E-95
Mission
Composition
The E-95 air target system is designed to lau nch and co ntrol the drone si mul atin g subso nic re motel y- piloted aircraft, cruise missiles, glide bombs, helicopters, and attack aircraft. The E-95 air target system is intended to support practice firings of air defence missile/artillery systems controlled by radar, optical and optronic target acquisition and tracking s ystems, as well as for firing tests of prototype air defence weapons.
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TEST RANGE EQUIPMENT
Ground-Launched Small-Size Air Target System
aerial target ground control station launcher mobile repair vehicle
Max level flight speed, km/h Flight altitude, m Max cruising endurance, min Max mission radius, km Radio control system operating range, km Radar cross-section, sq.m: conventional design with Luneberg lens with angle reflector Fuselage length, m Wing span, m Launch weight, kg Life time, flights Crew
300-400 200-3,000 30 50 25 0.15 7.5 0.8-1.2 2.1 2.4 70 up to 10 5
10 1
