Spacecraft power systems
Abstract
The power systems of space vehicles have undergone significant development during the previous decade, and will continue to do so in the immediate future. Until now, except for the scattered results of conferences and a few publications with sketchy coverage, no single volume has covered the entire spectrum of the subject. Spacecraft Power
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MPPT architectures demand at a minimum 4-7% of the solar array nominal output power to operate.
“MPPT architectures demand at a minimum one dedicated dc-dc converter in series with the PV array to drive the PV cell operating voltage and it demands at a minimum 4-7% of the solar array nominal output power to operate [36].”
From A Comprehensive Review on Small Satellite Microgrids (2022) · cites this paper as [36]
DET architectures are mostly encountered in applications with power budgets less than 100W.
“DET architectures are mostly encountered in applications with power budgets less than 100W [36].”
From A Comprehensive Review on Small Satellite Microgrids (2022) · cites this paper as [36]
MPPT architectures demand at a minimum one dedicated dc-dc converter in series with the PV array to drive the PV cell operating voltage.
“MPPT architectures demand at a minimum one dedicated dc-dc converter in series with the PV array to drive the PV cell operating voltage and it demands at a minimum 4-7% of the solar array nominal output power to operate [36].”
From A Comprehensive Review on Small Satellite Microgrids (2022) · cites this paper as [36]
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Sorted by citations
Jin, G., Matthews, D. E., & Zhou, Z. (2013) · Reliability Engineering & System Safety · doi:10.1016/j.ress.2012.12.011 · Cited by 163 · see citing works
A Comprehensive Review on Small Satellite Microgrids
Yaqoob, M., Lashab, A., Vasquez, J. C., Guerrero, J. M., Orchard, M. E., & Bintoudi, A. D. (2022) · IEEE Transactions on Power Electronics · doi:10.1109/tpel.2022.3175093 · Cited by 93 · see citing works
“DET architectures are mostly encountered in applications with power budgets less than 100 W [36].”
BackgroundSpacecraft Electrical Power System using Lithium-Ion Capacitors
Uno, M., & Tanaka, K. (2013) · IEEE Transactions on Aerospace and Electronic Systems · doi:10.1109/taes.2013.6404097 · Cited by 39 · see citing works
Kerrouche, K. D. E., Seddjar, A., Khorchef, N., Bendoukha, S. A., Wang, L., & Aoudeche, A. (2022) · Automatika · doi:10.1080/00051144.2022.2065420 · Cited by 21 · see citing works
Hybrid AC/DC Power Distribution Solution for Future Space Applications
Barave, S. P., & Chowdhury, B. H. (2007) · 2007 IEEE Power Engineering Society General Meeting · doi:10.1109/pes.2007.385901 · Cited by 11 · see citing works
- Authors
- Patel, M. R.
- Corresponding author
- Patel, Mukund R.
- ORCID
- Patel, Mukund R.
- Venue
- CRC Press eBooks
- Publisher
- CRC Press
- Published
- 2004-11-29
- OpenAlex
- W411548222
- Cited by
- 292
- References
- 0
- Citations by year
- 2026: 4 · 2025: 13 · 2024: 16 · 2023: 19 · 2022: 32 · 2021: 19 · 2020: 28 · 2019: 14 · 2018: 19 · 2017: 13 · 2016: 16 · 2015: 9 · 2014: 10 · 2013: 16 · 2012: 11
- FWCI
- 5.87
- Type
- book
- Language
- en
- Open access
- closed
- Locations
- CRC Press eBooks (publishedVersion)
- Topics
- Physical Sciences › Engineering › Aerospace Engineering › Spacecraft Design and Technology
- Physical Sciences › Energy › Renewable Energy, Sustainability and the Environment › Photovoltaic System Optimization Techniques
- Physical Sciences › Engineering › Automotive Engineering › Advanced Battery Technologies Research
- Keywords
- space power systems, spacecraft, electricity generation, power distribution, solar cells, batteries, fuel cells
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