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Vympel R-3


NATO: AA-2 Atoll


Overview


R-3S

Soviet R-3S (NATO: AA-2B Atoll B) infrared homing missile on display in a museum.
Source: cliff1066 - © CC BY-SA 2.0

Origin
Soviet Union
Type
Short range air to air missile
Entered service
1962 for R-3S
1967 for R-3R
Status
Limited service
Development
1954 - 1958 (R-3S)
1959 (Soviet state trials for R-3S)
1962 - 1966 (Soviet state trials for R-3R)
Developer
Soviet Union - OKB-134 Vympel design bureau
Production
1960 - ? (R-3S)
1966 - ? (R-3R)
Producer
Soviet Union
Number produced
Produced in large quantities
Designations
AA-2 Atoll (NATO reporting name)
K-13A (entire complex for R-3A)
K-13R (entire complex for R-3R)
Notable users
Soviet Union

Description


Introduction

The R-3 is an early Cold War era short range air to air missile of Soviet origin. Development began in the mid 1950's and was greatly influenced by espionage and captured American AIM-9B Sidewinder missiles. The decision was made to practically reverse engineer the entire AIM-9B and include only limited amounts of Soviet components. the NATO reporting name is AA-2 Atoll.

Design

The R-3S is a near direct copy of the American AIM-9B Sidewinder missile. The reverse engineering was carried out to such a degree that many parts are interchangeable. The main differences are a different type of rocket fuel and the design of the seeker head, although performance is roughly similar. The R-3R was introduced half a decade later and has a longer body with semi-active radar homing head. This was a domestic development analogous yet different to the American AIM-9C.

Guidance

The R-3S has a passive infrared homing seeker. The seeker is uncooled and has a limited tracking rate. This makes it vulnerable against flares and maneuvering targets. The R-3R is a variant with semi-active radar homing. It is intended for high altitude interception of non-maneuvering targets. The R-3S is a rear aspect only missile. The R-3R also has a limited head on capability.

Firepower

The R-3S provided a similar capability as the American AIM-9B Sidewinder. Maximum effective range was 7.6 km, with a minimum range of 0.9 km. The uncooled seeker of the R-3S is easily foiled by infrared flares. The same goes for the R-3R with chaff respectively.

Platforms

The R-3S was introduced on a wide range of Soviet fighter aircraft. These include (variants of) the MiG-17, MiG-19, MiG-21, MiG-23, Su-7, Yak-25 and various others. The R-3R requires a compatible radar to illuminate the target. The include the MiG-21S up to the final MiG-21bis variant and early models of the MiG-23.

Users

The R-3S was adopted by the Soviet Union in 1962 and used in large quantities on many types of aircraft. Large numbers were exported. China produced their local copy as the PL-2. The radar guided R-3R was less common, but still used in quantity. The R-3R was also exported to various nations. The introduction of the improved R-13M (NATO: AA-2D or AA-2-2 Advanced Atoll) or new R-60 (NATO: AA-8 Aphid) designs made the R-3S obsolete in Soviet service.

Variants


R-3S

Soviet R-3S (NATO: AA-2B Atoll B) infrared homing missile seen under the wing of a MiG-21 on display in a museum in Hungary in 2005.
Source: Varga Attila - © CC BY-SA 3.0

List of R-3 missiles

R-3
Prototype variant. Also known as the K-13 or Obyekt 300. Used in state testing project and possibly as a small first operational batch of missiles. NATO reporting name is AA-2A Atoll A.
R-3S
Infrared guided and most common version of the R-3 missile. Introduced in 1962. The S denotes it as the series production variant. Known as K-13A and Obyekt 310. Intended for high altitude interception of non-maneuvering targets. NATO reporting name is AA-2B Atoll B.
R-3R
Semi-active radar homing variant of the R-3 missile. Introduced in 1967. Known as K-13R and Obyekt 320. This model can only be launched from aircraft with a compatible radar sets, such as variants of the MiG-21 and MiG-23. The NATO reporting name is AA-2C Atoll C.

Details


Facts R-3S R-3R
General
Origin
Soviet Union
Type
Short range air to air missile
Dimensions
Length
2.838 mm
Diameter
127 mm
Wingspan
528 mm
Weight
75.3 kg
Guidance
Guidance mode
Passive infrared homing
Seeker model
TGS-13K
Cooling
Uncooled
Lock range
About 3.5 km
Aspect
Rear aspect only
Warhead
Type
High explosive fragmentation
Weight
11.3 kg total with 5.3 kg TGAF-5 explosive
Fuse
Optical proximity fuse
Secondary contact fuse
Propulsion
Type
Solid propellant rocket motor
Model
PRD-80A
Engagement envelope
Speed
550 m/s
Range
7.6 km maximum
0.9 km minimum
Altitude
21.5 km max operational altitude
Flight type
21 second controlled flight
G force
3 G target maneuvers

Media


Related articles


AIM-9B Sidewinder

The R-3S is a near direct copy of the American AIM-9B Sidewinder. One missile was recovered and sent to the Soviet Union for testing and reverse engineering after getting stuck in the fuselage of a Chinese MiG-17 during the Second Taiwan Strait Crisis in 1958.

AIM-9C Sidewinder

The R-3R was not a direct copy of the American AIM-9C but was a domestic development. The Soviet R-3R has a much larger homing section than the AIM-9C. Unlike the AIM-9C the R-3R proved relatively capable and successful under more capable designs were introduced.