Thruster.GetIsp() Method

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Description

Returns the effective specific impulse (Isp) based on the propulsion model Isp polynomial evaluation, scaled by the IspScaleFactor. The Isp polynomial coefficients are specified by the Thruster.ThrusterK1-ThrusterK16 properties.

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.GetIsp(

)

Return Value

Type:	number
Units:	s

Returns the effective specific impulse (Isp) of the Thruster.

Syntax

myVariable1 = myThruster1.GetIsp();