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Back-To-Back, Counterrotating TurbopumpsPair of counterrotating turbopumps mounted back to back in novel one-piece volute housing. Serves as spool piece into which pumps inserted, one from each end. Includes turbine inlet and outlet volutes. Enables easy replacement of each pump/turbine assembly. Designed to provide fuel and oxidizer to rocket engine at high pressures; modified versions useful in providing other two-fluid high-pressure flows or redundant high-pressure flow of single fluid.
Document ID
19900000243
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Palgon, Alfred M.
(United Technologies Corp.)
Branstrom, Bruce R.
(United Technologies Corp.)
Burgy, Frank N.
(United Technologies Corp.)
Date Acquired
August 14, 2013
Publication Date
May 1, 1990
Publication Information
Publication: NASA Tech Briefs
Volume: 14
Issue: 5
ISSN: 0145-319X
Subject Category
Machinery
Report/Patent Number
MFS-28349
ISSN: 0145-319X
Report Number: MFS-28349
Accession Number
90B10243
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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