Background and development phases of single seat fighter, powered by single Pegasus engine which is basically Bristol Siddeley Orpheus turbojet driving 2-stage ducted fan; P.1127 has supersonic capability at height and is designed fatigue-wise to cope with exacting requirements of high subsonic speed low level role; characteristics of aircraft with respect to control system, height and position control, accelerating and decelerating transition, short takeoffs and landings, and pilot conversion.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Hawker P.1127 V/STOL strike fighter


    Weitere Titelangaben:

    Roy Aeronautical Soc -- J


    Beteiligte:
    Bedford, A.W. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1962


    Format / Umfang :

    8 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Hawker Siddeley P.1127 V/STOL Strike Reconnaissance Aircraft

    Crampton, J. / Lickley, R. L. | SAE Technical Papers | 1964


    Hawker-Siddeley P.1127 V/STOL. Strike reconnaissance aircraft

    Lickley, R.L. / Crampton, J. | Engineering Index Backfile | 1964


    The Hawker P.1127 and Kestrel

    Mason, Francis K. | TIBKAT | 1967


    Hawker P.1127/bristol siddeley Pegasus combination

    Frost, T.P. | Engineering Index Backfile | 1962


    The Hawker P. 1127/Bristol Siddeley Pegasus Combination

    Frost, T.P. | Emerald Group Publishing | 1962