Please use this identifier to cite or link to this item: http://hdl.handle.net/2248/5354
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dc.contributor.authorBanyal, R. K-
dc.contributor.authorRavindra, B-
dc.date.accessioned2011-02-24T10:42:08Z-
dc.date.available2011-02-24T10:42:08Z-
dc.date.issued2011-08-
dc.identifier.citationNew Astronomy, Vol. 16, No. 5, pp. 328-336-
dc.identifier.urihttp://hdl.handle.net/2248/5354-
dc.descriptionRestricted Accessen
dc.description.abstractWe present a detailed thermal and structural analysis of a 2 m class solar telescope mirror which is subjected to a varying heat load at an observatory site. A 3-dimensional heat transfer model of the mirror takes into account the heating caused by a smooth and gradual increase of the solar flux during the day-time observations and cooling resulting from the exponentially decaying ambient temperature at night. The thermal and structural response of two competing materials for optical telescopes, namely Silicon Carbide – best known for excellent heat conductivity and Zerodur – preferred for its extremely low coefficient of thermal expansion, is investigated in detail. The insight gained from these simulations will provide a valuable input for devising an efficient and stable thermal control system for the primary mirror.en
dc.language.isoenen
dc.publisherElsevier B.V.en
dc.relation.urihttp://dx.doi.org/10.1016/j.newast.2011.01.003-
dc.rights© Elsevier B.V.en
dc.subjectSolar telescope mirroren
dc.subjectOptical materialsen
dc.subjectThermal effectsen
dc.subjectFinite element methodsen
dc.titleThermal characteristics of a classical solar telescope primary mirroren
dc.typeArticleen
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