Study on 6-degree-of-freedom fixed base simulator of ability of human pilot to modify hyperbolic ballistic trajectories of vehicle approaching moon to establish circular orbit 50 mi above surface; by hodograph presentation of rate of descent and circumferential velocity, altimeter, and vehicle attitude and rate meters, pilots could consistently establish final altitude and velocity combinations for orbits 10 to 90 mi above surface.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Fixed-base-simulator study of ability of pilot to establish close orbits around moon


    Weitere Titelangaben:

    NASA -- Tech Note


    Beteiligte:
    Queijo, M.J. (Autor:in) / Riley, D.R. (Autor:in)


    Erscheinungsdatum :

    1961


    Format / Umfang :

    53 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :