Description
Interface used to access the Turbojet propulsion options for a missile.
Public Properties
 BurnerEfficiency | Gets or sets the efficiency of the burner. |
| BurnerPressureRatio | Gets or sets the pressure ratio from the burner exit to the entrance. |
| CompressorEfficiency | Gets or sets the efficiency of the compressor. |
| CompressorPressureRatio | Gets or sets the maximum compressor pressure ratio. |
| DesignAltitude | Gets or sets the altitude design point of the engine. |
| DesignMach | Gets or sets the mach number design point of the engine. |
| DesignThrust | Gets or sets the thrust design point of the engine. |
| FuelHeatingValue | Gets or sets the heating value of the fuel. |
| InletSubsonicPressureRatio | Gets or sets the subsonic pressure ratio from the inlet exit to the entrance. |
| MechanicalEfficiency | Gets or sets the mechanical efficiency of the engine. |
| NoThrustWhenNoFuel | Opt to have no thrust if the fuel is empty. |
| NozzlePressureRatio | Gets or sets the pressure ratio from the nozzle exit to the entrance. |
| P0overP9 | Gets or sets the pressure ratio from ambient conditions to the engine exit. |
| TurbineEfficiency | Gets or sets the efficiency of the turbine. |
| TurbineTemp | Gets or sets the maximum temperature that the turbine material can support. |