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NPO Molniya Molniya-1 : ウィキペディア英語版
NPO Molniya Molniya-1

The Molniya-1 is a six-seater utility aircraft designed and built in Russia during the 1990s.
==Design and development==
The Molniya-1 six-seat aircraft is a three surface design with a forward balanced canard surface and a square section fuselage with a Vedeneyev M14P nine cylinder radial engine in the rear. Twin booms carry fins with balanced and trim tabbed rudders and a high set tailplane, similarly tabbed and balanced.
It was intended to cover a wide range of tasks including touring, cargo/mail carrying, business flights, aerial photography, patrol and air ambulance services. The three-surface configuration was intended to provide improved safety and fuel efficiency over conventional types, with the rear-mounted engine lowering cabin noise and vibration.〔(【引用サイトリンク】url=http://www.buran.ru/htm/mol-1.htm )〕 It flew for the first time on 18 December 1992.〔
A Westernised version with a Continental TSIO-550-B flat six engine and another, the Moliniya-3 with an Allison 250 turbopop, were proposed.〔 More broadly, the company were considering a number of larger types based on the three surface configuration.〔(【引用サイトリンク】url=http://www.buran.ru/htm/molniya9.htm )

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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