Neha Patil (Editor)

AutoGyro MT 03

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Top speed
  
185 km/h

Manufacturer
  
AutoGyro MT-03 wwwjetscoutcompicturesbig588pic2jpg

Autogyro mt 03


The AutoGyro MT-03 is a German autogyro, designed and produced by AutoGyro GmbH of Hildesheim. The aircraft is supplied as a complete ready-to-fly-aircraft.

Contents

The MT-03 was approved in the United Kingdom in 2007 in a modified form as the RotorSport UK MT-03.

Autogyro mt 03 d mlli full flight


Design and development

The MT-03 features a single main rotor, a two-seats in tandem open cockpit with an optional partial cockpit fairing, tricycle landing gear with wheel pants and a four-cylinder, air and liquid-cooled, four-stroke, dual-ignition 100 hp (75 kW) Rotax 912 engine or turbocharged 115 hp (86 kW) Rotax 914 engine in pusher configuration.

The aircraft fairing is made from composites. Its 8.4 m (27.6 ft) diameter rotor has a chord of 20 cm (7.9 in). The aircraft has an empty weight of 245 kg (540 lb) and a gross weight of 450 kg (990 lb), giving a useful load of 205 kg (452 lb).

The MT-03 was developed into the MTOsport and the fully enclosed AutoGyro Calidus.

Operational history

The MT-03 was flown on a world record-setting distance flight in Australia of 1,263 km (785 mi).

Variants

AutoGyro MT-03
Base model for the European and North American market. No longer in production.
RotorSport UK MT-03
Modified model for the United Kingdom market, imported assembled and modified by RotorSport UK.
AutoGyro MTOsport
Improved model for the European and North American market. This model offers a choice of three different rotor systems, two different propellers, two engine choices (Rotax 912S or 914) and floats.

Military

 Ethiopia

  • Ethiopian Air Force - 2 for special operations
  • Specifications (MT-03)

    Data from Bayerl and Duda

    General characteristics

  • Crew: one
  • Capacity: one passenger
  • Airfoil: NACA 8-H-12
  • Empty weight: 245 kg (540 lb)
  • Gross weight: 450 kg (992 lb)
  • Fuel capacity: 34 litres (7.5 imp gal; 9.0 US gal) or optionally 68 litres (15 imp gal; 18 US gal)
  • Powerplant: 1 × Rotax 912ULS four cylinder, liquid and air-cooled, four stroke aircraft engine, 75 kW (101 hp)
  • Main rotor diameter: 8.4 m (27 ft 7 in)
  • Main rotor area: 55.4 m2 (596 sq ft)
  • Propellers: 3-bladed variable pitch composite
  • Performance

  • Maximum speed: 185 km/h (115 mph; 100 kn)
  • Cruising speed: 160 km/h (99 mph; 86 kn)
  • Rate of climb: 5 m/s (980 ft/min)
  • Lift-to-drag: 4
  • Disk loading: 8.1 kg/m2 (1.7 lb/sq ft)
    Minimum speed: 20 knots
  • References

    AutoGyro MT-03 Wikipedia


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