What are the exhaust gas temperatures of the SSME rocket motor?

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The Space Shuttle Main Engine (SSME) reaches combustion chamber temperatures of approximately 3,300 °C (6,000 °F). The exhaust temperatures as it exits the nozzle are also of interest, although specific values were not provided in the discussion. The fuel mixture used in the SSME is rich in hydrogen (H2), which contributes to its high performance. Additional resources for detailed specifications include manufacturer data and historical engine information. Understanding these temperatures is crucial for insights into rocket motor efficiency and performance.
FiggyOO
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I was wondering if anyone here happens to know the temperatures related to the SSME's ( or any rocket motor like it ) exhaust just as it passes through the nozzle?

Actually, temperatures in the combustion chamber, nozzle, etc would be beneficial to know as well.

Thanks again.
 
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Thread 'Space Stuff and Launch Info'

Due to the constant never ending supply of "cool stuff" happening in Aerospace these days I'm creating this thread to consolidate posts every time something new comes along. Please feel free to add random information if its relevant. So to start things off here is the SpaceX Dragon launch coming up shortly, I'll be following up afterwards to see how it all goes. :smile: https://blogs.nasa.gov/spacex/
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