The DARPA/Air Force Falcon program is planning to flight test several hypersonic technology vehicles (HTV) in the next several years. A Materials Integrated Product Team (MIPT) was formed to lead the development of key thermal protection system (TPS) and hot structures technologies. The technologies being addressed by the MIPT are in the following areas: 1) less than 3000 F leading edges, 2) greater than 3000 F refractory composite materials, 3) high temperature multi-layer insulation, 4) acreage TPS, and 5) high temperature seals. Technologies being developed in each of these areas are discussed in this paper.


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    Titel :

    Materials Development for Hypersonic Flight Vehicles


    Beteiligte:
    Glass, David E. (Autor:in) / Dirling, Ray (Autor:in) / Croop, Harold (Autor:in) / Fry, Timothy J. (Autor:in) / Frank, Geoffrey J. (Autor:in)

    Kongress:

    14th AIAA/AHI International Space Planes and Hypersonics Systems and Technologies Conference ; 2006 ; Canberra, Australia


    Erscheinungsdatum :

    01.01.2006


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Materials Development for Hypersonic Flight Vehicles

    Glass, David / Dirling, Ray / Croop, Harold et al. | AIAA | 2006


    Materials requirements of hypersonic flight vehicles

    Pellini, W.S. | Engineering Index Backfile | 1960



    Aeroelastic Simulation of Hypersonic Flight Vehicles

    Gupta, K. K. / Voelker, L. S. | AIAA | 2012


    MHD flight control for hypersonic vehicles

    Robinson, Wesley / Gerwin, Richard | AIAA | 2001