Journal of the Korea Institute of Military Science and Technology (한국군사과학기술학회지)

The Korea Institute of Military Science and Technology (한국군사과학기술학회)
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The Design & Analysis of Pulse Separation Device with Thermal Barrier Type for Dual Pulse Rocket Motor

이중펄스 로켓모타의 격막형 펄스분리장치 설계 및 성능평가

  • 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)
  • 김진용 ((주)한화 대전사업장 개발팀) ;
  • 권태하 ((주)한화 대전사업장 개발팀) ;
  • 이원복 ((주)한화 대전사업장 개발팀) ;
  • 조원만 ((주)한화 대전사업장 개발팀) ;
  • 이방업 (국방과학연구소 제4기술연구본부 1부) ;
  • 정규동 (국방과학연구소 제4기술연구본부 1부) ;
  • 이영우 (충남대학교 에너지과학기술대학원)
  • Received : 2014.06.30
  • Accepted : 2015.01.30
  • Published : 2015.02.05
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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

References

  1. Stadler, L. J., Trouillot, P., et al., "The Dual Pulse Motor for LFK NG," AIAA, 2006-4762.
  2. Naumann, K. W., Stadler, L. J., "Double-Pulse Solid Rocket Motor Technology-Applications and Technical Solutions," AIAA, 2010-6754.
  3. Schilling, S., Trouillot, P., et al., "On the Development and Testing of a 120 mm Caliber Double Pulse Motor(DPM)," AIAA, 2004-3387.
  4. Kong, J. A. et al., "Multimission Propulsion Technology-Advanced Technology Demonstration (MMPT-ATD) Final Program Summary of Test Results and Conclusions," CPIA, Pub. 630, 1995.
  5. Cho, W. M., Kim, W. H., et al., "Study on Pulse Separation Device of Bulkhead Type for Solid Rocket Motors," KSPE Spring Conference, pp. 187- 190, 2009.
  6. Naumann, K. W. et al., "Double-pulse Solid Rocket Technology at BAYERN-CHEMIE/PROTAC," AIAA, 2006, 2006-4761.
  7. Kim, J. Y., Rho, T. H., et al., "The Case Thermal Design of Dual Pulse Rocket Motor with Bulkhead Pulse Separation Device," KIMST Conference, 2011.
  8. Ryu, J. H., Lee, W. B., et al., "Design, Manufacture and Test of Subscale Solid Rocket Motor with Pulse Separation Device," KSPE Spring Conference, 2010.
  9. Kim, W. H., Lee, B. E., et al., "Study on the Technical Trend of a Pulse Separation Device with Thermal Barrier Type," KSPE Fall Conference, pp. 225-228, 2010.
  10. Kim, J. Y., Kwon. T. H., et al., "Study on the Pulse Separation Device with Thermal Barrier Type for Dual Pulse Motor(I)," KSPE Spring Conference, pp. 10-13, 2013.
  11. Kim, J. Y., Kwon. T. H., et al., "Study on the Pulse Separation Device with Thermal Barrier Type for Dual Pulse Motor(II)," KSPE Fall Conference, pp. 204-207, 2013.