PURPOSE
Kh-31PK aircraft guided missile is a tactical high-speed missile with passive homing heads (HH) and designed for efficient attacking the RS, inclusive of those with the antennas removed upward (up to 15 m) as part of the medium- and long-range AAMS and other ground-based RS operated in the appropriate frequency band.
Kh-31PK missile was designed via Kh-31P missile modification with regard to its equipping with the non-contact detonation sensor and highly efficient warhead.
MAIN SPECIFICATIONS
Launch range, km |
up to 110 |
Launch speed range, km/s |
650–1 250 |
Launch altitude range, km |
0.1–15 |
Missile launch weight, kg |
605+(-)10 |
Overall missile dimensions, m:
length
diameter
canard span |
4.8
0.36
0.914 |
|