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Focke-Achgelis Fa 225 : ウィキペディア英語版
Focke-Achgelis Fa 225

The Focke-Achgelis Fa 225 was an experimental single-seat rotary wing glider built in Germany by Focke-Achgelis in 1942. Only a single example was constructed.
==Design and development==
In the first half of the Second World War, the DFS 230B assault glider was used primarily to land troops and supplies, but was found of limited capability as it needed a relatively large landing area. The Fa 225 was conceived to marry the rotor of the Focke-Achgelis Fa 223 with the fuselage of the DFS 230B, allowing the glider to land in 18m or less.〔Lepage 2009, p.381〕 The rotor was mounted on a framework of struts above the centre of gravity and strengthened long stroke undercarriage units were fitted either side and at the tail.〔Green 2010, p.337〕
Towed behind a Junkers Ju 52/3m, Carl Bode piloted the Fa 225 on its first flight in 1943.〔Kay and Smith 2002, p.291〕 Construction of the aircraft only took seven weeks,〔http://www.luftarchiv.de/index.htm?/hubschrauber/fa225.htm〕 but series production was not proceeded with due to the relatively slow aero-towing speed and changes in operational doctrine.〔

抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)
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