A reaction control system is defined in terms of the source of power available, the working fluid of the system, the delivery system, the thrust producing devices and their point of application -- the control point.The relationship of the propulsion and reaction control systems are identified as independent, partly dependent, and interdependent. Geometric configurations for reaction control systems are presented along with the classifications of the power source.Results of a sample reaction control systems analysis are presented showing the progressive systems comparison with respect to the impact on the total system weight (includes the propulsion and the reaction control system).


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    Titel :

    Reaction Control Systems for V/STOL Aircraft


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Thames, W. K. (Autor:in)

    Kongress:

    Aeronautic and Space Engineering and Manufacturing Meeting ; 1965



    Erscheinungsdatum :

    01.02.1965




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Reaction control systems for V/STOL aircraft

    Thames, W.K. | Engineering Index Backfile | 1965


    Reaction control system augmentation for V/STOL aircraft

    Streiff, H. G. / Donham, R. E. | NTRS | 1979


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