Please use this identifier to cite or link to this item: http://hdl.handle.net/10603/9567
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dc.coverage.spatialMechanical Engineeringen_US
dc.date.accessioned2013-06-27T05:34:37Z-
dc.date.available2013-06-27T05:34:37Z-
dc.date.issued2013-06-27-
dc.identifier.urihttp://hdl.handle.net/10603/9567-
dc.description.abstractThe capabilities of micro satellites continue to increase every year for better utilities to carryout different types of missions which previously required much large satellite platforms. The miniaturization of electronic components enabled to develop satellites of small size, with weight ranging from 10-100 kg. The benefits of developing a micro satellite leads to a shorter development time and much lower costs than that required for larger satellite while achieving the same and high levels of performance and capability. The present work is to design, analyze and develop a mechanical structure of a micro-satellite upon which the scientific and operational instruments are placed. This structure must be lightweight, and resistant to thermal fluctuations, fatigue, fracture, and corrosion. Furthermore, it must provide stability to the instruments against undesirable vibrations and shocks during the launch and transportation, and must dissipate heat from the internal components. To model the micro satellite structure with subsystems and to perform the following analyses namely static, normal modes, frequency response, transient response and random vibration analysis commercially available Finite Element Analysis software MSC PATRAN and MSC NASTRAN were used. From the results of the analyses it was possible to (a) verify preliminary design of the structure and define the necessary changes, (b) determine the first global frequencies of the assembly, (c) determine the level of stresses and buckling instability in the structure and (d) verify the acceleration levels on the micro-satellite subjected to the sine and random vibrations. The results of the analyses serve as the bases for structural design and optimum design of the micro-satellite structure.en_US
dc.format.extent221p.en_US
dc.languageEnglishen_US
dc.relationNo. of references 50en_US
dc.rightsuniversityen_US
dc.titleDesign, analysis and development of micro-satellite structureen_US
dc.title.alternative-en_US
dc.creator.researcherSuresh Ken_US
dc.subject.keywordMicro-satellite structureen_US
dc.description.noteReferences p. 215-219, List of publications p. 220en_US
dc.contributor.guideJayaraman Ken_US
dc.publisher.placeChennaien_US
dc.publisher.universityAnna Universityen_US
dc.publisher.institutionFaculty of Mechanical Engineeringen_US
dc.date.registered2009en_US
dc.date.completed2011en_US
dc.date.awarded09/08/2011en_US
dc.format.dimensions-en_US
dc.format.accompanyingmaterialNoneen_US
dc.source.universityUniversityen_US
dc.type.degreePh.D.en_US
Appears in Departments:Faculty of Mechanical Engineering

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01_title.pdf37.41 kBAdobe PDFView/Open
02_certificate.pdf277.02 kBAdobe PDFView/Open
03_abstract.pdf14.76 kBAdobe PDFView/Open
04_acknowledgements.pdf9.59 kBAdobe PDFView/Open
05_contents.pdf19.33 kBAdobe PDFView/Open
06_list of tables.pdf11.37 kBAdobe PDFView/Open
07_list of figures.pdf18.3 kBAdobe PDFView/Open
08_list of abbreviations.pdf21.14 kBAdobe PDFView/Open
09_chapter 1.pdf480.81 kBAdobe PDFView/Open
10_chapter 2.pdf35.59 kBAdobe PDFView/Open
11_chapter 3.pdf230.82 kBAdobe PDFView/Open
12_chapter 4.pdf296.44 kBAdobe PDFView/Open
13_chapter 5.pdf2.28 MBAdobe PDFView/Open
14_chapter 6.pdf680.85 kBAdobe PDFView/Open
15_chapter 7.pdf3.35 MBAdobe PDFView/Open
16_chapter 8.pdf999.71 kBAdobe PDFView/Open
17_chapter 9.pdf135.65 kBAdobe PDFView/Open
18_chapter 10.pdf32.05 kBAdobe PDFView/Open
19_chapter 11.pdf15.72 kBAdobe PDFView/Open
20_references.pdf21.45 kBAdobe PDFView/Open


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