Thermo-Mechanical Analysis of Continuous-Adjustment Thruster using Explosion Pressure |
Kim, Kyung-Sik
((주)한화 구미사업장 개발2부)
Kwon, Young-Doo (경북대학교 기계공학부) Kwon, Soon-Bum (경북대학교 기계공학부) Gil, Hyuck-Moon (경북대학교 기계공학부) |
1 | Park, M.S., Kang, T.H., Byun, Y.S., Song, J.B. (2008) Dynamic Analysis and Experiments of High Impulse Force Device with Isolation System, Journal of the KSPE, 25(10), pp.107-114. |
2 | 김광수, 장영순, 이영무 (2008) 우주발사체 구조 해석 소개, 한국전산구조공학회 논문집, 21(3), pp.43-50. |
3 | (주)한화 (2011) 대외비. |
4 | Ahmad, R.A. (2005) Convective Heat Transfer in the Reusable Solid Rocket Motor of the Space Transpor-Tation System, Heat Transfer Engineering, 26(10), pp.30-45. DOI ScienceOn |
5 | Choi, Y.G., Kwang, B.S., Kim, W.H. (2010) A Study on Size Optimization of Rocket Motor Case using the Modified 2D Axisymmetric Finite Element Model, International Journal of Precision Engineering and Manufacturing, 11(6), pp.901-907. DOI ScienceOn |
6 | Hirai. K (2003) Ablation Analysis for Solid Rocket Motor Nozzles, Proc. of Conf. on Aerospace Propulsion, 43(1), pp.49-54. |
7 | Kauffmann. J., Hervertz, A., Sippel, M. (2001) System Analysis of a High Thrust, Low-Cost Rocket Engine, Int. Conf. on Green Propellant for Space Propulsion, Netherland, pp.1-7. |
8 | Mcbride, B.J., Reno, M.A., Gordon, S. (1994) An Intrim Updated Version of the NASA Lewis Computer Program for Calculating Complex Chemical Equilibria with Application, NASA Technical Memorandum 4557, Cleveland, OH. |