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CAC K100

From Wikipedia, the free encyclopedia
K100
General information
TypeReconnaissance UAV
National originFrance
ManufacturerCAC Systèmes, EADS

The CAC K100 is a mini-UAV developed in France in the 1990s. The company sells a reconnaissance variant, the K100/R, and an antiradar loitering attack variant, the K100/A. The K100 is of conventional aircraft configuration, except for an upright vee tail and a pusher propeller. It has no landing gear.


Specifications

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General characteristics

  • Crew: None
  • Capacity: 5 kg (11 lb) payload
  • Length: 1.5 m (4 ft 11 in)
  • Wingspan: 2.60 m (8 ft 6 in)
  • Empty weight: 23 kg (47 lb)
  • Gross weight: 28 kg (62 lb)
  • Powerplant: 1 × piston engine , 5.0 kW (7.0 hp)

Performance

  • Maximum speed: 234 km/h (145 mph, 126 kn)
  • Endurance: 30 minutes

References

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This article contains material that originally came from the web article Unmanned Aerial Vehicles by Greg Goebel, which exists in the Public Domain.