Regenerative and radiation cooling, transpiration or film cooling, ablation and inert or endothermic heat sink, used in selecting optimum spacecraft engine thrust chamber cooling techniques


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    Title :

    SELECTING A THRUST CHAMBER COOLING TECHNIQUE FOR SPACECRAFT ROCKET ENGINES


    Contributors:

    Publication date :

    1963-06-20


    Type of media :

    Preprint


    Type of material :

    No indication


    Language :

    English