Independent Working Group Report: Missile Defense, the Space Relationship, and the Twenty-First Century. »»
| Country: | Russian Federation |
|---|---|
| Alternate Name: | Kent, Kh-555, Kh-55Sh, Kh-55SD, Kh-55SE |
| Class: | ALCM |
| Target: | Land |
| Length: | 7.10 m |
| Diameter: | 0.77 m |
| Launch Weight: | 1800.00 kg |
| Payload: | 200 kg HE, submunitions |
| Propulsion: | Turbofan |
| Range: | 3500.00 km |
| Guidance: | INS, TERCOM |
| Status: | Operational |
| In Service: | 2002-Present |
The AS-15C “Kent” (Kh-555, KH55Sh, Kh-55SD, or Kh-55SE) is an intermediate-range, air-launched, turbofan-powered, single warhead cruise missile developed and manufactured by the Soviet Union.
Development of the air-launched AS-15A “Kent” began in 1971. U.S. sources claim that the AS-15 was based on the U.S. Tomahawk, the blueprints of which the Soviets acquired at an early design stage. In 1976, the Soviets also began developing two variants of the AS-15, the ground-launched SSC-X-4 “Slingshot” (RK-55 Granat) and the submarine-launched SS-N-21 “Sampson” (RK-55 Granat/3M10) cruise missiles. The missiles are believed to have been developed and manufactured by the Raduga Mechanical Design Bureau (MKB Raduga).
The AS-15A is deployed on Tu-95 MS6 “Bear H6” and Tu-142M “Bear F” aircraft, each of which carries six missiles on an internal rotary launcher. The missile is also deployed on the TU-95 MS16 “Bear H16,” which carries six missiles on an internal rotary launch and 10 externally on five underwing pylons. Russia also developed a longer range version of the AS-15A known as the AS-15B (Kh-55SM or RKV-500B). This version is deployed on the Tu-160 “Blackjack” aircraft, which carries up to 12 missiles internally in two rotary launchers.
The AS-15C (Kh-555, KH55Sh, Kh-55SD, or Kh-55SE) is a conventionally armed version of the AS-15B. Development was completed in 1996, although the Russians continued to improve the missile’s guidance system and warhead until 2000. The AS-15C is similar in size and shape to the AS-15B, but with larger fuel tanks. The missile is 6.04 m long, has a body diameter of 6.04 m, and has a launch weight of 1,500 kg. Guidance is provided by an inertial navigation system (INS), with terrain contour matching (TERCOM) providing terminal guidance. The AS-15A has a minimum range of 50 km and an increased maximum range of 3,500 km. It carries a 400 kg high explosive unitary, penetration, or submunitions warhead.
The AS-15C is believed to have entered service in January 2002. Reports indicate that some AS-15A and AS-15B missiles have been modified to the AS-15C standard, which are carried on Tu-95, Tu-142, and Tu-160 aircraft. At present, approximately 624 AS-15 missiles are operational in Russia.(1)