As the size of rocket engines increase and due to specialized thrust vector control problems, additional emphasis is being given on thrust vector control by other than conventional means. One of the more promising means of thrust vector control is through secondary injection of either liquid or gas into the engine exhaust nozzle.Freon has been found to be one of the more successfully used liquid injectants. In the case of hot gas these might be obtained from either direct engine bleed or from a secondary solid propellant control source. Due to the 6000 F temperatures in this section of the engine, specialized design features are required.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Rocket Engine Thrust Vector Control Operation Through Secondary Injection


    Additional title:

    Sae Technical Papers


    Contributors:

    Conference:

    SAE World Congress & Exhibition ; 1964



    Publication date :

    1964-01-01




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English





    Secondary Injection Thrust Vector Control

    C. A. Zimmerman / D. Starrett / J. M. Vellinga | NTIS | 1964


    Thrust vector control for hybrid propellants rocket engine with embedded fluid injection ports

    ELZEIN BACHAR / GAGNON MIGUEL / GOULET-BOURDON MAXIME | European Patent Office | 2024

    Free access

    THRUST VECTOR CONTROL FOR HYBRID PROPELLANTS ROCKET ENGINE WITH EMBEDDED FLUID INJECTION PORTS

    ELZEIN BACHAR / GAGNON MIGUEL / GOULET-BOURDON MAXIME | European Patent Office | 2025

    Free access