| Contractor | NPO Mashinostroyenie
|
| Entered Service |
|
| Maximum range, Afternoon |
10,000 m
Effective against ground & air targets at converging speeds to 800 km/h.
|
| Maximum range, Night | 5 (6) km
|
| Starting height | 5 - 4000 [5] m
|
| Flight time |
|
| At maximum range | 28
|
| At the distance of 8000 m | 23
|
| At the distance of 6000 m | 14
|
| The average flight speed | 600 m / s
|
| Application temperature range | from -50 ° C to +50 ° C
|
| Rocket
|
| Acceptable types of missiles | 9A4172
|
| Weight and size characteristics |
|
| Rockets |
|
| Length | 2.75 m
|
| diameter of the housing (max) | 0,13 m
|
| Wing span | 0.24 m
|
| Stabilizers | 0.38 m
|
| Weight | 45 kg
|
| TPK |
|
| Length | 2.8 m
|
| Diameter | 0.14 m
|
| Weight | 59 kg
|
| Warhead |
|
| Type | tandem shaped-charge fragmentation
|
| Weight, Warhead | 8-12 kg
|
| Weight, Explosive | 4 - 5,5 kg
|
| Fuse | contact and non-contact (2.5 - 3 m)
|
| Management and guidance
|
| Possible control types | I-251 "Flurry"
|
| Guidance mode | Laser Beam Rider SACLOS
|
| Penetration | 900 mm
|
| Single-shot hit probability | 0.95 probability claimed
|
| control channels Day | TV
|
| control channels Night | a low-level TV
|
| Target tracking | automatic
|
| Launcher
|
| Possible types | APU-8/6-APA
|
| Media | Su-25T / 39 / Ka-50 / 52
|
| The number of missiles in PU | 8/6
|
| Weight and size characteristics |
|
| Length | 1.524 m
|
| Width | 0.72 m
|
| Height | 0.436 m
|
| Weight | 60 kg (empty)
|
| Pointing angle in a vertical plane | 10 °
|
