ST40

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Description

The ST-40 Hall-Effect Thruster with an anode layer is designed for use as part of the propulsion system for satellites mass up to 1 T. It is used to orient and stabilize of the spacecraft in various orbits. The propulsion system provides a thrust of up to 28 mN at a maximum electric power consumption of 600 W. The propulsion system that contains ST-40 can be used on satellites for various purposes.

 

Datasheet

Space Electric Thruster Systems – ST40

Overview
NameST40
ManufacturerSpace Electric Thruster Systems
SubsystemPropulsion
ClassificationElectric Propulsion Thruster
Form FactorSmallSat
Vendor Overview
Vendor NameSpace Electric Thruster Systems
Vendor Websitehttps://sets.space
Vendor LocationUnited States
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SPECIFICATIONS
SubsystemPropulsion
ClassificationElectric Propulsion Thruster
Form FactorSmallSat
VendorSpace Electric Thruster Systems
HeritageN/A
Mass1.1 kg
Nominal Power425.0 W

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