Abstract
To enable formation flying of micro satellites, small sized propulsion systems are required. Our research focuses on the miniaturization of a feeding and thruster system by means of micro system technology (MST). Three fabrication methods have been investigated to make a conical converging-diverging nozzle. These methods are reactive ion etching, femtosecond laser machining (FLM) and a combination of powderblasting and heat treatment. It is shown that the latter two methods are very promising.
Original language | Undefined |
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Title of host publication | MME 2008, 19th MicroMechanics Europe Workshop |
Place of Publication | Munchen, Germany |
Publisher | VDI/VDE IT |
Pages | 45-48 |
Number of pages | 4 |
ISBN (Print) | 978-3-00-025529-8 |
Publication status | Published - 28 Sept 2008 |
Event | 19th MicroMechanics Europe Workshop, MME 2008 - Aachen, Germany Duration: 28 Sept 2008 → 30 Sept 2008 Conference number: 19 |
Publication series
Name | |
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Publisher | VDI/VDE IT |
Number | WoTUG-31 |
Workshop
Workshop | 19th MicroMechanics Europe Workshop, MME 2008 |
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Abbreviated title | MME |
Country/Territory | Germany |
City | Aachen |
Period | 28/09/08 → 30/09/08 |
Keywords
- EWI-14567
- METIS-254975
- IR-65200