Space Environment Evaluation Test of Solid-State-Ceramic Battery Advanced Energy Storage Under Vacuum and Thermal Vacuum
The desired capabilities of small satellites to enable their applications in communication, earth observation, and new scientific instruments require advanced energy storage to face the design’s challenges with the constraints of volume and mass. Small batteries with high energy density may be the solution. New lithium-ion battery technologies areimproved in order to meet these requirements by bringing higher energy density and a wide temperature range than the commercially available ones as well as a lower risk of explosion. In this paper, the ability of solid-state-ceramic batteries to withstand the vacuum and thermal vacuum for low earth orbit applications has been demonstrated, with a minimum safety issue. So far, this technology has never been flown in space. This paper also provides a guideline for the battery evaluation test where the main lines are represented. Batteries are tested under vacuum and thermal vacuum, where they are discharged and charged during several cycles between two temperatures limits. The evaluation focuses on analyzing the physical degradation, the discharge capacity, and the internal resistance before and after each test. Batteries have showed promising results regarding their survivability to thermal vacuum. After several cycles, they have kept almost the same performances, with the same internal resistance and 98% of capacity.
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M. Langer and J. Boumeester, Reliability of CubeSats – Statistical Data, Developers’ Beliefs and the Way Forward, 30th Annual. AIAA/USU Conference of Small Satellite, Logan, UT, paper ID: SSC16-X-2, pp. 1–12, August 2016.
“Nanosatellite & CubeSat Database,” http://www.nanosats.eu, 2020.
J. Gonzalez-Llorente, D. Rodriguez-Duarte, S. Sanchez-Sanjuan, and A. Rambal-Vecino, Improving the efficiency of 3U CubeSat EPS by selecting operating conditions for power converters, 2015 IEEE Aerospace Conference, vol. 2015-June. March, 2015.
I. Vertat and A. Vobornik, Efficient and reliable solar panels for small CubeSat picosatellites, International Journal of Photoenergy, vol. 2014, pp. 8, 2014.
S. A. Ibrahim and E. Yamaguchi, Comparison of Solar Radiation Torque and Power Generation of Deployable Solar Panel Configurations on Nanosatellites, Journal of Aerospace (MDPI), vol. 6, no. 5, pp. 50, 2019.
G. A. Landis, Tabulation of power-related satellite failure causes, 11th International Energy Conversion Engineering Conference, July 2013.
M. Smart, J. Castillo, and T. Yi, NASA’s Technical Report, Energy Storage Technologies for Future Planetary Science Missions, issue December, pages 65, 2017.
M. Alkali, M. Y. Edries, and A. R. Khan, Design Considerations and Ground Testing of Electric Double-Layer Capacitors as Energy Storage Components for Nanosatellites, Journal of Small Satellites, vol. 4, no. 2, pp. 387–405, 2015.
K. C. Chin, N. W. Green, and E. J. Brandon, Evaluation of supercapacitors for space applications under thermal vacuum conditions, Journal of Power Sources (Elsevier), vol. 379, pp. 155-159, 2018.
I. Fajardo et al., Design, Implementation, and Operation of a Small Satellite Mission To Explore the Space Weather Effects in Leo, Journal of Aerospace (MDPI), vol. 6, n. 10, pp. 108, 2019.
J. Gonzalez-Llorente, A. A. Lidtke, K. Hatanaka, R. Kawauchi, and K.-I. Okuyama, Solar Module Integrated Converters as Power Generator in Small Spacecrafts: Design and Verification Approach, Journal of Aerospace (MDPI), vol. 6, no. 5, pp. 61, 2019.
Bendoukha, S., Tapia, I., Okuyama, K., Cho, M., An Experimental and Theoretical Study of Spatial Langmuir Probe Plasma System for a Small Lean Satellite Called Ten-Koh, (2019) International Review of Aerospace Engineering (IREASE), 12 (3), pp. 131-140.
M. Nestoridi and H. Barde, Beyond Lithium-Ion: Lithium- Sulphur Batteries for Space?, E3S Web Conference, vol. 16, no. 1, pp. 2-6, 2017.
