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...

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Veröffentlicht in:Semiconductor Physics Quantum Electronics & Optoelectronics
Datum:2008
1. Verfasser: Hornostaev, G.
Format: Artikel
Sprache:Englisch
Veröffentlicht: Інститут фізики напівпровідників імені В.Є. Лашкарьова НАН України 2008
Online Zugang:https://nasplib.isofts.kiev.ua/handle/123456789/119057
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Назва журналу:Digital Library of Periodicals of National Academy of Sciences of Ukraine
Zitieren: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
Beschreibung
Zusammenfassung: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