AA-2 ATOLL
K-13 (R-3 or Object 310)
PL-2 / PL-3 / PL-5
| Specifications | ||
|---|---|---|
| Year | 1961 | |
| Type | short-range missile | |
| Modifications |
AA-2 - infra-red guidance AA-2-2 "Advanced Atoll" - semi-active radar guidance | |
| Wingspan (AA-2) | 0.45 m | |
| Wingspan (AA-2-2) | 0.53 m | |
| Length (AA-2) | 2.8 m | |
| Length (AA-2-2) | 3.0 m | |
| Diameter | 0.12 m | |
| Launch weight | 70 kg | |
| Max. speed | 2850 km/h | |
| Maximum range | 6.5 km | |
| Propulsion | solid propellant rocket motor | |
| Guidance | passive infra-red homing or semi-active radar homing | |
| Warhead | proximity-fuzed blast fragmentation, 6 kg | |
| Service | USSR, India, South Yemen, Romania, Afghanistan, North Yemen, North Vietnam, Albania, Nigeria, Uganda, Iraq, Poland, Syria, Algeria, Sudan, Morocco, Somalia, Angola, Bangladesh, Peru, Yugoslavia, Mozambique, China, Libya, Hungary, Laos, North Korea, Ethiopia, East Germany, Finland, Czechoslovakia, Cuba, Bulgaria. | |
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