Kh-31 (NATO reporting name: AS-17 'Krypton') |
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Kh-31A
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Type | Medium-range air-to-surface missile |
Place of origin | Soviet Union |
Service history | |
In service | 1988–present |
Used by | Russia, China, India, Algeria |
Production history | |
Manufacturer |
Tactical Missiles Corporation (Zvezda-Strela before 2002) |
Unit cost | $550 000 (2010) |
Produced | 1982 |
Specifications | |
Weight | Kh-31A :610 kg (1,340 lb) Kh-31P :600 kg (1,320 lb) |
Length | Mod 1 : 4.700 m (15 ft 5.0 in) Mod 2 (AD/PD) : 5.3 m (17 ft 5 in) |
Diameter | 360 mm (14 in) |
Warhead | HE shaped charge |
Warhead weight | Kh-31A :94 kg (207 lb) Kh-31P :87 kg (192 lb) |
Detonation
mechanism |
Impact |
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Engine | Solid fuel rocket in initial stage, ramjet for rest of trajectory |
Wingspan | 914 mm (36.0 in) |
Propellant | kerosene |
Operational
range |
Kh-31A: 25 km–103 km (13.5–55.6 nmi; Kh-31P: up to 110 km (60 nmi; 70 mi) |
Speed | Kh-31A/P: 2,160–2,520 km/h (1,340–1,570 mph) MA-31: Mach 2.7 (low), Mach 3.5 (high) |
Guidance
system |
Kh-31A: inertial guidance with active radar homing Kh-31P: inertial with passive radar |
Launch
platform |
Both : Su-27SM, Su-30MKI, Su-34, Su-35, MiG-29M, HAL Tejas Mk1 and Mk2, MiG-29K Kh-31A only : Su-33 Also : Su-24M |
The Kh-31 (Russian: Х-31; AS-17 'Krypton') is a Russian air-to-surface missile carried by aircraft such as the MiG-29 or Su-27. It is capable of Mach 3.5 and was the first supersonic anti-ship missile that could be launched by tactical aircraft.
There are several variants, it is best known as an anti-radiation missile (ARM) but there are also anti-shipping and target drone versions. There has been talk of adapting it to make an "AWACS killer", a long-range air-to-air missile.
The proliferation of surface-to-air missiles (SAMs) has made the Suppression of Enemy Air Defence a priority for any modern air force intending offensive action. Knocking out air search radars and fire control radars is an essential part of this mission. ARMs must have sufficient range that the launch platform is out of range of the SAMs, high speed to reduce the risk of being shot down and a seeker that can detect a range of radar types, but they do not need a particularly big warhead.
The Soviet Union's first ARM was developed by the Raduga OKB engineering group responsible for the Soviet Union's missiles for heavy bombers. The Kh-22P was developed from the 6-tonne Raduga Kh-22 (AS-4 'Kitchen') missile. Experience gained with this led in 1973 to the Kh-28 (AS-9 'Kyle') carried by tactical aircraft such as the Su-7B, Su-17 and Su-24. It had Mach 3 capability and a 120 km (60 nmi) range, greater than the contemporary AGM-78 Standard ARM. The Kh-28 was succeeded by the Kh-58 in 1978, which has similar speed and range but replaces the dual-fuel rocket motor with a much safer RDTT solid propellant.