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.


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    Titel :

    Cryogenic Boil-Off Reduction System Testing


    Beteiligte:

    Kongress:

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


    Erscheinungsdatum :

    28.07.2014


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




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    Cryogenic Boil-Off Reduction System Testing

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    Cryogenic Propellant Boil-Off Reduction Approaches

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