Fuel Mass Flow rate evaluator uses Fuel Mass Flow Rate = Propellant Mass Flow Rate/(Propellant Mixture Ratio+1) to evaluate the Fuel Mass Flow Rate, The fuel mass flow rate in a rocket engine refers to the rate at which fuel is consumed or expelled from the engine, it is used to determine the flow rate of fuel into the combustion chamber, which in turn affects combustion efficiency, chamber pressure, and thrust generation. Fuel Mass Flow Rate is denoted by ṁf symbol.
How to evaluate Fuel Mass Flow rate using this online evaluator? To use this online evaluator for Fuel Mass Flow rate, enter Propellant Mass Flow Rate (ṁ) & Propellant Mixture Ratio (r) and hit the calculate button.