Indirect Lightning Induced Transient

Description

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.
The ETS 160MB test system includes various test auxiliary equipment to make it convenient to conduct tests, such as coupling transformer, power blocking device, transient blocking device, pin injection probe etc. What’s more, the Corelab software is also available for test remote control, which makes your test easy and convenient.

Features：

• Modular design, the waveform module is detachable;
• Capable of performing signal pins & power pins – direct injection method and cable bundle – cable induction method;
• Capable of generating waveforms 2, 3 and 6;
• 5.7” color touch screen with easy and distinct operation control;
• Phase synchronization function in signal pins & power pins-direct injection method;
• Corelab software are available for remote control;