Solid propellant vehicle to perform probe, re-entry, and orbital research missions may be ground launched or given initial boost by first stage using fin configuration to provide stability; tests to determine effects of fin area, antennas and wiring tunnels on stability at Mach 2.29, 2.96, 3.96, and 4.65 and Re of 3.5×106/ft.


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    Titel :

    Investigation of static longitudinal and lateral stability characteristics of 0.10-scale model of three-stage configuration of scout research vehicle at Mach numbers of 2.29, 2.96, 3.96, and 4.65


    Weitere Titelangaben:

    NASA -- Tech Note


    Beteiligte:
    Jernell, L.S. (Autor:in)


    Erscheinungsdatum :

    1961


    Format / Umfang :

    27 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :