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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

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

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

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

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

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

Returns false if either input parameter is negative.

Computes mass loss rate from the rocket equation