Sokol / Tranzas Altius-M ( Altair ) reconnaissance unmanned aerial vehicle,Russia

The reconnaissance unmanned aerial vehicle for medium-altitude large range type Altius-M is a response from the Kazan consultancies Sokol and St. Petersburg society Tranzas to enter the Ministry of Defense of Russia on a reconnaissance unmanned aerial vehicle take-off weight up to 5 tons.
In October 2011, this machine won the tender over the type of workshop aviation design bureau RSK MiG. After that, any further work on this topic conducted in the NIR (scientific research), Altius M- subsidized amount of 1 billion rubles. They said the state's finances while they cover not only the development but also the construction of a technological demonstrator. The launch date of flight tests yet been set for the years 2014 to 2015. The design team Sokol design bureau UAV type Altius-M took a rather large high-wing aircraft with a slender hull doutníkovitým, a pair of piston engines under the wing slim straight by a considerable margin and V-tail. In the case of powertrain choice fell to 500 hp liquid-cooled diesel type RED A03 / V12. Most of the onboard systems or certain components of this machine reportedly shared with parallel exerted UAV type Inochodec with a mass of 1 t order that emerged from the NIR Inochodec . Technology demonstrator UAV type Altius-M became known as Altair and its assembly plant ensure KAPO from Kazan. Tests Altair was reportedly launched in August 2014, directly on the corporate airport Kazan plant KAPO.



Guidance:   
inertial (autopilot) + satellite
Drive:         
two piston type engines RED A03 / V12 max. Output of 500 hp
Radar:          
radar sideways and high resolving power of an unknown type, installed inside the fuselage toe
Facilities:    
electro-optical tracking system of unknown type. Spherical optics housing of this device is located on the belly of the fuselage.
Armament:     
none
Wing span:
about 28.5 meters 
Length:  
about 11.6 meters
Height:
approx 6.0 m
Empty weight:
?
Max. Takeoff Weight:
to 5000 kg
Max. speed:
?
Practical ceiling:  
?
Max. range:  
to 10,000 km
Perseverance:
48 h


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