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J. KIMS Technol > Volume 18(1); 2015 > Article
Journal of the Korea Institute of Military Science and Technology 2015;18(1):93-99.
DOI: https://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
Jinyong Kim, Taeha Kwon, Wonbok Lee, Wonman Cho, Bangeop Lee, Gyoodong Jung, Youngwoo Rhee
1Development Team, Daejeon Plant, Hanwha Corporation
2The 4th Research and Development Institute, Agency for Defense Development
3Graduate School of Energy Science and Technology, Chungnam National University
이중펄스 로켓모타의 격막형 펄스분리장치 설계 및 성능평가
김진용, 권태하, 이원복, 조원만, 이방업, 정규동, 이영우
1(주)한화 대전사업장 개발팀
2국방과학연구소 제4기술연구본부 1부
3충남대학교 에너지과학기술대학원
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.
Key Words: Dual Pulse Rocket Motor, Pulse Separation Device, Bulkhead, Thermal Barrier
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