Federal Service

for Military-Technical Cooperation

ASF Armament and Equipment
RVV-SDAircraft Air-to-Air Missiles

 

SPECIFIC FEATURES

  • Propulsion system –  fixed thrust SRB.
  • Fuzes – laser non-contact target sensor.
  • Guidance system –  inertial radio-correction system at the initial path section with active radar homing at the end section.
  • Warhead –  rod multi-unit shaped charge.
 

PURPOSE AND MAIN TASKS

The medium-range aircraft air-to-air missile is designed for hitting the air-borne targets (fighters, attack aircraft, bombers, military carrier aircraft, helicopters, cruise missiles) day-and-night, at any angle under electronic countermeasures conditions against the earth and water surface background, inclusive of the multiple target “fire-and-forget” firing.

 

 

MAIN SPECIFICATIONS

Launch range, km:

maximum to the FA

minimum to the RA

 

up to 110

0.3

Hit target altitude, km

0.02...25

Hit target acceleration, g

up to 12

Warhead weight, kg

22.5

Launch weight, kg

190

Overall missile dimensions, mm:

length

diameter

wing span

control span

 

3 710

200

420

680