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Trio-Twister 103 : ウィキペディア英語版
Trio-Twister 103

The Trio-Twister 103 is an German powered parachute that was designed by Siegfried Stolle and produced by Trio-Twister of Eichwalde. 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 87. Pagefast Ltd, Lancaster UK, 2003. ISSN 1368-485X〕
The aircraft was introduced in 2003 and production ended when the company went out of business in 2005.〔(【引用サイトリンク】title=Internet Archive Wayback Machine )
==Design and development==
The Trio-Twister 103 was designed to comply with the Fédération Aéronautique Internationale microlight category and the U.S. FAR 103 Ultralight Vehicles rules, hence its designation. It carries a German DULV certification. It features a parachute-style wing, single-place accommodation, tricycle landing gear and one single cylinder, two-stroke, air-cooled Hirth F-33 aircraft engine mounted in pusher configuration.〔
The aircraft carriage is a simple frame design with a central canopy attachment, built from bolted aluminium tubing. In flight steering is accomplished via foot pedals that actuate the canopy brakes, creating roll and yaw. On the ground the aircraft has nosewheel steering. The main landing gear incorporates spring rod suspension. The design employs a tilting seat to allow the pilot to see up and backwards to ensure that canopy inflates correctly.〔
The aircraft has an empty weight of and a gross weight of , giving a useful load of . With full fuel of the payload for pilot and baggage is .〔




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「Trio-Twister 103」の詳細全文を読む



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