A method is described for forming the interior of a nozzle having uneven walls so that a throat of smooth converging and diverging sides is provided for passing flow. A metallic insert material is placed within the flow passageway adjacent to the area where the sharper throat constriction is to be formed, so that the material will flow through the inlet into the throat space when liquefied.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Method of Making a Rocket Nozzle


    Beteiligte:
    D. H. Campbell (Autor:in)

    Erscheinungsdatum :

    1966


    Format / Umfang :

    4 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Method of making a rocket nozzle

    Campbell, D. H. | NTRS | 1969



    Method of Making Rocket Motor Case with Integral Nozzle

    R. J. Thompson / O. C. Fruchtnicht | NTIS | 1982


    Rocket Nozzle System

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


    Rocket nozzle development

    Bunting, D. | Engineering Index Backfile | 1962