SPECTRAL DEPENDENCE OF ULTRAVIOLET-INDUCED DEGRADATION OF COATINGS FOR SPACECRAFT THERMAL CONTROL

Author:

Arvesen John C.

Publisher

Elsevier

Reference16 articles.

1. Arvesen, J. C. Neel, C. B. and Shaw, C. C. “Preliminary results from a round-robin study of ultraviolet degradation of spacecraft thermal control coatings,” NASA SP-55 (1965).

2. Neel, C. B. “Research on the stability of thermal control coatings for spacecraft,” Proceedings of the Fifth International Symposium on Space Technology and Science (Agne Corp. Tokyo, Japan, 1964

3. Measurement of thermal-radiation characteristics of temperature-control surfaces during flight in space;Neel;Instrument Soc. Am. Trans.,1964

4. Preliminary results from the Ames emissivity experiment on OSO-II;Pearson,1966

5. Spicer, W. E. “Radiation effects on optical materials,” NASA SP-71, pp. 123–129 (1964).

Cited by 3 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Bibliography;Coatings, Systems, and Composites;1973

2. Radiation-Induced Absorption Bands in Spacecraft Thermal Control Coating Pigments;Thermophysics: Applications to Thermal Design of Spacecraft;1970-01-01

3. RESULTS FROM THE THERMAL CONTROL COATINGS EXPERIMENT ON OSO-III;Thermal Design Principles of Spacecraft and Entry Bodies;1969

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