Exit Pressure in Rocket Propulsion Formulas

Exit Pressure is the pressure of the gases leaving the rocket nozzle. And is denoted by P_exit. Exit Pressure is usually measured using the Megapascal for Pressure. Note that the value of Exit Pressure is always positive. Typically, the value of Exit Pressure is greater than 0.

Formulas to find Exit Pressure in Rocket Propulsion

fxRocket Exit PressureGo

Rocket Propulsion formulas that make use of Exit Pressure

fxExit Velocity given Molar Specific Heat CapacityGo

fxExit Velocity given Molar MassGo

List of variables in Rocket Propulsion formulas

fx Chamber Pressure Go

fx Specific Heat Ratio Go

fx Mach Number Go

FAQ

What is the Exit Pressure?

Exit Pressure is the pressure of the gases leaving the rocket nozzle. Exit Pressure is usually measured using the Megapascal for Pressure. Note that the value of Exit Pressure is always positive. Typically, the value of Exit Pressure is greater than 0.

Can the Exit Pressure be negative?

No, the Exit Pressure, measured in Pressure cannot be negative.

What unit is used to measure Exit Pressure?

Exit Pressure is usually measured using the Megapascal[MPa] for Pressure. Pascal[MPa], Kilopascal[MPa], Bar[MPa] are the few other units in which Exit Pressure can be measured.

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