Optical-electronic sensor of spacecraft heat protection ablation

Block diagram and results of tests on gas-dynamic stands are represented to illustrate operation of the continuous ablation sensor, in which color light guides with a diameter of 1 mm are used. It is shown that the application of compensating light filter in the colorless channel makes it possibl...

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Bibliographic Details
Published in:Semiconductor Physics Quantum Electronics & Optoelectronics
Date:2008
Main Author: Hornostaev, G.
Format: Article
Language:English
Published: Інститут фізики напівпровідників імені В.Є. Лашкарьова НАН України 2008
Online Access:https://nasplib.isofts.kiev.ua/handle/123456789/119057
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Journal Title:Digital Library of Periodicals of National Academy of Sciences of Ukraine
Cite this:Optical-electronic sensor of spacecraft heat protection ablation / G. Hornostaev // Semiconductor Physics Quantum Electronics & Optoelectronics. — 2008. — Т. 11, № 3. — С. 245-247. — Бібліогр.: 3 назв. — англ.

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Digital Library of Periodicals of National Academy of Sciences of Ukraine
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Summary:Block diagram and results of tests on gas-dynamic stands are represented to illustrate operation of the continuous ablation sensor, in which color light guides with a diameter of 1 mm are used. It is shown that the application of compensating light filter in the colorless channel makes it possible to create the meter invariant to external radiant fluxes applied to the heat protection covering surface.
ISSN:1560-8034