A small experimental axial-flow turbojet engine in the 2,669-Newton (600-lbf) thrust class was designed, fabricated, and tested to demonstrate the feasibility of several low-cost concepts. Design simplicity was stressed in order to reduce the number of components and machining operations. Four engines were built and tested for a total of 157 hours. Engine testing was conducted at both sea-level static and simulated flight conditions for engine speeds as high as 38,000 rpm and turbine-inlet temperatures as high as 1,255 K (1,800 F).


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    Titel :

    Small, low-cost, expendable turbojet engine. 1: Design, fabrication, and preliminary testing


    Beteiligte:
    Dengler, R. P. (Autor:in) / Macioce, L. E. (Autor:in)

    Erscheinungsdatum :

    1976-05-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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