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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Variable-Area Rocket Nozzle


    Contributors:

    Publication date :

    1965


    Size :

    1 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Two Area Rocket Nozzle

    E. A. Pannella | NTIS | 1973


    Two Area Rocket Nozzle

    E. A. Panella | NTIS | 1973



    Rocket Nozzle System

    H. A. Krayenbuhl / G. Dolgonas / C. J. Rogers | NTIS | 1977


    Rocket nozzle development

    Bunting, D. | Engineering Index Backfile | 1962