Thrust chamber cooling Calculator

Thrust chamber cooling refers to the process of managing and dissipating the immense heat generated within the combustion chamber of a rocket engine during operation.

Where:

  • is the rate of heat transfer per unit length of the chamber.
  • is the temperature of the combustion chamber wall.
  • is the temperature of the coolant at the inlet.
  • is the thermal resistance of the nozzle material.
  • is the thermal resistance of the coolant.

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