Please use this identifier to cite or link to this item: http://10.1.7.192:80/jspui/handle/123456789/8673
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dc.contributor.authorKothadiya, Krupalkumar K.-
dc.date.accessioned2019-08-17T05:59:27Z-
dc.date.available2019-08-17T05:59:27Z-
dc.date.issued2017-06-01-
dc.identifier.urihttp://10.1.7.192:80/jspui/handle/123456789/8673-
dc.description.abstractThe optical primary mirror is the most critical and important component of an space optical telescope. The primary mirror is main heaviest component used for manufacturing the astronomical optical telescope. The optimization of the optical telescope design can be addressed by reducing mirror weight, cost, and mirror materials. For improvement of the mirror active surface configuring, polish- ing, and surface coating is required. Traditional way of fabricating techniques like milling is expensive and consume lots of time. Existing joining process like Hy- droxide bonding technique can be used for fabricating primary mirror. Establish the bonding between materials becomes a challenging task, when high stability is required at temperature variation. Stable, simple room temperature bonding process with less thickness and better strength makes hydroxide bonding process better option for making primary mirror. For making light weight and stable large primary mirror CFRP is the best candidate. By optical surface transfer method CFRP mirror can be manufacured. Due to use of coating and other suggestion like to add an extra resin layer, CFRP mirror active surface can improve.en_US
dc.publisherInstitute of Technologyen_US
dc.relation.ispartofseries15MMCC09;-
dc.subjectMechanical 2015en_US
dc.subjectProject Reporten_US
dc.subjectProject Report 2015en_US
dc.subjectMechanical Project Reporten_US
dc.subject15MMEen_US
dc.subject15MMCCen_US
dc.subject15MMCC09en_US
dc.subjectCAD/CAMen_US
dc.subjectCAD/CAM 2015en_US
dc.titleEmulsion Technique in Fabrication of Space Telescope Mirroren_US
dc.typeDissertationen_US
Appears in Collections:Dissertation, ME (CAD/CAM)

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