Thruster.GetThrust() Method

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Description

Returns the effective thrust based on the propulsion model thrust polynomial evaluation. The thrust polynomial coefficients are specified by the Thruster.ThrusterC1-ThrusterC16 properties. The Thruster Scale Factor and Duty Cycle are included in the calculation.

 

Timing Precision Mode

This page describes functionality in nanosecond timing precision mode.

Click here to see the documentation for this object in millisecond timing precision mode.

 

Method Signature

Thruster.GetThrust(

)

 

 

Return Value

Type:

number

Units:

N

 

 

Returns the effective thrust of the Thruster.

 

Syntax

myVariable1 = myThruster1.GetThrust();

 

 

See also

Thruster Object

Thrusters Guide