Most distinctive feature of any project analysis of vehicle designed to carry man into orbit in space and return him, is need to limit accelerations and retardations of his passage, and temperature of his environment; reentry may be effected, using glider (using aerodynamic lift), or by relying on aerodynamic drag alone, i.e. parachute reentry; some tentative weight assessments are made of glider suggested. (See also - discussion p 528-30)


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    Titel :

    Aerodynamic problems of manned space vehicles


    Weitere Titelangaben:

    Roy Aeronautical Soc -- J


    Beteiligte:

    Erschienen in:

    Erscheinungsdatum :

    1959


    Format / Umfang :

    8 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Shielding Problems in Manned Space Vehicles

    C. W. Hill / W. M. Schofield / E. C. Smith | NTIS | 1962


    Shielding problems in manned space vehicles

    Hill, C. W. / Schofield, W. M. / Smith, E. C. | NTRS | 1962


    Computer programs for shielding problems in manned space vehicles

    Douglass, C. C., Jr. / Hill, C. W. / Ritchie, W. B. et al. | NTRS | 1964


    Manned maintenance of space vehicles

    Powe, W.E. / Bailey, W.E. | Engineering Index Backfile | 1963


    Operational problems of manned orbital vehicles

    Bellman, D. R. / Drake, H. M. / Walker, J. A. | NTRS | 1958