Design of Solar Array Systems for Satellites
Kareem Ahmed Ahmed Morsy;
Abstract
Abstract
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).
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).
Other data
| Title | Design of Solar Array Systems for Satellites | Other Titles | تصميم أنظمة الخلايا الشمسية للأقمار الصناعية | Authors | Kareem Ahmed Ahmed Morsy | Issue Date | 2018 |
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