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Tri-R KIS TR-1
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Tri-R KIS TR-1 : ウィキペディア英語版
Tri-R KIS TR-1

The Tri-R KIS TR-1 is an American homebuilt aircraft that was designed by Rich Trickel and produced by Tri-R Technologies of Oxnard, California, introduced in the 1990s. When it was available the aircraft was supplied as a kit for amateur construction.〔Purdy, Don: ''AeroCrafter - Homebuilt Aircraft Sourcebook, Fifth Edition'', page 277. BAI Communications, 15 July 1998. ISBN 0-9636409-4-1〕
==Design and development==
Trickel's main business was High Tech Composites, a company that produced many airframe components under sub-contract for kit aircraft such as the Lancair 235, Lancair 320 and Lancair IV. Trickel originally drew a new aircraft as a set of three-views for a customer in Australia who was looking for a new, conventional aircraft concept. The customer liked the design, but never paid for the drawings, so Trickel brought them home and completed the design work himself. Eventually the new design became the KIS TR-1.〔
The KIS TR-1 features a cantilever low-wing, a two-seats-in-side-by-side configuration enclosed cockpit accessed via gull-wing doors, fixed tricycle landing gear or optionally conventional landing gear with wheel pants and a single engine in tractor configuration.〔
The aircraft is made from composites. Its span rectangular wing employs a NACA 63-215 airfoil, mounts flaps and has a wing area of . The acceptable power range is and the standard engines used are the Continental O-240, the Lycoming O-235-C1B or the Limbach L2000 powerplant.〔
The KIS TR-1 has a typical empty weight of and a gross weight of , giving a useful load of . With full fuel of the payload for the pilot, passenger and baggage is .〔
The standard day, sea level, no wind, take off with a engine is and the landing roll is .〔
The manufacturer estimated the construction time from the supplied kit as 1000 hours.〔


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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