Optical-electronic sensor of spacecraft heat protection ablation

dc.contributor.author	Hornostaev, G.
dc.date.accessioned	2017-06-03T04:49:55Z
dc.date.available	2017-06-03T04:49:55Z
dc.date.issued	2008
dc.identifier.citation	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.	uk_UA
dc.identifier.issn	1560-8034
dc.identifier.other	PACS 41.81.Pa
dc.identifier.uri	http://dspace.nbuv.gov.ua/handle/123456789/119057
dc.description.abstract	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.	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	Optical-electronic sensor of spacecraft heat protection ablation	uk_UA
dc.type	Article	uk_UA
dc.status	published earlier	uk_UA