What are the pros and cons of using same turbopump for fuel and oxidizer and using 2 different pumps for both?
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does this Q&A help? https://space.stackexchange.com/q/34016/ – Infinite_Maelstrom Nov 09 '23 at 20:55
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1It is not possible to use the same turbopump for fuel and oxidizer for all propellants that could be mixed only in the combustion chamber. – Uwe Nov 09 '23 at 23:19
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2Do you perhaps mean having fuel and oxidizer turbopumps on the same shaft, powered by a single turbine, as opposed to two shafts, each with its own turbine? – Ögmundur Eiriksson Nov 10 '23 at 10:46