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Interface Blanking Unit

It has developed to ensure compatibility between units that are in the air, land, and sea vehicles advanced for use in different fields and that simultaneously broadcast RF. It creates a blanking signal in various configurations depending on the vehicle it is used in and maintains RF compatibility between the units broadcasting in the vehicle. It offers solutions to fixed-wing and rotary-wing aircraft with its design and environmental tests by military standards.

  • Matrix Configuration for Different Scenarios
  • Programmable Blanking Inputs/Outputs
  • Blanking Pulse Modification
  • Repeater
  • Delay
  • Look Through Blanking Outputs Generation
  • Built-in Tests
  • 12 Low Voltage Blanking Output
  • 12 High Voltage Blanking Outputs
  • MIL-STD-1553 Communication
  • ARINC-429 Communication
  • RS422 Communication
  • 28 VDC Power Input
  • Power Hold-up for Short Power Interrupts
  • MIL-STD-810G, Compliance with Environmental Conditions in Standards
  • DO-254, Compliance with Aviation Standards
  • MIL-STD-461F, Compliance with Environmental Conditions in Standards
  • Operating Temperature and Altitude: -55°C / +95°C, 45.000 ft.
  • Storage Temperature: -55°C / +95°C