Humbert La Moto Du Ciel
The Humbert La Moto Du Ciel (Motorbike of the Sky) is a French ultralight aircraft, designed and produced by Humbert Aviation of Ramonchamp, introduced in the mid-1980s. The aircraft is supplied as a complete ready-to-fly-aircraft.[1]
La Moto Du Ciel | |
---|---|
Role | Ultralight aircraft |
National origin | France |
Manufacturer | Humbert Aviation |
Status | In production (2012) |
Unit cost |
€34,500 (2015) |
Design and development
The aircraft complies with the Fédération Aéronautique Internationale microlight rules. It features a strut-braced high-wing, a two-seats-in-tandem open cockpit under a bubble canopy, fixed tricycle landing gear and a single engine in pusher configuration.[1]
The aircraft fuselage is made from welded steel tubing, with the tailboom left uncovered. The flying surfaces are made from aluminium sheet, with a foam core. Its 11.3 m (37.1 ft) span wing has an area of 17.4 m2 (187 sq ft). Standard engines available are the 64 hp (48 kW) Rotax 582 two-stroke, the 80 hp (60 kW) Rotax 912UL, the 100 hp (75 kW) Rotax 912ULS four-stroke powerplants. Kits for aerial application are also available.[1]
Specifications (La Moto Du Ciel)
Data from Bayerl and Tacke[1]
General characteristics
- Crew: one
- Capacity: one passenger
- Wingspan: 11.3 m (37 ft 1 in)
- Wing area: 17.4 m2 (187 sq ft)
- Empty weight: 240 kg (529 lb)
- Gross weight: 450 kg (992 lb)
- Fuel capacity: 60 litres (13 imp gal; 16 US gal)
- Powerplant: 1 × Rotax 582 twin cylinder, liquid-cooled, two stroke aircraft engine, 48 kW (64 hp)
Performance
- Maximum speed: 150 km/h (93 mph, 81 kn)
- Cruise speed: 120 km/h (75 mph, 65 kn)
- Stall speed: 60 km/h (37 mph, 32 kn)
- Rate of climb: 6 m/s (1,200 ft/min)
- Wing loading: 25.9 kg/m2 (5.3 lb/sq ft)
References
- Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 59. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
- Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 61. Flying Pages Europe SARL, 2015. ISSN 1368-485X