Extensively axisymmetric and non-axisymmetric Single Stage To Orbit (SSTO) vehicles are considered. The information is presented in viewgraph form and the following topics are presented: payload comparisons; payload as a percent of dry weight - a system hardware cost indicator; life cycle cost estimations; operations and support costs estimation; selected engine type; and rocket engine specific impulse calculation.


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    Title :

    Review of Findings of a Study of Rocket Based Combined Cycle Engines Applied to Extensively Axisymmetric Single Stage to Orbit Vehicles


    Contributors:

    Publication date :

    1992


    Size :

    61 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English