Investigation of satellite structures under quasi-static acceleration loading / Adli Azeman
One of the essential asset of designing satellite is a highly efficient structure. It was seen that the design approaches used in satellite structures are the same as those used in larger satellites, with only a reduction in scale. There are new approaches and processes being implement to improve th...
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| Format: | Thesis |
| Language: | English |
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2010
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| Online Access: | https://ir.uitm.edu.my/id/eprint/31898/1/31898.pdf |
| _version_ | 1825737465914195968 |
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| author | Azeman, Adli |
| author_facet | Azeman, Adli |
| author_sort | Azeman, Adli |
| collection | UITM |
| description | One of the essential asset of designing satellite is a highly efficient structure. It was seen that the design approaches used in satellite structures are the same as those used in larger satellites, with only a reduction in scale. There are new approaches and processes being implement to improve the efficiency of structures and one of them was structural optimization method. In determine which method was better, the widely used method which are honeycomb and isogrid structure were analyzed. This project described the design and analysis of the satellite structure. Firstly, the paper will examine several previous satellite designs and their influence on the existing satellite structural design. Then, two satellite structures represent structural optimization method will be design. After that by using Finite Element Software (FEA) software, both structure strength will be evaluated. Finally, this paper presented the analysis result and the evaluation of both selected structure. The results are summarized in the conclusion which showed that isogrid structure was better than honeycomb structure. |
| first_indexed | 2024-03-06T02:18:34Z |
| format | Thesis |
| id | oai:ir.uitm.edu.my:31898 |
| institution | Universiti Teknologi MARA |
| language | English |
| last_indexed | 2024-03-06T02:18:34Z |
| publishDate | 2010 |
| record_format | dspace |
| spelling | oai:ir.uitm.edu.my:318982020-07-06T08:35:58Z https://ir.uitm.edu.my/id/eprint/31898/ Investigation of satellite structures under quasi-static acceleration loading / Adli Azeman Azeman, Adli Finite element method One of the essential asset of designing satellite is a highly efficient structure. It was seen that the design approaches used in satellite structures are the same as those used in larger satellites, with only a reduction in scale. There are new approaches and processes being implement to improve the efficiency of structures and one of them was structural optimization method. In determine which method was better, the widely used method which are honeycomb and isogrid structure were analyzed. This project described the design and analysis of the satellite structure. Firstly, the paper will examine several previous satellite designs and their influence on the existing satellite structural design. Then, two satellite structures represent structural optimization method will be design. After that by using Finite Element Software (FEA) software, both structure strength will be evaluated. Finally, this paper presented the analysis result and the evaluation of both selected structure. The results are summarized in the conclusion which showed that isogrid structure was better than honeycomb structure. 2010 Thesis NonPeerReviewed text en https://ir.uitm.edu.my/id/eprint/31898/1/31898.pdf Investigation of satellite structures under quasi-static acceleration loading / Adli Azeman. (2010) Degree thesis, thesis, Universiti Teknologi MARA Shah Alam. |
| spellingShingle | Finite element method Azeman, Adli Investigation of satellite structures under quasi-static acceleration loading / Adli Azeman |
| title | Investigation of satellite structures under quasi-static acceleration loading / Adli Azeman |
| title_full | Investigation of satellite structures under quasi-static acceleration loading / Adli Azeman |
| title_fullStr | Investigation of satellite structures under quasi-static acceleration loading / Adli Azeman |
| title_full_unstemmed | Investigation of satellite structures under quasi-static acceleration loading / Adli Azeman |
| title_short | Investigation of satellite structures under quasi-static acceleration loading / Adli Azeman |
| title_sort | investigation of satellite structures under quasi static acceleration loading adli azeman |
| topic | Finite element method |
| url | https://ir.uitm.edu.my/id/eprint/31898/1/31898.pdf |
| work_keys_str_mv | AT azemanadli investigationofsatellitestructuresunderquasistaticaccelerationloadingadliazeman |