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Screen Channel Liquid Acquisition Device Outflow Tests in Liquid HydrogenThis paper presents experimental design and test results of the recently concluded 1-g inverted vertical outflow testing of two 325x2300 full scale liquid acquisition device (LAD) channels in liquid hydrogen (LH2). One of the channels had a perforated plate and internal cooling from a thermodynamic vent system (TVS) to enhance performance. The LADs were mounted in a tank to simulate 1-g outflow over a wide range of LH 2 temperatures (20.3 – 24.2 K), pressures (100 – 350 kPa), and flow rates (0.010 – 0.055 kg/s). Results indicate that the breakdown point is dominated by liquid temperature, with a second order dependence on mass flow rate through the LAD. The best performance is always achieved in the coldest liquid states for both channels, consistent with bubble point theory. Higher flow rates cause the standard channel to break down relatively earlier than the TVS cooled channel. Both the internal TVS heat exchanger and subcooling the liquid in the propellant tank are shown to significantly improve LAD performance.
Document ID
20140010818
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
J W Hartwig ORCID
(Glenn Research Center Cleveland, United States)
D J Chato ORCID
(Glenn Research Center Cleveland, United States)
J B McQuillen
(Glenn Research Center Cleveland, United States)
J Vera
(Glenn Research Center Cleveland, United States)
M T Kudlac
(Glenn Research Center Cleveland, United States)
F D Quinn
(Glenn Research Center Cleveland, United States)
Date Acquired
August 19, 2014
Publication Date
March 4, 2014
Publication Information
Publication: Cryogenics
Publisher: Elsevier
Volume: 64
Issue Publication Date: November 1, 2014
ISSN: 0011-2275
e-ISSN: 1879-2235
Subject Category
Fluid Mechanics and Thermodynamics
Spacecraft Propulsion and Power
Report/Patent Number
GRC-E-DAA-TN10924
Meeting Information
Meeting: 25th Space Cryogenics Workshop (SCW)
Location: Girdwood, AK
Country: US
Start Date: June 23, 2013
End Date: June 25, 2013
Sponsors: Goddard Space Flight Center, Cryogenics Society of America
Funding Number(s)
WBS: 645454.01.04.04.02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
Single Expert
Keywords
Fuel Depot
Thermodynamic Vent Heat Exchanger
Subcooled Liquid
Cryogenic Fluid Management
Liquid Acquisition Device
Thermodynamic Vent System
Liquid Hydrogen
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