A design and analysis study was conducted to provide advanced engine descriptions and parametric data for space transfer vehicles. The study was based on an advanced oxygen/hydrogen engine in the 7,500 to 50,000 lbf thrust range. Emphasis was placed on defining requirements for high-performance engines capable of achieving reliable and versatile operation in a space environment. Four variations on the expander cycle were compared, and the advantages and disadvantages of each were assessed. Parametric weight, envelope, and performance data were generated over a range of 7,500 to 50,000 lb thrust and a wide range of chamber pressure and nozzle expansion ratio.


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    Titel :

    Advanced Engine Study Program


    Beteiligte:
    A. I. Masters (Autor:in) / D. E. Galler (Autor:in) / T. F. Denman (Autor:in) / R. A. Shied (Autor:in) / J. R. Black (Autor:in)

    Erscheinungsdatum :

    1993


    Format / Umfang :

    243 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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