|
The Kh-58E missile is designed to engage radars making part of land-based air defence systems, air defence early warning, target designation and control systems, and other emitting targets operating in A/A’, B/B’ and C frequency bands. The Kh-58E missile can be employed in any weather conditions (rain, snow, fog) or season, without any restrictions on geographical latitude of the launch site. The missile is guided by a passive radar homing head and an autonomous control system. The Kh-58E missile can be employed in weapon systems of the Su-24MK, Su-22M4, Su-25TK, MiG-25BM type combat aircraft equipped with an appropriate target designation system and airborne ejection unit for missile’s launch.
Basic Specifications
Max range (dependant on launch altitude at max speed), km |
46 – 200 |
| Launch altitudes, km |
0.2 – 20 |
| Launch speeds, Mach number |
0.47 – 2.35 |
| Min launch range, km |
8 – 60 |
| Missile launch weight, kg |
650 |
| Warhead weight, kg |
149 |
| Missile dimensions, m: |
|
| length |
4.8 |
| body diameter |
0.38 |
| wing span |
1.17 |
Developed by “Raduga” State Machine-Building Design Bureau
|