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SetThrustAndIsp Method (IAgGatorPluginResultEvalEngineModel)
See Also

Description

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

Syntax

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

[Visual Basic .NET]

Public Function SetThrustAndIsp( _
   ByVal Thrust As Double, _
   ByVal Isp As Double _
) As Boolean

[C#]
public bool SetThrustAndIsp( double Thrust, double Isp );

[C#]

public bool SetThrustAndIsp(

   double Thrust, 

   double Isp

);

[Managed C++]
public: bool SetThrustAndIsp( double Thrust, double Isp );

[Managed C++]

public: bool SetThrustAndIsp(

   double Thrust, 

   double Isp

);

[Java]
public bool setThrustAndIsp( double Thrust, double Isp );

[Java]

public bool setThrustAndIsp(

   double Thrust, 

   double Isp

);

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

[Unmanaged C++]

public: HRESULT SetThrustAndIsp(

   double Thrust, 

   double Isp, 

   VARIANT_BOOL * ReturnValue

);

Returns false if either input parameter is negative

Computes mass loss rate from the rocket equation