Each of following flight phases, namely, launching, flight in space, re-entry, and final descent, must be considered when establishing need of attitude control for each type of vehicle such as ballistic missile, manned satellite, and hypersonic rocket boosted glider; factors to consider in obtaining attitude control and problems of re-entry.


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    Titel :

    Attitude control for space vehicles


    Weitere Titelangaben:

    Astronautics


    Beteiligte:
    George, M.B.T. (Autor:in)

    Erschienen in:

    Astronautics ; 4 , n 3


    Erscheinungsdatum :

    1959


    Format / Umfang :

    2 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Attitude Control of Flexible Space Vehicles

    GIACOMO PORCELLI | AIAA | 1972


    Optimal attitude control of space vehicles

    Foy, Jr., W.H. / Lefferts, E.J. | Engineering Index Backfile | 1962


    Attitude control system for space vehicles

    Haeussermann, W. | Engineering Index Backfile | 1959


    Reaction wheel attitude control for space vehicles

    Froelich, R.W. / Patapoff, H. | Engineering Index Backfile | 1959


    Reaction Wheel Attitude Control for Space Vehicles

    R. W. Froelich / H. Patapoff | NTIS | 1959