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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Main Authors: Durmuş Türkmen, Ömer Soykasap, Şükrü Karakaya
Format: Article
Language:English
Published: Hindawi Limited 2012-01-01
Series:International Journal of Antennas and Propagation
Online Access:http://dx.doi.org/10.1155/2012/829780
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spelling 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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