Proposed method for accomplishing soft landings on moon is first to establish circumlunar orbit and then to transfer to lowest acceptable altitude by minimum-energy elliptical path; characteristic velocity increment for typical landing (starting from orbit) is 6880 fps; effects of trajectory errors and thrust level.


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    Titel :

    Some thrust and trajectory considerations for lunar landings


    Weitere Titelangaben:

    NASA -- Tech Note


    Beteiligte:
    Weber, R.J. (Autor:in) / Pauson, W.M. (Autor:in)


    Erscheinungsdatum :

    1959


    Format / Umfang :

    27 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Thrust vector orientation in pilot-controlled lunar landings.

    Barker, L. K. / Queijo, M. J. | NTRS | 1965


    Thrust Vector Orientation in Pilot-Controlled Lunar Landings

    L. KEITH BARKER AND M. J. QUEIJO | AIAA | 1965


    Descent trajectory optimization for soft lunar landings

    Mason, M. / Brainin, S.M. | Engineering Index Backfile | 1962


    Descent Trajectory Optimization for Soft Lunar Landings

    M. Mason / S. M. Brainin | NTIS | 1962


    Trajectory and rendezvous aspects of manned lunar landings

    Enderson, L. W., Jr. / Michael, W. H., Jr. | NTRS | 1964