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Feed system design for a reduced pressure tankThree designs were considered to satisfy the design objective. These designs were the current design, a Land Based Pressurized Feed System, and a fuel recirculation system. A computer code was developed to analyze the current feed system and assist in the analysis of the two experimental systems. After comparing the three concepts, the land Based Pressurized Feed System seemed to be the most promising new development. This design coupled with the piping configuration described in the report provides a justifiable fuel feed system which satisfies all the necessary requirements.
Document ID
19950019890
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Lui, Hurbert
(Vanderbilt Univ. Nashville, TN, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1994
Publication Information
Publication: The 1994 NASA(USRA)ADP Design Projects 19 p(SEE N95-26304 08-80)
Subject Category
Spacecraft Propulsion And Power
Accession Number
95N26310
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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