Army (TRECOM) sponsored V/STOL research program is designed to demonstrate performance of V/STOL gas coupled, lift fan system and its compatibility with high subsonic speed aircraft; XV-5A design gross weight of 9200 lb was established to permit vertical takeoff at 95 F. 2500 ft altitude, control powers reserved, with lift-to-weight ratio of 1.05; propulsion system, designated X353-5 V/STOL system, consists of 2 gas generators, diverter valves, wing lift fans, and one nose lift pitch control fan; aircraft configuration tail design, and fuselage; performance and design development testing.


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    Titel :

    Army XV-5A lift fan flight research airplane


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Morgan, W.R. (Autor:in) / True, H.C. (Autor:in) / Starkey, H.B. (Autor:in)

    Kongress:

    SAE Meeting ; 1964 VTOL-STOL



    Erscheinungsdatum :

    1964


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :