The Margański & Mysłowski EM-10 Bielik (English: white-tailed eagle) is a low-cost Polish military training aircraft prototype, built by Margański & Mysłowski Zakłady Lotnicze, and first flown on 4 June 2003. The single-engine aircraft has a composite (mostly carbon fibre) fuselage with a light-alloy aft section, and the pressurized cockpit is fitted with ejection seats.
== Specifications (EM-10 prototype) == Data from Jane's all the World's Aircraft 2004-05:General characteristics Crew: 2 Length: 9.00 m (29 ft 6 in) Wingspan: 6.60 m (21 ft 8 in) Height: 2.50 m (8 ft 2 in) Wing area: 11.90 m2 (128.1 sq ft) Aspect ratio: 3.7 Empty weight: 1,700 kg (3,748 lb) Max takeoff weight: 2,500 kg (5,512 lb) Fuel capacity: 850 kg (1,870 lb) Powerplant: 1 × General Electric CJ610-6 turbojet, 13.5 kN (3,000 lbf) thrust prototype; production aircraft 12.75 to 17.65 kN (2,870 to 3,970 lbf) turbojet / turbofan Performance
Maximum speed: 1,100 km/h (680 mph, 590 kn) Maximum speed: Mach 0.9 Stall speed: 165 km/h (103 mph, 89 kn) Ferry range: 2,500 km (1,600 mi, 1,300 nmi) with auxiliary tanks Rate of climb: 45 m/s (8,900 ft/min) Wing loading: 210.1 kg/m2 (43.0 lb/sq ft)
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Margański EM-10 Bielik