NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Due to the lapse in federal government funding, NASA is not updating this website. We sincerely regret this inconvenience.

Back to Results
Preliminary Study of a Piston Pump for Cryogenic FluidsPreliminary data are presented covering the performance of a low-speed, five-cylinder piston pump designed for handling boiling hydrogen. This pump was designed for a flow of 55 gallons per minute at 240 rpm with a discharge pressure of 135 pounds per square inch. Tests were made using JP-4 fuel, liquid nitrogen, and liquid hydrogen. Pump delivery and endurance characteristics were satisfactory for the range of operation covered. In connection with the foregoing pump development, the cavitation characteristics of a preliminary visual model, glass-cylinder pump and of a simple reciprocating disk were studied. Subcooling of approximately 0.60 F was obtained from the cavitation produced by reciprocating a disk in boiling nitrogen and in boiling water. The subcooling obtained in a similar manner with liquid hydrogen was somewhat less.
Document ID
19980228227
Acquisition Source
Headquarters
Document Type
Other - NASA Memorandum (MEMO)
Authors
Biermann, Arnold E.
(NASA Lewis Research Center Cleveland, OH United States)
Kohl, Robert C.
(NASA Lewis Research Center Cleveland, OH United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1959
Subject Category
Mechanical Engineering
Report/Patent Number
NASA-MEMO-3-6-59E
E-239
Report Number: NASA-MEMO-3-6-59E
Report Number: E-239
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available