IMPROVED FLOW REGULATING SYSTEM FOR SUPPLYING PROPELLANT FLUID TO AN ELECTRIC THRUSTER OF A SPACE VEHICLE

摘要

said system being characterized in that the computer also includes a plurality of empirical calibration curves that have been determined empirically for defining the flow rate of propellant fluid as a function of the magnitude of heating and as a function of environmental parameters, such that said computer also performs a function of determining the flow rate of the propellant fluid.