Purpose of the system

The E95M system is designed to provide combat training for troops and for testing air defense systems.  The E95M aerial target simulates manoeuvrable targets such as RPVs, gliding guided aerial bombs, cruise missiles, and select planes and helicopters of tactical and army aviation.


Technical characteristics of the E95M aerial target

Flight altitude, m up to 3,000
Operating range, km up to 50
Maximum level flight speed, km/h 300-400
Flight duration, hrs up to 0.5
Payload* Luneberg lens or corner reflector, pyro tracers, IR traps
Engine M135 Pulsejet
Fuel type Regular petrol
Available manoeuvres dive, pull-up, S-turn
Thrust, kgf 15
Take-off weight, kg 70
Length, m 2.1
Wingspan, m 2.4
Fuselage diameter, m 0.25

* Payload:


Luneberg lens — effective dispersion surface 7-8 m².

Corner reflector — effective dispersion surface 0.8-1.2 m²

Without supplementary means of increasing the EDS, the dispersion surface is 0.15 m².