Design of Solar Array Systems for Satellites - Couverture souple

Morsy, Kareem

9786200066282: Design of Solar Array Systems for Satellites

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ISBN 10 : 6200066280 ISBN 13 : 9786200066282

Editeur : Noor Publishing, 2019

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La plupart des satellites orbitaux comptent aujourd'hui sur des panneaux solaires pour g�n�rer l'�nergie n�cessaire � leur fonctionnement normal. Un syst�me d'alimentation �lectrique pour vaisseau spatial (SEPS) g�n�re des stockes, r�gule, contr�le et distribue l'�nergie �lectrique n�cessaire � des charges enti�res du vaisseau spatial pendant la dur�e de vie de la mission spatiale. Le (SEPS) se compose de trois sous-syst�mes principaux : le sous-syst�me d'alimentation primaire (PPSS), le sous-syst�me d'alimentation secondaire (SPSS) et le sous-syst�me de contr�le - r�gulation - distribution (CRDS). Cette recherche est ax�e sur la conception du PPSS. Dans ce travail, le syst�me con�u est bas� sur la conversion de l'�nergie PV en �nergie �lectrique via l'effet PV en utilisant les cellules solaires. L'objectif principal de la proc�dure de conception du vaisseau spatial (PPSS) est la v�rification de la solution optimale de g�n�ration de l'�nergie �lectrique n�cessaire pour les charges du vaisseau spatial, pendant la lumi�re du jour de l'orbite, et �galement capable de charger la batterie (SPSS) avec la puissance requise pour les charges du vaisseau spatial, pendant la p�riode d'�clipse de l'orbite. Les impacts du rayonnement spatial et la variation de la temp�rature de fonctionnement de la cellule sont pris en compte. Il peut �tre compar� entre les diff�rentes cat�gories de cellules photovolta�ques.

Les informations fournies dans la section � Synopsis � peuvent faire r�f�rence � une autre �dition de ce titre.

�diteur: Noor Publishing
Date d'�dition: 2019
Langue: anglais
ISBN 10: 6200066280
ISBN 13: 9786200066282
Reliure: Broch�
Nombre de pages: 128
Coordonn�es du fabricant: non disponible
Personne responsable: non disponible

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Design of Solar Array Systems for Satellites

Kareem Morsy

Edit� par Noor Publishing Jul 2019, 2019

ISBN 10 : 6200066280 ISBN 13 : 9786200066282

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Vendeur : BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, Allemagne

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Taschenbuch. Etat : Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -Most 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. 128 pp. Englisch. N� de r�f. du vendeur 9786200066282

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Design of Solar Array Systems for Satellites : parametric analysis and Comparative Study of Solar arrays in Space

Kareem Morsy

Edit� par Noor Publishing, 2019

ISBN 10 : 6200066280 ISBN 13 : 9786200066282

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Taschenbuch. Etat : Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - Most 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. N� de r�f. du vendeur 9786200066282

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Design of Solar Array Systems for Satellites

Kareem Morsy

Edit� par Noor Publishing, 2019

ISBN 10 : 6200066280 ISBN 13 : 9786200066282

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Etat : New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. Autor/Autorin: Morsy KareemEngineer Kareem Ahmed Ahmed Morsy B. Sc. Electronics and Communications, Military Technical College, 2009- Master Degree in Electrical Engineering,In the Electronics and Communications Department, Faculty of Engineer. N� de r�f. du vendeur 385662162

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Design of Solar Array Systems for Satellites

Kareem Morsy

Edit� par Noor Publishing Jul 2019, 2019

ISBN 10 : 6200066280 ISBN 13 : 9786200066282

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Vendeur : buchversandmimpf2000, Emtmannsberg, BAYE, Allemagne

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Taschenbuch. Etat : Neu. This item is printed on demand - Print on Demand Titel. Neuware -Most 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.Books on Demand GmbH, �berseering 33, 22297 Hamburg 128 pp. Englisch. N� de r�f. du vendeur 9786200066282

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