BRAND and MODEL
MAGNI M-22 VOYAGER
TYPE
ORIGIN
Italy
ENGINE
(M-22): one 75 kw (100 hp) Rotax 912S four-cylinder horizontally-opposed liquid and air cooled engine.
SPECIFICATIONS
Rotor diameter: 8.53 m (28 ft)
Propeller diameter: 1,7 m (67 in)
Overall width: 1.8 m (71 in)
Overall length: 4.65 m (15 ft 4 in)
Overall height: 2.6 m (8 ft 7 in)
Max speed: 185 km/h (115 mph)
Cruising speed: 145 km/h (90 mph)
Stalling speed: 30 km/h (19 mph)
Rate of climb: 290 m/min (950 ft/min)
Absolute ceiling: 4,000 m (13,000 ft)
Service ceiling: 3,500 m (11,400 ft)
Take-off roll: 70 m (230 ft)
Landing roll 0 to: 30 m (0 to 100 ft)
Fuel capacity: 72 litres (16 Imp gals
Endurance: 3.4 hrs
Range, no reserve: 482 km (300 miles)
Empty weight: 272 kg (600 lb)
Loaded weight: 550 kg (1,212 lb)
PHOTO
jetphotos.com:Source of phothograph
