AERIAL TARGET E95M
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.
