MITCHELL WING U-2

 

 ORIGIN:

United States of America

DESCRIPTION:

Single-seat ultralight sport aircraft

POWER PLANT:

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 SOURCE:

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