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침식연소에 따른 고체 로켓 내탄도 특성 변화 분석

Analysis of Internal Ballistic Characteristics of Solid Rocket with Erosive Burning

  • Cho, Mingyoung (Research & Development Team, Daejeon plant, Hanwha Corporation) ;
  • Kim, Jinyong (Research & Development Team, Daejeon plant, Hanwha Corporation) ;
  • Park, Sunghan (Sixth Research & Development Institution, Agency for Defence Development)
  • 투고 : 2013.06.03
  • 심사 : 2014.05.09
  • 발행 : 2014.06.01

초록

본 연구에서는 침식연소를 고려한 내탄도 프로그램을 이용하여 침식연소 모델에 따른 해석결과를 비교하였다. 동일한 추진제를 적용한 이형 그레인 형상을 적용한 추진기관의 연소 시 연소실 압력 변화를 비교 분석하여 연소가스의 유량 변화에 따른 침식연소 경향성 변화를 고찰 하였다. 고찰 결과 연소 면적이 클수록 연소실 단면적이 작을수록 침식연소 경향이 증가함을 알 수 있었다.

Two erosive burning models were applied to compare analysis results of ballistic for the internal ballistics of solid rocket motors. By comparing motor tests with results of analysis, the variance of a grain shape was analyzed and coefficients of erosive burning were drawn. Results of comparison presents that the coefficient of erosive burning was proportional to the change of burning area, while inversely proportional to the change of cross area.

키워드

참고문헌

  1. Srinivasan K., Narayanan S., Sharma O.P., "Numerical studies on erosive burning in cylindrical solid propellant grain", Springer-Verlag, Heat Mass Transfer 44:579-585, 2008. https://doi.org/10.1007/s00231-007-0280-5
  2. Moss J., Heister S., Linke K., "Experimental Program to Assess Erosive Burning in Segmented Solid Rocket Motors", 43rd AIAA Joint Propulsion Conference & Exhibit, Jul. 2007.
  3. Heister, S. D. "Analysis of Ballistic Anomalies in Solid Rocket Motors." Journal of propulsion and power, Vol. 7, No. 6, pp. 887-893, 1991. https://doi.org/10.2514/3.23406
  4. Ellis M. Landsbaum, "Erosive Burning Revisited", 39th AIAA Joint Propulsion Conference & Exhibit, Jul. 2003.
  5. Sutton, G. P., "Rocket Propulsion Elements, 7th ed.", John Wiley & Sons Inc., 2001.

피인용 문헌

  1. Modeling of Erosive Burning for Fluid-Structure Integration Analysis of Solid Rocket Motor vol.20, pp.4, 2016, https://doi.org/10.6108/KSPE.2016.20.4.009