Kh-25

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Kh-25M
Type MP: SEAD
Service history
In service 1975
Production history
Manufacturer Zvezda-Strela
Specifications
Weight MP: 320kg
MR/ML: 300 kg
Length MP: 4.19 m
MR: 3.69 m
ML: 3.71 m
Diameter 275 mm

Warhead 90 kg TNT equivalent
Detonation
mechanism
Impact

Operational
range
MP: 25 km
MR: 10 km
ML: 20 km
Speed Mach 0.7
Guidance
system
MP: inertial and passive radar
MR: radio-command
ML: semi-active laser
MTP: thermal-imaging
Launch
platform
Helicopters

Aircraft

The Kh-25 is a Russian AGM that can be carried on double or single ejector racks on most Russian strike aircraft. It has been developed by Zvezda-Strela in cooperation with Sukhoi in order to replace the Kh-23 missile which was too complicated to guide in a combat situation.

The most popular version of the missile is the Kh-25M variant, where the M stands for "Modulnaya" or modular. All the M missiles are made up out of the same components, with the exception of the guidance head. There are four known variants of this missile:

  • Kh-25MP with inertial and passive radar guidance
  • Kh-25MR with radio-command guidance
  • Kh-25ML with semi-active laser guidance
  • Kh-25MLT with thermal-imaging guidance

All of the missiles are assigned the NATO codename AS-10 Karen, with the exception of the Kh-25MP which is designated AS-12 Kegler.

Kh-25ML.
Kh-25ML.

[edit] Kh-25ML

The Kh-25ML is a variant of the Kh-25. The missile is designed to engage pinpoint ground and waterborne targets, such as missile systems, open and sheltered aircraft, armored vehicles, artillery pieces, light bridges and ferries, as well as small-displacement ships, in visual meteorological conditions both day and night.

The missile is provided with a semiactive laser homing head. It features a canard configuration with cruciform wings and ruddervators.

A target is detected by the pilot visually or with the aid of a forward air controller. A target is laser-illuminated from the carrier aircraft, another aircraft or helicopter as well as from a groundbased target designator. Upon receipt of a signal on lockon of a target-reflected laser beam, with the aircraft being in range, the pilot launches a missile in level flight or at a dive of up to 40°. After launch, the missile homes to the target by signals of its head. A steep climb is expedient to increase a target approach angle and use warhead more effectively.


[edit] References

  1. http://www.fas.org/man/dod-101/sys/missile/row/as-10.htm