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- W2065824994 abstract "Foam multilayer insulation (FMLI), a reusable thermal control system (TCS), was evaluated in a simulated orbit hold environment on a test tank of 3.0 ft diameter, 5.6 ft length, and 34.5 cu ft volume. The TCS consisted of a 0.44-inch thick foam and a 16-layer (17 sheet) MLI blanket attached to the tank barrel and lower bulkhead, with the upper bulkhead covered with a 2.7-inch foam and a 31-layer (32 sheets) MLI blanket. Average insulation heating rates during orbit hold simulations ranged from 10.5 to 28.1 Btu/hr for warm boundary temperatures from 300 to 460 R, respectively. These rates corresponded to liquid losses of 0.9 and 2.3 percent of the tank's volume per day. This liquid loss rate would be significantly reduced for full size vehicle tanks due to the decreased surface area-to-volume ratio as compared to the test tank." @default.
- W2065824994 created "2016-06-24" @default.
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- W2065824994 date "1992-07-06" @default.
- W2065824994 modified "2023-10-16" @default.
- W2065824994 title "Cryogenic testing of a foam-multilayer insulation concept in a simulated prelaunch environment" @default.
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- W2065824994 doi "https://doi.org/10.2514/6.1992-3182" @default.
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