Introduction
When an aircraft is flying in severe convection environment, it will be frequently affected by lightning stroke, which will generate transient induced voltage or current on circuits and cables of airborne equipment, such phenomenon is called indirect lightning effect. It may make the aircraft get out of control, even bring about fuselage fire and other serious accidents. For safety reasons, the airborne equipment must be designed properly and tested completely to ensure the system and equipment with critical safety function to perform normally and its flight security when the aircraft is influenced by lightning stroke.
The ETS 160MB test system is capable of generating waveforms 2,3 and 6 specified in RTCA/DO-160 Section 22, test level is from 1 to 5 for pins direct injection method and cable bundle cable induction method; Additionally, the test system is not only meet the test requirement of lightning induced transients conducted susceptibility in MIL-STD-461G CS117, but also the A/B/C/D EUT pulse injection level requirement in GJB 8848: 2016 is satisfied.> Corelab software are available for remote control;
For more information, please click : Indirect Lightning Induced Transient Susceptibility Test System (Waveforms 2,3 and 6) ETS 160MB
