InletTemperature

Declared in FuelSourceThermalModel

Declaration

[Unit("K")]
[Range(0, 1.7976931348623157E+308)]
double InletTemperature;

Description

Temperature (K) of incoming propellant during fill. When > 0, used with for training-grade inlet enthalpy: ṁ·cp·(T_in − T_gas). Default 0 disables this term (preserves legacy compression-only ullage behaviour); transfer/fill presets e.g. sets a positive inlet temperature.