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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$\begingroup$ does this Q&A help? space.stackexchange.com/q/34016 $\endgroup$– Infinite_MaelstromNov 9 at 20:55
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1$\begingroup$ It is not possible to use the same turbopump for fuel and oxidizer for all propellants that could be mixed only in the combustion chamber. $\endgroup$– UweNov 9 at 23:19
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2$\begingroup$ Do 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? $\endgroup$– Ögmundur EirikssonNov 10 at 10:46
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