Combustion Chamber

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Combustion Chamber

(symbol c used as a subscript) 

Any chamber for the combustion of fuel, specifically that part of the rocket engine in which the combustion of propellants takes place at high pressure. Also called chamber, firing chamber.
The combustion chamber plus the diverging section of the nozzle comprise the rocket thrust chamber.

References

This article is based on NASA's Dictionary of Technical Terms for Aerospace Use