NASA NTRS · 19710000114
Computer program for thermal analysis of shadow shields in a vacuum
Abstract
Computer program determines temperature profiles and heat transfer rates for shadow shielded cryogenic tank. Tank, shields, and thermal radiation heat source are all axisymmetric. Thermal analysis considers varying shield and tank temperatures, surface properties, and geometric arrangements. Similar heat source properties are also considered.
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Boyle, R. J., Knoll, R. H.. 1971-05-01. Computer program for thermal analysis of shadow shields in a vacuum. https://ntrs.nasa.gov/citations/19710000114
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