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X-25

X-25 (according to the classification of the US Ministry of Defense and NATO - AS-10 Karen ) [3] - Soviet / Russian high-precision short-range air-to-surface aircraft missile .

X-25
designation of the Ministry of Defense of the USA and NATO : AS-10 Karen
AS-12 Kegler
Sketch of KH-25MP.svg
Projection of the X-25MP rocket
Type ofair-to-surface class , tactical ; anti-radar missile (X-25MP)
Statusoperated by
DeveloperUnion of Soviet Socialist Republics OKB Star / Russia Tactical Missile Arms Corporation
Chief DesignerKorolev, Yuri Nikolaevich
Bugaysky, Victor Nikiforovich [1]
Years of developmentSince 1970
Test startZLI : May-July 1973
GI : August 1973 - November 1974 [2]
AdoptionFebruary 3, 1976
ManufacturerUnion of Soviet Socialist Republics KPO Strela / Russia Tactical Missile Arms Corporation
Years of production1975 - 1983
Units produced25,000 missiles, type X-25M [2]
Main operatorsFlag of the Russian Air Force.svg Russian Air Force
Naval Ensign of Russia.svg Russian Navy
Base modelX-23
↓ All specifications

The development of the X-25 guided missile (“product 69”) began at OKB Zvezda in 1970. The Kh-25 missile was put into service in 1976, and has been exported since 1992.

Designed to destroy armored vehicles, radar stations, surface ships and other purposes.

The X-25 missile family has a high-explosive fragmentation warhead weighing from 86 kg to 136 kg (depending on version).

Content

Modifications

 
Installation of the X-25 on the pylon of the aircraft

The following modifications of the X-25 were developed (the letter "M" in the name means " modular "):

  • X-25 ("product 69", X-25L) - the basic version with a laser seeker
  • X-25MA - with active radar seeker , has been offered for export since 1999
  • X-25ML (“product 713”) - with a semi-active laser GSN 24N1 and a tandem warhead capable of punching up to 1 meter of concrete [4]
  • X-25R / X-25MR (“product 714”) - with interference-protected radio command guidance
  • X-25MT - with a television seeker
  • X-25MSE
  • X-25MTP - with thermal imaging (infrared) homing head
  • X-27PS ("product 72", has the NATO designation: AS-12 Kegler ) - the basic anti - radar version of the X-25
  • X-25MP (“product 711”, AS-12 Kegler ) - a modular anti-radar missile (with passive radar seeker PRGS-1VP or PRGS-2VP) designed to destroy radars of widespread “Hawk” and “Advanced Hawk” air defense systems . It is basically identical to the X-27PS, it has a control system modified in terms of introducing the feature of the guidance system and changing the control law, which made it possible to reduce the minimum launch range from 9.5-10 km for the X-27PS rocket to 3-5 km for the X-25MP rocket. Also, the tail fairing, which was previously part of the power supply compartment, was lengthened and became an independent sixth compartment.
  • X-25MPU ( AS-12 Kegler ) - an upgraded version of the X-25MP. It has a radar homing system with an extended frequency range capable of operating on radar systems of the Crotale and Roland type , and the missile is equipped with an inertial guidance system, which made it possible to prolong the guidance and re-capture the target in case of temporary shutdown of the radar target. It has a significantly increased range compared to the X-25MP.

Performance Specifications

X-25X-25MLX-25MRX-25MP
factory indexproduct 69product 713product 714product 711 /
product 712
year of adoption1976198119811981
Control systemSUR-71 autopilot with laser seekerSUR-73 autopilot with laser seekerautopilot SUR-73 with radio command SN
GOSsemi-active laser 24H1semi-active laser 24H1passive radar PRGS-1VP / PRGS-2VP
engineRDTT PRD-228Two-mode RDTT PRD-276
combat characteristics
minimum launch range, km3
maximum launch range, km7tenten40
KVO , m6.4 [5] (5-10 m [6] )6 [7] (5-10 m [8] )
carrier speed, km / h700-1000700-1250
minimum application height, km0.50.05
maximum application height, kmfourfive12
maximum flight speed, m / s850870860920
average flight speed, m / s400-450
flight time at maximum range, s15-18
mass and dimensional characteristics
length mm3750370538304194/4294
diameter mm275
wing span, mm820755
feathering range, mm493
starting weight, kg320299 ± 8320315 ± 8
main warheadF25-1M
high-explosive fragmentation
F27
DOS weight Warhead, kg11286-9014086-90
explosive mass, kg80
additional warheadF25-2M
high-explosive fragmentation
-
weight extra Warhead, kg24-
explosive mass, kg13-
dimensions of the transport container (LxWxH), mm4200x860x8064816x855x816
weight in launch container, kg540530
compatibility
separation devices:APU-68, APU-68UM, APU-68-85, APU-68UM2, APU-68UM3
carriers:Su-17 , Su-24 , Su-25 , Su-27 , MiG-27 , MiG-29 , MiG-31 BM, Ka-50 (X-25ML)
economic indicators
unit cost:

Notes

  1. ↑ Chief constructors Of. Tactical Missile Weapons Corporation website
  2. ↑ 1 2 X-25MP. History of . Tactical Missile Weapons Corporation website
  3. ↑ The Many-Faced Tactical Missile X-25
  4. ↑ Friedman, Norman (2006), The Naval Institute Guide to World Naval Weapon Systems (5 ed.), Naval Institute Press, p. 838, ISBN 9781557502629 , < https://books.google.co.uk/books?id=4S3h8j_NEmkC&pg=PA838 >  
  5. ↑ Markovsky, Perov, 2005 , p. eleven.
  6. ↑ X-25 (neopr.) . The site " Corner of the Sky " (2004). Archived on June 19, 2013.
  7. ↑ Markovsky, Perov, 2005 , p. nineteen.
  8. ↑ X-25ML (Russian) . The site " Corner of the Sky " (2004). Date of treatment June 17, 2013. Archived June 16, 2013.

Literature

  • Markovsky V.Yu., Perov K. Soviet air-to-ground aviation missiles. - M .: Exprint, 2005.
  • Shirokorad A. B. History of aircraft weapons. Short essay / Under the general ed. A.E. Taras. - Minsk: Harvest, 1999 .-- 560 s. - (Library of military history). - 11,000 copies. - ISBN 985-433-695-6 .

Links

  • Aviation weapons. Air-to-surface guided missiles Sky corner
  • Documentary: Shock Force - X-25 Rocket The film tells about the creation of missiles with laser guidance systems.


Source - https://ru.wikipedia.org/w/index.php?title=X-25&oldid=95430231


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