Design requirements and operational constraints are reviewed for small manually controlled flying vehicle which could provide astronauts with mobility for lunar exploration; numerous flight trajectories and vehicle performance have been analyzed and are presented; it is concluded that to attain desired flight ranges, flight velocities must be relatively high (200 fps or more); range of thrust level required is determined; flyer configuration is highly dependent on method of control (either mechanical engine gimballing or kinesthetic control).


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    Titel :

    Manned lunar flying machines -- Operational characteristics


    Weitere Titelangaben:

    SAE -- Proc


    Beteiligte:

    Kongress:

    Proceedings of Space Technology Conference ; 1968 Lunar


    Erschienen in:

    Erscheinungsdatum :

    1968


    Format / Umfang :

    21 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Manned Lunar Flying Machines - Operational Characteristics

    Meyer, Andre J. / Kitchens, Marion D. | SAE Technical Papers | 1968


    Manned lunar flying machines - Operational characteristics.

    Kitchens, M. D., Jr. / Meyer, A. J., Jr. | NTRS | 1968


    Manned flying system for lunar exploration.

    Bradford, L. L. | NTRS | 1966


    Lunar dust/debris hazards associated with the manned flying system

    Bhalla, L. M. / Hsu, H. W. / Stark, R. L. et al. | NTRS | 1965


    Lunar Dust/Debris Hazards Associated with the Manned Flying System

    L. M. Bhalla / H. W. Hsu / R. L. Stark et al. | NTIS | 1965