A Study of Core Water Injection Effect Influencing Plume in 75 tf $1^{st}$ Stage Liquid Propellant Rocket Engine Ground Test

75톤 1단 액체로켓엔진 지상시험에서 중앙 물분사가 후류에 미치는 영향 고찰

  • 문윤완 (한국항공우주연구원 발사체엔진팀) ;
  • 설우석 (한국항공우주연구원 발사체엔진팀)
  • Received : 2010.12.21
  • Accepted : 2011.07.01
  • Published : 2011.07.01

Abstract

A study of efficient plume cooling by core water injection type was performed by computational fluid dynamics. A side injection type is well known, on the contrary, a core injection type is not well known. In order to figure out the characteristics of core injection type, several calculations were performed by computational fluid dynamics along various mass flow rates and locations of water injection. On the basis of analysis it was the adequate cooling condition that water mass flow rate to total mass flow rate was two times at least and location of water injections was L/De=1.2.

본 연구는 중앙 물분사 방식을 채택한 액체로켓엔진 후류의 냉각에 대해 전산유체역학을 통한 특성을 고찰하였다. 중앙 물분사 방식의 냉각은 측면 물분사 방식과는 달리, 잘 알려져 있지 않기 때문에 다양한 물분사량과 유량을 통해 효율적으로 후류를 냉각시킬 수 있는 조건을 찾았으며, 해석을 통해 후류의 변화 특성을 살펴보았다. 이로부터 물분사 유량이 총추진제 유량의 2배 이상, 위치는 L/De=1.2일 때가 적당함을 알 수 있었다.

Keywords

References

  1. Gordan, S. and McBride, B.J., Computer Program for Calculation of Complex Chemical Equilibrium Compositions and Applications, I. Analysis, NASA RP-1311, 1994.
  2. Fluent Inc., User Manual for Fluent, V6.3.
  3. Wang, T.S., Warsi, S. and Chen, Y.S., "Computational Pollutant Environment Assessment from Propulsion-System Testing, " Journal of Spacecraft and Rocket, Vol. 33, No. 3, 1996, pp.386-392 https://doi.org/10.2514/3.26772
  4. Reitz, R.D., "Modeling Atomization Processes in High-Pressure Vaporizing Sprays," Atomization and Spray Technology, Vol. 3, 1987, pp.309-337,
  5. 문윤완, 설우석, 75톤 1단 액체로켓엔진 지상시험에서 물분사가 후류에 미치는 영향 고찰:중앙 물분사 방식, KARI-RET-TM-2010-003, 2010, pp.1-19.