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Characterization of a T6 Based Hollow Cathode Thruster

Record type: Conference or Workshop Item (Paper)

This paper characterizes thrust performance of a variant of the T6 hollow cathode modified for improved operational characteristics. The device displays promising performance and highlights the potential for application as a microthruster. The T6 cathode is able to produce specific impulse of over 1050s with xenon and argon; however the dominant acceleration mechanism at low flow rates is shown to be almost entirely electromagnetic effectively constituting a low power, magneto-plasma-dynamic thruster. The modified cathode also displayed very low discharge voltages ~12V and stable operation while carrying currents as high as 30-Amps on flow rates of less than 0.1mgs-1 down to 0.04mgs-1 with xenon. This investigation also highlights the importance of electrode geometry in hollow cathode thruster design and indeed in all other applications of hollow cathode where flow rates should be minimized.

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Citation

Grubisic, A.N., Gabriel, S.B. and Fearn, D.G. (2007) Characterization of a T6 Based Hollow Cathode Thruster At 58th International Astronautical Federation Congress. 24 - 28 Sep 2007. 15 pp.

More information

Published date: 10 September 2007
Venue - Dates: 58th International Astronautical Federation Congress, 2007-09-24 - 2007-09-28
Keywords: hollow cathode, plasma, ion propulsion, micro thruster
Organisations: Astronautics Group

Identifiers

Local EPrints ID: 48318
URI: http://eprints.soton.ac.uk/id/eprint/48318
PURE UUID: 5a38ba29-0fc4-4c49-8cca-511d3cc2f894

Catalogue record

Date deposited: 11 Sep 2007
Last modified: 17 Jul 2017 15:00

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Contributors

Author: A.N. Grubisic
Author: S.B. Gabriel
Author: D.G. Fearn

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