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The Kh-25MSE multi-purpose missile is intended for hitting a wide range of surface and ground small targets (single target, as well as one of a group) under good and adverse weather, day and night. Typical targets are fixed and restrictedly moving objects with coordinates specified in Geographical Reference System. Airborne control system of the missile combines a navigation system, a receiver of navigation signals of space navigation system and a receiver of coastal station of differential corrections. Carriers: tactical attack aircrafts, ground-based and marine-based helicopters.
Basic Specifications
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Launch range, km |
up to 40 |
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Launch altitudes, m |
50...12000 |
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Maximum speed of missile, m/s |
920 |
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Type of warhead |
high-explosive
or piercing |
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Warhead weight, kg |
not exceeding 90 |
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Launch weight of missile, kg |
up to 323 |
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Overall dimensions, m |
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length |
4.355 |
| body diameter |
0.275 |
| wing span |
0.755 |
Developed and manufactured by Tactical Missiles Corporation JSC.
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