Please use this identifier to cite or link to this item:
http://10.1.7.192:80/jspui/handle/123456789/8673
Title: | Emulsion Technique in Fabrication of Space Telescope Mirror |
Authors: | Kothadiya, Krupalkumar K. |
Keywords: | Mechanical 2015 Project Report Project Report 2015 Mechanical Project Report 15MME 15MMCC 15MMCC09 CAD/CAM CAD/CAM 2015 |
Issue Date: | 1-Jun-2017 |
Publisher: | Institute of Technology |
Series/Report no.: | 15MMCC09; |
Abstract: | The 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. |
URI: | http://10.1.7.192:80/jspui/handle/123456789/8673 |
Appears in Collections: | Dissertation, ME (CAD/CAM) |
Files in This Item:
File | Description | Size | Format | |
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15MMCC09.pdf | 15MMCC09 | 8.57 MB | Adobe PDF | ![]() View/Open |
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