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Development of RF Plasma Thruster for Space Enabling Technologies at DLR

Chan, Yung-An and Grabe, Martin and Ammer, Julian and Geile, Christopher and Plettenberg, Felix and Schwendtke, Ingo (2024) Development of RF Plasma Thruster for Space Enabling Technologies at DLR. In: 9th Edition of the 3AF International Conference on Space Propulsion 2024. 9th Edition of the 3AF International Conference on Space Propulsion 2024, 2024-05-20 - 2024-05-23, Glasgow, Scotland.

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Official URL: https://www.3af-spacepropulsion.com/

Abstract

Neutralizer-free or electroless thruster concept, such as the helicon plasma thruster (HPT) and electroncyclotron-resonance (ECR) thruster, relies on the electromagnetic wave to achieve plasma generation. Eliminating electrode exposure to the plasma provides superior compatibility with alternative propellants such as water or Iodine, offering promising advantages for new space applications. DLR kicked off a development project, Decentralized Energy supplied Electrical Propulsion (DEEP) in 2022, aiming to demonstrate a neutralizer-free EP system on a 12U CubeSat in 2027 to promote future space mobility and sustainability. The concept of HPT is one of the candidates, named ALFVEN thruster, within the scope of the DEEP project. The thrust efficiency of HPT has been significantly improved to nearly 30%, mainly attributed to the improvement of the electric circuitry and the understanding of the plasma dynamics in magnetic nozzles. However, the low-power HPT, i.e., few-hundredwatt class and sub-hundred-watt class, still remains relatively low in performance. One of the possible reasons is the poor power coupling between the antenna and plasma. Thus, besides the mission perspective, the ALFVEN thruster also aims to optimize radio-frequency (RF) power delivery by investigating the coupling mechanism between the antenna and plasma.

Item URL in elib:https://elib.dlr.de/199457/
Document Type:Conference or Workshop Item (Speech)
Title:Development of RF Plasma Thruster for Space Enabling Technologies at DLR
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Chan, Yung-Anyung-an.chan (at) dlr.dehttps://orcid.org/0000-0001-5494-0514163318071
Grabe, MartinMartin.Grabe (at) dlr.dehttps://orcid.org/0000-0003-0361-2734UNSPECIFIED
Ammer, Julianjulian.ammer (at) dlr.deUNSPECIFIEDUNSPECIFIED
Geile, Christopherchristopher.geile (at) dlr.deUNSPECIFIEDUNSPECIFIED
Plettenberg, FelixFelix.Plettenberg (at) dlr.deUNSPECIFIEDUNSPECIFIED
Schwendtke, IngoIngo.Schwendtke (at) dlr.deUNSPECIFIEDUNSPECIFIED
Date:23 May 2024
Journal or Publication Title:9th Edition of the 3AF International Conference on Space Propulsion 2024
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Editors:
EditorsEmailEditor's ORCID iDORCID Put Code
UNSPECIFIED3AFUNSPECIFIEDUNSPECIFIED
Status:Published
Keywords:RF, plasma thruster, Neutralizer-free, electroless, helicon, electromagnetic, DEEP
Event Title:9th Edition of the 3AF International Conference on Space Propulsion 2024
Event Location:Glasgow, Scotland
Event Type:international Conference
Event Start Date:20 May 2024
Event End Date:23 May 2024
Organizer:3AF – Association Aéronautique et Astronautique de France
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space System Technology
DLR - Research area:Raumfahrt
DLR - Program:R SY - Space System Technology
DLR - Research theme (Project):R - Project Decentralized Energy Supplied Electrical Propulsion
Location: Göttingen
Institutes and Institutions:Institute for Aerodynamics and Flow Technology > Spacecraft, GO
Deposited By: Chan, Dr.-Ing. Yung-An
Deposited On:10 Jul 2024 10:51
Last Modified:10 Jul 2024 10:51

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