Aero-Kros MP-02 Czajka
MP-02 Czajka | |
---|---|
Role | Ultralight aircraft |
National origin | Poland |
Manufacturer | Aero-Kros |
First flight | 2009 |
Introduction | 2009 |
Status | Under development |
Unit cost |
€65,500 (2011) |
The Aero-Kros MP-02 Czajka (English: Lapwing) is a Polish ultralight aircraft designed and produced by Aero-Kros of Krosno, introduced at the Aero show held in Friedrichshafen in 2009. The aircraft is supplied ready-to-fly.[1]
Design and development
The Czajka was designed to comply with the Fédération Aéronautique Internationale microlight rules and US light-sport aircraft rules. It features a cantilever high-wing, a two seats in side-by-side configuration enclosed cockpit, tricycle landing gear and a single engine in tractor configuration.[1]
The aircraft is made from carbon-fiber-reinforced polymer. Its 9.72 m (31.9 ft) span wing employs Fowler flaps to keep the stall speed low enough for the FAI microlight category. The standard engine provided is the 100 hp (75 kW) Rotax 912ULS four-stroke powerplant which gives a cruise speed of 230 km/h (143 mph). The cockpit is 1.215 m (48 in) wide.[1]
Specifications (MP-02)
Data from Bayerl[1]
General characteristics
- Crew: one
- Capacity: one passenger
- Wingspan: 9.72 m (31 ft 11 in)
- Wing area: 10.2 m2 (110 sq ft)
- Empty weight: 268 kg (591 lb)
- Gross weight: 472.5 kg (1,042 lb)
- Powerplant: 1 × Rotax 912ULS four cylinder, liquid and air-cooled, four stroke, 75 kW (101 hp)
Performance
- Maximum speed: 250 km/h (155 mph; 135 kn)
- Cruising speed: 230 km/h (143 mph; 124 kn)
- Stall speed: 65 km/h (40 mph; 35 kn)
- Rate of climb: 6.5 m/s (1,280 ft/min)
References
External links
Wikimedia Commons has media related to MP-02 Czajka. |