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Dale Weejet 800 : ウィキペディア英語版 | Dale Weejet 800
The Dale Weejet 800'', or Weejet VT-1 was an early light jet intended for high-speed personal transport or primary military training.〔(【引用サイトリンク】url=http://www.airspacemag.com/history-of-flight/personal_jets.html )〕 ==Design and development== Harold Dale, an engineer at North American Aviation who had designed several homebuilt aircraft, teamed up with Edward Gagnier, a former North American engineer, to develop the Weejet. The name was registered in February 1952 and the prototype was built in 2 1/2 years.〔(【引用サイトリンク】url=http://machdiamonds.com/weejet.html )〕 The Weejet was a two seat side-by-side, mid-winged all-aluminum, retractable tricycle gear aircraft with a V-tail arrangement. The aircraft was powered by a 920lb thrust Continental-Turbomeca Marbore II J-69-T-15 engine. Air was fed to the engine through two triangular inlets mounted on the inboard wing roots. Fuel was carried in the leading edge of the wings, and tip tanks. The aircraft had oxygen tanks and was pressurized to 3 psi differential pressure. The seats were designed to accommodate parachutes. The rudder pedals were adjustable for different pilot heights.
抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)』 ■ウィキペディアで「Dale Weejet 800」の詳細全文を読む
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