BRAND and MODEL
MAGNI M-24 ORION
TYPE
Two-seat sport gyrocopter
ORIGIN
Italy
ENGINE
(M-24): one 86 kw (115 hp) Rotax 914 turbocharged 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: 4.33 m (14 ft 2 in)
Overall height: 2.8 m (9 ft 2 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: 82 litres (18 Imp gals
Endurance: 3.4 hr
Range no reserve: 482 km (300 miles)
Empty weight: 290 kg (639 lb)
Loaded weight: 450 kg (992 lb)
PHOTO
flugzeug-bild.de:Source of phothograph
