Galileo Mirach 26

__NOTOC__ Infobox Aircraft
name=Mirach 26


caption=
type=Reconnaissance UAV
national origin=Italy
manufacturer=Meteor CAE, Galileo Avionica
designer=
first flight=avyear|1992
introduced=
retired=
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variants with their own articles=The Galileo Mirach 26 is a reconnaissance UAV developed in Italy during the 1990s, based on the Mirach 20 target drone. The initial work on the design was carried out by Meteor CAE before this company was absorbed by Galileo Avionica.

The Mirach 26 is of typical twin-boom pusher-prop battlefield surveillance UAV configuration. It is very similar to the older Mirach 20 in appearance but slightly bigger, the most visible difference being that the Mirach 26 has antenna disks on the top of the tailfins. It is powered by a 20 kW (26 hp) Sachs piston engine.

pecifications

aerospecs
ref=
met or eng?= met

crew=None
capacity=50 kg (110 lg) payload
length m=3.85
length ft=12
length in=8
span m=4.73
span ft=15
span in=6
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height m=1.27
height ft=4
height in=2
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gross weight kg=200
gross weight lb=440
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eng1 number=1
eng1 type=Sachs SF-350
eng1 kw= 20
eng1 hp= 27
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max speed kmh=220
max speed mph=138
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endurance h= >6
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ceiling m=3,500
ceiling ft=11,500
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armament6= aircontent
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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.
* [http://www.janes.com/extracts/extract/juav/juav0035.html Jane's Unmanned Aerial Vehicles and Targets]