thermodynamic efficiency of a propulsion system Calculator

The specific heat is also relevant when calculating the thermodynamic efficiency of a propulsion system, such as a rocket or a jet engine. The efficiency (η) can be calculated using the specific heat at constant pressure (Cp) and the specific heat at constant volume (Cv) as follows:

η=1Cv/Cp

This equation indicates how efficiently the energy is converted into thrust or work in the propulsion system, and Cp and Cv play a crucial role in this calculation.

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