How to Calculate Rocket Exit Temperature?
Rocket Exit Temperature calculator uses Exit Temperature = Chamber Temperature*(1+(Specific Heat Ratio-1)/2*Mach Number^2)^-1 to calculate the Exit Temperature, The Rocket Exit Temperature formula defines the exit temperature at an exhaust, given that we know the total temperature and Mach number. Exit Temperature is denoted by Texit symbol.
How to calculate Rocket Exit Temperature using this online calculator? To use this online calculator for Rocket Exit Temperature, enter Chamber Temperature (Tc), Specific Heat Ratio (γ) & Mach Number (M) and hit the calculate button. Here is how the Rocket Exit Temperature calculation can be explained with given input values -> 18.13511 = 24.6*(1+(1.33-1)/2*1.4^2)^-1.