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Rigault RP.01B : ウィキペディア英語版 | Rigault RP.01B
The Rigault RP.01B was a French-built high-wing single-engined ultralight aircraft of the 1950s. ==Development==
The RP.01B was a one-off aircraft which was designed and built by Monsieur Paul Rigault at Mitry-Mory airfield to the NE of Paris.〔Butler, 1963, p. 113〕 The airfield now forms part of the site of Paris-Charles de Gaulle airport. The aircraft was fitted with high-set wings which were supported by twin struts, a fixed tailwheel undercarriage and a single seat for the pilot owner. It was powered by a nine-cylinder Salmson 9 ADB air-cooled radial engine. It was of conventional wooden construction with plywood and fabric-covered fuselage and fabric-covered wings and control surfaces.〔Green, 1965, p. 62〕
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「Rigault RP.01B」の詳細全文を読む
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