Design of optical-electronic sensor for ablation of spacecraft heat protection

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Фізико-технічні та математичні науки
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Відділення фізики і астрономії
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Semiconductor Physics Quantum Electronics & Optoelectronics
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Semiconductor Physics Quantum Electronics & Optoelectronics, 2008, том 11
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Semicond. Physics Quantum Electronics & Optoelectronics, 2008, № 2
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dc.contributor.author	Hornostaev, G.
dc.contributor.author	Pasichny, V.
dc.contributor.author	Lytvynenko, Yu.
dc.date.accessioned	2017-05-31T19:32:36Z
dc.date.available	2017-05-31T19:32:36Z
dc.date.issued	2008
dc.identifier.citation	Design of optical-electronic sensor for ablation of spacecraft heat protection / G. Hornostaev, V. Pasichny, Yu. Lytvynenko // Semiconductor Physics Quantum Electronics & Optoelectronics. — 2008. — Т. 11, № 2. — С. 159-162. — Бібліогр.: 2 назв. — англ.	uk_UA
dc.identifier.issn	1560-8034
dc.identifier.other	PACS 41.81.Pa
dc.identifier.uri	http://dspace.nbuv.gov.ua/handle/123456789/118861
dc.description.abstract	Results of designing and studying the characteristics of the fiber-optic sensor for the ablation of the low-sublimating heat protection which intended for the use on the being got down module of article “Mars-5” are represented. The originality of development consists of guarantee for continuous measurement of the instantaneous value of thickness of heat protective coating of the article during its descent. Achieving this goal is ensured by the application of two light-guide sensors, one of which is made from color glass-light filter.	uk_UA
dc.language.iso	en	uk_UA
dc.publisher	Інститут фізики напівпровідників імені В.Є. Лашкарьова НАН України	uk_UA
dc.relation.ispartof	Semiconductor Physics Quantum Electronics & Optoelectronics
dc.title	Design of optical-electronic sensor for ablation of spacecraft heat protection	uk_UA
dc.type	Article	uk_UA
dc.status	published earlier	uk_UA