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SetThrustAndMassFlowRate Method (IAgGatorPluginResultEvalEngineModel)
See Also

MassFlowRate: Mass loss rate. May be entered as positive or negative number, but is always considered a mass loss, not a mass gain.

Description

Sets the current thrust(N) and mass flow rate (kg/sec). Computes the isp using the rocket equation. Returns false on an error.

Syntax

[Visual Basic .NET]
Public Function SetThrustAndMassFlowRate( _ ByVal Thrust As Double, _ ByVal MassFlowRate As Double _ ) As Boolean

[Visual Basic .NET]

Public Function SetThrustAndMassFlowRate( _
    ByVal Thrust As Double, _
    ByVal MassFlowRate As Double _
) As Boolean

[C#]
public bool SetThrustAndMassFlowRate( double Thrust, double MassFlowRate );

[Managed C++]
public: bool SetThrustAndMassFlowRate( double Thrust, double MassFlowRate );

[Unmanaged C++]
public: HRESULT SetThrustAndMassFlowRate( double Thrust, double MassFlowRate, VARIANT_BOOL * pReturn );

[Unmanaged C++]

public: HRESULT SetThrustAndMassFlowRate(
    double Thrust,
    double MassFlowRate,
    VARIANT_BOOL * pReturn
);

[Java]
public bool setThrustAndMassFlowRate( double Thrust, double MassFlowRate );

[Python - STK API ]
def SetThrustAndMassFlowRate(self, Thrust:float, MassFlowRate:float) -> bool:

Thrust: Must be positive.
MassFlowRate: Mass loss rate. May be entered as positive or negative number, but is always considered a mass loss, not a mass gain.

Returns false if thrust is not positive.

Computes Isp from the rocket equation