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http://dx.doi.org/10.9766/KIMST.2019.22.2.224

A Study on Electromagnetic Environmental Effects(E3) Test and Evaluation of a Commercial Derivative Military Aircraft  

Kim, Junghoon (The 2nd Research and Development Institute, Agency for Defense Development)
Jung, Inhwan (The 2nd Research and Development Institute, Agency for Defense Development)
Lee, Kwangill (The 2nd Research and Development Institute, Agency for Defense Development)
Lee, Kyusong (The 2nd Research and Development Institute, Agency for Defense Development)
Oh, Seong (The 2nd Research and Development Institute, Agency for Defense Development)
Publication Information
Journal of the Korea Institute of Military Science and Technology / v.22, no.2, 2019 , pp. 224-232 More about this Journal
Abstract
This paper presents guidelines for the verification test on electromagnetic environmental effects of a commercial derivative military aircraft. To prove the safety-of-flight of a renovated aircraft and appropriate working of electronic system/device, E3 test and analysis at the system level should be performed prior to its operations on real warfare. For the aircraft modified with Falcon 2000S, we concentrate on intra-system EMC, EMRADHAZ (Electromagnetic Radiation Hazards), electrical bonding, P-Static as test and lightning as analysis from a airworthiness certification point of view based on MIL-STD-464, MIL-HDBK-516. As a result, it is verified that the modified aircraft has enough electromagnetic compatibility capabilities under EME(Electromagnetic Environment). In the process, test and analysis methods considering shielding effectiveness(SE) are applied.
Keywords
E3; Intra-system EMC; EMRADHAZ; Lightning; Airworthiness Certification;
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  • Reference
1 MIL-HDBK-516B, Airworthiness Certification Criteria Expanded Version, Sep. 2005.
2 MIL-STD-461F, Requirements for the Control of Electromagnetic Interference Characteristics of Subsystems and Equipment, Dec. 2007.
3 MIL-STD-464C, Electromagnetic Environmental Effects Requirements for Systems, Dec. 2010.
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