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The question Performance of a pumpless liquid rocket engine is thoughtful and provocative and pretty much all answers include a mention of the extremely high pressure necessary to push propellants into a high pressure combustion chamber and the use of turbo pumps for this purpose.

But this is based on steady-state combustion in the chamber, and the rotating detonation rocket engine is a horse of a different color.

Question: Would rotating detonation rocket engines always require high pressure fuel pumps?

uhoh
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