MissileRamjetPropulsion#

class ansys.stk.core.stkobjects.aviator.MissileRamjetPropulsion#: Class defining the Ramjet propulsion options for a missile.

Overview#

Properties

`design_mach`	Get or set the mach number design point of the engine.
`design_altitude`	Get or set the altitude design point of the engine.
`design_thrust`	Get or set the thrust design point of the engine.
`engine_temp`	Get or set the maximum temperature that the engine material can support.
`fuel_heating_value`	Get or set the heating value of the fuel.
`inlet_pressure_ratio`	Get or set the pressure ratio from the inlet exit to the entrance.
`burner_pressure_ratio`	Get or set the pressure ratio from the burner exit to the entrance.
`nozzle_pressure_ratio`	Get or set the pressure ratio from the nozzle exit to the entrance.
`p_0over_p9`	Get or set the pressure ratio from ambient conditions to the engine exit.
`burner_efficiency`	Get or set the efficiency of the burner.
`no_thrust_when_no_fuel`	Opt to have no thrust if the fuel is empty.

from ansys.stk.core.stkobjects.aviator import MissileRamjetPropulsion

property MissileRamjetPropulsion.design_mach: float#: Get or set the mach number design point of the engine.

property MissileRamjetPropulsion.design_altitude: float#: Get or set the altitude design point of the engine.

property MissileRamjetPropulsion.design_thrust: float#: Get or set the thrust design point of the engine.

property MissileRamjetPropulsion.engine_temp: float#: Get or set the maximum temperature that the engine material can support.

property MissileRamjetPropulsion.fuel_heating_value: float#: Get or set the heating value of the fuel.

property MissileRamjetPropulsion.inlet_pressure_ratio: float#: Get or set the pressure ratio from the inlet exit to the entrance.

property MissileRamjetPropulsion.burner_pressure_ratio: float#: Get or set the pressure ratio from the burner exit to the entrance.

property MissileRamjetPropulsion.nozzle_pressure_ratio: float#: Get or set the pressure ratio from the nozzle exit to the entrance.

property MissileRamjetPropulsion.p_0over_p9: float#: Get or set the pressure ratio from ambient conditions to the engine exit.

property MissileRamjetPropulsion.burner_efficiency: float#: Get or set the efficiency of the burner.

property MissileRamjetPropulsion.no_thrust_when_no_fuel: bool#: Opt to have no thrust if the fuel is empty.