K. Takada, Progress in solid electrolytes toward realizing solid-state lithium batteries, Journal of Power Sources (Elsevier), vol. 394, pp. 74-85, 2018.
J. W. Fergus, Ceramic and polymeric solid electrolytes for lithium-ion batteries, Journal Power Sources (Elsevier), vol. 195, no. 15, pp. 4554-4569, 2010.
Li, X., Koseki, H., Thermal Analysis on Lithium Primary Batteries, (2014) International Journal on Energy Conversion (IRECON), 2 (4), pp. 133-136.
Dongxu Ouyang, Mingyi Chen, Jian Wang, Que Huang, Jingwen Weng, Zhi Wang, Jian Wang, A Review on the Thermal Hazards of the Lithium-Ion Battery and the Corresponding Countermeasures, Journal of Applied Sciences (MDPI), vol. 9, no. 12, pp. 2483, 2019.
X. Wang, Y. Sone, and S. Kuwajima, Effect of operation conditions on simulated low-earth orbit cycle-life testing of commercial lithium-ion polymer cells, Journal of Power Sources (Elsevier), vol. 142, no. 1-2, pp. 313-322, 2005.
C. S. Clark and E. Simon, Evaluation of Lithium Polymer Technology for Small Satellite Applications, 21st Annual. AIAA/USU Conference of Small Satellite, paper ID: SSC07-X-9,August, pp. 1–11, 2007.
N. Navarathinam, R. Lee, and H. Chesser, Characterization of Lithium-Polymer batteries for CubeSat applications, Journal Acta Astronautical (Elsevier), vol. 68, no. 11-12, pp. 1752-1760, 2011.
J. Claricoats, S.M. Dakka, Design of Power, Propulsion, and Thermal Sub-Systems for a 3U CubeSat Measuring Earth’s Radiation Imbalance, Journal of Aerospace (MDPI), Vol. 5, n. 2, pp. 63, 2018.
G. Kissel, R. Loehrlein, N. Kalsch, W. Helms, Z. Snyder, S. Kaphle, UNITE CubeSat: From Inception to Early Orbital Operations, Small Satellite Conference, Utah State University, Logan, UT, article ID SSC19-WKI-08, 2019.
Scott Higginbotham, MissidAManager, NASA KSC VA — C,FCC’s report, Orbital Debris Assessment for The CubeSats on the CRS OA—10/ELaNa—21 Mission, 2018.
Burt Robert, Distributed Electrical Power Systems in Cubesat Application, Master’s Thesis, Master of Science in Electrical engineering, Utah State University, Logan, UT, USA, December 2011.
J. Oyola Alvarado, J. Rodríguez Mora, Designs and Implementations for CubeSat Colombia 1 Satellite Power Module, International Journal of Applied Engineering Research, vol. 12, n. 18 , pp. 7360–7371, 2017.
A.Y. Yu Miao, Patrick Hynan, Annette von Jouanne, Current Li-Ion Battery Technologies in Electric Vehicles and Opportunities for Advancements, Journal of Energies (MDPI), vol. 12, n. 6, pp. 1074, 2019.
Ewang, E., Miyahara, A., Khan, A., Toyoda, K., Cho, M., Photoelectron Current Measurement in Low Earth Orbit Using a Lean Satellite, HORYU-IV, (2017) International Review of Aerospace Engineering (IREASE), 10 (3), pp. 140-153.
JAXA, JAXA’ Technical Standars, Spacecraft general test standard Handbook JERG-2-130-HB007A, Tokyo, 2017
G. Pistoia, Lithium-Ion Batteries: Advances and Applications, First edit, Elsevier B.V, pp. 664, 2014.
Samuel Russell, David Delafuente, Eric Darcy, Karla Bradley, Edgar O. Castro, and Lauri Hansen, NASA’s Technical Standars. Crewed Space Vehicle Battery Safety Requirements, Houston, Texas, pp. 124, 2017.
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