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- W1654017740 abstract "For a number of years, we have been studying the application of advanced ceramic fabric materials to spacecraft heat rejection systems. Our studies indicated that significant mass and launch volume savings could be realized through such application, but concrete evidence to support this contention was lacking. Recently, we have performed tests that support our claims. Test results demonstrate that thin (about 130 ..mu..m) fabric tubes lined with metal foil can sustain pressures to 3 MPa. Even more intriguing are the results of heat transfer measurements. Although several of the ceramic fabrics exhibit promising optical properties, these would require considerable improvement if transmission of radiant energy from the metal foil through the fabrics were to be the chief heat rejection mechanism. Instead, we have found that a complex combination of conduction and radiation-absorption-reradiation mechanisms, which are poorly understood yet, achieves an effective emittance of about 0.7. That is, a ceramic fabric material such as aluminoborosilicate, which is normally considered a thermal insulator, acts as a moderate-emittance coating on the metal foil. 3 refs., 4 figs., 3 tabs." @default.
- W1654017740 created "2016-06-24" @default.
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- W1654017740 date "1989-01-01" @default.
- W1654017740 modified "2023-09-27" @default.
- W1654017740 title "Construction and testing of advanced ceramic fabric radiator components" @default.
- W1654017740 hasPublicationYear "1989" @default.
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