MarCO: Interplanetary Mission Development on a CubeSat Scale
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The two MarCO CubeSats had Li-ion batteries kept within 273 to 303 K during all mission phases.
“The two MarCO CubeSats had Li-ion batteries kept within 273 to 303 K during all mission phases.”
From An Integrated Thermal-Electrical Model for Simulations of Battery Behavior in CubeSats (2021) · cites this paper as [10]
Cites
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“Heaters attached to the battery were used to sustain the temperature, and passive materials were employed to allow heat exchanging with other satellite parts [10,11].”
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- Authors
- Schoolcraft, J., Klesh, A., & Werne, T.
- Affiliations
- Jet Propulsion Laboratory (US)
- Corresponding author
- Schoolcraft, Josh
- ORCID
- Klesh, Andrew
- Venue
- Space Operations: Contributions from the Global Community
- Publisher
- Springer International Publishing
- Published
- 2017
- Pages
- 221-231
- OpenAlex
- W2369012463
- Cited by
- 80
- References
- 3
- Citations by year
- 2026: 2 · 2025: 7 · 2024: 6 · 2023: 7 · 2022: 8 · 2021: 18 · 2020: 13 · 2019: 9 · 2018: 7 · 2017: 3
- FWCI
- 28.43
- Type
- book chapter
- Language
- en
- Open access
- closed
- Locations
- Springer eBooks (publishedVersion)
- Topics
- Physical Sciences › Engineering › Aerospace Engineering › Spacecraft Design and Technology
- Physical Sciences › Physics and Astronomy › Astronomy and Astrophysics › Planetary Science and Exploration
- Physical Sciences › Engineering › Electrical and Electronic Engineering › Space Technology and Applications
- Keywords
- MARCO, CubeSat, InSight mission, Deep Space Network, Mars entry, descent and landing
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