An escape system extraction rocket proposed for use on the Rotor Systems Research Aircraft was tested at Mach numbers of 0.1 and 0.3 through an angle of attack range from -2 deg to 102 deg and an angle of sideslip range from 0 deg to 15 deg in the Langley 7- by 10-foot high speed tunnel. The data are presented without analysis.


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    Titel :

    Longitudinal and Lateral-Directional Static Aerodynamic Characteristics of an Unpowered Escape System Extraction Rocket Model with Attached Launch Tubes


    Beteiligte:
    J. K. Huffman (Autor:in) / C. H. Fox (Autor:in) / R. E. Satterthwaite (Autor:in)

    Erscheinungsdatum :

    1977


    Format / Umfang :

    26 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch