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Lockspeiser LDA-01 : ウィキペディア英語版 | Lockspeiser LDA-01
The Lockspeiser LDA-01 ("Land Development Aircraft") was a British seven-tenths scale research and development tandem wing aircraft, which was designed and built by David Lockspeiser to prove a concept for a low-cost utility transport. ==Design and development== The LDA-01 was a single-seat canard monoplane, fabric covered with metal construction. It had a canard foreplane which was the same size as each mainplane. The wing was mounted at the rear-end of the box structure fuselage which was fitted with a four wheeled landing gear. It was designed to be fitted with a detachable payload container to allow easy conversion between roles, and was powered by a rear-mounted pusher engine. The LDA-01 ''G-AVOR'' first flew on 24 August 1971 at Wisley in Surrey, under the power of an 85 hp (63 kW) Continental C85 piston engine, but was later refitted with a more powerful Lycoming O-320 engine. The aircraft (which by this time had been re-registered ''G-UTIL''), and had been renamed the Boxer 500, was being modified to planned production configuration by Brooklands Aerospace at Old Sarum Airfield when it was destroyed in a fire on 16 January 1987.〔Walters ''Air International'' August 1991, pp. 71–72.〕
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「Lockspeiser LDA-01」の詳細全文を読む
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