The patent application describes a method of making a rocket motor case with an integral nozzle in which the rocket motor has a large length to diameter ratio and is made by applying a linear wrap of fibers as a first layer on a mandrel and then by applying radial wraps over said linear wrap and also conforming the linear fibers to the shape of the nozzle after applying the linear fibers on said mandrel to provide a structure that has sufficient stiffness to accomplish the desired result of a large length to diameter rocket motor case.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Method of Making Rocket Motor Case with Integral Nozzle


    Beteiligte:

    Erscheinungsdatum :

    1982


    Format / Umfang :

    12 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    INTEGRAL COMPOSITE ROCKET MOTOR DOME/NOZZLE STRUCTURE

    FACCIANO ANDREW B / MOORE ROBERT T / SINNOCK KELLY J et al. | Europäisches Patentamt | 2018

    Freier Zugriff

    Method of making a rocket nozzle

    Campbell, D. H. | NTRS | 1969



    Method of Making a Rocket Nozzle

    D. H. Campbell | NTIS | 1966