AGI AgGator 11	Send comments on this topic.
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 );

[C#]

public bool SetThrustAndMassFlowRate(

   double Thrust, 

   double MassFlowRate

);

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

[Managed C++]

public: bool SetThrustAndMassFlowRate(

   double Thrust, 

   double MassFlowRate

);

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

[Java]

public bool setThrustAndMassFlowRate(

   double Thrust, 

   double MassFlowRate

);

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

[Unmanaged C++]

public: HRESULT SetThrustAndMassFlowRate(

   double Thrust, 

   double MassFlowRate, 

   VARIANT_BOOL * ReturnValue

);

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