EXPERIMENTAL AVIATION “BERKUT”
STANDARD DATA: Gross wt. 2,000. Empty wt. 1,035. Fuel capacity 55. Engine 205-hp IO-36-B1A Lycoming. PERFORMANCE: Top mph 250. Cruise mph 220. Initial climb rate 2,000. Ceiling 29,500. Range 1,228. Takeoff distance 1,000. Landing distance 1,000. Since Burt Rutan made the advantages of a canard design configuration so apparent with his line of composite aircraft, […]