Exit Temperature in Rocket Propulsion Formulas

Exit temperature is the degree of measure of heat at exit to the system. And is denoted by T_exit. Exit Temperature is usually measured using the Kelvin for Temperature. Note that the value of Exit Temperature is always negative.

Formulas to find Exit Temperature in Rocket Propulsion

fxRocket Exit TemperatureGo

Rocket Propulsion formulas that make use of Exit Temperature

fxExit Velocity given Mach Number and Exit TemperatureGo

List of variables in Rocket Propulsion formulas

fx Chamber Temperature Go

fx Specific Heat Ratio Go

fx Mach Number Go

FAQ

What is the Exit Temperature?

Exit temperature is the degree of measure of heat at exit to the system. Exit Temperature is usually measured using the Kelvin for Temperature. Note that the value of Exit Temperature is always negative.

Can the Exit Temperature be negative?

Yes, the Exit Temperature, measured in Temperature can be negative.

What unit is used to measure Exit Temperature?

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

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