Design Point Operating Characteristics of an Oxidizer Rich Preburner
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Moon, Ilyoon
(Advanced Rocket Research Team, Korea Aerospace Research Institute)
Moon, Insang (Advanced Rocket Research Team, Korea Aerospace Research Institute) Kang, Sang Hun (Advanced Rocket Research Team, Korea Aerospace Research Institute) Ha, Seong-Up (Advanced Rocket Research Team, Korea Aerospace Research Institute) Lee, Soo Young (Advanced Rocket Research Team, Korea Aerospace Research Institute) |
1 | Katorgin, B.I., Chvanov, V.K., Chelkis, F.J., Irina G. Lozino-Lozinskaya, I.G. and Tanner, L.G., "Oxidizer-Rich Staged Combustion Rocket Engines Use and Development in Russia," AIAA Space Programs and Technlogies Coference, 1995. |
2 | Ha, S.U., Yoo, J.H., Moon, I.Y. and Moon, I.S., "Development History and Modern Trends of Oxidizer-Rich Prebrner," Proceedings of the 2012 Korean Society of Propulsion Engineers Spring Conference, pp. 461-464, 2012. |
3 | Ha, S.U., Lee, S.M., Kang, S.H. and Lee, S.Y., "Numerical Analysis on the Supercritical Combustion in Oxidizer-Rich Preburner with Triplex Injector," Proceedings of the 2012 Korean Society of Propulsion Engineers Fall Conference, pp. 490-493, 2012. |
4 | Yi, Y.S., Hong, M.G. and Lee, S.Y., "Study on the Spray Pattern of a Gas-centered Swirl Coaxial Injector with Various Injection Conditions," The 16th Annual Conference on Liquid Atomization and Spray Systems, pp. 64-65, 2012. |
5 | Moon, I.Y., Moon, I.S., Yoo, J.H., Jeon, J.H., Lee, S.M., Hong, M.G., Ha, S.U., Kang, S.H. and Lee, S.Y., "Ignition Test of an Oxidizer Rich Preburner," Proceedings of the 2011 Korean Society of Propulsion Engineers Fall Conference, pp. 869-872, 2011. 과학기술학회마을 |
6 | Moon, I.Y., Moon, I.S. and Lee. S.M., "Study on the Product Gas Temperature Uniformity from a Mixing Head of an Oxidizer Rich Preburner," Proceedings of the 7th National Congress on Fluids Engineering, pp. 455-456, 2012. |
7 | Kim, Y.J., Hong, M.G., Lee, S.Y. and Sohn, C.H., "A Numerical Study on Mixing Characteristics for Recess Length of Swirl Coaxial Injector," Proceedings of the 2011 Korean Society of Propulsion Engineers Fall Conference, pp. 74-77, 2011. 과학기술학회마을 |
8 | Huzel, D.K. and Huang, D.H., "Modern Engineering for Design of Liquid-propellant Rocket Engines," AIAA, 1992. |
9 | Parsley, R.C., Zhang, B., "Thermodynamic Power Cycles for Pump-Fed Liquid Rocket Engines," Liquid Rocket Thrust Chambers: Aspects of Modeling, Analysis, and Design, Progress in Astronautics and Aeronautics, Vol. 200, AIAA, Chap. 18, 2004. |
10 | Farhangi, S., Jensen, R.J., Hunt, K., Tuegel, L. and Yu, T., "Oxidizer-Rich Preburner Technology for Oxygen/Hydrogen Full Flow Cycle Applications," Progress in Astronautics and Aeronautics, Vol. 200, 2004. |
11 | Knuth, W.K. and Crawford, R.C., "Oxygen-Rich Combustion Process Applications and Benefits," Modern Engineering for Design of Liquid-propellant Rocket Engines", AIAA, 1992. |
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