NASA’s Space Launch System (SLS) and Orion Crew Module have been studied in wind tunnels using the planar laser-induced fluorescence (PLIF) technique for flow visualization and quantitative thermometry and in flight using high-resolution imagery and quantitative infrared surface heating measurements. This paper reviews both types of measurements. OCIS codes: (120.1740) Combustion diagnostics; (300.2530) Fluorescence, laser-induced; (110.3080) Infrared imaging.


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    Titel :

    From Wind Tunnels to Flight Vehicles: Visualization and quantitative measurements supporting NASA’s space program


    Beteiligte:
    J. Inman (Autor:in) / P. Danehy (Autor:in) / R. Schwartz (Autor:in) / T. Horvath (Autor:in)

    Erscheinungsdatum :

    2020


    Format / Umfang :

    66 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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