Guidance method is described for space vehicles that use atmospheric forces to permit maneuvers during ascent to orbit, ascend directly to orbital rendezvous, and perform hypersonic, in-atmosphere cruise before light-off of rocket-powered ascent to orbit; method can accept moving-rocket ignition point because place and time of rendezvous are not specified in advance but depend upon geocentric lead angle between vehicle and target at ignition.


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    Titel :

    Rendezvous guidance of lifting aerospace vehicles


    Weitere Titelangaben:

    J Spacecraft Rockets


    Beteiligte:
    Vaccaro, R.J. (Autor:in) / Kirby, M.J. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1965


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    Rendezvous guidance of lifting aerospace vehicles

    KIRBY, M. J. / VACCARO, R. J. | AIAA | 1965


    Rendezvous guidance of space vehicles

    Tschauner, J. / Hempel, P. | Engineering Index Backfile | 1964


    Rendezvous guidance

    Mcguire, Andrew T. | NTRS | 1990


    Rendezvous Guidance

    A. T. Mcguire | NTIS | 1990