Hypersonic vehicles are envisioned to require, in addition to carbon-carbon and ceramic-matrix composities for leading edges heated to above 2000 F, such 600 to 1800 F operating temperature materials as advanced Ti alloys, nickel aluminides, and metal-matrix composited; These possess the necessary low density and high strength and stiffness. The primary design drivers are maximum vehicle heating rate, total heat load, flight envelope, propulsion system type, mission life requirements and liquid hydrogen containment systems. Attention is presently given to aspects of these materials and structures requiring more intensive development.


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    Titel :

    Materials and structures for hypersonic vehicles


    Beteiligte:

    Kongress:

    Congress of the International Council of Aeronautical Sciences (ICAS) ; 1988 ; Jerusalem, Israel


    Erscheinungsdatum :

    1988-10-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Materials and Structures for Hypersonic Vehicles

    Darrel R Tenney / W Barry Lisagor / Sidney C Dixon | NTRS | 1989


    Materials and structures for hypersonic vehicles

    TENNEY, DARREL R. / LISAGOR, W. BARRY / DIXON, SIDNEY C. | AIAA | 1989


    Structures and materials for hypersonic vehicles

    Childers, M.G. | Engineering Index Backfile | 1966


    Materials and Structures for Hypersonic Vehicles

    D. R. Tenney / W. B. Lisagor / S. C. Dixon | NTIS | 1988


    Smart structures applications for hypersonic vehicles

    August, James A. / Joshi, Shiv P. | SPIE | 1996