Skopiński Puma
| Puma | |
|---|---|
 | |
| Role | ultralight |
| Manufacturer | Aero-service Jacek Skopiński |
| Designer | Jan Fiala |
| Produced | 2010- |
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The Puma is a two-seater ultralight manufactured by Aero-service Jacek Skopiński.
Design
The Puma is a single engine, two-seater, low-wing ultralight with classically arranged tail and tricycle retractable landing gear. The trapezoidal wing has one main and one secondary spar. The aircraft can be fitted with the Rotax 912 or Rotax 914 engine.
Specifications
General characteristics
- Length: 6.27 m (20 ft 7 in)
- Wingspan: 9.15 m (30 ft 0 in)
- Height: 2.3 m (7 ft 7 in)
- Wing area: 11.3 m2 (122 sq ft)
- Airfoil: root:NACA 4415 tip:NACA 4412
- Empty weight: 290 kg (639 lb)
- Gross weight: 472.5 kg (1,042 lb)
- Fuel capacity: 100 l (22.00 imp gal; 26.42 US gal) in two tanks
- Powerplant: 1 × Rotax 912 4-cyl. air-cooled horizontally-opposed piston engine
Performance
- Maximum speed: 270 km/h (168 mph; 146 kn)
- Cruising speed: 240 km/h (149 mph; 130 kn)
- Stall speed: 61 km/h (38 mph; 33 kn) with flaps
- Range: 1,200 km (746 mi; 648 nmi) 45 minutes reserve
- Service ceiling: 3,650 m (11,975 ft)
- g limits: +4 -2
- Rate of climb: 8 m/s (1,600 ft/min)
See also
External links
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