Study made of various propulsion and performance aspects of single-stage long range Mach 7 delta wing transport of 30,000 lb payload (125 passengers and cargo), encompasses consideration of propulsive performance of hypersonic ramjet design featuring lift augmentation; results indicate that 700,000-lb configuration could transport payload 3600 nautical mi with fuel reserve for descent and landing techniques similar to those presently used. (See also SAE -- Paper 427C for meeting Oct 9-13 1961 35 p)


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    Title :

    Feasibility of Mach 7 transport employing airbreathing propulsion systems


    Additional title:

    SAE -- J


    Contributors:


    Publication date :

    1961


    Size :

    7 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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