The thrust and therefore the range of a solid propellant rocket missile is varied by expansion and contraction of the divergent portion of the missile nozzle. A thirty percent variation in thrust can be obtained by varying the area-ratio of the nozzle. A further control effect is obtained by venting the divergent section of the nozzle.


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    Titel :

    Variable-Area Rocket Nozzle


    Beteiligte:
    L. V. Divone (Autor:in)

    Erscheinungsdatum :

    1965


    Format / Umfang :

    1 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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