Thermal protection systems for intermediate duration missions require use of radiation barriers such as superinsulation (multiple foil) or shadow shields; radiation barriers must be in vacuum environment to be effective, which makes them incompatible with operations within Earth's atmosphere; problems involved in applying both foil and shadow shields; weight estimates and experimental data indicate that foil outperforms all nonfoil insulations; shadow shield systems can be extremely light weight.


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    Titel :

    Lightweight thermal protection systems for space vehicle propellant tanks


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Knoll, R.H. (Autor:in) / Oglebay, J.C. (Autor:in)

    Kongress:

    SAE Meeting ; 1963 Insulation



    Erscheinungsdatum :

    1963


    Format / Umfang :

    16 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Lightweight Thermal Protection Systems for Space Vehicle Propellant Tanks

    Oglebay, Jon C. / Knoll, Richard H. | SAE Technical Papers | 1964


    Lightweight thermal protection systems for space vehicle propellant tanks

    Knoll, R.H. / Oglebay, J.C. | Engineering Index Backfile | 1965



    Analysis of thermal protection systems for space vehicle cryogenic propellant tanks

    Smolak, George R. ;Knoll, Richard H. ;Wallner, Lewis E. | SLUB | 1962


    Composite reinforced propellant tanks

    Brown, L. D. / Martin, M. J. / Aleck, B. J. et al. | NTRS | 1975