4.3 Article

A steady state pressure drop model for screen channel liquid acquisition devices

期刊

CRYOGENICS
卷 64, 期 -, 页码 260-271

出版社

ELSEVIER SCI LTD
DOI: 10.1016/j.cryogenics.2014.03.005

关键词

Liquid acquisition devices; Liquid hydrogen; Cryogenic fluid management; Porous screen; Thermodynamic vent heat exchanger; Fuel depot

资金

  1. Cryogenic Propellant Storage and Transfer (CPST) Project under the Space Technology Mission Directorate's (STMD) Technology Demonstration Program at NASA

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This paper presents the derivation of a simplified one dimensional (1D) steady state pressure drop model for flow through a porous liquid acquisition device (LAD) inside a cryogenic propellant tank. Experimental data is also presented from cryogenic LAD tests in liquid hydrogen (LH2) and liquid oxygen (LOX) to compare against the simplified model and to validate the model at cryogenic temperatures. The purpose of the experiments was to identify the various pressure drop contributions in the analytical model which govern LAD channel behavior during dynamic, steady state outflow. LH2 pipe flow of LAD screen samples measured the second order flow-through-screen (FfS) pressure drop, horizontal LOX LAD outflow tests determined the relative magnitude of the third order frictional and dynamic losses within the channel, while LH2 inverted vertical outflow tests determined the magnitude of the first order hydrostatic pressure loss and validity of the full ID model. When compared to room temperature predictions, the FTS pressure drop is shown to be temperature dependent, with a significant increase in flow resistance at LH2 temperatures. Model predictions of frictional and dynamic losses down the channel compare qualitatively with LOX LADs data. Meanwhile, the 1D model predicted breakdown points track the trends in the LH2 inverted outflow experimental results, with discrepancies being due to a non-uniform injection velocity across the LAD screen not accounted for in the model. Published by Elsevier Ltd.

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