Abstract

The age of space electric propulsion arrived and found the space exploration endeavors at a paradigm shift in the context of new space. Mega-constellations of small satellites on low-Earth orbit (LEO) are proposed by many emerging commercial actors. Naturally, the boom in the small satellite market drives the necessity of propulsion systems that are both power and fuel efficient and accommodate small form-factors. Most of the existing electric propulsion technologies have reached the maturity level and can be the prime choices to enable mission versatility for small satellite platforms in Earth orbit and beyond. At the Plasma Sources and Applications Centre/Space Propulsion Centre (PSAC/SPC) Singapore, a continuous effort was dedicated to the development of low-power electric propulsion systems that can meet the small satellites market requirements. This review presents the recent progress in the field of electric propulsion at PSAC/SPC Singapore, from Hall thrusters and thermionic cathodes research to more ambitious devices such as the rotamak-like plasma thruster. On top of that, a review of the existing vacuum facilities and plasma diagnostics used for electric propulsion testing and characterization is included in the present research.

Highlights

  • The deployment of large low-Earth orbit (LEO) satellite constellations became reality in the past couple of years, with hundreds of small satellites being placed on LEO [1,2]

  • Previous studies showed that the vacuum facility can impact the performance of the electric propulsion devices such as Hall thrusters and emissive cathodes [18,19,20,21]

  • At PSAC/SPC a continuous effort was invested in the development of a large-scale vacuum facility to meet the purpose of Hall thruster and cubesat testing

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Summary

Introduction

The deployment of large low-Earth orbit (LEO) satellite constellations became reality in the past couple of years, with hundreds of small satellites being placed on LEO [1,2]. It came with no surprise when the mission planners opted for electric propulsion as main propulsive system of their satellites. Hall thrusters [6], and navigation market with the with first GEO platform equipped with four [6], the satellite failed to reach its orbit due to launch vehicle malfunction.

Approximate number of electric systems launched between
Vacuum Test Facilities and Plasma Diagnostics
Space Environment Simulation Chamber
Vacuum facilities at the PlasmaSources
Quadfilar Thrust Pendulum
Plasma Diagnostics for Electric Propulsion Systems
Hall Thrusters
Low-power
Cathodeless Hall Thrusters
Cathode Discharge Modes and Mode Transition
12. Cathode
Onecurrent of the criteria are presented in Figure
Knife-Edge Emitter Cathodes
14. Knife-edge
Mathematical Analysis and Plasma Simulations for the Rotamak
15. Rotamak
Transition into the Rotamak-Like Thruster
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