The apparatus provides pitch, yaw and roll control for a rocket propelled missile. The propulsion system includes a thrust nozzle and a secondary injection thrust vector control system. A roll control capability is added to the secondary injection thrust vector control system. An arrangement is shown for deflecting the secondary jet by use of a tertiary injection system.


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    Titel :

    Tertiary Injector for Propulsion System Roll Control


    Beteiligte:
    B. A. Jones (Autor:in)

    Erscheinungsdatum :

    1966


    Format / Umfang :

    1 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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