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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    Title :

    Applications Study for a High-Performance Cryogenic Aerospike Rocket Engine


    Contributors:
    M. Schneider (author) / F. B. Lary (author)

    Publication date :

    1967


    Size :

    409 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English