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Performance measurements using a sub-micronewton resolution thrust standThis paper describes the development and testing of a microthrust stand in the Advanced Propulsion Technology Laboratory at NASA/JPL.
Document ID
20060031972
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
Authors
Ziemer, J. K.
Date Acquired
August 23, 2013
Publication Date
October 15, 2001
Subject Category
Spacecraft Propulsion And Power
Distribution Limits
Public
Copyright
Other
Keywords
thrust measurement micropropulsion

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