«KORNET-EM»

MULTI-PURPOSE LONG-RANGE
MISSILE SYSTEM

Is designed to engage existing and future combat tanks protected by explosive reactive armor, light armored vehicles, fortifications, surface, low-speed air targets (helicopters, UAVs) by day and at night, in adverse weather conditions as well as in optical and radio jamming environment.
  • Photo

  • Basic Performances

Firing range
min .............................................. 150 m
max .............................................. 10000 m
Guidance system ........................ semi-automatic,
laser beam riding
Armor penetration
capability behind ERA. ...............

1100-1300 mm
TNT equivalent
for HE warhead ............................

at least 7 kg
Weight
launcher ...................................... 26 kg
thermal imager ......................... 8.7 kg
  • System components

  • Combat equipment:
    • launcher
      • Launcher

      1. Sighting and guidance unit.
      2. Tripod.

      Sighting and guidance unit provides visual detection and tracking of the target, range finding up to target, laser beam control field forming and missile launch signals generation.

      Basic Characteristics

      Laying angles
      on azimuth ................................ 360 deg
      on elevation .............................. from -5 to +20 deg
      Sighting and guidance unit FOV
      when magnification 12x ......... 5 deg
      when magnification 20x ......... 3 deg
    • 9М133М-2 antitank guided missile
      • 9М133М-2 antitank guided missile

      Flight range ............................................................. 150-8000 m
      Armor penetration .................................................. 1100-1300 mm
      Max flying speed ..................................................... 300 m/sec
      Weight with the container ...................................... 31 kg
      Container length ..................................................... 1210 mm
    • 9М133FМ-3 guided missile
      • 9М133FМ-3 guided missile

      Flight range ............................................................ 150-10000 m
      TNT equivalent ...................................................... 7 kg
      Max flying speed ................................................... 320 m/sec
      Weight with the container .................................... 33 kg
      Container length .................................................... 1210 mm
    • thermal imaging sight
      • Thermal imaging sight

      3-rd generation thermal imaging sight of Kornet EM vehicle carried\portable system is designed on matrix photodetector basis. Its peculiar feature – complete absence of mechanical scanning. Photosensitive matrix is cooled by miniature gas cryogenic machine operating under Stirling cycle.

      Field of view (FOV)
      narrow .................................... 1.9х2.4 deg
      wide ........................................ 5.9х7.3 deg
      Photodetector .......................... matrix type
      with thermal
      enclosure system
      Power supply .......................... from battery
      Continuous
      operation time .........................

      at least 1.5 h
      Cooling time ............................ not more than 7 min
  • Maintenance facilities
    • Maintenance facilities

    Test equipment to check the launcher

    Test equipment to check thermal imaging sight

  • Training facilities
    • Training facilities

    Computer-based simulator for operators indoor training

    Field simulator for operators training in launcher field operation

  • Advantages and operating features

  • Enhanced energy potential of laser beam riding system.
  • Sighting channel with variable zoom factor 12х and 20х, providing targets detection range increase and reduction of sighting errors.
  • Possibility to install the system (using the bracket) on wide range of wheeled and tracked vehicles.
  • System provides firing by all missiles of Kornet-E family.