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Performance characterization of the Vaporizing Liquid Micro Thruster (VLM)A Vaporizing Liquid Micro-Thruster (VLM) microfabricated thruster was tested on water propellant on a thrust stand and performance data obtained.
Document ID
20060040034
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
hdl:2014/7121
Authors
Mueller, J.
Ziemer, J.
Green, A.
Bame, D.
Date Acquired
August 23, 2013
Publication Date
March 17, 2003
Subject Category
Spacecraft Propulsion And Power
Distribution Limits
Public
Copyright
Other
Keywords
micropropulsion microspacecraft constellations micro-thrust

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