Integrated pulse modulated rocket chamber design with 60 lb thrust using nitrogen tetroxide and hydrazine mixture


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    Title :

    Design and development of an integrated pulse modulated sixty pound thrust chamber Final report


    Contributors:
    Berst, J. A. (author) / Mudryk, M. (author)

    Publication date :

    1963-04-24


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English