Vacuum Environment
    ASTM E 2089 : 2015 : REDLINE Standard Practices for Ground Laboratory Atomic Oxygen Interaction Evaluation of Materials for Space Applications
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