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Temperature automation for a propellant mixerThe analysis and installation of an automatic temperature controller on a propellant mixer is presented. Ultimately, the entire mixing process will come under automation, but since precise adherence to the temperature profile is very difficult to sustain manually, this was the first component to be automated. Automation is not only important for producing a uniform product, but it is necessary for envisioned space-based propellant production.
Document ID
19910015918
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Vincent, T. L.
(Arizona Univ. Tucson, AZ, United States)
Wilson, R. G.
(Arizona Univ. Tucson, AZ, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1990
Publication Information
Publication: NASA Space Engineering Research Center for Utilization of Local Planetary Resources
Subject Category
Propellants And Fuels
Accession Number
91N25232
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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