"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 Engineering v 182 n 4721 Aug 31 1956 p 281-2)


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    Titel :

    Rocket power plant


    Weitere Titelangaben:

    Engineer


    Erschienen in:

    Engineer ; 202 , n 5244


    Erscheinungsdatum :

    1956


    Format / Umfang :

    2 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch




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