CAC K100

CAC K100

__NOTOC__ Infobox Aircraft
name=K100


caption=
type=Reconnaissance UAV
national origin=France
manufacturer=CAC Systèmes, EADS
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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.

pecifications

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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
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empty weight kg=23
empty weight lb=47
gross weight kg=28
gross weight lb=62
lift kg=
lift lb=

eng1 number=1
eng1 type=piston engine
eng1 kw= 5
eng1 hp= 7
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max speed kmh=234
max speed mph=145
max speed mach=
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range km=
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endurance h=
endurance min= 30
ceiling m=
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References

This article contains material that originally came from the web article [http://www.vectorsite.net/twuav.html "Unmanned Aerial Vehicles"] by Greg Goebel, which exists in the Public Domain.


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