• Title/Summary/Keyword: 2D Guidance Fuze

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A Study on Configuration Design of the 2D Course Correction Munition (2D 탄도수정탄의 형상설계 연구)

  • Kim, Ki-Pyo;Chung, Myung-Jee;Hong, Jong-Tai
    • Journal of the Korea Institute of Military Science and Technology
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    • v.11 no.4
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    • pp.5-12
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    • 2008
  • There are some ways to improve precision of conventional munitions by low-cost method. 2D Course Correction Munition(CCM) is one of those ways, which is a 155mm projectile integrated with 2D Guidance Fuze(GF) instead of conventional fuze. 2D GF can correct the projectile trajectory and minimize range and deflection errors from its aimpoint using canard control. In this paper 2D CCM system concept is introduced and its course correction capability is analyzed using PRODAS.

Aerodynamic Design of a Canard Controlled 2D Course Correction Fuze for Smart Munition (카나드 기반의 지능탄 조종 장치 공력설계)

  • Park, Ji-Hwan;Bae, Ju-Hyeon;Song, Min-Sup;Myong, Rho-Shin;Cho, Tae-Hwan
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.43 no.3
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    • pp.187-194
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    • 2015
  • Course correction munition is a smart projectile which improves its accuracy by the control mechanism equipped in the fuze section with canard. In this paper, various aerodynamic configurations of the fuze section were analysed by utilizing a semi-empirical method and a CFD method. A final canard configuration showing the least drag was then determined. During the CFD simulation, it was found that the k-${\omega}$ SST turbulence model combined with O-type grid base is suitable for the prediction of the base drag. Finally, the aerodynamic characteristics of the smart munition and the change of drag due to the canard installation were analysed.