MITCHELL WING B-10

 

ORIGIN:

United States of America

TYPE:

Single-seat ultralight sport aircraft

ENGINE:

One 16 kw (22 hp) Zenoah G-25B1 single-cylinder two-stroke air-cooled engine

SPECIFICATIONS:

  • Wingspan: 10.36 m (34 ft)
  • Length: 2.44 m (8 ft)
  • Height: 1.2 m ( 4 ft)
  • Wing area: 12.6 m² (136 sq ft)
  • Max speed: 105 km/h (65 mph)
  • Cruising speed: 88 km/h (55 mph)
  • Stalling speed: 40 km/h (25 mph)
  • Rate of climb: 183 m/min (600 ft/min)
  • Service ceiling: 3,658 m (12,000 ft)
  • Range: 483 km (300 miles)
  • Max glide ratio: 16:1
  • Wing loading: 21 kg/m² (4.4 lb/sq ft)
  • Empty weight: 113 kg (250 lb)
  • Loaded weight: 249 kg (550 lb)

PHOTO SOURCE:

File:Mitchell Wing B-10 - Oregon Air and Space Museum - Eugene, Oregon - DSC09834.jpg - Wikimedia Commons

Categories

M