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


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    Titel :

    Reaction control systems for V/STOL aircraft


    Weitere Titelangaben:

    SAE -- Paper


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

    Kongress:

    SAE Meeting ; 1965



    Erscheinungsdatum :

    1965


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Reaction Control Systems for V/STOL Aircraft

    Thames, W. K. | SAE Technical Papers | 1965


    Reaction control system augmentation for V/STOL aircraft

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


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