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http://dx.doi.org/10.12673/jant.2022.26.2.47

Design and Implementation of test system for safety separation and performance verification of aircraft weapons/equipment  

Kim, Hyo-joung (R&D Center of LIGNex1Co, Ltd)
Kim, Yang-won (R&D Center of LIGNex1Co, Ltd)
Kwon, Byung-Gi (R&D Center of LIGNex1Co, Ltd)
Publication Information
Journal of Advanced Navigation Technology / v.26, no.2, 2022 , pp. 47-53 More about this Journal
Abstract
With the recent development of defense technology, various aircraft armaments/equipments are being developed. Among them, cruise guided weapons(missile) for launching aircraft can be installed on aircraft aftersecuring reliability and safety through varioustests. In order to avoid collision with aircraft, missile separated from aircraft must release restraint of wing at the specified time, control wing in the specified direction. In order to confirm this, a test system that can control MIL-STD-1760 according to safety separation procedure and verify release performance is required. test system needs a function to check circuit for release of restraints and a function to check driving performance by controlling MIL-STD-1760. In addition, test system should be simulate environment separated from aircraft. This paper presented a testsystemthat can verify circuit and driving performance mounted on missile according to the safety separation procedure, and it was confirmed that it was normally separated from aircraft through flight tests.
Keywords
Air to surface missile; MIL-STD-1760; Pyro test system; Safety critical separation;
Citations & Related Records
Times Cited By KSCI : 2  (Citation Analysis)
연도 인용수 순위
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