# Exhaust Velocity Calculator

## About Exhaust Velocity Calculator (Formula)

The Exhaust Velocity Calculator is a tool used to determine the exhaust velocity of a propulsion system, often employed in the field of rocketry or jet propulsion. The exhaust velocity represents the speed at which the gases are expelled from the system, contributing to the generation of thrust.

The formula used to calculate the Exhaust Velocity is as follows:

Exhaust Velocity (V) = (Thrust Force – (Exit Pressure – Atmospheric Pressure) * Exhaust Area) / Mass Flow Rate

Where: V = Exhaust Velocity (in meters per second, m/s) Thrust Force = The force generated by the propulsion system (in Newtons, N) Exit Pressure = The pressure at the exhaust nozzle (in Newtons per square meter, N/m²) Atmospheric Pressure = The pressure of the surrounding atmosphere (in Newtons per square meter, N/m²) Exhaust Area = The cross-sectional area of the exhaust nozzle (in square meters, m²) Mass Flow Rate = The rate at which mass is expelled from the system (in kilograms per second, kg/s)

To use the calculator, you need to input the values for the thrust force, exit pressure, atmospheric pressure, exhaust area, and mass flow rate. The thrust force is the force generated by the propulsion system, while the exit pressure and atmospheric pressure represent the pressures at the exhaust nozzle and in the surrounding environment, respectively. The exhaust area denotes the cross-sectional area of the exhaust nozzle, and the mass flow rate signifies the rate at which mass is expelled from the system.

By applying the formula, the calculator computes the exhaust velocity in meters per second (m/s). This value represents the speed at which the gases are expelled from the propulsion system, indicating the efficiency and performance of the system.

The Exhaust Velocity Calculator is useful in fields such as aerospace engineering, rocketry, and jet propulsion. It enables engineers and researchers to evaluate the velocity of the exhaust gases and assess the thrust capabilities and efficiency of the propulsion system.

Please note that the formula assumes ideal conditions and neglects factors such as heat transfer, expansion losses, and variations in gas composition. In practical scenarios, additional considerations and corrections may be necessary for accurate exhaust velocity calculations.