Design and operation data on hypersonic research aircraft; details of vehicle and systems description, materials and fabrication, and substitution of XLR-11 engine; development of new turborocket engine, designated XLR-99; propellants are liquid oxygen and anhydrous ammonia supplied from gas pressurized tanks; engine is of variable thrust design capable of operating over range of 50 to 100% of full thrust. (p 12-13, 26, 28-30, 32, 34-36, 38)


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    Title :

    X-15


    Additional title:

    Aerospace Eng


    Contributors:

    Published in:

    Publication date :

    1961


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English