Browsing by Author "Kahraman, M."
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Assessment of using electric pumps on hybrid rockets Gegeoglu, K.; Kahraman, M.; Üçler, Çağlar; Karabeyoglu, A. (American Institute of Aeronautics and Astronautics Inc, AIAA, 2019)In small hybrid rockets, liquid oxidizer is fed into the combustion chamber by pressurizing the oxidizer tank to achieve the desired injector pressure. However, larger applications employ propellant pumps to keep the ...
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