Difference between revisions of "File:WT missiles 16.jpg"

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{| class="wikitable"
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|SYSTEM FEATURES
  
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* Multi-purpose missile for use by infantry, armoured or helicopter forces against modern threats
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* Crossfire copebily from adjacent platforms
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* High-speed launch from helicopter platforms
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* Fire-on-the-move from land plattarms
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* High countermeasure resstonce
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* High-accuracy laser beam-riding guidance
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* Short: and long-range opplication (250 m to 5 000 m)
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* Easy to use, with automatic target tracking 
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|PRINCIPLE OF
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OPERATION
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Ingwe uses laser beam-riding guidance. The missile automatically determines its own position in the laser beam and manoeuvres onto the line of sight. The missile follows the line of sight until the target is hit. The warhead ensures effective target neutralization.
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The sighting system can vary from a non-stabilized optical sight for light vehicles to a more complex and integrated stabilized day/night sight for moving platforms such as helicopters. Automatic target-tracking modules can be added to ensure fully automatic missile guidance after target lock-on by the operator.
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|-
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|SYSTEM
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DESCRIPTION
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The system is designed to ensure that it can be installed easily on most aircraft in either standard two- or four-missile configuration.
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Electrical integration with aircraft avionics is achieved with standard serial communication interfaces.
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Other platform options include heavy IFV turrets fitted with stabilized sighting systems, to light vehicle- and even tripod-mounted solutions.
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|
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|}

Revision as of 13:45, 30 August 2021

SYSTEM FEATURES
  • Multi-purpose missile for use by infantry, armoured or helicopter forces against modern threats
  • Crossfire copebily from adjacent platforms
  • High-speed launch from helicopter platforms
  • Fire-on-the-move from land plattarms
  • High countermeasure resstonce
  • High-accuracy laser beam-riding guidance
  • Short: and long-range opplication (250 m to 5 000 m)
  • Easy to use, with automatic target tracking 
PRINCIPLE OF

OPERATION

Ingwe uses laser beam-riding guidance. The missile automatically determines its own position in the laser beam and manoeuvres onto the line of sight. The missile follows the line of sight until the target is hit. The warhead ensures effective target neutralization.

The sighting system can vary from a non-stabilized optical sight for light vehicles to a more complex and integrated stabilized day/night sight for moving platforms such as helicopters. Automatic target-tracking modules can be added to ensure fully automatic missile guidance after target lock-on by the operator.

SYSTEM

DESCRIPTION

The system is designed to ensure that it can be installed easily on most aircraft in either standard two- or four-missile configuration.

Electrical integration with aircraft avionics is achieved with standard serial communication interfaces.

Other platform options include heavy IFV turrets fitted with stabilized sighting systems, to light vehicle- and even tripod-mounted solutions.

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current12:56, 30 August 2021Thumbnail for version as of 12:56, 30 August 20211,241 × 1,754 (279 KB)VolgaIgor (talk | contribs)
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