The Cryogenic Boil-Off Reduction System was tested with LH2 and LOX in a vacuum chamber to simulate space vacuum and the temperatures of low Earth orbit. Testing was successful and results validated the scaling study model that predicts active cooling reduces upper stage cryogenic propulsion mass for loiter periods greater than 2 weeks.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Cryogenic Boil-Off Reduction System Testing


    Contributors:

    Conference:

    AIAA/ASME/SAE/ASEE Joint Propulsion Conference ; 2014 ; Cleveland, OH, United States


    Publication date :

    2014-07-28


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




    Cryogenic Boil-Off Reduction System Testing

    W. D. Plachta / L. W. Johnson / J. Feller | NTIS | 2014


    Cryogenic Boil-Off Reduction System Testing

    Plachta, David W. / Johnson, Wesley L. / Feller, Jeffrey R. | NTRS | 2014


    Cryogenic Boil-Off Reduction System Testing

    W. D. Plachta / L. W. Johnson / R. J. Feller | NTIS | 2014


    Cryogenic Propellant Boil-Off Reduction Approaches

    Nast, Ted / Frank, David / Burns, K. | AIAA | 2011


    CRYOGENIC PROPELLANT BOIL-OFF REDUCTION APPROACHES

    Nast, T. / Frank, D. / Burns, K. et al. | British Library Conference Proceedings | 2011