CAC K100
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.
| K100 | |
|---|---|
| Role | Reconnaissance UAV |
| National origin | France |
| Manufacturer | CAC Systèmes, EADS |
Specifications
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
This article contains material that originally came from the web article Unmanned Aerial Vehicles by Greg Goebel, which exists in the Public Domain.
This article is issued from Wikipedia. The text is licensed under Creative Commons - Attribution - Sharealike. Additional terms may apply for the media files.