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Kh-22 (AS-4 'Kitchen')

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Kh-22 (AS-4 'Kitchen')
NameKh-22 (AS-4 'Kitchen')
OriginSoviet Union
TypeCruise missile / Anti-ship missile / Anti-radiation
Service1960s–present
Used bySoviet Navy, Russian Aerospace Forces
ManufacturerRaduga Design Bureau
Weight~5,800 kg (varies by variant)
Length~10.6 m
Diameter~0.9 m
Wingspan~3.6 m
SpeedMach 4 (approx)
Range600–600+ km (variant-dependent)
Warhead900–1,000 kg conventional or nuclear
Guidanceinertial, active radar, passive radar homing

Kh-22 (AS-4 'Kitchen') is a Soviet-designed long-range, high-speed cruise missile originally developed for use against aircraft carriers and large surface combatants. Introduced during the Cold War, it combined a large booster, ramjet sustainer and heavy warhead to provide stand-off strike capability for strategic and maritime aircraft. The missile has been carried on strategic bombers and adapted into several variants for anti-ship, anti-radiation and land-attack roles, remaining notable in post‑Soviet inventories.

Development and Design

Development began in the late 1950s at the Raduga Design Bureau under directives tied to the Soviet Navy and the Ministry of Aviation Industry to counter carrier battle groups fielded by the United States United States Navy and allied Royal Navy task forces. The project aligned with requirements set by the Council of Ministers and selected bomber platforms such as the Tupolev Tu-22M and Tupolev Tu-95 to provide long-range strike similar to contemporaneous systems like the Raduga KS-1 Komet and later relatives including the Kh-15 family. Design choices—large rocket booster, solid-fuel first stage and ramjet or turbojet sustainer—reflected advances demonstrated in programs like the Mikoyan-Gurevich and captured research from interwar and wartime aerospace engineering efforts. Integration of inertial navigation with active and passive seekers drew on sensors developed for the Zvezda and other avionics suites used across Soviet strategic aviation.

Technical Specifications

The Kh-22's airframe combines a high-subsonic to supersonic boost phase with a Mach 3–4 cruise or terminal sprint, achieving speeds comparable to high-performance interceptors of the era such as the MiG-25. Typical dimensions approximate 10–11 m in length and nearly 6,000 kg launch mass, with folding cruciform wings and a large monopropellant or ramjet sustainer engine. Guidance begins with an inertial navigation system augmented by active radar homing for the anti-ship variant and passive radar homing for the anti-radiation variant; seeker electronics drew on systems employed in the Soviet electronic warfare and radar development programs. Warhead options ranged from a ~900–1,000 kg high-explosive fragmentation charge to tactical thermonuclear devices, reflecting doctrine overlap with programs such as the RDS nuclear testing series. Launch profiles included medium-altitude and high-altitude release modes to maximize range and speed while complicating interception by surface-to-air systems like the MIM-14 Nike Hercules or fighter escorts such as the F-14 Tomcat.

Operational History

The Kh-22 entered service in the mid-1960s and was fielded aboard Tu-22M and Tu-95 platforms during heightened tensions with the United States and NATO alliance partners in the Cold War. It featured in Soviet naval exercises and strategic patrols intended to deter carrier operations by forces including the United States Sixth Fleet and Royal Navy Carrier Battle Groups. During the late Cold War and post-Soviet conflicts, modified Kh-22s and their derivatives were deployed for long-range strike missions in regional theaters, operating alongside systems like the Kh-55 and Kh-101. Training, test firings and export considerations involved institutions such as the Ministry of Defense of the Russian Federation and aviation research centers including the Gromov Flight Research Institute.

Variants and Modifications

Several official and field-reported variants exist. The baseline anti-ship model used active radar homing; an anti-radiation variant employed passive radar seekers to target emitters similar to those in the SA-2 Guideline and other radar networks. Later modifications focused on electronic countermeasure hardening, updated seekers, warhead changes and integration on multiple launch aircraft; these echoed modernization trends seen with missiles like the Kh-22M family and the Kh-32 follow-on program. Experimental conversions tested extended-range boosters, alternative propulsion and inertial/GPS-like navigation augmentation comparable to adaptations made for the Kh-55 series.

Strategic Role and Doctrine

Strategically, the Kh-22 fulfilled a Soviet anti-access/area-denial intent targeted at carrier strike groups and maritime logistics, complementing submarine-launched weapons and surface-to-air threats. Doctrine tied employment of the missile to long-range aviation wings of the Soviet Air Force and Soviet Navy maritime aviation, coordinating with reconnaissance platforms such as the Tu-95RTs and signals intelligence assets to locate targets. The availability of a nuclear warhead option linked the system to wider nuclear strategies codified in arms control dialogues like the Strategic Arms Reduction Treaty discussions, while conventional employment aligned with sea denial operations similar to those advocated by Soviet naval theorists and planners.

Operators and Deployment

Primary operators were the Soviet Union and, after 1991, the Russian Federation, with deployment aboard strategic and maritime bomber squadrons at bases such as Olenya Air Base and Engels Air Base. Limited export or transfer offers were discussed with allied states and client regimes during Cold War diplomacy, analogous to negotiations around platforms like the S-300 and MiG-31. Contemporary inventories have seen many airframes retired, storage at facilities administered by the Ministry of Defence of the Russian Federation, and select missiles retained in active units or put into refurbishment programs alongside other legacy missiles.

Accidents and Incidents

Accidents and incidents involving the Kh-22 include test failures, accidental detonations during handling and several high-profile crash or stray-fire events during training and conflict-era operations; investigative responses involved agencies such as the Moscow bureau of aviation safety and military commissions. Incidents influenced safety protocols, transport regulations modeled on civil aviation standards like those in the International Civil Aviation Organization sphere, and drove modernization to mitigate risks comparable to lessons learned from other large missile programs such as the R-36 siloed ICBM series.

Category:Ramjet-powered missiles Category:Soviet cruise missiles Category:Anti-ship missiles