Thruster.ThrusterInletPressure Property

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Description

Pressure at the Thruster inlet. This is calculated based on the Thruster.AveragePreInletPressure property and the pressure drop coefficients, Thruster.PC1-6. This property is used in the calculation of Thrust and Isp along with the AveragePreInletTemp, AveragePreInletRefTemp, and Thruster coefficients.

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.

Attributes

Type:	number
Access:	read

Syntax

myVariable1 = myThruster1.ThrusterInletPressure;