A Conceptual Design of Deployable Antenna Mechanisms

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Publicat a:Aerospace vol. 11, no. 11 (2024), p. 938
Autor principal: Kang, Hyeongseok
Altres autors: Hwang, Bohyun, Kim, Sooyoung, Lee, Hyeonseok, Koo, Kyungrae, Seonggun Joe, Kim, Byungkyu
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MDPI AG
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024 7 |a 10.3390/aerospace11110938  |2 doi 
035 |a 3132818234 
045 2 |b d20240101  |b d20241231 
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100 1 |a Kang, Hyeongseok  |u Department of Smart Air Mobility, Korea Aerospace University, Goyang 10540, Republic of Korea; <email>khsork0115@naver.com</email> 
245 1 |a A Conceptual Design of Deployable Antenna Mechanisms 
260 |b MDPI AG  |c 2024 
513 |a Journal Article 
520 3 |a Over the last decade, large-scale antennas have been developed to enhance precise blue force tracking and improve situational awareness. In general, such large-scale antennas, ranging from 1 to up to 10 m, need a specific mechanism that can reconfigure their shapes and morphologies, resulting in stowing and deploying upon the given environment. In parallel, it must be noted that such deployable mechanisms should accommodate a large aperture diameter while ensuring they are lightweight, robust, and structurally rigid to avoid undesired deformations due to the deployment. With these in mind, this work presents a large frustum-shaped deployable antenna mechanism with a large aperture diameter of 7.5 m. The deployable mechanism is composed of hierarchical bayes the radial direction at 30° intervals. Twelve bayes in total identify the overall morphology of the deployable antenna, which features a dodecagon. Specifically, the bay is composed of three linkage structures: a six-bar linkage mechanism, a V-folding mechanism, and a single pantograph mechanism. As a result of static and dynamic simulations, it is identified that the mechanism achieves an area-to-mass ratio of 5.003 m2/kg and a safety factor of 323.8 upon deployment. Conclusively, this work demonstrates a strong potential of the deployable antenna mechanism, providing high rigidity and large aperture diameter while ensuring high stability in space environments. 
653 |a Situational awareness 
653 |a Antennas 
653 |a Apertures 
653 |a Antenna design 
653 |a Safety factors 
653 |a Diameters 
653 |a Morphology 
653 |a Aerospace environments 
653 |a Rigidity 
653 |a Ground stations 
653 |a Linkage mechanisms 
700 1 |a Hwang, Bohyun  |u Department of Mechanical and Aerospace Engineering, Korea Aerospace University, Goyang 10540, Republic of Korea 
700 1 |a Kim, Sooyoung  |u Department of Mechanical and Aerospace Engineering, Korea Aerospace University, Goyang 10540, Republic of Korea 
700 1 |a Lee, Hyeonseok  |u Department of Mechanical and Aerospace Engineering, Korea Aerospace University, Goyang 10540, Republic of Korea 
700 1 |a Koo, Kyungrae  |u Satellite System Team 1, Hanwha Systems, Yongin 17121, Republic of Korea 
700 1 |a Seonggun Joe  |u Department of Autonomous Vehicle Engineering, Korea Aerospace University, Goyang 10540, Republic of Korea 
700 1 |a Kim, Byungkyu  |u Department of Smart Air Mobility, Korea Aerospace University, Goyang 10540, Republic of Korea; <email>khsork0115@naver.com</email>; Department of Mechanical and Aerospace Engineering, Korea Aerospace University, Goyang 10540, Republic of Korea 
773 0 |t Aerospace  |g vol. 11, no. 11 (2024), p. 938 
786 0 |d ProQuest  |t Advanced Technologies & Aerospace Database 
856 4 1 |3 Citation/Abstract  |u https://www.proquest.com/docview/3132818234/abstract/embedded/ZKJTFFSVAI7CB62C?source=fedsrch 
856 4 0 |3 Full Text + Graphics  |u https://www.proquest.com/docview/3132818234/fulltextwithgraphics/embedded/ZKJTFFSVAI7CB62C?source=fedsrch 
856 4 0 |3 Full Text - PDF  |u https://www.proquest.com/docview/3132818234/fulltextPDF/embedded/ZKJTFFSVAI7CB62C?source=fedsrch