The Club ULM Rotor Ptenets-2 (Russian: Птенец-2, ) is a Russian ultralight aircraft, designed and produced by Club ULM Rotor of Kumertau, Bashkortostan. The aircraft is supplied complete and ready-to-fly.Bertrand, Noel; Rene Coulon; et al: World Directory of Leisure Aviation 2003-04, page 132. Pagefast Ltd, Lancaster UK, 2003. ISSN 1368-485XBayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 35. WDLA UK, Lancaster UK, 2011. ISSN 1368-485XTacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 38. Flying Pages Europe SARL, 2015.
Design and development The aircraft was designed to comply with the Fédération Aéronautique Internationale microlight rules. It features a strut-braced high-wing, a two-seats-in-side-by-side configuration enclosed cockpit, fixed tricycle landing gear and a single engine in pusher configuration.
The aircraft is made from aluminum tubing, with its flying surfaces covered in Dacron sailcloth. The fuselage is made from fibreglass. Its span wing has an area of . The tail is supported by four tubes that allow space for the pusher propeller. Standard engines available are the Rotax 503 and Rotax 582 two-strokes and the HKS 700E four-stroke powerplant.
Specifications (Ptenets-2)
References
External links Official website