Expedition Global Eagle - Technical Specifications

Technical Specifications

The Magni gyrocopter model: Magni VPM M16 (Similar to the Magni M16 - 2000) used in the expedition had the following specifications:

  • Weight: Empty weight 261/266 kg, maximum take-off gross weight 450 kg
  • Maximum speed 115 mph
  • Cruising speed 90 mph
  • Absolute ceiling 4000 m
  • Service ceiling 3500 m
  • Take-off roll 70 m
  • Landing roll from 0 to 30 m
  • Rate of climb 5 m/s
  • Fuel tank capacity 72 L
  • Rotor diameter 8230/8535 mm
  • Propeller diameter 1700 mm
  • Overall width 1800 mm
  • Overall length 4655 mm
  • Overall height 2600 mm
  • Airframe: chrome-alloy aeronautical 4130 steel, tig welded. Fiberglass fairing, wheel pants and instrument panel.
  • Seat: epoxy / fiberglass with integral fuel-tank,
  • Instruments: rotor tachometer, altimeter, air speed indicator, Flydat and fuel gauge
  • Engine used for expedition: 914 Rotax Turbo, 4 cylinders, 4 stroke, water cooled, 115 hp, with electric starter and mechanical prerotator. (Also available: Rotax 912 ULS, 100 Hp)
  • Propeller: three-blades, carbon fiber, ground adjustable pitch.
  • Rotor: two-blades, composite.
  • Controls: double. Electric trim.

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