ControlEngineIon

class ansys.stk.core.stkobjects.astrogator.ControlEngineIon

IntEnum

Overview

Members

FLOW_RATE_CONSTANT_TERM	FlowRateModel.C0 - the constant coefficient.
FLOW_RATE_LINEAR_TERM	FlowRateModel.C1 - the linear coefficient.
FLOW_RATE_QUADRATIC_TERM	FlowRateModel.C2 - the quadratic coefficient.
FLOW_RATE_CUBIC_TERM	FlowRateModel.C3 - the cubic coefficient.
GRAV	Gravitational acceleration constant at sea level on the Earth.
ISP_CONSTANT_TERM	IspModel.C0 - the constant coefficient.
ISP_LINEAR_TERM	IspModel.C1 - the linear coefficient.
ISP_QUADRATIC_TERM	IspModel.C2 - the quadratic coefficient.
ISP_CUBIC_TERM	IspModel.C3 - the cubic coefficient.
MASS_FLOW_EFFICIENCY_CONSTANT_TERM	MassFlowEfficiencyModel.C0 - the constant coefficient.
MASS_FLOW_EFFICIENCY_LINEAR_TERM	MassFlowEfficiencyModel.C1 - the linear coefficient.
MASS_FLOW_EFFICIENCY_QUADRATIC_TERM	MassFlowEfficiencyModel.C2 - the quadratic coefficient.
MASS_FLOW_EFFICIENCY_CUBIC_TERM	MassFlowEfficiencyModel.C3 - the cubic coefficient.
MAX_INPUT_POWER	Minimum power required for the engine to produce thrust.
MIN_REQUIRED_POWER	Maximum power that can be used by the engine to produce thrust.
PERCENT_DEGRADATION_PER_YEAR	The degradation factor is (1 - x)n, where n is the time since epoch in years, and x is the percent degradation per year.
PERCENT_THROTTLE	Percentage of available thrust to use (100 is full on, 0 is off).
POWER_EFFICIENCY_CONSTANT_TERM	PowerEfficiencyModel.C0 - the constant coefficient.
POWER_EFFICIENCY_LINEAR_TERM	PowerEfficiencyModel.C1 - the linear coefficient.
POWER_EFFICIENCY_QUADRATIC_TERM	PowerEfficiencyModel.C2 - the quadratic coefficient.
POWER_EFFICIENCY_CUBIC_TERM	PowerEfficiencyModel.C3 - the cubic coefficient.
REFERENCE_EPOCH	The date and time used as a reference epoch for degradation.

Import detail

from ansys.stk.core.stkobjects.astrogator import ControlEngineIon