Mach at Exit in Rocket Propulsion Formulas

The Mach at Exit in rocketry refers to the Mach number of the exhaust gases as they exit the rocket engine nozzle. And is denoted by M₂.

Rocket Propulsion formulas that make use of Mach at Exit

fxArea Ratio of NozzlesGo

What is the Mach at Exit?

The Mach at Exit in rocketry refers to the Mach number of the exhaust gases as they exit the rocket engine nozzle.

Can the Mach at Exit be negative?

{YesorNo}, the Mach at Exit, measured in {OutputVariableMeasurementName} {CanorCannot} be negative.

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