Airborne guided missile Χ-31PK (Kh-31PK) © Konstantinos Panitsidis

Photos from the personal collection of Kostas Panitsidis


 Technical specifications      Photos      Video

 

 

Kh-31PK airborne guided missile is a tactical high-speed missile with passive homing heads (GSN) and intended for effective hitting of radars, including radars with antennas brought up (up to 15 m), from configuration of medium-range and long-range anti-aircraft missile systems, and also other ground-based radars that operate in the appropriate wavelength range. 

Kh-31PK is developed by upgrading of Kh-31P missile as related to equipping with non-contact sensor of destruction and warhead with higher efficiency.

 


TECHNICAL SPECIFICATIONS

Design Bureau "Zvezda"
Launch ranges, km 15-110
Launch altitudes, m 100-15.000
Launch speeds, km/h (Mach) 650-1.250
Warhead weight, kg 88,5 ± 2,5
Launch weight of missile, kg 605 ± 10
Overall dimensions, m  
length 4,8
shell diameter 0,36
wing span 0,914

  


PHOTOS Χ-31PK (Kh-31PK)