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Rocket engines are cooled by fuel and oxidizer (e.g. liquid oxygen) circulating in pipes along their hot parts, before being burned. What do you think needs the cooling most--the combustion chamber or the wide "bell" through which the gases exit?
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I'd say the combustion chamber probably needs it more but both require some form of cooling.
i'd say its bell cause ignition is in combustion chamber but most intense temperature would be in bell, my opinion...
After a bit of reading on the NASA site...I think you're right.
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