Margański & Mysłowski EM-10 Bielik
| EM-10 Bielik | |
|---|---|
| |
| EM-10 Bielik at Polish Aviation Museum | |
| Role | Training aircraft |
| National origin | Poland |
| Manufacturer | Margański & Mysłowski |
| Designer | Edward Margański |
| First flight | 4 June 2003 |
| Status | prototype |
| Number built | 1 |
The EM-10 Bielik (Template:Lang-en) 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 (620 mph, 540 kn)
- Stall speed: 155 km/h (96 mph, 84 kn)
- Range: 2,500 km (1,600 mi, 1,300 nmi)
- Rate of climb: 75 m/s (14,800 ft/min)
External links
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