4.3 Article

Screen channel liquid acquisition device outflow tests in liquid hydrogen

期刊

CRYOGENICS
卷 64, 期 -, 页码 295-306

出版社

ELSEVIER SCI LTD
DOI: 10.1016/j.cryogenics.2014.02.011

关键词

Liquid acquisition devices; Liquid hydrogen; Cryogenic fluid management; Subcooled liquid; Thermodynamic vent heat exchanger; Fuel depot

资金

  1. Cryogenic Propellant Storage and Transfer (CPST) Project under the Office of the Chief Technologist (OCT) at NASA

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This paper presents experimental design and test results of the recently concluded 1-g inverted vertical outflow testing of two 325 x 2300 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 LH2 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. Published by Elsevier Ltd.

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