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

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 g...

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Veröffentlicht in:Semiconductor Physics Quantum Electronics & Optoelectronics
Datum:2008
Hauptverfasser: Hornostaev, G., Pasichny, V., Lytvynenko, Yu.
Format: Artikel
Sprache:Englisch
Veröffentlicht: Інститут фізики напівпровідників імені В.Є. Лашкарьова НАН України 2008
Online Zugang:https://nasplib.isofts.kiev.ua/handle/123456789/118861
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Назва журналу:Digital Library of Periodicals of National Academy of Sciences of Ukraine
Zitieren: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.

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Digital Library of Periodicals of National Academy of Sciences of Ukraine
Beschreibung
Zusammenfassung: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.
ISSN:1560-8034