EM-10 Bielik

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The EM-10 Bielik (English: White-tailed Eagle) is low cost Polish military training aircraft prototype, built by Margański & Mysłowski and first flown on 4 June 2003. The single engine aircraft had a composite (mostly carbon fibre) fuselage with a light alloy aft section. The pressurized cockpit had ejection seats.

Specifications

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)
Empty weight: 1,700 kg (3,748 lb)
Max takeoff weight: 2,500 kg (5,512 lb)
Powerplant: 1 × Single-shaft turbojet General Electric J85, 13.5 kN (3,000 lbf) thrust

Performance

Maximum speed: 1,000 km/h (621 mph; 540 kn)
Stall speed: 155 km/h (96 mph; 84 kn)
Range: 2,500 km (1,553 mi; 1,350 nmi)
Rate of climb: 75 m/s (14,800 ft/min)

External links

Wikimedia Commons has media related to EM-10 Bielik.

ZRPSL EM-10 Bielik data sheet at Flug Revue

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