MITCHELL WING U-2

 

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