Missile R-3 (AA-2 Atoll)

Summary

NATO DesignationAA-2 Atoll
CategoryAir-to-Air Missiles
Sub-typeAir-to-Air Missile
Origin country ๐Ÿ‡ท๐Ÿ‡บ Russia ๐Ÿ‡จ๐Ÿ‡ณ Ex-USSR
ManufacturerVympel
StatusIn service
Year of service1960

Technical specifications

WarheadBlast-fragmentation
Warhead weight11 kg (24 lb)
Diameter127 mm (5.0 in)
Span530 mm (20.9 in)
Length3,420 mm (134.6 in)
Weight93 kg (205 lb)
Range 8.0 km (5.0 mi)
Max. speed3,063 km/h (Mach 3.1)

R-3 scale diagram

R-3 โ€” Air-to-Air 1.75 m 3.42 m
Range
8.0 km
Speed
Mach 3.1
Weight
93 kg
Warhead
11 kg

Operators

๐Ÿ‡ฆ๐Ÿ‡ซ Afghanistan • ๐Ÿ‡ฆ๐Ÿ‡ด Angola • ๐Ÿ‡ฆ๐Ÿ‡ฟ Azerbaijan • ๐Ÿ‡ง๐Ÿ‡ฉ Bangladesh • ๐Ÿ‡ง๐Ÿ‡ฌ Bulgaria • ๐Ÿ‡ง๐Ÿ‡พ Belarus • ๐Ÿ‡จ๐Ÿ‡ณ China • ๐Ÿ‡จ๐Ÿ‡ฌ Congo • ๐Ÿ‡จ๐Ÿ‡บ Cuba • ๐Ÿ‡จ๐Ÿ‡ฟ Czechia • ๐Ÿ‡ฉ๐Ÿ‡ช Germany • ๐Ÿ‡ฉ๐Ÿ‡ฟ Algeria • ๐Ÿ‡ช๐Ÿ‡ฌ Egypt • ๐Ÿ‡ช๐Ÿ‡น Ethiopia • ๐Ÿ‡ซ๐Ÿ‡ฎ Finland • ๐Ÿ‡ฌ๐Ÿ‡ช Georgia • ๐Ÿ‡ฌ๐Ÿ‡ณ Guinea • ๐Ÿ‡ญ๐Ÿ‡ท Croatia • ๐Ÿ‡ญ๐Ÿ‡บ Hungary • ๐Ÿ‡ฎ๐Ÿ‡ฉ Indonesia • ๐Ÿ‡ฎ๐Ÿ‡ณ India • ๐Ÿ‡ฎ๐Ÿ‡ถ Iraq • ๐Ÿ‡ฐ๐Ÿ‡ฟ Kazakhstan • ๐Ÿ‡ฐ๐Ÿ‡ญ Cambodia • ๐Ÿ‡ฑ๐Ÿ‡ฆ Laos • ๐Ÿ‡ฑ๐Ÿ‡พ Libya • ๐Ÿ‡ฒ๐Ÿ‡ฉ Moldova • ๐Ÿ‡ฒ๐Ÿ‡ฌ Madagascar • ๐Ÿ‡ฒ๐Ÿ‡ฑ Mali • ๐Ÿ‡ฒ๐Ÿ‡ณ Mongolia • ๐Ÿ‡ฒ๐Ÿ‡ฟ Mozambique • ๐Ÿ‡ณ๐Ÿ‡ฌ Nigeria • ๐Ÿ‡ต๐Ÿ‡ช Peru • ๐Ÿ‡ต๐Ÿ‡ฑ Poland • ๐Ÿ‡ฐ๐Ÿ‡ต North Korea • ๐Ÿ‡ท๐Ÿ‡ด Romania • ๐Ÿ‡ธ๐Ÿ‡ฉ Sudan • ๐Ÿ‡ธ๐Ÿ‡ด Somalia • ๐Ÿ‡ธ๐Ÿ‡ฐ Slovakia • ๐Ÿ‡ธ๐Ÿ‡พ Syria • ๐Ÿ‡บ๐Ÿ‡ฌ Uganda • ๐Ÿ‡บ๐Ÿ‡ฆ Ukraine • ๐Ÿ‡ป๐Ÿ‡ณ Vietnam • ๐Ÿ‡พ๐Ÿ‡ช Yemen • ๐Ÿ‡ฟ๐Ÿ‡ฒ Zambia

Description

The R-3 (K-13) is a short-range air-to-air missile developed by the Soviet Union as a reverse-engineered copy of the American AIM-9 Sidewinder. During the Second Taiwan Strait Crisis in 1958, a Taiwanese F-86 Sabre fired an AIM-9 Sidewinder that became lodged in a Chinese MiG-17 without exploding. China subsequently transferred the intact missile to the Soviet Union. The missile entered limited Soviet service in 1960, with the improved R-3S variant entering widespread production in 1962.

The missile shares physical design characteristics with the AIM-9, allowing parts between the two systems to be interchanged. Early variants utilize infrared homing, though the R-3S variant is characterized by a long seeker settling time. In 1967, the R-3R variant entered service, employing semi-active radar homing for high-altitude engagements in conjunction with fighter radar systems. Later upgrades, such as the R-13M, introduced a nitrogen-cooled seeker head, increased propellant, and a new proximity fuze, though none of the infrared variants possess all-aspect capability. The missile carries a blast-fragmentation warhead detonated by proximity or contact fuzing. Training variants include the R-3U (inert body with active seeker), R-3P (operational missile without explosive warhead), and RM-3V (aerial target).

The missile was widely deployed within the Warsaw Pact, exported globally, and licensed for production in Romania as the A-91 and in China as the PL-2. It remains in active service with several air forces in Africa, Asia, and South America.

In combat, Chinese forces used the PL-2 variant to intercept United States unmanned aerial vehicles. During the Vietnam War, North Vietnamese MiG-21 pilots utilized the missile against United States aircraft, typically firing in volleys before executing high-speed egress. The Indian Air Force deployed the missile from MiG-21FL fighters during the Indo-Pakistani War of 1971, downing Pakistani F-104 Starfighters.

In the Middle East, Israel captured R-3 missiles during the Six-Day War and subsequently deployed them during the War of Attrition, though pilots recorded no successful engagements. Arab air forces utilized the missile during the Yom Kippur War in 1973, and the Iraqi Air Force deployed it during the Iranโ€“Iraq War. During the 1981 Gulf of Sidra incident, a Libyan Su-22 fired an R-3 head-on at United States Navy F-14As, which successfully evaded the missile.

Frequently Asked Questions

What type of missile is the R-3?
The R-3 (NATO reporting name: AA-2 Atoll) is an air-to-air missile developed by Russia and the Ex-USSR. It entered service in 1960.
What is the range of the R-3?
The R-3 has a maximum range of approximately 8.0 km (5.0 miles). Effective range varies with launch platform, altitude, and flight profile.
How fast is the R-3?
The R-3 reaches a maximum speed of 3,063 km/h (Mach 2.5).
What warhead does the R-3 carry?
The R-3 carries a blast-fragmentation warhead weighing 11 kg.
How is the R-3 guided?
The R-3 uses infrared homing guidance.
Which countries use the R-3?
The R-3 is in service with 45 countries: Afghanistan, Angola, Azerbaijan, and 42 other countries.
Wikipedia (CC BY-SA) and other open sources. Last updated on 10 July 2026. Suggest a change