RF Helicon-based Inductive Plasma Thruster (IPT) Design for an Atmosphere-Breathing Electric Propulsion system (ABEP)

Abstract

Challenging space missions include those at very low altitudes, where the atmosphere is source of aerodynamic drag on the spacecraft. To extend such missions lifetime, an efficient propulsion system is required. One solution is Atmosphere-Breathing Electric Propulsion (ABEP). It collects atmospheric particles to be used as propellant for an electric thruster. The system would minimize the requirement of limited propellant availability and can also be applied to any planet with atmosphere, enabling new mission at low altitude ranges for longer times. Challenging is also the presence of reactive chemical species, such as atomic oxygen in Earth orbit. Such species cause erosion of (not only) propulsion system components, i.e. acceleration grids, electrodes, and discharge channels of conventional EP systems. IRS is developing within the DISCOVERER project, an intake and a thruster for an ABEP system. The paper describes the design and implementation of the RF helicon-based inductive plasma thruster (IPT). This paper deals in particular with the design and implementation of a novel antenna called the birdcage antenna, a device well known in magnetic resonance imaging (MRI), and also lately employed for helicon-wave based plasma sources in fusion research. This is aided by the numerical tool XFdtd®. The IPT is based on RF electrodeless operation aided by an externally applied static magnetic field. The IPT is composed by an antenna, a discharge channel, a movable injector, and a solenoid. By changing the operational parameters along with the novel antenna design, the aim is to minimize losses in the RF circuit, and accelerate a quasi-neutral plasma plume. This is also to be aided by the formation of helicon waves within the plasma that are to improve the overall efficiency and achieve higher exhaust velocities. Finally, the designed IPT with a particular focus on the birdcage antenna design procedure is presented.

Publication DOI: https://doi.org/10.1016/j.actaastro.2020.07.008
Divisions: College of Engineering & Physical Sciences > School of Infrastructure and Sustainable Engineering > Chemical Engineering & Applied Chemistry
College of Engineering & Physical Sciences
Aston University (General)
Funding Information: This project has received funding from the European Union’s Horizon 2020 research and innovation programme under grant agreement No. 737183 . This reflects only the author’s view and the European Commission is not responsible for any use that may be made
Additional Information: © 2020, Elsevier. Licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International http://creativecommons.org/licenses/by-nc-nd/4.0/
Uncontrolled Keywords: ABEP,Birdcage,Helicon,IPT,VLEO,Aerospace Engineering
Publication ISSN: 0094-5765
Last Modified: 11 Nov 2024 08:29
Date Deposited: 17 Aug 2020 08:37
Full Text Link: https://arxiv.o ... /2007.06397.pdf
Related URLs: http://www.scop ... tnerID=8YFLogxK (Scopus URL)
https://www.sci ... 4264?via%3Dihub (Publisher URL)
PURE Output Type: Article
Published Date: 2020-11
Published Online Date: 2020-07-10
Accepted Date: 2020-07-04
Authors: Romano, F.
Chan, Y. A.
Herdrich, G.
Traub, C.
Fasoulas, S.
Roberts, P. C.E.
Smith, K.
Edmondson, S.
Haigh, S.
Crisp, N. H.
Oiko, V. T.A.
Worrall, S. D. (ORCID Profile 0000-0003-1969-3671)
Livadiotti, S.
Huyton, C.
Sinpetru, L. A.
Straker, A.
Becedas, J.
Domínguez, R. M.
González, D.
Cañas, V.
Sulliotti-Linner, V.
Hanessian, V.
Mølgaard, A.
Nielsen, J.
Bisgaard, M.
Garcia-Almiñana, D.
Rodriguez-Donaire, S.
Sureda, M.
Kataria, D.
Outlaw, R.
Villain, R.
Perez, J. S.
Conte, A.
Belkouchi, B.
Schwalber, A.
Heißerer, B.

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