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Conceptual design of a closed loop nutrient solution delivery system for CELSS implementation in a micro-gravity environmentDescribed here are the results of a study to develop a conceptual design for an experimental closed loop fluid handling system capable of monitoring, controlling, and supplying nutrient solution to higher plants. The Plant Feeder Experiment (PFE) is designed to be flight tested in a microgravity environment. When flown, the PFX will provide information on both the generic problems of microgravity fluid handling and the specific problems associated with the delivery of the nutrient solution in a microgravity environment. The experimental hardware is designed to fit into two middeck lockers on the Space Shuttle, and incorporates several components that have previously been flight tested.
Document ID
19910022484
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Schwartzkopf, Steven H.
(Lockheed Missiles and Space Co. Sunnyvale, CA., United States)
Oleson, Mel W.
(Boeing Aerospace Co. Seattle, WA., United States)
Cullingford, Hatice S.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1990
Publication Information
Publication: NASA. Ames Research Center, Controlled Ecological Life Support Systems: CELSS '89 Workshop
Subject Category
Man/System Technology And Life Support
Accession Number
91N31798
Funding Number(s)
CONTRACT_GRANT: NAS9-17981
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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