Author:
Haemisch Jan,Suslov Dmitry,Deeken Jan C.
Reference19 articles.
1. M Borner, C Manfletti, J Hardi, D Suslov, G Kroupa, and M Oschwald. Laser ignition of a multi-injector lox/methane combustor. CEAS Space Journal, 10:273-286, 2018.
2. T. Kato, D. Terakado, H. Nanri, T. Morito, I. Masuda, H. Asakawa, H. Sakaguchi, Y. Ishikawa, T. Inoue, S. Ishihara, and M. Sasaki. Subscale firing test for regenerative cooling lox/methane rocket engine. 7th European Conference for Aeronautics and Space Science (EUCASS), 2017.
3. Hiroya Asakawa, Hideaki Nanri, Kenji Aoki, Isao Kubota, Hatsuo Mori, Yasuhiro Ishikawa, Kenichi Kimoto, Shinji Ishihara, and Shinichiro Ishizaki. The status of the research and development of lng rocket engines in japan. Springer Aerospace Technology, Chemical Rocket Propulsion: A Comprehesive Survey of Energetic Materials, 2017.
4. Jan Haemisch, Dmitry Suslov, and Michael Oschwald. Experimental study of methane heat transfer deterioration in a subscale combustion chamber. Journal of Propulsion and Power, 2019.
5. Jan Haemisch, Dmitry Suslov, and Michael Oschwald. Experimental and numerical investigation of heat transfer processes in rocket engine cooling channels operated with cryogenic hydrogen and methane at supercritical conditions. Transactions of the Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan 19(1):96-105, 2021.