Kh-55

Kh-55/65/555
AS-15 Kent
Kh-55 in the Ukrainian Air Force Museum
TypeAir-launched cruise missile
Place of originSoviet Union
Service history
In service1983–present
Used bySoviet Union, Russia, China, Iran
WarsSyrian Civil War
Russo-Ukrainian war
Production history
Designed1971–1981
ManufacturerRaduga OKB, KhAZ (Kharkiv), Novator (MZiK) & NPP Temp (Eka) NPO Strela (Oren), else
Produced1981
Specifications
Mass1,650 kg (3,640 lb) (Kh-65SE)
2,400 kg (5,300 lb) (Kh-101)
Length604 cm (19 ft 10 in) (Kh-65SE)
745 cm (24 ft 5 in) (Kh-101)
Diameter51.4 cm (20.2 in) (Kh-55/Kh-55SM)
Wingspan310 cm (122.0 in) (Kh-55/Kh-55SM)
WarheadThermonuclear weapon or Conventional warhead
Blast yield200kt Nuclear (Kh-55/Kh-55SM)

EngineR95TP-300 Turbofan/turbofan (Kh-55/Kh-55SM)
360-400 kgf (Kh-55/Kh-55SM)
Propellantjet fuel
Operational
range
2,500 km (1,300 nmi) (Kh-55)
3,000 km (1,600 nmi) (Kh-55SM)
600 km (320 nmi) (Kh-65SE)
300 km, later 600 km (Kh-SD)
Flight altitudeunder 110 m/300 ft
Maximum speedMach 0.75 (KH-SD)
Mach 0.6-0.78 (Kh-101)
Guidance
system
inertial guidance with Doppler radar/terrain map updates; Kh-SD had a TC/IIR terminal guidance system, and an alternative active radar homing seeker was proposed
Launch
platform
Tu-95MS, Tu-160, Su-34

The Kh-55 (Russian: Х-55, also known as RKV-500; NATO reporting name: AS-15 "Kent") is a Soviet/Russian subsonic air-launched cruise missile, designed by MKB Raduga in the 1970s. It has a range of up to 2,500 km (1,350 nmi) and can carry nuclear warheads. Kh-55 is launched exclusively from bomber aircraft and has spawned a number of conventionally armed variants mainly for tactical use, such as the Kh-65SE and Kh-SD, but only the Kh-555 appears to have been put into service. The Kh-55 was not the basis of the submarine and ground-launched S-10 Granat or RK-55 Relief (SS-N-21 "Sampson" and SSC-X-4 "Slingshot") designed by NPO Novator. The RK-55 is very similar to the air-launched Kh-55 (AS-15 "Kent") but the Kh-55 has a drop-down turbofan engine and was designed by MKB Raduga.