Federal Service

for Military-Technical Cooperation

ASF Armament and Equipment
Kh-31PKAircraft High-Speed Air-to-RS Missile

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

6501 250

Launch altitude range, km

0.115

Missile launch weight, kg

605+(-)10

Overall missile dimensions, m:

length

diameter

canard span

 

4.8

0.36

0.914