Aerotechnik WGM.21

The Aerotechnik WGM.21 is a quadrotor helicopter that was developed in the 1970s.

WGM.21
Role Quadrotor helicopter
National origin Germany
Manufacturer Aerotechnik
Introduction 1969

Design and development

The WGM.21 is an open cockpit quadrotor. Four rotors are mounted at the end of a four tubular supports arranged into a X shape. Cyclic and collective controls are mixed into a single control yoke. Pitch is controlled by foot pedals. A second model, the WGM.22, was developed with side-by-side configuration seating and an enclosed cockpit.[1]

Variants

WGM.21
Single seat prototype
WGM.22
Two seat enclosed version

Aircraft on display

Specifications (WGM.21)

Data from Air Progress

General characteristics

  • Crew: 1
  • Empty weight: 90 kg (198 lb)
  • Gross weight: 335 kg (739 lb)
  • Powerplant: 1 × BMW 700 Automotive conversion, 40 kW (54 hp)
  • Main rotor area: 21.3 m2 (229 sq ft)

Performance

  • Maximum speed: 125 km/h (78 mph, 67 kn)
  • Cruise speed: 115 km/h (71 mph, 62 kn)
  • Service ceiling: 2,100 m (6,900 ft)

References

  1. "none". Air Progress: 21. December 1971.
This article is issued from Wikipedia. The text is licensed under Creative Commons - Attribution - Sharealike. Additional terms may apply for the media files.