Design and Verification of Electric Pump for Small LOX/Methane Rocket Engine
Author:
Funder
Korea Foundation for the Advancement of Science and Creativity
Publisher
Springer Science and Business Media LLC
Subject
Electrical and Electronic Engineering,Aerospace Engineering,General Materials Science,Control and Systems Engineering
Link
https://link.springer.com/content/pdf/10.1007/s42405-022-00561-5.pdf
Reference30 articles.
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4. da Cás PLK, Veras CAG, Shynkarenko O, Leonardi R (2019) A Brazilian space launch system for the small satellite market. Aerospace 6:123. https://doi.org/10.3390/aerospace6110123
5. Liu Y, Yang J, He Y, Ni Z, Wu Y (2021) Concept and key technology analysis of electric-pump-fed liquid propellant rocket engine. IOP Conf Ser: Earth Environ Sci. https://doi.org/10.1088/1755-1315/781/4/042016
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