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SetIspAndMassFlowRate 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 isp and mass flow rate. Computes the thrust using the rocket equation. Returns false on an error.

Syntax

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

[Visual Basic .NET]

Public Function SetIspAndMassFlowRate( _
   ByVal Isp As Double, _
   ByVal MassFlowRate As Double _
) As Boolean

[C#]
public bool SetIspAndMassFlowRate( double Isp, double MassFlowRate );

[C#]

public bool SetIspAndMassFlowRate(

   double Isp, 

   double MassFlowRate

);

[Managed C++]
public: bool SetIspAndMassFlowRate( double Isp, double MassFlowRate );

[Managed C++]

public: bool SetIspAndMassFlowRate(

   double Isp, 

   double MassFlowRate

);

[Java]
public bool setIspAndMassFlowRate( double Isp, double MassFlowRate );

[Java]

public bool setIspAndMassFlowRate(

   double Isp, 

   double MassFlowRate

);

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

[Unmanaged C++]

public: HRESULT SetIspAndMassFlowRate(

   double Isp, 

   double MassFlowRate, 

   VARIANT_BOOL * ReturnValue

);

Isp: Must be non-negative
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 Isp is negative

Computes thrust from the rocket equation