With demise of Dyna-Soar, research into re-entry vehicle configurations is concentrated on lifting body designs; under study at NASA are half-cone family of metal glider designs, M-2 and HL-10, M-1 and M-3; M-2 is round-bottom half-cone design, while HL-10 is flat-bottom half-cone; M-1 has 30° cone angle and makes use of inflatable afterbody; M-3 is hybrid, using lifting body combined with variable wing geometry; possible missions and military application.


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    Titel :

    Manned maneuverable reentry


    Weitere Titelangaben:

    Space/Aeronautics


    Beteiligte:
    Stambler, I. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1964


    Format / Umfang :

    9 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    Reentry control of a low-lift maneuverable spacecraft

    ROENNEKE, AXEL / WELL, KLAUS | AIAA | 1992


    Supercircular entry and recovery with maneuverable manned vehicles

    Smith, R.H. / Menard, J.A. | Engineering Index Backfile | 1961


    Trajectory control for a low-lift maneuverable reentry vehicle

    ROENNEKE, AXEL / CORNWELL, PHILLIP | AIAA | 1992