n 12 Dec 1967 p 429-32. Performance of rocket or missile is very sensitive to nozzle efficiency, increase of 1% yielding in some cases 100% increase in payload; concept of plug-type nozzle, in which expansion fan rather than gradual increase of passage area is employed to expand combustion products to supersonic velocity. n 1 Jan 1968 p 33-6. Characteristics of truncated plug, annular and throttleable plug nozzles were investigated at Von Karman Institute for Fluid Dynamics and at Centro Nazionale di Ricerca sulla Tecnologia della Propulsione e dei Materiali Relativi, Milano, Italy; evaluation of performance and results of tests. (v 9 n 12 Dec 1967 p 429-32)


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    Title :

    Experimental study on application of plug nozzles to solid-propellent rockets


    Additional title:

    Spaceflight


    Contributors:
    Casci, C. (author) / Gismondi, E. (author) / Angelino, G. (author)

    Published in:

    Spaceflight ; 10 , n 1


    Publication date :

    1967


    Size :

    4 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Liquid propellent sounding rockets for upper atmosphere research

    Hurden, D. | Engineering Index Backfile | 1963


    Solid Propellent Burning Rate Theory

    Gutman, V.R. | Emerald Group Publishing | 1960


    Use of solid propellent rocket motors for space application

    Morgan, F.C. / Trubridge, G.F.P. | Engineering Index Backfile | 1967


    High Temperature Propellent Reactions

    Osborne, F.E. | Emerald Group Publishing | 1952


    NOZZLES FOR LIQUID ROCKETS

    KOPITUK, RAYMOND C. | SAE Technical Papers | 1961