Open Access
MATEC Web Conf.
Volume 114, 2017
2017 International Conference on Mechanical, Material and Aerospace Engineering (2MAE 2017)
Article Number 02010
Number of page(s) 7
Section Chapter 2: Materials
Published online 10 July 2017
  1. C. Goertz, “A modular method for the analysis of liquid rocket engine cycles,” 1995. [Google Scholar]
  2. K. Liu and Y. Zhang, “A study on versatile simulation of liquid propellant rocket engine systems transients,” 2000. [Google Scholar]
  3. J. M. C. R. Koppel, R. Perez, J. Steelant, P. Omaly, “A Platform Satellite Modelling With EcosimPro: Simulation Results,” presented at the 45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Denver, Colorado, 2-5 August, 2009. [Google Scholar]
  4. F. Di Matteo and M. De Rosa, “Steady State Library for Liquid Rocket Engine Cycle Design,” 2011. [Google Scholar]
  5. X. H. P. Z. Yan, Y. Q. Cheng, J. J. Wu, “System Dynamic Characteristic Simulation of Spacecraft Propulsion System Based on AMESim,” Advanced Materials Research, vol. 605-607, pp. 679-683, 2013 [CrossRef] [Google Scholar]
  6. A. R. J. M. Naderi, H. karimi, “Modeling And Simulation Of Open Cycle Liquid Propellant Engines,” Journal of Science and Engineering, vol. Vol. 1, 2013. [Google Scholar]
  7. C. L. L. Wei, X. Gang, D. Jing, Z. Haiming, Y. Hao, “Modeling and Simulation of Liquid Propellant Rocket Engine Transient Performance Using Modelica,” presented at the Proceedings of the 11th International Modelica Conference, Versailles, France, September 21-23, 2015. [Google Scholar]
  8. M. Chitsaz, E. A. Tahmasebi, and H. Karimi M, “A Method for Simulation of a Cryogenic Liquid Propellant Engine,” Applied Mechanics and Materials, vol. 110-116, pp. 2370-2376, 2011. [CrossRef] [Google Scholar]
  9. D. H. H. Dieter K Huzel, Modern Engineering for Design of Liquid Propellant Rocket Engines. Washington DC, USA: American Institute of Aeronautics and Astronautics, 1992. [Google Scholar]
  10. H. L. Humble, Space Propulsion Analysis and Design USA: McGraw-Hill Inc., 2007 [Google Scholar]
  11. “Space Shuttle Main Engine Orientation,” in “BC98-04,” Rocketdyne Propulsion and Power, Boeing June 1998. [Google Scholar]
  12. (March, 2016). [Google Scholar]
  13. N. Dynamics, “SSME Model Dynamic Characteristics Related to POGO,” Rocketdyne Division Rockwel International, 30th September, 1973. [Google Scholar]

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