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http://dx.doi.org/10.9766/KIMST.2015.18.1.093

The Design & Analysis of Pulse Separation Device with Thermal Barrier Type for Dual Pulse Rocket Motor  

Kim, Jinyong (Development Team, Daejeon Plant, Hanwha Corporation)
Kwon, Taeha (Development Team, Daejeon Plant, Hanwha Corporation)
Lee, Wonbok (Development Team, Daejeon Plant, Hanwha Corporation)
Cho, Wonman (Development Team, Daejeon Plant, Hanwha Corporation)
Lee, Bangeop (The 4th Research and Development Institute, Agency for Defense Development)
Jung, Gyoodong (The 4th Research and Development Institute, Agency for Defense Development)
Rhee, Youngwoo (Graduate School of Energy Science and Technology, Chungnam National University)
Publication Information
Journal of the Korea Institute of Military Science and Technology / v.18, no.1, 2015 , pp. 93-99 More about this Journal
Abstract
The dual pulse rocket motor(DPRM) distributes the propellant energy effectively via pulse separation device(PSD) to improve the range and terminal velocity of the missile. There are two types of PSD such as bulk head type and thermal barrier type. A subscale thermal barrier type DPRM was designed, manufactured, and tested. The results showed good understanding of the characteristics of the PSD and will be applied to the design of the full scale DPRM.
Keywords
Dual Pulse Rocket Motor; Pulse Separation Device; Bulkhead; Thermal Barrier;
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  • Reference
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