| Kh-66/Kh-23Grom (NATO reporting name: AS-7 'Kerry') | |
|---|---|
 AS-7 'Kerry' | |
| Type | Tacticalair-to-surface missile |
| Place of origin | Soviet Union |
| Service history | |
| In service | Kh-66 :20 June 1968[1] Kh-23 :1973[2] Kh-23M :1974[2] |
| Used by | FSU, Warsaw Pact, Iraq, India[3] |
| Production history | |
| Designer | Yurii N. Korolyov[1] |
| Manufacturer | Zvezda-Strela |
| Specifications | |
| Mass | A921 :287 kg (633 lb)[3] |
| Length | A921 :3.525 m (11 ft 7 in)[3] |
| Diameter | 27.5 cm (10.8 in)[3] |
| Wingspan | 78.5 cm (2 ft 6.9 in)[3] |
| Warhead weight | 111 kg (245 lb)[3] |
| Engine | Solid fuel rocket[3] |
Operational range | 2–10 km (1.1–5.4 nmi)[3] |
| Maximum speed | 2,160–2,700 km/h (1,340–1,680 mph)[3] |
Guidance system | Kh-66: Line-Of-SightBeam riding Kh-23: Radiocommand guidance Grom-B:TV guidance |
Launch platform | Yak-38,MiG-21PFM,MiG-23,MiG-27, Su-17M3/20/22/22M3/M4,[3] |
The ZvezdaKh-66 andKh-23Grom (Russian:Х-23 Гром 'Thunder';NATO:AS-7 'Kerry') are a family of earlySoviet tacticalair-to-surface missiles with a range of 10 km. They were intended for use against small ground or naval targets. The Kh-66 was effectively a heavy-warhead, beam-riding version of theK-8 (AA-3 'Anab') air-to-air missile rushed into service in Vietnam in 1968. The Kh-23 was an improved Kh-66 with command-guidance, similar to theAGM-12 Bullpup.
Work on air-to-air missiles had started at the Kaliningrad Engineering Plant (then known as Plant #455, and later merged into Zvezda-Strela) in 1955.[1] This had resulted in theKaliningrad K-5 (AA-1 'Alkali') family of beam-guided missiles, including the K-51 (RS-2-US) carried by theSu-9 'Fishpot'.OKB-4 Molniya (laterVympel NPO) underMatus Bisnovat would go on to produce missiles such as theAA-6 Acrid.[1] Meanwhile, in 1963 the RS-2-US was tested as an air-to-surface missile.[1] It was concluded that the small warhead and inaccurate guidance made such an application "pointless".[1]
However, in 1965North Vietnam requested an air-to-surface missile from the Soviet government;[1] theAGM-12 Bullpup had entered service with the US Air Force before the start of theVietnam War. In April 1965 OKB-134 (later NPO Vympel) started work on this missile under the project name Kh-23, but they had problems developing a guidance system that would work with existing aircraft.[3] As a result, Yurii N. Korolyov came up with his own proposals based on the earlier experiments with the RS-2-US. A design bureau to develop the RS-2-US for surface targets was set up under Korolyov by decree #100 of 12 March 1966 of the Ministry of the Aircraft Industry;[1] this bureau would become the Zvezda OKB in 1976.[4]
The resulting weapon used the body of aK-8 (AA-3 'Anab'), K-5 guidance and propulsion systems, but increased the warhead from 13 kg (29 lb) to 100 kg (220 lb).[5] This had the big advantage of allowing the new weapon to be fitted to any aircraft capable of firing the K-5.[3] Design began in 1966,[4] so the project was known asKh-66 orIzdeliye 66 ('Article 66'). The Kh-66 was a beam-riding weapon that was first tested on theMiG-21PFM,[4] with the first launches of the missile in September 1966[6].It entered production in 1968 for that aircraft. The Kh-66 was only an interim solution as it required the launch aircraft to dive towards the target to maintain lock on the target. It entered service on 20 June 1968[1].The reason it was only carried on the MIG-21PFM was, since it was a beam-riding missile, it was paired with a radar, the RP-21M, which other aircraft did not have.
Meanwhile, Korolyov took over work on theKh-23 project intended for carriage on the Soviet Union's new MiG-23.[3] The Kh-23 became a development of the Kh-66 design with an improved propellant and new Delta-R1M guidance system.[3] The main practical difference was that it was a line-of-sight radio-command weapon similar to the Bullpup, allowing it to be fired in level flight (unlike the Kh-66). The first ten were tested in early 1968,[3] but significant delays were caused by problems with unreliable guidance which was eventually traced to the smoke generator which interfered with the antenna.[3] Once the receiver had been moved to a tail extension,[3] the government tested the missile on the MiG-23 and MiG-23B between 20 March 1970 and 3 October 1973.[1] and it entered service in 1973.[2] A laser-guided version of the Kh-23, the Kh-25, became the basis for the AS-10 'Karen' family of missiles.[1] Technology from these was 'backported' to the Kh-23 to create the Kh-23M in 1974.[2]
The Kh-23 was later licensed for local production in both Romania and Yugoslavia.[3] In 1977 a dummy Kh-23 was fired from a Ka-252TB helicopter,[1] the prototype of theKamov Ka-29TB 'Helix-B' assault transport.
The Kh-66 used the airframe of theKaliningrad K-8 (AA-3 'Anab') air-to-air missile, with the nozzle split to make room for the antenna of the beam-riding guidance system of theKaliningrad K-5 (AA-1 'Alkali').[3] It has cruciform control fins on the nose, and four clipped-tip delta-wings at the rear with elevators for control.
The Kh-66 entered production for the MiG-21 in 1968, and the Kh-23 was certified for the MiG-23 'Flogger' in 1973.
Afghanistan[9]
Algeria[9]
Angola[9]
Azerbaijan[9]
Belarus[9]
Bulgaria[3]
Cambodia[9]
Congo[9]
Cuba[9]
Czechoslovakia − Passed on to successor states[9] Czech Republic[9]
East Germany[10] − Passed on to the unified German state[9]
Egypt[9]
Finland[9]
Georgia[9]
Germany[9]
Hungary[9]
India[3]
Iraq[3]
Kazakhstan[9]
Libya[11]
Nigeria[9]
Poland[3]
Romania − Locally produced as the A-921[3][9]
Serbia −Grom[3]
Slovakia[9]
Soviet Union[3] − passed on to successor states[9]
Sudan[9]
Syria[12]
Ukraine[9]
Vietnam[9]
Yugoslavia − Passed on to successor states[9]
