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Liquid Transfer Cryogenic Test Facility: Initial hydrogen and nitrogen no-vent fill dataThe Liquid Transfer Cryogenic Test Facility is a versatile testbed for ground-based cryogenic fluid storage, handling, and transfer experimentation. The test rig contains two well instrumented tanks, and a third interchangeable tank, designed to accommodate liquid nitrogen or liquid hydrogen testing. The internal tank volumes are approx. 18, 5, and 1.2 cu. ft. Tank pressures can be varied from 2 to 30 psia. Preliminary no vent fill tests with nitrogen and hydrogen were successfully completed with the test rig. Initial results indicate that no vent fills of nitrogen above 90 percent full are achievable using this test configuration, in a 1-g environment, and with inlet liquid temperatures as high as 143 R, and an average tank wall temperature of nearly 300 R. This inlet temperature corresponds to a saturation pressure of 19 psia for nitrogen. Hydrogen proved considerably more difficult to transfer between tanks without venting. The highest temperature conditions resulting in a fill level greater than 90 percent were with an inlet liquid temperature of 34 R, and an estimated tank wall temperature of slightly more than 100 R. Saturation pressure for hydrogen at this inlet temperature is 10 psia. All preliminary no vent fill tests were performed with a top mounted full cone nozzle for liquid injection. The nozzle produces a 120 degree conical droplet spray at a differential pressure of 10 psi. Pressure in the receiving tank was held to less than 30 psia for all tests.
Document ID
19900011979
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)
Papell, S. Stephen
(Analex Corp. Cleveland, OH., United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1990
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
E-5396
NASA-TM-102572
NAS 1.15:102572
Report Number: E-5396
Report Number: NASA-TM-102572
Report Number: NAS 1.15:102572
Accession Number
90N21295
Funding Number(s)
PROJECT: RTOP 591-23-00
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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