Lightning Protection Test for Aircraft MIL-464C DO-160F G Section23 Lightning Protection Test for Aircraft MIL-464C DO-160F G Section23 Lightning Protection Test for Aircraft MIL-464C DO-160F G Section23 Lightning Protection Test for Aircraft MIL-464C DO-160F G Section23

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Lightning Protection Test for Aircraft MIL-464C DO-160F G Section23

Lightning protection test for aircraft as per MIL-464C / DO-160F / G Section23, including a set of complicated impulse current test system with 4 impulse current generators.

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  • Description

Product Details

Aircraft is vulnerable to be directly adhered by lightening when they fly in severe convention weather. High temperature, high voltage and strong electromagnetic force produced by lightening would cause fire, corrosion, explosion, structure distortion and strength reduction on aircraft.

The dedicated Lightening protection test system for aircraft is a set of complicated impulse current test system with 4 impulse current generators, which fully meets the requirements of MIL-STD-464C, SAE ARP5412 and DO160 section23. The adhered area should bear continuous waveforms formed by A, B, C and D waveforms.

Specifications

Model：FICG-A
Standard：MIL-464C DO-160F G Section23

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