Liquid propellant rocket motor with max thrust of 2000 lb; fuel was mixture of 65% methyl alcohol and 35% water, while oxidizer was liquid oxygen; weight 215 lb; Snarler was intended for boosting climb on aircraft already powered by gas turbine and was flight tested during 1950 in "Hawker" P.1072 aircraft. (See also Brit Interplanetary Soc -- J v 14 n 1 Jan-Feb 1955 p 13-6)


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    Titel :

    Armstrong siddeley "snarler"


    Weitere Titelangaben:

    Engineering


    Beteiligte:
    Hurden, D. (Autor:in)

    Erschienen in:

    Engineering ; 179 , n 4650


    Erscheinungsdatum :

    1955


    Format / Umfang :

    3 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch




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