Adi Bumble Bee

The ADI Bumble Bee is an ultralight gyrocopter, the first of its kind when it flew in 1983 and still available in plans form for home-building. It was designed by Martin Hollmann after a back injury (sustained in the crash of the ADI Condor) prevented him from flying his previous design (the ADI Sportster) on account of not being able to lift the rotor assembly.

Specifications (ADI Bumble Bee)

General Characteristics

  • Crew: one pilot
  • Capacity: pilot only
  • Length: 10 ft 0 in (3.05 m)
  • Main rotor diameter: 23 ft 0 in (7.01 m)
  • Height: 7 ft 6 in (2.29 m)
  • Main rotor area: 415 ft² (39 m²)
  • Empty: 213 lb (97 kg)
  • Loaded: 500 lb (227 kg)
  • Maximum takeoff: lb ( kg)
  • Powerplant: 1x Rotax 446, 40 hp (30 kW)

Performance

  • Maximum speed: 56 mph (90 km/h)
  • Range:65 miles (104 km)
  • Service ceiling: 16,000 ft (4.878 m)
  • Rate of climb: 1,500 ft/min (457 m/min)
  • Wing loading: 1.2 lb/ft² (6 kg/m²)
  • Power/Mass: 0.08 hp/lb (0.13 kW/kg)

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