The purpose of this report is to present a test plan for thermodynamic heat transfer and pressure tests of a 9-percent Gemini B model in the hypervelocity impulse tunnel. The model will have interchangeable re-entry module-adapter interconnect fairings which will simulate the NASA Gemini and Gemini B configurations. (Author)


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    Titel :

    Test Plan for Aerodynamic Heating and Pressure Tests of a 9-Percent Gemini B Re-Entry Configuration Model in the McDonnell Hypervelocity Impulse Tunnel


    Beteiligte:
    M. A. Haefner (Autor:in)

    Erscheinungsdatum :

    1967


    Format / Umfang :

    31 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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