Improving the Reliability of a CubeSat Power System by Combining Small-Sized Monocrystalline Cells With Triple-Junction Solar Cells

Electrical Power System (EPS) failures are well-known challenges for small satellites, particularly CubeSats. These failures can arise from various causes, including short circuits, solar cell degradation, battery malfunctions, and harness failures. Due to their limited power resources, any negative...

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Үндсэн зохиолчид:	Hari Ram Shrestha, Jose Rodrigo Cordova-Alarcon, Necmi Cihan Orger, Victor Hugo Schulz, Fahd Moumni, Takashi Yamauchi, Mengu Cho
Формат:	Artigo
Хэл сонгох:	Inglês
Хэвлэсэн:	IEEE 2026-01-01
Цуврал:	IEEE Access
Нөхцлүүд:	CubeSat <monospace xmlns:ali="http://www.niso.org/schemas/ali/1.0/" xmlns:mml="http://www.w3.org/1998/Math/MathML" xmlns:xlink="http://www.w3.org/1999/xlink" xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance">CURTIS</monospace> <monospace xmlns:ali="http://www.niso.org/schemas/ali/1.0/" xmlns:mml="http://www.w3.org/1998/Math/MathML" xmlns:xlink="http://www.w3.org/1999/xlink" xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance">MicroOrbiter-1</monospace> electrical power system small solar cells reliability
Онлайн хандалт:	https://ieeexplore.ieee.org/document/11395955/
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