Abstract The threshold values of the annual fluence of atomic oxygen (FAO ≈ $ 10^{20} $ $ cm^{−2} $), as well as the ratios of the energy-flux density of vacuum ultraviolet radiation of the solar spectrum to the flux density of atomic oxygen ($ Φ_{ν} $/$ Φ_{AO} $ ≈ 8 × $ 10^{−15} $ mJ) were determined, which are characterized the influence of the synergistic effect on the mass loss of Kapton-H, PM-A, and PM-1E polyimide films, which are spacecraft materials.


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    Title :

    The mass loss of spacecraft polyimide films under the action of atomic oxygen and vacuum ultraviolet radiation


    Contributors:

    Published in:

    Publication date :

    2014




    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English



    Classification :

    BKL:    55.60 Raumfahrttechnik / 39.00 Astronomie: Allgemeines / 50.93 Weltraumforschung
    Local classification TIB:    770/3520/8000



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    Effects of vacuum ultraviolet radiation on thin polyimide films

    Dever, J.A. / Messer, R. / Powers, C. et al. | Tema Archive | 2001



    Vacuum ultraviolet radiation/atomic oxygen synergism in materials reactivity

    Koontz, Steven / Leger, Lubert / Albyn, Keith et al. | NTRS | 1990


    Vacuum ultraviolet radiation/atomic oxygen synergism in materials reactivity

    KOONTZ, STEVEN / LEGER, LUBERT / ALBYN, KEITH et al. | AIAA | 1990