AA-3 ANAB
K-8
PL-2 [China]
| Specifications | |
|---|---|
| Contractor | |
| Year | 1961 |
| Type | medium-range intercept missile |
| Modifications |
Semi-active I-band and J-band radar guidance Passive infra-red guidance |
| Wingspan | 1.3 m |
| Length (SAR version) | 4.1 m |
| Length (IR version) | 4.0 m |
| Diameter | 0.28 m |
| Launch weight | 275 kg |
| Max. speed | 3420 km/h (Mach=3.0) |
| Maximum range | 19 km |
| Propulsion | single stage solid propellant rocket motor |
| Guidance | semi-active I-band and J-band radar homing or passive infra-red homing |
| Warhead | proximity-fuzed high-explosive blast |
| Carried by | Yak-28, Su-15 |
| Service | USSR, Bulgaria, Romaina, Poland, East Germany, Hungary, Czechoslovakia |
