The oxidizer mass fraction is a crucial parameter in rocket propulsion systems, determining the proportion of oxidizer to the total propellant mass. To comprehend its significance, consider its impact on rocket performance and efficiency.
In this formula:
- Mass of Oxidizer refers to the mass of the oxidizing agent used in the propulsion system.
- Total Mass of Propellant refers to the combined mass of both the fuel and the oxidizer used in the system.