Description
Interface used to access the Rocket propulsion options for a missile.
Public Properties
 BoostChamberPressure | The combustion chamber pressure during the boost phase. |
| BoostFuelFraction | The amount of fuel that is consumed during the boost phase. |
| CombustionChamberPressure | The pressure in the combustion chamber. |
| NoThrustWhenNoFuel | Opt to have no thrust if the fuel is empty. |
| NozzleExitDiameter | The diameter of the nozzle exit. |
| NozzleExpansionRatio | The exit area divided by the throat area. |
| PropellantCharacteristicVelocity | The propellant's characteristic velocity (Chamber Pressure * Throat Area / Mass Flow Rate of the engine). |
| PropellantSpecificHeatRatio | The ratio of the propellant's constant-pressure specific heat to the constant volume specific heat. |
| UseBoostSustainMode | Opt for the engine to use a boost phase to achieve a target velocity and then transition to a sustenance phase. |