Improving the performance of LOX/kerosene upper stage rocket engines

Author:

Nikischenko IgorN.,Wright Raymond D.,Marchan Roman A.

Publisher

Elsevier BV

Subject

Fluid Flow and Transfer Processes,Mechanical Engineering,Fuel Technology,Aerospace Engineering,Automotive Engineering

Reference56 articles.

1. D.K. Huzel, D.H. Huang, Modern engineering for design of liquid-propellant rocket engines, Progress in Astronautics and Aeronautics, Washington, DC, AIAA 147 (1992) 437.

2. L. De Rose, P. Parmigiani, V. Shnyakin, V. Shulga, V. Pereverzev, Main engine of the Vega fourth stage: characteristic and heritage, in: Proceedings of the 4th International Conference of Launcher Technology “Space Launcher Liquid Propulsion”, Liege, Belgium, 2002.

3. P. Alliot, E. Dalbies, A. Pacros, J.M. Ruault, Overview of the development progress of the Ariane 5 upper stage Vinci engine, in: Proceedings of the 53rd International Astronautical Congress, Houston, Texas, 2002.

4. H. Verning, P. Pempe, LOX/CH4 and LOX/LH2 heavy launch vehicle comparison, AIAA 2009-5133, 2009.

5. O. Kimihito, T. Takashi, N. Kenichi, LOX/kerosene fueled rocket engine study in MHI, in: Proceedings of the 27th International Symposium on Space Technology and Science, Tsukuba, 5-12 July, 2009.

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