Missile 9M14 Malyutka (AT-3 Sagger)

Summary

NATO DesignationAT-3 Sagger
CategoryAnti-Tank Missiles
Sub-typeAnti-tank Guided Missile
Origin country ๐Ÿ‡ท๐Ÿ‡บ Russia
ManufacturerSoviet Union
StatusIn service
Year of service1963
Est. avg unit price$0.0 million

Technical specifications

WarheadTandem HEAT
Diameter125 mm (4.9 in)
Span393 mm (15.5 in)
Length1,005 mm (39.6 in)
Weight13 kg (29 lb)
Range 3.0 km (1.9 mi)
Max. speed414 km/h (Mach 0.4)

Operators

๐Ÿ‡ฆ๐Ÿ‡ซ Afghanistan • ๐Ÿ‡ฆ๐Ÿ‡ด Angola • ๐Ÿ‡ฆ๐Ÿ‡ฑ Albania • ๐Ÿ‡ฆ๐Ÿ‡ฒ Armenia • ๐Ÿ‡ฆ๐Ÿ‡ฟ Azerbaijan • ๐Ÿ‡ง๐Ÿ‡ฉ Bangladesh • ๐Ÿ‡ง๐Ÿ‡ฌ Bulgaria • ๐Ÿ‡ง๐Ÿ‡ฆ Bosnia and Herzegovina • ๐Ÿ‡จ๐Ÿ‡ณ China • ๐Ÿ‡จ๐Ÿ‡ฌ Congo • ๐Ÿ‡จ๐Ÿ‡บ Cuba • ๐Ÿ‡จ๐Ÿ‡ฟ Czech Republic • ๐Ÿ‡ฉ๐Ÿ‡ฟ Algeria • ๐Ÿ‡ช๐Ÿ‡ฌ Egypt • ๐Ÿ‡ช๐Ÿ‡ท Eritrea • ๐Ÿ‡ช๐Ÿ‡น Ethiopia • ๐Ÿ‡ซ๐Ÿ‡ฎ Finland • ๐Ÿ‡ฌ๐Ÿ‡ช Georgia • ๐Ÿ‡ฌ๐Ÿ‡ณ Guinea • ๐Ÿ‡ฌ๐Ÿ‡ผ Guinea-Bissau • ๐Ÿ‡ญ๐Ÿ‡ท Croatia • ๐Ÿ‡ญ๐Ÿ‡บ Hungary • ๐Ÿ‡ฎ๐Ÿ‡ฉ Indonesia • ๐Ÿ‡ฎ๐Ÿ‡ณ India • ๐Ÿ‡ฎ๐Ÿ‡ท Iran • ๐Ÿ‡ฎ๐Ÿ‡ถ Iraq • ๐Ÿ‡ฎ๐Ÿ‡ฑ Israel • ๐Ÿ‡ฐ๐Ÿ‡ฌ Kyrgyzstan • ๐Ÿ‡ฐ๐Ÿ‡ญ Cambodia • ๐Ÿ‡ฑ๐Ÿ‡พ Libya • ๐Ÿ‡ฑ๐Ÿ‡ป Latvia • ๐Ÿ‡ฒ๐Ÿ‡ฆ Morocco • ๐Ÿ‡ฒ๐Ÿ‡ฐ North Macedonia • ๐Ÿ‡ฒ๐Ÿ‡ฑ Mali • ๐Ÿ‡ฒ๐Ÿ‡ณ Mongolia • ๐Ÿ‡ฒ๐Ÿ‡ฟ Mozambique • ๐Ÿ‡ณ๐Ÿ‡ฎ Nicaragua • ๐Ÿ‡ต๐Ÿ‡ช Peru • ๐Ÿ‡ต๐Ÿ‡ฑ Poland • ๐Ÿ‡ฐ๐Ÿ‡ต North Korea • ๐Ÿ‡ท๐Ÿ‡ด Romania • ๐Ÿ‡ท๐Ÿ‡บ Russia • ๐Ÿ‡ธ๐Ÿ‡ฉ Sudan • ๐Ÿ‡ธ๐Ÿ‡ด Somalia • ๐Ÿ‡ท๐Ÿ‡ธ Serbia • ๐Ÿ‡ธ๐Ÿ‡ธ South Sudan • ๐Ÿ‡ธ๐Ÿ‡ฐ Slovakia • ๐Ÿ‡ธ๐Ÿ‡ฎ Slovenia • ๐Ÿ‡ธ๐Ÿ‡พ Syria • ๐Ÿ‡น๐Ÿ‡ฒ Turkmenistan • ๐Ÿ‡น๐Ÿ‡ผ Taiwan • ๐Ÿ‡บ๐Ÿ‡ฌ Uganda • ๐Ÿ‡บ๐Ÿ‡ฟ Uzbekistan • ๐Ÿ‡ป๐Ÿ‡ณ Vietnam • ๐Ÿ‡พ๐Ÿ‡ช Yemen • ๐Ÿ‡ฟ๐Ÿ‡ฒ Zambia

Description

Development of this wire-guided anti-tank missile began in 1961, with the project aiming to create a man-portable and vehicle-mountable system based on contemporary Western designs. Following tests in 1962, the system entered service in 1963.

The missile utilizes Manual Command to Line of Sight (MCLOS) guidance in its initial configuration. Operators control the flight path via a joystick, with commands transmitted through a thin wire that trails behind the missile. The system employs a gyroscope for orientation and maintains flight stability through wing-induced rotation. The missile's flight profile includes an immediate climb after launch to avoid ground obstacles. Later variants introduced Semi-Automatic Command to Line of Sight (SACLOS) guidance for ground vehicle and helicopter mounts, which simplified operator input requirements. Launch platforms include a portable suitcase that doubles as a launching base, armored vehicles such as the BMP-1 and BRDM-2, and various helicopters.

Warhead options evolved to address advancing armor technology. Early models featured standard High-Explosive Anti-Tank (HEAT) warheads. Subsequent developments introduced tandem-charge warheads and standoff probes designed to counter explosive reactive armor. A thermobaric variant was also produced for use against personnel and unarmored targets. Modernized versions have been integrated with thermal imaging systems for target acquisition.

The system is widely deployed and has been manufactured under license or as domestic versions in numerous countries, including China, Iran, North Korea, Serbia, Vietnam, Romania, and Taiwan. In Soviet service, the man-portable version was assigned to anti-tank platoons within motor rifle battalions, often paired with RPG-7 teams to cover the deadzone created by the missile's minimum engagement distance.

Combat use began during the Vietnam War in 1972, where it was employed against M48 Patton tanks and M113 armored vehicles. During the Yom Kippur War, Arab forces utilized the missile to destroy several hundred Israeli armored vehicles, leading to the development of specific artillery and maneuver countermeasures by Israeli forces. The system has been used in numerous regional conflicts, including the Iran-Iraq War, the Lebanese Civil War, and the Gulf War. It remains in service with various state militaries and non-state actors, including Hezbollah and Hamas, and has been documented in recent conflicts in Libya, Syria, Yemen, and Ethiopia.

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