A discussion of the thermal enviornments experienced by cryogenic propulsion vehicles is given. Various aspects of thermal protection systems for cryogenic propellant tanks are discussed including multilayer insulation schemes and solar shielding. The effects of propellant stratification and use of reliquefiers for stratification reduction systems, and initial propellant conditioning for cryogenic storage systems are briefly reviewed. (Author)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Cryogenic rocket propellants.

    Douglass, H. W. | NTRS | 1968


    Development Progress of MB-XX Cryogenic Upper Stage Rocket Engine

    Sack, William / Watanabe, Julie / Atsumi, Masahiro et al. | AIAA | 2003


    A single stage to orbit rocket with non-cryogenic propellants

    CLAPP, MITCHELL / HUNTER, MAXWELL | AIAA | 1993


    Cryogenic rocket propellants

    Douglass, H.W. | Engineering Index Backfile | 1968


    Cryogenic Rocket Engine Test

    Kitsche, W. | British Library Conference Proceedings | 2010