BRAND and MODEL
GYRODYNE XRON
TYPE
Single or two-seat light helicopter
ORIGIN
United States of America
ENGINE
One 54 kw (72 hp) Porsche YO-95-6 four-cylinder horizontally-opposed engine
SPECIFICATIONS
Length of fuselage: 3.5 m (11 ft 6 in)
Rotor disc area: 29.18 m² (314.2 sq ft)
Rotor diameter: 6.09 m (20 ft)
Height: 2.74 m (9 ft)
Width: 1.03 m (3 ft 4 in)
Max speed at sea level: 109 km/h (68 mph)
Cruising speed: 84 km/h (52 mph)
Rate of climb at sea level: 299 m/min (980 ft/min)
Max rate of climb at sea level: 543 m/min (1,780 ft/min)
Service ceiling: 3,932 m (12,900 ft)
Combat range: 79 km (49 miles)
Max endurance: 1.12 hrs
Empty weight: 195 kg (430 lb)
Payload weight: 27 kg (60 lb)
Loaded weight: 371 kg (818 lb)
PHOTO
Flickr:Source of phothograph
