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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| Datum: | 2008 |
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| 1. Verfasser: | |
| Format: | Artikel |
| Sprache: | English |
| Veröffentlicht: |
Інститут фізики напівпровідників імені В.Є. Лашкарьова НАН України
2008
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| Schriftenreihe: | Semiconductor Physics Quantum Electronics & Optoelectronics |
| Online Zugang: | http://dspace.nbuv.gov.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. |
Institution
Digital Library of Periodicals of National Academy of Sciences of Ukraine| 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. |
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