Design requirements of aircraft capable of exploring problems of hypersonic speed and space flight; development of turbo-rocket engine, XLR99; propellants are liquid oxygen and anhydrous ammonia supplied from gas-pressurized tanks; engine is of variable-thrust design operating over range of 50 to 100% of full thrust; description of various systems, materials and fabrication; flight demonstration and current status.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Design and operation of X-15 hypersonic research airplane


    Weitere Titelangaben:

    AGARD -- Report


    Beteiligte:

    Erschienen in:

    Erscheinungsdatum :

    1960


    Format / Umfang :

    31 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Structural Design for a Hypersonic Research Airplane

    L. Robert Jackson / Allan H. Taylor | AIAA | 1978


    Scramjet integration on hypersonic research airplane concepts

    Weidner, J. P. / Small, W. J. / Penland, J. A. | NTRS | 1976


    Propulsion Options for the Hypersonic Research Airplane

    Verle V. Van Camp / E.T. Williams | AIAA | 1975


    Heat-Sink Structural Design Concepts for a Hypersonic Research Airplane

    Allan H. Taylor / L. Robert Jackson | AIAA | 1978