Colyaer Martin3 S100
The Colyaer Martin3 S100 is a Spanish ultralight aircraft, designed and produced by Colyaer of Portonovo.[1][2]
Design and development
The aircraft was designed to comply with the Fédération Aéronautique Internationale microlight rules. It features a cantilever high-wing, a two-seats-in-side-by-side configuration enclosed cockpit, fixed tricycle landing gear and a single engine in pusher configuration.[1][2]
The aircraft is made from composites. Its 12.4 m (40.7 ft) span wing has an area of 12.0 m2 (129 sq ft) and flaps that can be deployed for landing and reflexed for cruise flight. The long wingspan gives the Martin3 a glide ratio of 23:1 and allows power-off soaring flights. The standard engine is the 100 hp (75 kW) Rotax 912ULS four-stroke powerplant.[1][2]
Specifications (Martin3 S100)
Data from Bayerl[1]
General characteristics
- Crew: one
- Capacity: one passenger
- Wingspan: 12.4 m (40 ft 8 in)
- Wing area: 12.0 m2 (129 sq ft)
- Empty weight: 280 kg (617 lb)
- Gross weight: 450 kg (992 lb)
- Fuel capacity: 140 litres (31 imp gal; 37 US gal)
- Powerplant: 1 × Rotax 912ULS four cylinder, liquid and air-cooled, four stroke aircraft engine, 75 kW (101 hp)
Performance
- Maximum speed: 260 km/h (162 mph; 140 kn)
- Cruising speed: 180 km/h (112 mph; 97 kn)
- Stall speed: 65 km/h (40 mph; 35 kn)
- Rate of climb: 5 m/s (980 ft/min)
- Wing loading: 37.5 kg/m2 (7.7 lb/sq ft)
References
- ↑ 1.0 1.1 1.2 1.3 Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 36. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
- ↑ 2.0 2.1 2.2 Bertrand, Noel; Rene Coulon; et al: World Directory of Leisure Aviation 2003-04, page 132. Pagefast Ltd, Lancaster UK, 2003. ISSN 1368-485X
External links
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