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Messerschmitt Bf 163 : ウィキペディア英語版 | Messerschmitt Bf 163
The Messerschmitt Bf 163 was a STOL aircraft designed by BFW and built by Weserflug before World War II. == Design and development ==
During the autumn of 1935, the considerable potential of the Fieseler Fi 156 project for the tasks of short range reconnaissance and aerial observation had prompted the RLM to draw up a requirement for an army co-operation and observation aircraft with its performance parameters. The requirement stipulated the use of the Argus As 10 or the Hirth HM 508 engine and placed emphasis on short field performance, maximum possible all-round view for the two crew members, and a wide range of speed. It was intended that the resultant aircraft, which the Siebel Si 201 was also designed to compete for, would be evaluated in competition with the Fi 156. The Bf 163 followed closely the formula established by the Fi 156 in being a high-wing braced monoplane with a metal structure, automatic leading edge wing slots, double slotted flaps, and an exceptionally tall undercarriage. The aircraft's most interesting feature was the provision for varying the incidence of the entire wing which swivelled on its mainspar, the bracing struts being attached to the fuselage by ball joints and changing their angle with movement of the wing. Construction of the sole prototype was entrusted to Weserflug, though due to its origin with the ''Bayerische Flugzeugwerke'' before mid-July 1938, it retained the ''Bf'' RLM prefix for the earlier firm.
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「Messerschmitt Bf 163」の詳細全文を読む
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