Guepe - Design and Development

Design and Development

The aircraft was designed to comply with the Fédération Aéronautique Internationale microlight rules. It features a V-strut-braced high-wing, a two seats in tandem open cockpit, conventional landing gear and a single engine in pusher configuration.

The aircraft is made from bolted-together aluminum tubing, with a single tube serving as the keel tube. A small cockpit fairing and windshield are optional. Its 8.6 m (28.2 ft) span wing has an aluminium structure with its flying surfaces covered in doped aircraft fabric. Standard engines available are the 64 hp (48 kW) Rotax 582 two-stroke and the 60 hp (45 kW) HKS 700E four-stroke powerplant.

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