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Degradation testing of spacecraft materials for long flights in low Earth orbitстатья
Информация о цитировании статьи получена из
Web of Science,
Scopus
Статья опубликована в журнале из списка Web of Science и/или Scopus
Дата последнего поиска статьи во внешних источниках: 18 июля 2013 г.
- Авторы: Novikov L.S., Chernik V.N., Naumov S.F., Sokolova S.P., Gerasimova T.I., Kurilyonok A.O., Smirnova T.N.
- Журнал: Journal of Spacecraft and Rockets
- Том: 43
- Номер: 3
- Год издания: 2006
- Издательство: American Institute of Aeronautics and Astronautics
- Местоположение издательства: United States
- Первая страница: 534
- Последняя страница: 538
- DOI: 10.2514/1.15661
- Аннотация: Results of simulation tests of the influence of the protective and functional coatings on the resistance of polymeric constructional spacecraft materials to the impact of atomic oxygen with fluences up to 3.5 × 10 22 cm -2 are presented. It was demonstrated that oxygen plasma beams can be used in accelerated tests of carbon-based and polymeric material structures (with the exception of filled and fluorinated hydrocarbons) to evaluate their resistance to the atomic oxygen impact in low Earth orbit. For unprotected materials, a sharp fall of mechanical properties and a deterioration of optical characteristics were observed. The application of protective coatings is shown to reduce this degradation
- Добавил в систему: Воронина Екатерина Николаевна