RU

/

EN
burger-menu

Поиск по сайту:

airplane photo

Страна : Великобритания

Год : 1980

(проект)

  • Мировая Авиация 170

    Hawker/BAe P.1214-3 - 1980 год. P.1214-3 предлагался в качестве замены СВВП семейства Harrier. Согласно расчетам, он должен был иметь лучшие характеристики на сверхзвуковых скоростях, улучшенные взлетно-посадочные характеристики и оснащаться современной авионикой. Была выбрана двухбалочная схема, а вот от применения КОС специалисты "BAe" почти сразу отказались - выгоды, получаемые от КОС, не стоили трудностей решения объема появляющихся при этом технических задач.
    This futuristic-looking "X-Wing" design, the P 1214, emerged from BAe's Kingston design office in 1982 when the company was studying supersonic STOVL projects.

  • Air International 1980-12 / R.Braybrook - Charting a course for V/STOL

    An artist's impression, prepared by Rolls-Royce Ltd, of a possible future supersonic V/STOL aircraft powered by a single augmented vectored-thrust engine. This engine would be derived from the Pegasus and would have a plenum chamber burning (PCB) thrust - augmentation system in the front nozzles and a single thrust vectoring rear tailpipe and nozzles.

  • Air International 1980-12 / R.Braybrook - Charting a course for V/STOL

    Another possible supersonic V/STOL layout, with a single intake, PCB and two thrust-vectoring nozzles.

  • Air International 1980-12 / R.Braybrook - Charting a course for V/STOL

    British Aerospace has been investigating a number of possible supersonic V/STOL configurations in the content of a Harrier successor for the RAF. This Kingston project is of similar layout to the aircraft shown in the artist's impression on the previous drawing.

  • Air International 1990-11 / Airdata File

    Models on the British Aerospace stand showed the Harrier III.

  • Aviation Historian 38 / G.Inchbald - Outside edge

    Outboard tailplanes were a feature of British Aerospace's 1982 P.1219 study, although the aim of the latter was to explore methods of saving weight, rather than incorporate advanced aerodynamic concepts.