MissileTurbojetPropulsion#

class ansys.stk.core.stkobjects.aviator.MissileTurbojetPropulsion#: Class defining the Turbojet 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.
`turbine_temp`	Get or set the maximum temperature that the turbine material can support.
`compressor_pressure_ratio`	Get or set the maximum compressor pressure ratio.
`fuel_heating_value`	Get or set the heating value of the fuel.
`inlet_subsonic_pressure_ratio`	Get or set the subsonic 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.
`compressor_efficiency`	Get or set the efficiency of the compressor.
`turbine_efficiency`	Get or set the efficiency of the turbine.
`burner_efficiency`	Get or set the efficiency of the burner.
`mechanical_efficiency`	Get or set the mechanical efficiency of the engine.
`no_thrust_when_no_fuel`	Opt to have no thrust if the fuel is empty.

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

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

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

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

property MissileTurbojetPropulsion.turbine_temp: float#: Get or set the maximum temperature that the turbine material can support.

property MissileTurbojetPropulsion.compressor_pressure_ratio: float#: Get or set the maximum compressor pressure ratio.

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

property MissileTurbojetPropulsion.inlet_subsonic_pressure_ratio: float#: Get or set the subsonic pressure ratio from the inlet exit to the entrance.

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

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

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

property MissileTurbojetPropulsion.compressor_efficiency: float#: Get or set the efficiency of the compressor.

property MissileTurbojetPropulsion.turbine_efficiency: float#: Get or set the efficiency of the turbine.

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

property MissileTurbojetPropulsion.mechanical_efficiency: float#: Get or set the mechanical efficiency of the engine.

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