The integrated space shuttle vehicle was tested to determine proximity force and moment data for the orbiter/external tank and solid rocket booster (SRB) with and without separation rockets firing for both single and dual booster runs. Data were obtained at points t = 0 sec, t = 1.25 sec, and t = 2 sec on the nominal SRB separation trajectory.


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    Titel :

    Aerodynamic results of wind tunnel separation tests on a 0.01-scale model (32-OTS) space shuttle integrated vehicle in the AEDC-VKF-SWTA (IA57)


    Beteiligte:
    Daileda, J. J. (Autor:in)

    Erscheinungsdatum :

    1974-11-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch