Moragon Stela
| Moragon Stela | |
|---|---|
| Role | Fixed-wing microlight aircraft |
| National origin | Spain |
| Manufacturer | Aeromoragon |
|
| |
The Moragon Stela is a Spanish two-seat fixed-wing microlight aircraft designed and built Aeromoragan based at Casarrubios del Monte, Spain.[1] The aircraft was supplied as complete or as a kit for amateur construction.[1]
The Stela is a two-seat side-by-side high-wing braced monoplane with a composite structure.[1] It has a fixed tricycle landing gear and can be powered by a 80 hp (60 kW) Jabiru 2200 engine or a Rotax 912 or 912S.[1]
Specifications
Data from [1]World Directory of Leisure Aviation 2005/2006
General characteristics
- Crew: 2
- Wingspan: 9.60 m (31 ft 6 in)
- Wing area: 12.04 m2 (129.6 sq ft)
- Empty weight: 260 kg (573 lb)
- Max takeoff weight: 450 kg (992 lb)
- Powerplant: 1 × Jabiru 2200 flat four piston engine, 60 kW (80 hp)
- Propellers: 2-bladed
Performance
- Maximum speed: 195 km/h (121 mph; 105 kn)
- Cruising speed: 175 km/h (109 mph; 94 kn)
- Minimum control speed: 63 km/h (39 mph; 34 kn)
- Rate of climb: 10 m/s (2,000 ft/min)
References
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