Puneet Varma (Editor)

Margański and Mysłowski EM 10 Bielik

Updated on
Edit
Like
Comment
Share on FacebookTweet on TwitterShare on LinkedInShare on Reddit
Top speed
  
1,000 km/h

Length
  
9 m

First flight
  
June 4, 2003

Wingspan
  
6.6 m

Manufacturer
  
Margański & Mysłowski

Designer
  
Edward Margański

Margański & Mysłowski EM-10 Bielik Polot Edward Margaski EM10 Bielik

The EM-10 Bielik (English: white-tailed eagle) is a low cost Polish military training aircraft prototype, built by Margański & Mysłowski Zakłady Lotnicze, 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.

Margański & Mysłowski EM-10 Bielik Polot Edward Margaski EM10 Bielik

Specifications

General characteristics

Margański & Mysłowski EM-10 Bielik Polot Edward Margaski EM10 Bielik

  • 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)

    • Margański & Mysłowski EM-10 Bielik TheBlueprintscom Blueprints gt Modern airplanes gt Modern M

    Margański & Mysłowski EM-10 Bielik httpsuploadwikimediaorgwikipediacommonsthu

    Margański & Mysłowski EM-10 Bielik Marganski Myslowski EM10 Bielik Jet YouTube

    Margański & Mysłowski EM-10 Bielik EM10 Bielik YouTube

    References

    Margański & Mysłowski EM-10 Bielik Wikipedia
    (Text) CC BY-SA