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Characteristic Property of Combustion and Internal Ballistics of Triple-Based Propellant according to Particle Size of RDX

RDX 입도에 따른 다기추진제의 연소 및 강내탄도 특성

  • Soojung Son (R&D Team, Yeosu-Plant, Hanwha Aerospace) ;
  • Wonmin Lee (R&D Team, Yeosu-Plant, Hanwha Aerospace) ;
  • Woojin Lee (R&D Team, Yeosu-Plant, Hanwha Aerospace) ;
  • Daegeon Kim (Guided Weapon & Firepower system Team, Korea Research Institute for Defense Technology Planning and Advancement)
  • 손수정 (한화에어로스페이스(주) 여수사업장 개발팀) ;
  • 이원민 (한화에어로스페이스(주) 여수사업장 개발팀) ;
  • 이우진 (한화에어로스페이스(주) 여수사업장 개발팀) ;
  • 김대건 (국방기술진흥연구소 유도화력기술팀)
  • Received : 2023.12.04
  • Accepted : 2024.03.20
  • Published : 2024.06.05

Abstract

The important factors in the design of the gun propellant are impetus, flame temperature and pressure. In this paper, we considered a nitrocellulose based propellant composition that replaced sensitive NG(Nitroglycerin) with RDX(Cyclotrimethylenetrinitramine) and DEGDN(Diethylene glycol dinitrate) which high energy and low sensitivity. Particle size and content of RDX are the two main factors that affect the burning stability of RDX-based propellants. Among them, the characteristics of the propellant according to the particle size of RDX were confirmed. The relative combustion rate(R.Q., Relative Quickness) of the propellant changed according to the RDX particle size, and internal ballistics of properties of propellant were also varied. The particle size of RDX can be confirmed as a major factor in the combustion and internal ballistics characteristics of the propellant.

Keywords

Acknowledgement

이 논문은 2023년도 정부(방위사업청)의 재원으로 국방기술진흥연구소의 지원을 받아 수행된 연구임(No. KRIT-CT-22-003, 둔감화 단위장약 기술)

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