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Evaluation of proportional flow control valvesFlow control of propellant to an electric thruster is an important parameter in the design of reliable, versatile and cost effective electric propulsion subsystems for spacecraft.
Document ID
20060033165
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
hdl:2014/15776
Authors
Shortwell, R.
Butler, B.
Bushway, D.
Perini, D.
Gross, S.
Kelly, R.
Date Acquired
August 23, 2013
Publication Date
July 16, 2000
Subject Category
Spacecraft Propulsion And Power
Distribution Limits
Public
Copyright
Other
Keywords
valve proportional flow feed system electric propulsion

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