Mitchell U-2 Superwing

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A Mitchell U-2 superwing at the Steven F. Udvar-Hazy Center
A Mitchell U-2 superwing at the Steven F. Udvar-Hazy Center

The Mitchell U-2 Superwing features a Mitchell wing design. The first variation of this popular ultralight aircraft flew in 1977.


Contents

[edit] Specifications (typical U-2)

[edit] General characteristics

  • Crew: one, pilot
  • Capacity: pilot only
  • Length: 8 ft 0 in (2.4 m)
  • Wingspan: 34 ft 0 in (10.3 m)
  • Height: 3 ft 0 in (0.9 m)
  • Wing area: 136 ft² (12.6 m²)
  • Empty: 335 lb (136 kg)
  • Loaded: 580 lb (263 kg)
  • Powerplant: 1x Zenoah 250, 19 hp (14 kW)

[edit] Performance

  • Maximum speed: 95 mph (153 km/h)
  • Service ceiling: 12,000 ft (3,657 m)
  • Rate of climb: 600 ft/min (183 m/min)
  • Wing loading: 4 lb/ft² (21 kg/m²)
  • Power/mass: 0.03 hp/lb (50 W/kg)

[edit] External links

[edit] Related content

 

Comparable aircraft

 

 

See also