This report presents application data for an advanced aerospike rocket engine utilizing LO2/LH2 propellants. The engine concept was applied to six different stage configurations defined by the Air Force to represent the diversity of potential applications; six vehicles were defined at 250K vacuum thrust level and six defined at a 350K level. A common engine module is defined for the six vehicle cases at each thrust level. (Author)


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    Titel :

    Applications Study for a High-Performance Cryogenic Aerospike Rocket Engine


    Beteiligte:
    M. Schneider (Autor:in) / F. B. Lary (Autor:in)

    Erscheinungsdatum :

    1967


    Format / Umfang :

    409 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch