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