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Thermal/Stress Finite Element Analysis Applied to the Design and Packaging of Vaporizing Liquid MicrothrusterThe Jet Propulsion Laboratory is currently under NASA contract to develop a vaporizing liquid microthruster.
Document ID
20060041671
Acquisition Source
Jet Propulsion Laboratory
Document Type
Reprint (Version printed in journal)
External Source(s)
hdl:2014/21708
Authors
Wallace, A.
Date Acquired
August 23, 2013
Publication Date
January 1, 1997
Publication Information
Publication: Finite Elements in Analysis and Design
Subject Category
Spacecraft Propulsion And Power
Distribution Limits
Public
Copyright
Other
Keywords
vaporizing liquid microthruster

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