| Specifications |
|---|
| NATO Code | AA-12 Adder
|
| Developer | State Design Bureau "Vympel"
|
| Chief Designer | GA Sokolov . works of VA Pustovoytov, VG Bogatsky
|
| Manufacturer | before 1991 production in Ukraine, currently mastered in Russia JSC "Dux"
|
| Type | high-maneuverable medium-range missile of the fourth generation
|
| Arms | since 1994
|
| carrier aircraft | Su-27, MiG-29, MiG-29M, MiG-29SMT, MiG-29UBT, MiG-29K, MiG-31, MiG-31M, Yak-141, Su-27IB, Su-35, Su-37 , MiG-21-93, MiG-23-98
|
| Warhead | type rod with microcumulative elements -
|
| developer | State NIIMash
|
| designer | SNNikitin
|
| warhead weight, kg | 18 (21-22)
|
| fuse type | non-contact laser and contact
|
| developer | NIIEP
|
| Combined | inertial control system with radiorecretion and active RLGSN
|
| Self-guidance head | type multipurpose monopulse Doppler active radar 9B-1348E (9B-1348)
|
| developer | MNII "Agat" and GNPP "Istok"
|
| target acquisition range | with EPR = 5m2 16 -20
|
| ready time after pre-activation | 2 min. with the procedure of self-tuning of the parameters of the detection and tracking channels for speed and angles, with 1
|
| target designation angle, deg. | +9020
|
| method of aiming | proportional or by special trajectories with organized enemy interference
|
| range of the radio-correction channel (with the MiG-29 airplane), km |
the first export options up to 50 in the PPS at a maximum range of up to 80
|
| weight of the fairing, kg | 16
|
| length, mm | 604
|
| diameter, mm | 200
|
| Controls | aerodynamic rudders
|
| Steering | collapsible aerodynamic latticework - electric control drive
|
| Angles of attack, degrees. | up to 40
|
| Type of air launch | dropping from the carrier aircraft (catapult) or descent from the guiding range
|
| Range, km: | in the PPS (first versions) 0.3 - 70 - in the PPS (serial missile) 0.3-100
|
| Target speed, km / h | up to 3600-3700
|
| Missile speed, the number | M 4 - 4,5
|
| height of the launch, km: | - in the PPS 0,02-25 (28 - 30)
|
| Height of the target's excess (decrease) | km 10
|
| Probability of target destruction | 0.7
|
| Number of stages | 1
|
| Length of rocket, mm | 3600
|
| Max. diameter of the body, mm | 200
|
| Wingspan, mm | 454-530 (420)
|
| Width of rudders, mm | 740-750 (folded) 300
|
| Starting weight, kg | 175-180
|
| engine: - type | RDTT
|
| manufacturer of charge | SMKirova
|
