"Screamer" rocket engine is readily started, stopped and controlled, one combustion chamber only being employed; unusual features are throatless chamber and tri-propellant system -- fuel, oxidant, and coolant, developed by Armstrong Siddeley. (See also Engineer v 202 n 5244 July 27 1956 p 117-8)


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Rocket power plant


    Additional title:

    Engineering


    Published in:

    Engineering ; 182 , n 4721


    Publication date :

    1956


    Size :

    2 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




    Rocket power plant

    Engineering Index Backfile | 1956


    Use of diffusers to test rocket power plant

    Massier, P.F. / Roschke, E.J. | Engineering Index Backfile | 1962


    Sea Dragon Concept (Liquid Rocket Plant)

    Aerojet General Corporation | NTRS | 1963


    Rocket power for helicopters

    Bergaust, E. | Engineering Index Backfile | 1955


    Rocket and Jet Power

    I. Bjoerk / A. Hjertstrand / T. Marklund | NTIS | 1969