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Performance characterization of the Vaporizing Liquid Micro Thruster (VLM)

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dc.contributor.author Mueller, J. en_US
dc.contributor.author Ziemer, J. en_US
dc.contributor.author Green, A. en_US
dc.contributor.author Bame, D. en_US
dc.date.accessioned 2004-09-16T22:02:56Z
dc.date.available 2004-09-16T22:02:56Z
dc.date.issued 2003-03-17 en_US
dc.identifier.citation International Electric Propulsion Conference 2003 en_US
dc.identifier.citation Toulouse, France en_US
dc.identifier.clearanceno 03-0734
dc.identifier.uri http://hdl.handle.net/2014/7121
dc.description.abstract A Vaporizing Liquid Micro-Thruster (VLM) microfabricated thruster was tested on water propellant on a thrust stand and performance data obtained. en_US
dc.format.extent 3766470 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US
dc.subject.other micropropulsion microspacecraft constellations micro-thrust en_US
dc.title Performance characterization of the Vaporizing Liquid Micro Thruster (VLM) en_US


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