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IAgAvtrMissileRamjetProp Interface

Description

Interface used to access the Ramjet propulsion options for a missile.

Public Properties

Public Property BurnerEfficiencyGets or sets the efficiency of the burner.
Public Property BurnerPressureRatioGets or sets the pressure ratio from the burner exit to the entrance.
Public Property DesignAltitudeGets or sets the altitude design point of the engine.
Public Property DesignMachGets or sets the mach number design point of the engine.
Public Property DesignThrustGets or sets the thrust design point of the engine.
Public Property EngineTempGets or sets the maximum temperature that the engine material can support.
Public Property FuelHeatingValueGets or sets the heating value of the fuel.
Public Property InletPressureRatioGets or sets the pressure ratio from the inlet exit to the entrance.
Public Property NoThrustWhenNoFuelOpt to have no thrust if the fuel is empty.
Public Property NozzlePressureRatioGets or sets the pressure ratio from the nozzle exit to the entrance.
Public Property P0overP9Gets or sets the pressure ratio from ambient conditions to the engine exit.

CoClasses that Implement IAgAvtrMissileRamjetProp

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