m (Remove some templates. interwiki links, delink non military terms, cleanup and move Wikipedia link above categories) |
m (→Specifications: Remove some templates. interwiki links, delink non military terms, cleanup and move Wikipedia link above categories) |
||
| Line 133: | Line 133: | ||
{{Aircontent| |
{{Aircontent| |
||
|related= |
|related= |
||
| + | |||
| − | |similar aircraft=<!-- similar or comparable aircraft --> |
||
|sequence= |
|sequence= |
||
| − | |lists=<!-- related lists --> |
||
| − | |see also=<!-- other relevant information --> |
||
}} |
}} |
||
| + | |||
==External links== |
==External links== |
||
{{Commons|EM-10 Bielik}} |
{{Commons|EM-10 Bielik}} |
||
Revision as of 19:25, 11 December 2014
| 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 (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. |
The original article can be found at EM-10 Bielik and the edit history here.