Results are presented from a wind-tunnel investigation of the flow field around a 0.45-scale model of a Mars lander. The tests were conducted in air at values of Reynolds number equivalent to those anticieffects of Reynolds number equivalent to those anticipated on Mars. The effects of Reynolds number, model orientation with respect to the airstream, and the position of a dish-type antenna on the flow field were determined. An appendix is included which describes the calibration and operational characteristics of hot-film anemometers under simulated Mars surface conditions. (Author)


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    Titel :

    Flow Field Measurements around a MARS Lander Model Using Hot Film Anemometers under Simulated MARS Surface Conditions


    Beteiligte:
    G. C. Greene (Autor:in) / L. S. Keafer (Autor:in) / C. G. Marple (Autor:in) / J. T. Foughner (Autor:in)

    Erscheinungsdatum :

    1972


    Format / Umfang :

    132 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch