References
- Moon, Y.J., "Conceptual Design of Lunar Exploration Mission," Master Dissertation, Korea Advanced Institute of Science and Technology, 2011.
- Japan Aerospace Exploration Agency (JAXA), "KAGUYA(SELENE) World's First Image Taking of the Moon by HDTV," World Wide Web location http://global.jaxa.jp/index.html/, 2007.
- Choe, N.M., Young, S.S., Ju, G.H., Lee, S.R. and Sim, E.S., "Validity and Mission of Korean Lunar Exploration," 2008 KSAS Fall Conference, Jeju, Korea, pp. 1288-1291, Nov. 2008.
- Kim, S.K., Yu, M.J., Choi, J.Y. and Lee, J. W., "Preliminary Design of Lunar Lander Ground Test Model," 2011 KSPE Spring conference, Uiwang, Korea, pp. 27-30, May 2011.
-
Oh, H.Y., Moon, S.H. and Huh, H.I., "Flow Rate Control of Gaseous Oxygen for a HTPB/GO
$_2$ Hybrid Rocket," 2004 KSPE Fall Conference, Seoul, Korea, pp. 251-254, Oct. 2004. - Choi, J.S., Kang, W.K. and Huh, H.I., "Study of Thrust Control Performance Improvement for Hybrid Rocket Applications," Journal of the Korean Society of Propulsion Engineers, Vol. 15, No. 1, pp. 55-62, 2011.
- Martin, F., Chapelle, A., Orlandi, O. and Yvart, P., "Hybrid Propulsion Systems for Future Space Applications," 46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Nashville, T.N., U.S.A., AIAA 2010-6633, Jul. 2010.
- Marxman, G.A., Wooldrige C.E. and Muzzy, R.J., "Fundamentals of Hybrid Boundary Layer Combustion," Progress in Astronautics and Aeronautics, Vol. 15, pp. 185-522, New York, N.Y., U.S.A., 1964.
- Sutton, G.P., Rocket Propulsion Elements, 7th ed., John Wiley & Sons Inc., New York, N.Y., U.S.A., 2001.
- Robert, A.B., "Lunar Module Descent Simulation," World Wide Web location http://www.braeunig.us/apollo/LM-descent.html, 2009.
- Gordon, S. and Mcbride, B.J., "Computer Program for Calculation of Complex Chemical Equilibrium Composition and Applications," NASA Reference Publication 1311, 1996.
- Yoon, C.J., Song, N.Y., Yoo, W.J., Jeon, C.S., Kim, J.K., Sung, H.G. and Moon, H.J., "Performance Analysis of PE-GOX Hybrid Rocket Motor, Part I : Regression Rate Characterisitcs," Journal of the Korean Society of Propulsion Engineers, Vol. 11, No. 2, pp. 71-78, 2007.