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Preliminary design of a 1 kN liquid propellant rocket engine testing platform
This work presents a preliminary design of a liquid rocket engine test platform to support research into liquid propulsion systems and rocket engine components, including injectors, ignition systems, combustion chambers and engine cooling systems. The liquid propellants, specifically liquid oxygen a...
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| Format: | Thesis |
| Language: | English |
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Department of Electrical Engineering
2022
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