| Specifications |
|---|
| Contractor |
|
|
Year | 1975
|
|
Type | medium-range missile
|
|
Modifications |
Semi-active radar guidance
Passive infra-red guidance
|
|
Wingspan | 1.0 m
|
|
Length (SAR version) | 4.5 m
|
|
Length (IR version) | 4.2 m
|
|
Diameter | 0.22 m
|
|
Launch weight | 320 kg
|
|
Max. speed | 3420 km/h (Mach=3.0)
|
|
Maximum range (SAR version) | 35 km
|
|
Maximum range (IR version) | 15 km
|
|
Propulsion | two stage solid propellant rocket motor
|
|
Guidance | semi-active radar homing or passive infra-red homing
|
|
Warhead | proximity-fuzed high-explosive, 40 kg
|
|
Carried by | MiG-23
|
|
Service | USSR, Czechoslovakia, Libya, India, East Germany. |
