Configuration which employs winged payload and stabilizing fins at rear of booster will develop sizable rolling moments due to winds during ascent which exceed control authority of vehicle; analysis of modification of control system configuration to minimize rolling moments; summary of significant aspects of roll control problem.


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    Title :

    Roll control problem of finned rocket vehicles with winged payloads


    Additional title:

    Aerospace Eng


    Contributors:

    Published in:

    Aerospace Engineering ; 21 , n 11 ; p 58-59 + 83


    Publication date :

    1962


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English





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