Development of Electric and Chemical Microthrusters

The increasing application of microsatellites (from 10 kg up to 100 kg) as well as CubeSats for a rising number of various missions demands the development of miniaturized propulsion systems. Fotec and The University of Applied Sciences at Wiener Neustadt is developing a number of micropropulsion te...

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Main Authors: M. Tajmar, C. A. Scharlemann
Format: Article
Language:English
Published: Wiley 2011-01-01
Series:International Journal of Aerospace Engineering
Online Access:http://dx.doi.org/10.1155/2011/361215
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author M. Tajmar
C. A. Scharlemann
author_facet M. Tajmar
C. A. Scharlemann
author_sort M. Tajmar
collection DOAJ
description The increasing application of microsatellites (from 10 kg up to 100 kg) as well as CubeSats for a rising number of various missions demands the development of miniaturized propulsion systems. Fotec and The University of Applied Sciences at Wiener Neustadt is developing a number of micropropulsion technologies including both electric and chemical thrusters targeting high performance at small scales. Our electric propulsion developments include a series of FEEP (field emission electric propulsion) thrusters, of which the thrust ranges from μN to mN level. The thrusters are highly integrated into clusters of indium liquid-metal-ion sources that can provide ultralow thrust noise and long-term stability. We are also developing a micro PPT thruster that enables pointing capabilities for CubeSats. For chemical thrusters, we are developing novel micromonopropellant thrusters with several hundred mN as well as a 1–3 N bipropellant microrocket engine using green propellants and high specific impulse performance. This paper will give an overview of our micropropulsion developments at Fotec, highlighting performance as well as possible applications.
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institution Kabale University
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publishDate 2011-01-01
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spelling doaj-art-3eac5008366a43bba458c1a3b533b4092025-02-03T07:25:19ZengWileyInternational Journal of Aerospace Engineering1687-59661687-59742011-01-01201110.1155/2011/361215361215Development of Electric and Chemical MicrothrustersM. Tajmar0C. A. Scharlemann1Department of Aerospace Engineering, KAIST, Daejeon 305-701, Republic of KoreaAerospace Engineering Department, University of Applied Sciences at Wiener Neustadt, 2700 Wiener Neustadt, AustriaThe increasing application of microsatellites (from 10 kg up to 100 kg) as well as CubeSats for a rising number of various missions demands the development of miniaturized propulsion systems. Fotec and The University of Applied Sciences at Wiener Neustadt is developing a number of micropropulsion technologies including both electric and chemical thrusters targeting high performance at small scales. Our electric propulsion developments include a series of FEEP (field emission electric propulsion) thrusters, of which the thrust ranges from μN to mN level. The thrusters are highly integrated into clusters of indium liquid-metal-ion sources that can provide ultralow thrust noise and long-term stability. We are also developing a micro PPT thruster that enables pointing capabilities for CubeSats. For chemical thrusters, we are developing novel micromonopropellant thrusters with several hundred mN as well as a 1–3 N bipropellant microrocket engine using green propellants and high specific impulse performance. This paper will give an overview of our micropropulsion developments at Fotec, highlighting performance as well as possible applications.http://dx.doi.org/10.1155/2011/361215
spellingShingle M. Tajmar
C. A. Scharlemann
Development of Electric and Chemical Microthrusters
International Journal of Aerospace Engineering
title Development of Electric and Chemical Microthrusters
title_full Development of Electric and Chemical Microthrusters
title_fullStr Development of Electric and Chemical Microthrusters
title_full_unstemmed Development of Electric and Chemical Microthrusters
title_short Development of Electric and Chemical Microthrusters
title_sort development of electric and chemical microthrusters
url http://dx.doi.org/10.1155/2011/361215
work_keys_str_mv AT mtajmar developmentofelectricandchemicalmicrothrusters
AT cascharlemann developmentofelectricandchemicalmicrothrusters