과제정보
이 성과는 2018년도 정부(과학기술정보통신부)의 재원으로 한국연구재단 - 우주기술개발사업의 지원을 받아 수행된 연구임. (NRF-2018M1A3A3A02065851)
참고문헌
- Pempie, P., and Boussif, H., "Cryogenic upper stage engine trade-off," 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Las Vegas, N.V., U.S.A., AIAA 2000--3449, 2000.
- Robinson, J.,W., and Rhodes, R.,E., "Next Generation Reusable Space Transportation System," 53rd AIAA/SAE/ASEE Joint Propulsion Conference, Atlanta, GA, U.S.A., AIAA 2017-4606, 2017.
- Burkhardt, H., Sippel, S., Herbertz, A., and Klevanski, J,. "Comparative study of kerosene and methane propellant engines for reusable liquid booster stages," 4th International Conference on Launcher Technology Space Launcher Liquid Propulsion, At Liege, Belgium, pp. 1-3, Dec. 2002.
- Koroneos, C., Dompros, A., Roumbas, G., and Moussiopoulos, N., "Advantages of the use of hydrogen fuel as compared to kerosene," Resources, Conservation and Recycling, Vol. 44, No. 2, pp. 99-113, 2005. https://doi.org/10.1016/j.resconrec.2004.09.004
- Mpstme, "A Review on Different Propellant Materials for Space Vehicles and Their Characterisation.", International Journal of Mechanical and Production, pp. 93-102, 2018.
- Atsumi, M., Yoshikawa, K., Ogawara, A., and Onga, T., "Development of the LE-X Engine." Mitsubishi Heavy Industries Technical Review, Vol. 48, No. 4, pp. 36-43, 2011.
- Leonardi, M., Nasuti, F., and Onofri, M., "Basic Analysis of a LOX/Methane Expander Bleed Engine," 7th European Conference for Aerospace Sciences, Rome, Italy, EUCASS2017-332, 2017.
- Krach, A.E., and Sutton, A.M., "Another look at the practical and theoretical limits of an expander cycle, LOX/H2 engine," 35th Joint Propulsion Conference and Exhibit, Los Angeles, C.A., U.S.A., AIAA 1999-2473, 1999.
- Sippel, M., and Herbertz, A. "High Thrust Bleed Rocket Engines for a Fly-Back Booster Application," 6th International Symposium Propulsion for the XXIst Century, Palais des Congress, Versailles, France, 2002.
- Sippel, M., Herbertz, A., Manfletti, C., and Burkhardt, H., "Studies on expander bleed cycle engines for launchers," 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Huntsville, Alabama, U.S.A., AIAA 2003-4597, 2003.
- Ernst, R.R.L., "Liquid Rocket Analysis (LiRA): development of a liquid bi-propellant rocket engine design, analysis and optimization tool," Master's Dissertation, Department of Space Systems Engineering, Delft University of Technology, Delft, Nederlands, 2014.
- Cho, W.K., and Kim, C.W., "Analysis of Expander Cycle LRE Performance: RL10A-3-3 Benchmarking," 86th KSAS Fall Conference, Jeju, Korea, pp. 1230-1231, Nov. 2019.
- Kim, C.W., and Roh, W.R., "Cycle Analysis on a Methane-fueled Expander Rocket Engine," 52th KSPE Spring Conference, Jeju, Korea, pp. 561-563, May. 2019.
- Kim, J.E., and Choi, J.,Y., "Analysis of orbital input performance of KSLV-II equipped with hydrogen top engine", Proceedings of the Korean Society of Propulsion Engineers Conference, pp. 557-558, Apr, 2018.
- J.W. Leachman, R.T. Jacobsen, S.G. Penoncello, and E.W. Lemmon, "Fundamental Equations of State for Parahydrogen, Normal Hydrogen, and Orthohydrogen", Journal of Physical and Chemical Reference Data, Vol. 38, No. 3, pp. 721-748, 2009. https://doi.org/10.1063/1.3160306
- "Thermophysical Properties of Fluid Systems," retrieved 10 Mar. 2020 from https://webbook.nist.gov/chemistry/fluid/
- Essler, J., and Haberstroh, C., "Performance of an ortho-para concentration measurement cryostat for hydrogen," American Institute of Physics Conference Proceedings, Vol. 1434, No. 1, pp 1865-1872, 2012.
