A thruster nozzle (24) includes a throat (28) and a nozzle end portion (30) that is integral with the throat. The nozzle end portion includes an outer wall (32) that has a plurality of circumferentially-disposed nozzle features or connectors (34). A brace (26) may be disposed at least partially around the thruster nozzle and mated with the nozzle features to restrict relative movement between the thruster nozzle and the brace. The brace may be attached with a vehicle body (22) of a vehicle.


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    Titel :

    Rocket thruster nozzle with connectors and brace


    Beteiligte:

    Erscheinungsdatum :

    05.05.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F02K JET-PROPULSION PLANTS , Strahltriebwerke / B64G Raumfahrt , COSMONAUTICS



    Performance of high-area-ratio nozzle for a small rocket thruster

    Kushida, Raymond / Hermel, Jerry / Apfel, Steve et al. | NTRS | 1987


    Performance of high-area-ratio nozzle for a small rocket thruster

    KUSHIDA, RAYMOND / HERMEL, JERRY / APFEL, STEVE et al. | AIAA | 1987



    Laser-Heated Rocket Thruster

    J. M. Shoji | NTIS | 1977


    Laser-heated rocket thruster

    Shoji, J. M. | NTRS | 1977