Emissivity estimation of spacecraft thermal control surfaces at cryogenic temperatures – a novel experimental approach

Author:

Yenni Govinda Rao,Ambirajan Amrit,Balaji C.,Venkateshan S. P.

Publisher

Springer Science and Business Media LLC

Subject

Fluid Flow and Transfer Processes,Condensed Matter Physics

Reference16 articles.

1. Kauder L (2005) Spacecraft thermal control coatings references, NASA/ Goddard Space Flight Center, Greenbelt, MD, NASA Report TP–2005–212792

2. Fabron C, Meurat A (2001) Measurement of total hemispheric emissivity at low temperatures-designing a cryogenic test bench, Proceedings of 4th International Symposium on Environmental Testing for Space Programs, Liege, Belgium (Report No. ESA SP-467)

3. Yenni GR, Ambirajan A, Balaji C, Venkateshan SP (2017) A novel experimental approach to measure the emissivity of spacecraft thermal control coatings at cryogenic temperatures, Proceedings of the 24th National and 02nd International ISHMT-ASTFE Heat and Mass Transfer Conference, BITS Pilani, Hyderabad, India

4. Bass M, Van Stryland EW, Williams DR, Wolfe WL (1995) Handbook of optics – devices, measurements and properties, volume II, 2nd edn. McGRAW-HILL INC., New York

5. Product Brochure (2004) Aeroglaze Z307 absorptive conductive polyurethane, black, ©Lord Corporation, DS3018 (Rev. 3, 11/04). http://www.lord.com

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