NASA NTRS · 19690000537
Spacecraft Thermal Radiation Environment Computer Program
Abstract
Computer program computes the total thermal radiation flux on each of a set of exposed surface elements of a spacecraft in the vicinity of a celestial body. The incident flux consists of solar, both direct and planetary-reflected, and planetary-emitted infrared radiation as functions of time.
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Paoletti, C. J., Scates, J. H.. 1969-10-01. Spacecraft Thermal Radiation Environment Computer Program. https://ntrs.nasa.gov/citations/19690000537
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