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Rotating and positive-displacement pumps for low-thrust rocket engines. Volume 2: Fabrication and testingRotating and positive displacement pumps of various types were studied for pumping liquid fluorine for low thrust high performance rocket engines. Included in the analysis were: centrifugal, pitot, Barske, Tesla, drag, gear, vane, axial piston, radial piston, diaphragm and helirotor pump concepts. The centrifugal and gear pumps were carried through detail design and fabrication. After preliminary testing in Freon 12, the centrifugal pump was selected for further testing and development. It was tested in Freon 12 to obtain the hydrodynamic performance. Tests were also conducted in liquid fluorine to demonstrate chemical compatibility.
Document ID
19740015231
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Csomor, A.
(Rockwell International Corp. Canoga Park, CA, United States)
Date Acquired
September 3, 2013
Publication Date
February 1, 1974
Subject Category
Propulsion Systems
Report/Patent Number
R-8494-2-VOL-2
NASA-CR-72966
Report Number: R-8494-2-VOL-2
Report Number: NASA-CR-72966
Accession Number
74N23344
Funding Number(s)
CONTRACT_GRANT: NAS3-12022
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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