Development of a miniature gridded ion thruster

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Journal Title

Journal ISSN

Volume Title

Sähkötekniikan korkeakoulu |

Date

2017-10-23

Department

Major/Subject

Space Science and Technology

Mcode

ELEC3039

Degree programme

Erasmus Mundus Space Master

Language

en

Pages

30

Series

Abstract

Electric propulsion has matured to the point where it starts credibly to challenge chemical propulsion systems. The high efficiency and larger specific impulse have allowed to lower the weight of the satellites and therefore costs. Even though the thrust of an electric propulsion systems is still just a fraction of that chemical rockets, the possibility of keeping it on for months eventually gives the same amount of momentum. While CubeSat projects are getting more popular by universities only a few have developed their own miniature ion thruster. These mini thrusters have a thrust force of sub mN to few mN, but they still enable up to 100 kg almost any kind of altering to satellites orbital position and attitude. Another, issue on electric propulsion is the propellant. Xenon is most used propellant fuel in ion thrusters, but because of its high costs, it is out of the reach for many universities. This study tried tackling into those two topics and create a design of a miniature ring cusp gridded ion thruster. The study wanted to research possibilities of using 3D printing technology and this way simplify the fabrication process. The goal was to create a design which could be used as a foundation for Aalto University’s propulsion development and also enable testing of alternative propellants. The propellants studied were iodine, adamantane, and diamantane. All of them are in a solid-state at room temperature, which would be practical for storage. The design is presented at the end of the study.

Description

Supervisor

Praks, Jaan

Thesis advisor

Kestilä, Antti

Keywords

Propulsion, space propulsion, ion engine, propellant

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