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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    Titel :

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


    Beteiligte:
    R. W. Foster (Autor:in)

    Erscheinungsdatum :

    1992


    Format / Umfang :

    61 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch