The R-73E air-to-air missile is designed to engage air targets (fighters, bombers, military transport aircraft) in dogfight from any direction, day or night, against the earth background and in a heavy ECM environment. It is used on fighters, bombers and attack aircraft.
Its high agility is achieved through the use of a unique combined gas/aerodynamic control system enabling thrust vectoring.
The missile attacks a target within the off-boresight angles of ± 45˚ at line-of-sight rates of up to 60 deg/s. It is capable of intercepting targets flying at speeds up to 2,500 km/h and altitudes of 0.02 to 20 km.
| Firing range, km: | |
| max (in FHS) | 30 |
| min (in RHS) | 0,3 |
| - | - |
| Launch/warhead weight, kg | 105/8 |
| Warhead type | rod |
| Guidance system | all-aspect passive infrared homing |
| Fuzing device | radar proximity target sensor |
| Off-boresight/seeker deflection angle, deg | ±45/±75 |
| Target load factor, g | up to 12 |
| Dimensions (length/diameter/wingspan), m | 2,9 х 0,17 х 0,51 |
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