Problems involved in safe recovery and landing of vehicle from satellite orbit or space mission; there are 2 principal methods of achieving recovery from satellite orbits -- (a) pure ballistic re-entry as typified by Mercury capsule, (b) glide re-entry in which aerodynamic lift provides maneuverability, and in which peak heating rates are less than in (a), but total heat load is greater due to longer time involved in re-entry maneuver; characteristics of lifting and nonlifting re-entry vehicles; lifting re-entry and heating characteristics; problem areas. Shortened version of paper "Re-Entry and Landing" presented before symposium held by Brit Interplanetary Soc, London Nov 13, 1963.


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    Titel :

    Re-entry problems


    Weitere Titelangaben:

    Flight


    Beteiligte:
    Crabtree, L.F. (Autor:in) / Peckham, D.H. (Autor:in)

    Erschienen in:

    Flight ; 84 , n 2858 ; p 1011-1012


    Erscheinungsdatum :

    1963


    Format / Umfang :

    2 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Problems of atmospheric entry

    Bobbitt, P. J. | NTRS | 1971



    Progress and problems in atmosphere entry

    Cohen, N. B. / Eggers, A. J., Jr. | NTRS | 1965


    Progress and problems in atmosphere entry

    Eggers, A. J., Jr. / Cohen, N. B. | NTRS | 1973


    Progress and problems in atmosphere entry.

    Cohen, N. B. / Eggers, A. J., Jr. | NTRS | 1966