The nozzle is for use with a missile or rocket motor. It controls the amount of thrust and the direction of thrust of the missile or rocket in flight. Two movable shrouds are used in the nozzle.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Variable Thrust and Variable Direction Nozzle


    Contributors:

    Publication date :

    1965


    Size :

    1 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    VARIABLE DIRECTION THRUST UNMANNED AERIAL VEHICLE

    BOEHNKE RYAN L | European Patent Office | 2016

    Free access

    Measuring in-flight thrust of variable nozzle jets

    Patton, R.J. | Engineering Index Backfile | 1960


    POWER PLANT WITH VARIABLE THRUST DIRECTION, AND AIRCRAFT

    HU HUAZHI / DING KAI | European Patent Office | 2024

    Free access

    Power device with variable thrust direction and aircraft

    HU HUAZHI / DING KAI | European Patent Office | 2023

    Free access

    Integrated thrust reverser actuator and variable area fan nozzle actuator

    JONES TEDDY L | European Patent Office | 2015

    Free access