Calculate Aerodynamic Heating Rate for Re-Entry Vehicle

 Method to Calculate the Aerodynamic Heating Rate for a Re-Entry Vehicle into the Earth's Atmosphere

• Calculate Trajectory of Space Vehicle

• Calculate Period of Revolution

• Calculate Orbital and Escape Velocity

• Calculate Altitude Maximum Deceleration, Value, Velocity at Impact

• Calculate Aerodynamic Heating Rate for Re-entry Vehicle

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Aerodynamic Heating Rate for Re-Entry Vehicle

In order to Calculate the Aerodynamic Heating Rate for a Re-entry vehicle entering into the Earth's atmosphere we must enter the Altitude, S in ft of Re-entry vehicle.

We must enter both Velocities V1, and V2 in ft/sec into the equation.

And the Aerodynamic Heating Rate, dq/dt in Btu/ft^2s.

Doing the Calculation, the following parameters are computed.

The value of Stanton Number, C(H)

And the Value of the Aerodynamic Heating Rate at the Same Altitude.

Download Free Program to Calculate the Aerodynamic Heating Rate for Re-entry Vehicle