The Rensselaer RP-2 (for Rensselaer Polytechnic design 2) is an American mid-wing, single-seat glider that was designed by Steven J. Winckler and produced by the Rensselaer Polytechnic Institute of Troy, New York.[1][2]
| RP-2 | |
|---|---|
| Role | Glider Type of aircraft |
| National origin | United States |
| Manufacturer | Rensselaer Polytechnic Institute |
| Designer | Steven J. Winckler |
| First flight | 1985 |
| Status | Production completed |
| Number built | 1 |
The RP-2 was the second aircraft in Rensselaer's Composite Aircraft Program and first flew in 1985.[1]
The aircraft is of mixed construction, made from carbon-fiber-reinforced polymer, Kevlar and fiberglass. Its 44.25 ft (13.5 m) span wing employs a Boeing 80-163 airfoil and features split flaps. The aircraft weighs just 273 lb (124 kg) empty. The landing gear consists of a conventional glider-style monowheel. The aircraft achieved a 29:1 glide ratio.[1][3]
Initially registered with the Federal Aviation Administration in the Experimental - Amateur-built category, by August 2011 the sole RP-2 built had been removed from the registry.[2]
Data from Sailplane Directory[1]
General characteristics
Performance
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