As for a fully reusable space transportation system of a single stage to orbit(SSTO) of horizontal take-off and landing type, experimental studies on low-speed aerodynamic characteristics have been done. The wind tunnel tests were conducted using NAL's gust wind tunnel. Six-component force and moment data were obtained over an angle of attack range from -14° to 44°. In this paper, the aerodynamic test results are presented for the low-speed aerodynamics of a generic SSTO configuration.


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    Titel :

    Experimental Studies on Aerodynamic Characteristics of SSTO Vehicle at Low Subsonic Speeds


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:

    Kongress:

    International Pacific Air & Space Technolgy Conference ; 1991



    Erscheinungsdatum :

    01.09.1991




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch






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