- Alliot, P., Lassoudiere, F., Fiorentino, C., and Ruault, J.M., "Development status of the VINCI engine for the Ariane 5 upper stage,", 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Tucson, Arizona, U.S.A., AIAA 2005-3755, 2005.
- Alliot, P., Dalbies, E. and Delie, V., "Overview of the Development Progress of the Ariane 5 Upper Stage Vinci Engine," 54th International Astronautical Congress of the International Astronautical Federation, Bremen, Germany, pp S-1, Oct. 2003.
- Bartz and Donald R., "A simple equation for rapid estimation of rocket nozzle convective heat transfer coefficients", Jet Propulsion, Vol. 27, No. 1, pp. 49-51, Jan. 1957. https://doi.org/10.2514/8.12572
- Johnsson, R., Brodin, S., and Pettersson, A., "Development of Hydrogen and Oxygen Pump Turbines for Vinci Engine," 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Indianapolis, Indiana, U.S.A., AIAA 2002-4331, 2002.
- Gordon, S. and McBride, B.J., "Computer Program for Calculation of Complex Chemical Equilibrium Compositions and Applications," NASA RP-1311, 1994.
- Rao, G.V.R., "Exhaust Nozzle Contour for Optimum Thrust," Journal of Jet Propulsion, Vol. 28, No. 6, pp. 377-382, Jun. 1958. https://doi.org/10.2514/8.7324
- Murch, C.K, Broadwell, J.E., Silver, A.H., Marcisz, T.J., "Performance losses in low-Reynolds-number nozzles," Journal of Spacecraft and Rockets Vol. 5, No. 9, pp. 1090-1094, 1968. https://doi.org/10.2514/3.29426
- Fukushima, Y., Nakatsuzi, H., Nagao, R., Kishimoto, K., Hasegawa, K., Koganezawa, T., and Warashina, S., "Development status of LE-7A and LE-5B engines for H-IIA Family," Acta Astronautica, Vol. 50, No. 5, pp. 275-284, 2002. https://doi.org/10.1016/S0094-5765(01)00165-5
- Binder, M., Tomsik, T., and Veres, J. P., "RL10A-3-3A Rocket Enigne Modeling Project," NASA TM-107318, 1997.
- Larson, W. J., Henry, G.N., and Humble, R.W., Space propulsion analysis and design, McGraw-Hill, New York, N.Y., U.S.A., Ch. 5, 1995.
- Kesaev, K.V., Almeida D.S., "Teoria e calculo de motores foguete a propelente liquido," IAE Internal Report. 2005
- NASA, "Liquid rocket valve Assmblies," NASA SP-8097, 1973.
- NASA, "Liquid rocket valve components," NASA SP-8094, 1973
- B. Zandbergen, B.T.C, Thermal Rocket Propulsion,. Delft University of Technology, 2.04 ed., 2012.
- Antonio Cantiani, "Design of a Centrifugal Pump for an Expander Cycle Rocket Engine," Master's Dissertation, Department of Mechanical Engineering, University of Basilicata, Potenza, Italy, 2014
- Aungier, and Ronald, H., Turbine aerodynamics- axial flow and radial flow turbine design and analysis, ASME Press, New York, N.Y., U.S.A., Ch. 10, 2006.
- Sekita, R., Yasui, M., and Warashina, S., "The LE-5 series development, approach to higher thrust, higher reliability and greater flexibility," 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Huntsville, Alabama, U.S.A., AIAA 2000-3453, 2000.
- Pichon, T., Coperet, H., Foucault, A., and Lacombe, A., "Vinci upper stage engine nozzle extension development status," 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Tucson, Arizona, U.S.A., AIAA 2005-3757, 2005.
- Mc Hugh. B. "Numerical analysis of existing liquid rocket engines as a design process starter," 31st AIAA, ASME, SAE, and ASEE, Joint Propulsion Conference and Exhibit, San Diego, CA, U.S.A, AIAA 95-2970, 1995.