Analysis is presented for optimization of space vehicle thrust program with prespecified directions of thrust and numerical comparison in vehicle performance between constant-attitude thrust program and optimum variable direction program by means of series of Earth-Mars rendezvous and flyby trajectories, using power-limited propulsion system; it is shown that constant-attitude thrust program with two or more optimized thrust directions is competitive in vehicle performance with variable direction program for interplanetary mission.


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    Titel :

    Constant-attitude thrust program optimization


    Weitere Titelangaben:

    AIAA J


    Beteiligte:

    Erschienen in:

    AIAA Journal ; 3 , n 8


    Erscheinungsdatum :

    1965


    Format / Umfang :

    4 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Constant-attitude thrust program optimization.

    Melbourne, W. G. / Sauer, C. G., Jr. | NTRS | 1965


    Constant-attitude thrust program optimization

    MELBOURNE, W. G. / SAUER, C. G. | AIAA | 1965


    CONSTANT ATTITUDE THRUST PROGRAM OPTIMIZATION

    Melbourne, W. G. / Sauer, C. G., Jr. | NTRS | 1963


    CONSTANT ATTITUDE THRUST PROGRAM OPTIMIZATION

    Melbourne, W. G. / Sauer, C. G., Jr. | NTRS | 1963


    CONSTANT ATTITUDE THRUST PROGRAM OPTIMIZATION

    MELBOURNE, W. / SAUE, C. | AIAA | 1963