Abstract
The performance of white paint S781 applied to the Fengyun-3 Satellite A and B in space is investigated in this paper. The solar absorptance of S781, including the degradation value in orbit in 5 years, are accumulated and analyzed by calculating the telemetry temperature data from the satellites. The result could provide the reference for other spacecrafts thermal design using the same white paint.
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References
Gilmore DG (2002) Spacecraft thermal control handbook, vol 1, 2nd edn, Fundamental technologies. The Aerospace Press, California
Min G (1991) Satellite thermal control technology. Aerospace Press, Beijing (In Chinese)
Min G (1998) Spacecraft thermal control, 2nd edn. Science Press, Beijing (In Chinese)
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Tao, X., Binbin, C., Xiaoxiang, Z. (2017). Analysis of the Performance of White Paint S781 in Space. In: Kleiman, J. (eds) Protection of Materials and Structures from the Space Environment. Astrophysics and Space Science Proceedings, vol 47. Springer, Cham. https://doi.org/10.1007/978-3-319-19309-0_7
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DOI: https://doi.org/10.1007/978-3-319-19309-0_7
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Online ISBN: 978-3-319-19309-0
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