Chamber Temperature in Rocket Propulsion Formulas

Chamber Temperature refers to the temperature of the combustion chamber in a propulsion system, such as a rocket or jet engine. And is denoted by T_c. Chamber Temperature is usually measured using the Kelvin for Temperature. Note that the value of Chamber Temperature is always positive.

Rocket Propulsion formulas that make use of Chamber Temperature

fxRocket Exit TemperatureGo

fxExit Velocity given Molar MassGo

FAQ

What is the Chamber Temperature?

Chamber Temperature refers to the temperature of the combustion chamber in a propulsion system, such as a rocket or jet engine. Chamber Temperature is usually measured using the Kelvin for Temperature. Note that the value of Chamber Temperature is always positive.

Can the Chamber Temperature be negative?

No, the Chamber Temperature, measured in Temperature cannot be negative.

What unit is used to measure Chamber Temperature?

Chamber Temperature is usually measured using the Kelvin[K] for Temperature. Celsius[K], Fahrenheit[K], Rankine[K] are the few other units in which Chamber Temperature can be measured.

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