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Effects of extractor axial position on porous ionic liquid Ion source performance

Effects of extractor axial position on porous ionic liquid Ion source performance
Effects of extractor axial position on porous ionic liquid Ion source performance
A porous-media type, passively-fed, single emitter ionic liquid ion source electrospray thruster with variable extractor electrode to emitter axial distance was tested. Plume current-voltage curves and extractor current-voltage curves were measured for extractor to emitter distances from -0.1 mm (below emitter apex) to +0.5 mm (above emitter apex). After onset, the formation of a secondary and tertiary emission site was identified via step change in current and shift in current-voltage slope. Results show a linear increase in onset voltage with increasing emitter-extractor distance and a reduction in slope of the plume current to applied voltage curve, with extractor positions below the emitter having the highest current to voltage slope.Temporally-resolved plume current and extractor current behaviour in the onset voltage region was also examined. A time delay between applied potential and plume current emission of 0.48s at the initial onset voltage of 2070 V decreased to zero after 2160 V when the extractor was co-planar with the emitter tip. This ΔVbetween first delayed emission and immediate emission remained constant as the extractor was moved downstream of the emitter.
Kerber, Thomas
7ceadecd-6d4d-44a9-b9ef-4af2244af1d0
Sargent, Hannah
8866a668-fce0-4339-9f49-742da9e6d584
Lemmer, Kristina
02d0c1c0-bd2d-4d8d-a388-77de4c2619f7
Ryan, Charles
3627e47b-01b8-4ddb-b248-4243aad1f872
Kerber, Thomas
7ceadecd-6d4d-44a9-b9ef-4af2244af1d0
Sargent, Hannah
8866a668-fce0-4339-9f49-742da9e6d584
Lemmer, Kristina
02d0c1c0-bd2d-4d8d-a388-77de4c2619f7
Ryan, Charles
3627e47b-01b8-4ddb-b248-4243aad1f872

Kerber, Thomas, Sargent, Hannah, Lemmer, Kristina and Ryan, Charles (2022) Effects of extractor axial position on porous ionic liquid Ion source performance. In Proceedings of the 37th International Electric Propulsion Conference. 9 pp .

Record type: Conference or Workshop Item (Paper)

Abstract

A porous-media type, passively-fed, single emitter ionic liquid ion source electrospray thruster with variable extractor electrode to emitter axial distance was tested. Plume current-voltage curves and extractor current-voltage curves were measured for extractor to emitter distances from -0.1 mm (below emitter apex) to +0.5 mm (above emitter apex). After onset, the formation of a secondary and tertiary emission site was identified via step change in current and shift in current-voltage slope. Results show a linear increase in onset voltage with increasing emitter-extractor distance and a reduction in slope of the plume current to applied voltage curve, with extractor positions below the emitter having the highest current to voltage slope.Temporally-resolved plume current and extractor current behaviour in the onset voltage region was also examined. A time delay between applied potential and plume current emission of 0.48s at the initial onset voltage of 2070 V decreased to zero after 2160 V when the extractor was co-planar with the emitter tip. This ΔVbetween first delayed emission and immediate emission remained constant as the extractor was moved downstream of the emitter.

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IEPC_2022_194 - Author's Original
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Published date: 19 July 2022
Venue - Dates: 37th International Electric Propulsion Conference, Massachusetts Institute of Technology, Cambridge, MA, USA, June 19-23, 2022, Massachusetts Institute of Technology, Massachusetts, United States, 2022-06-19 - 2022-06-23

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Local EPrints ID: 474443
URI: http://eprints.soton.ac.uk/id/eprint/474443
PURE UUID: 3c256fc0-71f4-48e5-9c06-a7bcaea67daf

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Date deposited: 22 Feb 2023 17:50
Last modified: 17 Mar 2024 00:14

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Contributors

Author: Thomas Kerber
Author: Hannah Sargent
Author: Kristina Lemmer
Author: Charles Ryan

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