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Explosion Shock Measurement System of the Precursor Warhead for the Tandem Projectile

탠덤 비행체의 선구탄두 기폭 충격 측정 시스템 구현

  • Choi, Donghyuk (Fuze & Sonar systems center, Gumi Plant, Hanwha Corp.) ;
  • An, Jiyeon (Fuze research Laboratory, Agency for Defense Development) ;
  • Kim, Yubeom (Fuze & Sonar systems center, Gumi Plant, Hanwha Corp.) ;
  • Son, Joongtak (Fuze research Laboratory, Agency for Defense Development) ;
  • Lee, Ukjun (Research and Development Institute, Radar R&D Center, Hanwha Systems) ;
  • Park, Hyunsoo (Fuze & Sonar systems center, Gumi Plant, Hanwha Corp.)
  • 최동혁 ((주)한화 구미사업장 신관해중연구센터) ;
  • 안지연 (국방과학연구소 신관연구실험실) ;
  • 김유범 ((주)한화 구미사업장 신관해중연구센터) ;
  • 손중탁 (국방과학연구소 신관연구실험실) ;
  • 이욱준 (한화시스템(주) 연구개발본부 레이다연구소) ;
  • 박현수 ((주)한화 구미사업장 신관해중연구센터)
  • Received : 2021.04.30
  • Accepted : 2021.09.03
  • Published : 2021.10.05

Abstract

This paper presents a system that measures the acceleration of the shock caused by the explosion of the precursor warhead for the tandem projectile. The proposed system, which is implemented based on the MIL-STD-810G, Method 517.1, consists of a miniaturized shock measurement device, a cable, accelerometers, and a trigger circuit. The shock measurement device has a size of ¢102 × 171 mm and cable has a length of 3 m. The operational confirmation test is conducted by implementing the measurement system. The Analysis of shock data(accelerometer output data) is carried out using Shock Response Spectrum(SRS), pseudo velocity and plot of acceleration time transient. Through measurement analysis, one can predict the damage of electronics in projectile when precursor warhead is exploded.

Keywords

Acknowledgement

본 연구는 국방과학연구소의 지원으로(계약번호: UC150044GD) 수행하며 진행되었습니다.

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