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Wrobel Vroby 2
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Wrobel Vroby 2 : ウィキペディア英語版
Wrobel Vroby 2

The Wrobel Vroby 2 is a French powered parachute that was designed by Gerard Wrobel and produced by Wrobel of Beynes, Alpes-de-Haute-Provence. Now out of production, when it was available the aircraft was supplied as a complete ready-to-fly-aircraft.〔Bertrand, Noel; Rene Coulon; et al: ''World Directory of Leisure Aviation 2003-04'', page 88. Pagefast Ltd, Lancaster UK, 2003. ISSN 1368-485X〕
==Design and development==
The Vroby 2 was designed to comply with the Fédération Aéronautique Internationale microlight category, including the category's maximum gross weight of . The aircraft has a maximum gross weight of . It features a parachute-style wing, two-seats-in-tandem accommodation in an open-frame structure, tricycle landing gear and a single cylinder Zanzottera MZ 34 engine in pusher configuration.〔
The aircraft carriage is built from 4130 steel tubing. In flight steering is accomplished via handles that actuate the canopy brakes, creating roll and yaw. On the ground the aircraft has lever-controlled nosewheel steering. The main landing gear incorporates triangulated spring rod suspension.〔
The aircraft has an empty weight of and a gross weight of , giving a useful load of . With full fuel of the payload for crew and baggage is .〔
Reviewer Jean-Pierre le Camus, writing in 2003, described the design as "carefully constructed".〔




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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