MIGNET HM-1000 BALERIT

 

ORIGIN:

France

TYPE:

Two-seat light sporting aircraft

ENGINE:

One 48 kw (64 hp) Rotax 582 UL-DCDI two-cylinder, two-stroke, liquid-cooled engine with dual electronic ignition

SPECIFICATIONS:

  • Wingspan [front]: 7.5 m (24 ft)
  • Wingspan [rear]: 5.5 m (18 ft)
  • Length: 5 m (16 ft 4 in)
  • Height: 1.96 m (6 ft 4 in)
  • Total wing area: 17.55 m² (188.83 sq ft)
  • With extensional surfaces: 19.24 m² (207 sq ft)
  • Max speed: 150 km/h (93 mph)
  • Minimum speed: 55 km/h (34 mph)
  • Take-off distance: 60 m (198 ft)
  • Landing distance: 25 m (83 ft)
  • Minimum sink rate: 150 m/min (492 ft/min)
  • Range at cruising speed: 150 km (94 miles)
  • Fuel capacity: 44 litres (9.7 Imp gals)
  • Empty weight: 174 kg (384 lb)
  • Payload: 200 kg (441 lb)
  • Max wing loading: 21.3 kg/m² (4.36 lb/sq ft)
  • Loaded weight: 450 kg (992 lb)

PHOTO SOURCE:

http://www.samolotypolskie.pl/samoloty/14479/126/Mignet-HM-1000-Balerit2

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