View source for CAC K100

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{|{{Infobox Aircraft Begin
 |name=K100
 |image=
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}}{{Infobox Aircraft Type
 |type=Reconnaissance UAV
 |national origin=France
 |manufacturer=[[CAC Systèmes]], [[EADS]]
 |designer=
 |first flight=
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 |primary user=
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}}
|}
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.

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==Specifications==
{{Aircraft specs
|prime units? = met
|crew=None
|capacity=5 kg (11 lb) payload
|length m=1.5
|length ft=4
|length in=11
|span m=2.60
|span ft=8
|span in=6
|empty weight kg=23
|empty weight lb=47
|gross weight kg=28
|gross weight lb=62
|eng1 number=1
|eng1 name=piston engine
|eng1 kw=<!-- prop engines -->5
|eng1 hp=<!-- prop engines -->7
|max speed kmh=234
|max speed mph=145
|endurance=30 minutes}}

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|related=<!-- related developments -->
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==References==
This article contains material that originally came from the web article {{usurped|1=[https://web.archive.org/web/20110902194407/http://www.vectorsite.net/twuav.html ''Unmanned Aerial Vehicles'']}} by Greg Goebel, which exists in the Public Domain.
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[[Category:1990s French military reconnaissance aircraft]]
[[Category:Unmanned aerial vehicles of France]]
[[Category:CAC Systèmes aircraft|K100]]


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