Development of Full-Scale Ultrathin Shell Reflector
It is aimed that a new ultrathin shell composite reflector is developed considering different design options to optimize the stiffness/mass ratio, cost, and manufacturing. The reflector is an offset parabolic reflector with a diameter of 6 m, a focal length of 4.8 m, and an offset of 0.3 m and has t...
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Online Access: | http://dx.doi.org/10.1155/2012/829780 |
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doaj-112b7daf7ecd440a85fc7179db0bb1052020-11-25T00:19:57ZengHindawi LimitedInternational Journal of Antennas and Propagation1687-58691687-58772012-01-01201210.1155/2012/829780829780Development of Full-Scale Ultrathin Shell ReflectorDurmuş Türkmen0Ömer Soykasap1Şükrü Karakaya2Department of Mechanical Engineering, Pamukkale University, 20070 Denizli, TurkeyDepartment of Material Science and Engineering, Afyon Kocatepe University, 03200 Afyonkarahisar, TurkeyDepartment of Mechanical Education, Afyon Kocatepe University, 03200 Afyonkarahisar, TurkeyIt is aimed that a new ultrathin shell composite reflector is developed considering different design options to optimize the stiffness/mass ratio, cost, and manufacturing. The reflector is an offset parabolic reflector with a diameter of 6 m, a focal length of 4.8 m, and an offset of 0.3 m and has the ability of folding and self-deploying. For Ku-band missions a full-scale offset parabolic reflector antenna is designed by considering different concepts of stiffening: (i) reflective surface and skirt, (ii) reflective surface and radial ribs, and (iii) reflective surface, skirt, and radial ribs. In a preliminary study, the options are modeled using ABAQUS finite element program and compared with respect to their mass, fundamental frequency, and thermal surface errors. It is found that the option of reflective surface and skirt is more advantageous. The option is further analyzed to optimize the stiffness/mass ratio considering the design parameters of material thickness, width of the skirt, and ply angles. Using the TOPSIS method is determined the best reflector concept among thirty different designs. Accordingly, new design can be said to have some advantages in terms of mass, natural frequency, number of parts, production, and assembly than both SSBR and AstroMesh reflectors.http://dx.doi.org/10.1155/2012/829780 |
collection |
DOAJ |
language |
English |
format |
Article |
sources |
DOAJ |
author |
Durmuş Türkmen Ömer Soykasap Şükrü Karakaya |
spellingShingle |
Durmuş Türkmen Ömer Soykasap Şükrü Karakaya Development of Full-Scale Ultrathin Shell Reflector International Journal of Antennas and Propagation |
author_facet |
Durmuş Türkmen Ömer Soykasap Şükrü Karakaya |
author_sort |
Durmuş Türkmen |
title |
Development of Full-Scale Ultrathin Shell Reflector |
title_short |
Development of Full-Scale Ultrathin Shell Reflector |
title_full |
Development of Full-Scale Ultrathin Shell Reflector |
title_fullStr |
Development of Full-Scale Ultrathin Shell Reflector |
title_full_unstemmed |
Development of Full-Scale Ultrathin Shell Reflector |
title_sort |
development of full-scale ultrathin shell reflector |
publisher |
Hindawi Limited |
series |
International Journal of Antennas and Propagation |
issn |
1687-5869 1687-5877 |
publishDate |
2012-01-01 |
description |
It is aimed that a new ultrathin shell composite reflector is developed considering different design options to optimize the stiffness/mass ratio, cost, and manufacturing. The reflector is an offset parabolic reflector with a diameter of 6 m, a focal length of 4.8 m, and an offset of 0.3 m and has the ability of folding and self-deploying. For Ku-band missions a full-scale offset parabolic reflector antenna is designed by considering different concepts of stiffening: (i) reflective surface and skirt, (ii) reflective surface and radial ribs, and (iii) reflective surface, skirt, and radial ribs. In a preliminary study, the options are modeled using ABAQUS finite element program and compared with respect to their mass, fundamental frequency, and thermal surface errors. It is found that the option of reflective surface and skirt is more advantageous. The option is further analyzed to optimize the stiffness/mass ratio considering the design parameters of material thickness, width of the skirt, and ply angles. Using the TOPSIS method is determined the best reflector concept among thirty different designs. Accordingly, new design can be said to have some advantages in terms of mass, natural frequency, number of parts, production, and assembly than both SSBR and AstroMesh reflectors. |
url |
http://dx.doi.org/10.1155/2012/829780 |
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