Please use this identifier to cite or link to this item: https://hdl.handle.net/10356/78362
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dc.contributor.authorLuo, Ruikang
dc.date.accessioned2019-06-19T02:22:20Z
dc.date.available2019-06-19T02:22:20Z
dc.date.issued2019
dc.identifier.urihttp://hdl.handle.net/10356/78362
dc.description.abstractSince the first cube satellites were launched in 1994, the government has become more open in the civil aerospace industry due to the advantages of satellite technology and the low cost-barrier. Mission design, which contains orbit simulation, link budget and power budget calculation, is essential before each launch of satellite to ensure the feasibility and success rate. In the project, the Satellite Tool Kit was used to simulate the orbit characteristics for SCOOBI to choose the most suitable orbit under the constraints of requirements. Referred other subsystems and collaborated with other groups to get useful parameters’ value to figure out the uplink and downlink budget for Telecommunication subsystem. MATLAB was used for investigating the status of solar panels on SCOOBI and plotting the diagrams of power generation and state of charge. The suitable orbit was chosen. The communication link budget and power budget were calculated. The power generated and consumption were also figured out. The proposed Electrical Power Subsystem was verified to be feasible and competent for this operation.en_US
dc.format.extent68 p.en_US
dc.language.isoenen_US
dc.rightsNanyang Technological University
dc.subjectDRNTU::Engineering::Electrical and electronic engineeringen_US
dc.titleMission design for the VELOX- Lyon-1 (rebranded SCOOBI) student CubeSaten_US
dc.typeFinal Year Project (FYP)en_US
dc.contributor.supervisorAmal Chandranen_US
dc.contributor.schoolSchool of Electrical and Electronic Engineeringen_US
dc.description.degreeBachelor of Engineering (Electrical and Electronic Engineering)en_US
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Appears in Collections:EEE Student Reports (FYP/IA/PA/PI)
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