A lightweight, flexible thermal micrometeoroid garment (TMG) design for enhanced space suit micrometeoroid/debris (M/D) protection is described. It will consist of an outer layer comprised of orthofabric, multilayers of aluminized Mylar, and a layer of silicone rubber loaded with micron sized particles of tungsten. The shield layers would fragment and/or vaporize the M/D projectile while the backup sheet would stop the resultant debris cloud.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Enhanced softgoods structures for spacesuit micrometeoroid/debris protective systems


    Contributors:

    Conference:

    SAE, International Conference on Environmental Systems ; 1992 ; Seattle, WA, United States


    Publication date :

    1992-07-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




    Enhanced Softgoods Structures for Spacesuit Micrometeriod/Debris Protective Systems

    Remington, Brian / Cadogan, David / Kosmo, Joseph | SAE Technical Papers | 1992



    Micrometeoroid and Orbital Debris Enhancements of Shuttle Extravehicular Mobility Unit Thermal Micrometeoroid Garment

    Cadogan, David / Graziosi, David / Zetune, David et al. | SAE Technical Papers | 2006


    Micrometeoroid/Space Debris Effects on Materials

    Zwiener, J. M. / Finckenor, M. M. / National Aeronautics and Space Administration | British Library Conference Proceedings | 1994