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
Hydrogen no-vent fill testing in a 1.2 cubic foot (34 liter) tankExperimental results of no-vent fill testing with liquid hydrogen in a 1.2 cubic foot (34 liter) stainless steel tank are presented. More than 40 tests were performed with various liquid inlet temperatures, inlet flowrates, initial tank wall temperatures, and liquid injection techniques. Fill levels equal to or exceeding 90 percent by volume were achieved in 40 percent of the tests with the tank pressure limited to a maximum of 30 psia. Three liquid injection techniques were employed; top spray, upward pipe discharge, and bottom diffuser. Effects of each of the varied parameters on the tank pressure history and final fill level are evaluated. The final fill level is found to be indirectly proportional to the initial wall and inlet liquid temperatures and directly proportional to the inlet liquid flowrate. Furthermore, the top spray is the most efficient no-vent fill method of the three configurations examined. The success of this injection method is primarily due to condensation of the ullage vapor onto the incoming liquid droplets. Ullage condensation counteracts the tank pressure rise resulting from energy exchange between the fluid and the warmer tank walls, and ullage compression. Upward pipe discharge from the tank bottom is the next most efficient method. Fluid circulation induced by this fill configuration tends to diminish thermal stratification in the bulk liquid, thus enhancing condensation at the liquid gas interface.
Document ID
19920004183
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Moran, Matthew E.
(NASA Lewis Research Center Cleveland, OH, United States)
Nyland, Ted W.
(NASA Lewis Research Center Cleveland, OH, United States)
Driscoll, Susan L.
(NASA Marshall Space Flight Center Huntsville, AL., United States)
Date Acquired
September 6, 2013
Publication Date
October 1, 1991
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
E-6596
NASA-TM-105273
NAS 1.15:105273
Report Number: E-6596
Report Number: NASA-TM-105273
Report Number: NAS 1.15:105273
Accession Number
92N13401
Funding Number(s)
PROJECT: RTOP 593-21-41
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available