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Experimental findings from zero-tank net positive suction head operation of the J-2 hydrogen pumpThe results of a series of liquid hydrogen turbopump tests to demonstrate the feasibility of zero-tank net positive suction head are presented. A J-2 engine hydrogen pump and S-IVB stage fuel feed system were used for this investigation. The pump was operated at flows and speeds equivalent to normal J-2 engine operating conditions and at hydrogen bulk temperatures between 39 and 45 R. These tests show zero-tank not positive suction head to be a realistic operating mode that should be considered for future applications.
Document ID
19720022157
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Stinson, H. P.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Strickland, R. J.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1972
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TN-D-6824
M-368
Report Number: NASA-TN-D-6824
Report Number: M-368
Accession Number
72N29807
Funding Number(s)
PROJECT: RTOP 128-31-63-00-62
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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