Future Directions for Electric Propulsion Research

The research challenges for electric propulsion technologies are examined in the context of s-curve development cycles. It is shown that the need for research is driven both by the application as well as relative maturity of the technology. For flight qualified systems such as moderately-powered Hal...

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Veröffentlicht in:Aerospace 2020-09, Vol.7 (9), p.120
Hauptverfasser: Dale, Ethan, Jorns, Benjamin, Gallimore, Alec
Format: Artikel
Sprache:eng
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Zusammenfassung:The research challenges for electric propulsion technologies are examined in the context of s-curve development cycles. It is shown that the need for research is driven both by the application as well as relative maturity of the technology. For flight qualified systems such as moderately-powered Hall thrusters and gridded ion thrusters, there are open questions related to testing fidelity and predictive modeling. For less developed technologies like large-scale electrospray arrays and pulsed inductive thrusters, the challenges include scalability and realizing theoretical performance. Strategies are discussed to address the challenges of both mature and developed technologies. With the aid of targeted numerical and experimental facility effects studies, the application of data-driven analyses, and the development of advanced power systems, many of these hurdles can be overcome in the near future.
ISSN:2226-4310
2226-4310
DOI:10.3390/aerospace7090120