Studies are being conducted regarding new launch vehicle configurations which may effectively and economically share the delivery of payloads to orbit with the present Space Transportation System (STS). The role envisaged for these launch vehicles is related to the execution of missions whose requirements exceed the STS Shuttle capabilities, taking into account the delivery of much heavier or larger payloads. One class of advanced launch vehicles is configured to take advantage of the existing Shuttle hardware and facilities. Such vehicles are referred to as Shuttle Derived Vehicles (SDV). One version of an SDV consists of two STS elements, including the external tank (ET) and solid rocket boosters, and a cargo carrier. Attention is given to wind tunnel tests, which are being conducted with SDV sidemount configurations incorporating various size payload modules.


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    Titel :

    Shuttle derived launch vehicle wind tunnel tests


    Beteiligte:
    Tewell, J. R. (Autor:in) / Buell, D. N. (Autor:in)

    Erscheinungsdatum :

    1985-10-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Shuttle derived launch vehicle wind tunnel tests

    TEWELL, J. / BUELL, D. | AIAA | 1985



    Wind tunnel test evaluation of a Shuttle derived launch system

    Tewell, J. R. / Buell, D. N. | NTRS | 1986


    Shuttle Derived Launch Vehicle Concepts

    Rothschild, William / Boyd, Debra / Henderson, Edward | AIAA | 2005


    Shuttle Derived Launch Vehicle Concepts

    Rothschild, W. J. / Bailey, D. A. / Henderson, E. M. et al. | British Library Conference Proceedings | 2005