Author:
Zips Julian,Traxinger Christoph,Pfitzner Michael
Funder
German Research Foundation
Subject
Fluid Flow and Transfer Processes,Mechanical Engineering,Condensed Matter Physics
Reference92 articles.
1. S. Zurbach, J.L. Thomas, P. Vuillermoz, L. Vingert, M. Habiballah, Recent Advances on LOx/Methane Combustion for Liquid Rocket Engine Injector, in: 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit: AIAA paper 2002-4321, 2002. https://doi.org/10.2514/6.2002-4321.
2. LOx/hydrocarbon preparatory thrust chamber technology activities in Germany;Preclik,2005
3. H. Kawashima, A. Kumakawa, T. Onodera, S. Yoshida, N. Azuma, K. Aoki, H. Negishi, K. Okita, H. Manako, T. Koganezawa, T. Kaneko, Combustion and Regenerative Cooling Characteristics of LOx/Methane Engine, in: Proceedings of the 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit: AIAA paper 2008-4837, 2008. https://doi.org/10.2514/6.2008-4837.
4. LOX/methane technology efforts for future liquid rocket engines;Preuss,2008
5. Subscale firing test for regenerative cooling LOx/methane rocket engine;Kato,2017
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