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 millisecond timing precision mode. Millisecond timing precision mode is deprecated and will be removed in a future release. We recommend that you migrate your Mission Plans to nanosecond timing precision mode.

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

Method Signature

Thruster.GetThrust(

)

Return Value

Type:	number
Units:	N

Returns the effective thrust of the Thruster.

Syntax

myVariable1 = myThruster1.GetThrust();