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Max Holste MH.52 : ウィキペディア英語版 | Max Holste MH.52
The Max Holste MH.52 was a 1940s French-built two-seat touring or training monoplane designed and constructed by Avions Max Holste. ==Development and construction== Developed in the mid-1940s, the MH.52 was a low-wing cantilever monoplane with twin fins and rudders and a fixed tricycle landing gear. It had a cockpit with side-by-side seating for the pilot and trainee or passenger. The canopy was framed with forward-opening transparent sliding doors. The prototype first flew on 21 August 1945. The aircraft was powered by a variety of inline engines developing between 95 and 150 hp (71 to 112 kW).〔Simpson, 2005, p.158〕 A development of the MH.52 was the sole MH.53 Cadet which had a fixed tailwheel landing gear and a lower powered 135 hp (101 kW) de Havilland Gipsy Major 10 engine.〔Green, 1965, p.100〕
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「Max Holste MH.52」の詳細全文を読む
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