MissileRocketPropulsion#

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

Overview#

Properties

`nozzle_expansion_ratio`	Get or set the exit area divided by the throat area.
`nozzle_exit_diameter`	Get or set the diameter of the nozzle exit.
`combustion_chamber_pressure`	Get or set the pressure in the combustion chamber.
`propellant_specific_heat_ratio`	Get or set the ratio of the propellant’s constant-pressure specific heat to the constant volume specific heat.
`propellant_characteristic_velocity`	Get or set the propellant’s characteristic velocity (Chamber Pressure * Throat Area / Mass Flow Rate of the engine).
`use_boost_sustain_mode`	Opt for the engine to use a boost phase to achieve a target velocity and then transition to a sustenance phase.
`boost_fuel_fraction`	Get or set the amount of fuel that is consumed during the boost phase.
`boost_chamber_pressure`	Get or set the combustion chamber pressure during the boost phase.
`no_thrust_when_no_fuel`	Opt to have no thrust if the fuel is empty.

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

property MissileRocketPropulsion.nozzle_expansion_ratio: float#: Get or set the exit area divided by the throat area.

property MissileRocketPropulsion.nozzle_exit_diameter: float#: Get or set the diameter of the nozzle exit.

property MissileRocketPropulsion.combustion_chamber_pressure: float#: Get or set the pressure in the combustion chamber.

property MissileRocketPropulsion.propellant_specific_heat_ratio: float#: Get or set the ratio of the propellant’s constant-pressure specific heat to the constant volume specific heat.

property MissileRocketPropulsion.propellant_characteristic_velocity: float#: Get or set the propellant’s characteristic velocity (Chamber Pressure * Throat Area / Mass Flow Rate of the engine).

property MissileRocketPropulsion.use_boost_sustain_mode: bool#: Opt for the engine to use a boost phase to achieve a target velocity and then transition to a sustenance phase.

property MissileRocketPropulsion.boost_fuel_fraction: float#: Get or set the amount of fuel that is consumed during the boost phase.

property MissileRocketPropulsion.boost_chamber_pressure: float#: Get or set the combustion chamber pressure during the boost phase.

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