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OverviewMost orbital satellites today rely on solar panels to generate the necessary power for their normal operation. A spacecraft electrical power system (SEPS) generates stores, regulates, control, and distributes required electric power to whole spacecraft loads during the space mission life time. The (SEPS) consists of three main subsystems: primary power supply subsystem (PPSS), secondary power supply subsystem (SPSS), and control - regulation -distribution subsystem (CRDS). This search is focused on the designing of the PPSS. In this work the designed system is based on the conversion of PV energy into electric power via the (PV effect) using the solar cells. The main goal of the design procedure of the spacecraft (PPSS) is the verification of the optimal solution of generating the electric power required for the spacecraft loads, during the daylight of the orbit, and also able to charge the battery (SPSS) with the required power for the spacecraft loads, during the eclipse period of the orbit. the impacts of space radiation and the variation of the operating temperature of the cell are considered, And it can compare between the several categories of PV cells. Full Product DetailsAuthor: Kareem MorsyPublisher: Noor Publishing Imprint: Noor Publishing Dimensions: Width: 15.20cm , Height: 0.80cm , Length: 22.90cm Weight: 0.200kg ISBN: 9786200066282ISBN 10: 6200066280 Pages: 128 Publication Date: 12 July 2019 Audience: General/trade , General Format: Paperback Publisher's Status: Active Availability: In stock We have confirmation that this item is in stock with the supplier. It will be ordered in for you and dispatched immediately. Table of ContentsReviewsAuthor InformationTab Content 6Author Website:Countries AvailableAll regions |