Generated by GPT-5-mini| 9K114 Shturm | |
|---|---|
| Name | 9K114 Shturm |
| Origin | Soviet Union |
| Type | Anti-tank guided missile |
| Service | 1976–present |
| Used by | See Operators |
| Designer | KB Mashinostroyeniya |
| Design date | 1960s–1970s |
| Manufacturer | Degtyarev Plant |
| Production date | 1970s–1980s |
| Filling | HEAT |
| Engine | Solid-fuel rocket |
| Vehicle range | 400–5,000 m |
| Guidance | Tube-launched SACLOS radio/command link |
9K114 Shturm is a Soviet-era tube-launched anti-tank guided missile system developed in the Cold War period for engagement of armored vehicles, fortifications, and low-flying helicopters. Introduced into service in the 1970s, it complemented platforms such as the Mil Mi-24 and various armored vehicles, and saw export to allied states across Asia, Africa, and the Middle East. The system reflects design trends established by Soviet design bureaus and was employed in multiple regional conflicts during the late 20th and early 21st centuries.
Development began under direction of KB Mashinostroyeniya and serial production involved manufacturers like the Degtyarev Plant and other Soviet industrial complexes linked to the Ministry of Defence of the USSR. The program followed doctrinal requirements influenced by lessons from the Yom Kippur War and study of Western systems such as the BGM-71 TOW and M47 Dragon, aiming for a missile with semi-automatic command to line-of-sight guidance for use from rotary-wing and tracked platforms. Designers incorporated a solid-propellant motor, tandem-charge and single HEAT warhead options, and a radio-command link derived from earlier projects associated with the 9K112 Kobra and elements traced to work at Tula Arms Plant facilities. Flight-control surfaces, launch tube integration, and seeker electronics were developed with inputs from institutes that collaborated with the Soviet Ground Forces and Aviation Industry design teams.
The system's baseline performance metrics reflect Soviet prioritization of range and platform flexibility: effective engagement envelope approximately 400–5,000 m, missile length and diameter sized for carriage in tube launchers fitted to platforms like the Mil Mi-24 and infantry fighting vehicles such as the BMP-2. Guidance is semi-automatic command to line-of-sight (SACLOS) using a radio or wire command link, compatible with onboard sighting systems influenced by optics standards employed by the Zvezda and BelOMO instrument makers. The warhead variants include shaped-charge HEAT warheads intended to defeat armor comparable to contemporary main battle tanks fielded by the NATO members, and fragmentation/thermobaric options for use against fortifications. The missile's propulsion is a two-stage solid rocket motor allowing a boost phase and sustain flight, with control surfaces similar in concept to those used on contemporaneous Soviet anti-armor guided munitions developed under oversight by the Soviet Academy of Sciences research institutes.
Introduced in the 1970s, the system entered service with the Soviet Army and was integrated into platforms serving in Warsaw Pact countries including East Germany, Czechoslovakia, and Poland. Exports reached client states such as Syria, Iraq, Libya, Egypt, India, and several African militaries, shaping its operational record in conflicts like the Iran–Iraq War, the Soviet–Afghan War, and various engagements during the Lebanese Civil War. The system's deployment on rotary-wing platforms influenced tactics for anti-armor employment adopted by air arms including the Soviet Air Force and later successor services in the Russian Aerospace Forces. Post-Soviet successor states evaluated and retained stocks, while some units were modified for use by irregular forces during regional insurgencies across the Middle East and North Africa.
Variants include baseline tube-launched missiles for helicopter mounting, vehicle-fired versions integrated on tracked chassis similar to platforms used by Soviet Ground Forces, and export models adapted to local sighting and power systems supplied to customers like India and Egypt. Improved guidance and warhead upgrades paralleled developments seen in later systems such as 9K121 Vikhr and were sometimes retrofitted to extend service life. Licensed-production or locally produced derivatives appeared in some recipient states, reflecting manufacturing collaborations between firms influenced by treaties and agreements involving entities like the Interkosmos-era industrial linkages.
Primary original operator was the Soviet Union; successor and export users included Russia, Ukraine, Syria, Iraq, Libya, Egypt, India, Poland, Czech Republic, Slovakia, Bulgaria, Romania, Algeria, Angola, Ethiopia, Sudan, and several other African and Middle Eastern states. Non-state actors captured stocks during conflicts in Iraq and Syria and subsequently employed them. Some NATO countries studied captured examples during exercises coordinated with organizations like NATO and bilateral exchanges involving the United States and United Kingdom.
Combat records indicate mixed effectiveness: in engagements against older generation main battle tanks fielded by adversaries during the Iran–Iraq War and other 1980s conflicts, the system achieved successful penetrations attributed to its HEAT warhead design, but effectiveness decreased against later generations of explosive reactive armor and composite armor introduced by NATO states. Helicopter-launched employment exposed vulnerabilities to air defenses used by forces such as those trained by United States advisers in client states; however, in asymmetric conflicts with limited air-defense capability, the missile remained a potent anti-armor and anti-material weapon. Analyses by defense research bodies in Russia and Western institutes compared its performance to contemporaries like the BGM-71 TOW and Euromissile HOT, noting advantages in integration with Soviet platforms and limitations in countermeasure resistance and penetration versus modern armor arrays.
Category:Anti-tank guided missiles