BRAND and MODEL
MITCHELL WING U-2
TYPE
Single-seat ultralight sport aircraft
ORIGIN
United States of America
ENGINE
One 15 kw (20 hp) Komatsu Zenoah G-25 air-cooled engine
SPECIFICATIONS
Wingspan: 10.36 m (34 ft)
Length: 2.8 m (9 ft 2 in)
Wing area: 12.6 m² (135.63 sq ft)
Cruising speed: 102 km/h (63 mph)
Stalling speed: 42 km/h (26 mph)
Max glide ratio at 72 km/h (45 mph): 20:1
Rate of climb: 122 m/min (400 ft/min)
Range: 290 km (180 miles)
Fuel capacity: 11 litres (2.5 Imp gals)
Empty weight: 109 kg (240 lb)
Loaded weight: 249 kg (550 lb)
PHOTO
sharpwings.ivao.cz:Source of phothograph
