Results from wind tunnel tests to determine hypersonic aerodynamic heating rates on a NASA/Rockwell Space Shuttle Orbiter are reported. The tests were to determine Mach number effects, if any, and to obtain overall heating rate data at high Mach numbers from 10.5 to 16. The model used was a 0.0175-scale model built to Rockwell Orbiter lines VL70-000139. The model identity number is 29-0. These tests, designated OH11, were conducted in the AEDC Tunnel F. (Author)


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    Titel :

    Results of Tests of a Rockwell International Space Shuttle Orbiter (-139 Configuration) 0.0175-Scale Model (No. 29-0) in AEDC Tunnel F to Determine Hypersonic Heating Effects (OH11)


    Beteiligte:
    M. Quan (Autor:in)

    Erscheinungsdatum :

    1975


    Format / Umfang :

    103 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch