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...
Saved in:
Main Authors: | , |
---|---|
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 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
_version_ | 1832545567042961408 |
---|---|
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. |
format | Article |
id | doaj-art-3eac5008366a43bba458c1a3b533b409 |
institution | Kabale University |
issn | 1687-5966 1687-5974 |
language | English |
publishDate | 2011-01-01 |
publisher | Wiley |
record_format | Article |
series | International Journal of Aerospace Engineering |
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 |