In numbers Through the lens Video
NATO reporting name: AA-3 Anab
Αlso known as: Izdeliye 24M, R-8M
Design and development of the missile began in the 1950s (specifically in 1955) by the OKB-4 design bureau, as a first-generation missile. Its first launch was made by a Yak-28K aircraft.
However, the final product, version K-8-2 (later K-8M - Izdelie 24M) was intended for the Su-11 fighters carrying the "Eagle" type radar. The K-8M missile could engage targets at heights of up to 500 m (while the K-8 had a minimum range of 5ю000 m).
Their speed reached almost 1,015 m/sec. In February 1962 the missile entered service and armed Su-11-8M aircraft. Its last, most improved version was the K-98M missile (NATO designation AA-3-2 Advanced Anab).
Technical specifications
| DESIGNER | "Vympel" Design buream |
| COUNTRY | Russia |
| TYPE |
Short range air-to-air missile
|
| Aircraft-bearer (aerial means) |
Yak-28K, Su-11-VM, Su-9-51, Su-11
|
|
POWER-PLANT
|
Solid fuel booster rocket engine
|
|
Thrust, kg
|
- |
|
DIMENSIONS
|
|
|
Length, m
|
|
|
R-8M1R
|
4,18
|
|
R-8M1T
|
4,05
|
|
Diameter, m
|
0,275
|
|
Wing span, m
|
-
|
|
Fin span, m
|
1,233
|
|
WEIGHT
|
|
|
Maximum missile weight, kg
|
|
|
R-8M1R
|
285
|
|
R-8M1T
|
265
|
|
Warhead weight, kg
|
40
|
|
PERFORMANCE
|
|
|
Maximum speed, km/h
|
+2.124 |
|
Target g-load, g
|
|
|
Flight altitude, km
|
- |
|
Maximum launch range, km
|
|
|
R-8M1R
|
2-20
|
|
R-8M1T
|
2-14
|
|
Caliber, mm
|
-
|
|
Warhead type
|
High-explosive |
|
Target capture, flying at supersonic speeds, km/h
|
- |
|
Fighter type target kill probability
|
- |
|
Guidance system
|
|
|
R-8M1R
|
Semiactive radar
|
|
R-8M1T
|
Infrared (IR)
|