| Aerosette | |
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HW100 - 45000
UAW55 - 105000 RRW100 - 175000 PKRR - 7500 |
Aerosette MH-46 Eclipse MH-46 Eclipse Role - Ultralight aircraft National origin - Czech Republic Manufacturer - Aerosette Introduction - 2002 Status - In production The Aerosette MH-46 Eclipse is a Czech ultralight aircraft, designed and produced by Aerosette of Chrastava. The aircraft is supplied as a complete ready-to-fly-aircraft. Design and development The MH-46 was designed to comply with the Fédération Aéronautique Internationale microlight rules and intended for personal use and flight training. It features a strut-braced high-wing, a two-seats-in-side-by-side configuration enclosed cockpit, fixed tricycle landing gear and a single engine in tractor configuration. The aircraft is made from composites. Its 9.71 m (31.9 ft) span wing is supported by a single strut on each side. Standard engines available are the 64 hp (48 kW) Rotax 582 two-stroke and the 100 hp (75 kW) Rotax 912ULS four-stroke powerplant. The cockpit was designed for comfort and is 1.2 m (47 in) wide at the pilot's elbow. Specifications (MH-46 Eclipse) Data from Bayerl, Tacke and Aerosette General characteristics Crew: one Capacity: one passenger Length: 6.34 m (20 ft 10 in) Wingspan: 9.71 m (31 ft 10 in) Height: 2.18 m (7 ft 2 in) Wing area: 11.5 m2 (124 sq ft) Empty weight: 285 kg (628 lb) Gross weight: 472.5 kg (1,042 lb) Fuel capacity: 130 litres (29 imp gal; 34 US gal) Powerplant: 1 × Rotax 912ULS four cylinder, liquid and air-cooled, four stroke, 75 kW (101 hp) Performance Maximum speed: 250 km/h (160 mph, 130 kn) Cruise speed: 220 km/h (140 mph, 120 kn) Stall speed: 65 km/h (40 mph, 35 kn) flaps down Never exceed speed: 298 km/h (185 mph, 161 kn) g limits: +4/-2 Rate of climb: 8.7 m/s (1,710 ft/min) |