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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    Title :

    Reaction control systems for V/STOL aircraft


    Additional title:

    SAE -- Paper


    Contributors:

    Conference:

    SAE Meeting ; 1965



    Publication date :

    1965


    Size :

    6 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English


    Keywords :


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