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- W2074539142 abstract "The capabilities of a heated tube facility used for testing rocket engine coolant channels at the NASA Lewis Research Center are presented. The facility uses high current, low voltage power supplies to resistively heat a test section to outer wall temperatures as high as 730 C (1350 F). Liquid or gaseous nitrogen, gaseous helium, or combustible liquids can be used as the test section coolant. The test section is enclosed in a vacuum chamber to minimize heat loss to the surrounding system. Test section geometry, size, and material; coolant properties; and heating levels can be varied to generate heat transfer and coolant performance data bases." @default.
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- W2074539142 date "1995-07-10" @default.
- W2074539142 modified "2023-09-27" @default.
- W2074539142 title "A heated tube facility for rocket coolant channel research" @default.
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- W2074539142 doi "https://doi.org/10.2514/6.1995-2936" @default.
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