Design of the Electrical Power System for the ESTCube-1 Satellite

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Design of the Electrical Power System for the ESTCube-1 Satellite

In this work, the design of the electrical power system developed for ESTCube-1 - the first Estonian satellite with the first test mission of electric solar wind sail - is presented. The mission is highly energy-intensive, and, since its complexity might lead to many possible failure cases, it requires a very efficient and fault-tolerant solution. The system has been developed from ground up, using only commercial-off-the-shelf components and student workforce. It includes several innovations, which help the system to be more reliable, efficient and controllable than earlier nanosatellite power system designs.

Woellert, K., Ehrenfreund, P., Ricco, A. J., & Hertzfeld, H. (2011). Cubesats: Cost-effective science and technology platforms for emerging and developing nations. Advances in Space Research, 47 (4), 663-684, DOI: 10.1016/j.asr.2010.10.009.

Pukniel, A., Coverstone, V., Burton, R., & Carroll, D. (2011). The dynamics and control of the CubeSail mission: A solar sailing demonstration. Advances in Space Research, 48 (11), 1902-1910, DOI: 10.1016/j.asr.2011.07.014.

Lappas, V., Adeli, N., Visagie, L., Fernandez, J., Theodorou, T., Steyn, W., et al. (2011). CubeSail: A low cost CubeSat based solar sail demonstration mission. Advances in Space Research, 48 (11), 1890-1901, DOI: 10.1016/j.asr.2011.05.033.

Nasila, A., Hakkarainen, A., Praks, J., Kestila, A., Nordling, K., Modrzewski, R., et al. (2011). Aalto-1: a hyperspectral Earth observing nanosatellite. In Sensors, Systems, and Next-Generation Satellites XV 19-22 September 2011, (pp. 81760C), Prague, Czech Republic.

Ashida, H., Fujihashi, K., Inagawa, S., Miura, Y., Omagari, K., Miyashita, N., et al. (2010). Design of Tokyo Tech nano-satellite Cute-1.7+APD II and its operation. Acta Astronautica, 66 (9-10), 1412-1424, 10.1016/j.actaastro.2009.10.035.

Santoni, F., Piergentili, F., & Graziani, F. (2010). Broglio Drag Balance for neutral thermosphere density measurement on UNICubeSAT. Advances in Space Research, 45 (5), 651-660, 10.1016/j.asr.2009.10.001.

Janhunen, P. (2004). Electric sail for spacecraft propulsion AIAA Journal of Propulsion and Power, 20 (4), 763-764.

Janhunen, P., Toivanen, P. K., Polkko, J., Merikallio, S., Salminen, P., Haeggstrom, E., et al. (2010). Electric solar wind sail: Toward test missions. Review of Scientific Instruments, 81 (11), 111301.

Girish, T. E., Aranya, S., & Nisha, N. G. (2007). Photovoltaic power generation using albedo and thermal radiations in the satellite orbits around planetary bodies. Solar Energy Materials and Solar Cells, 91 (15-16), 1503-1504. DOI: 10.1016/j.solmat.2007.03.013.

Esram, T., & Chapman, P. L. (2007). Comparison of Photovoltaic Array Maximum Power Point Tracking Techniques. IEEE Transactions on Energy Conversion, 22 (2), 439-449. DOI: 10.1109/TEC.2006.874230.

Avery, K., Finchel, J., Mee, J., Kemp, W., Netzer, R., Elkins, D., et al. (2011). Total Dose Test Results for CubeSat Electronics. In Radiation Effects Data Workshop (REDW), 2011 IEEE, 25-29 July 2011 (pp. 1-8), Las Vegas, Nevada, USA.

Stras, L. N., Kekez, D. D., Wells, G. J., Jeans, T., Zee, R. E., Pranajaya, F. M., et al. (2003). The design and operation of the Canadian advanced nanospace eXperiment (CanX-1). In Proceedings of the AMSAT-NA 21st Space Symposium, October 2003 (pp. 150-160), Toronto, Canada.

Philofsky, E. M. (1996). FRAM-the ultimate memory. In Nonvolatile Memory Technology Conference, 1996., Sixth Biennial IEEE International, 24-26 Jun 1996 (pp. 99-104).

Latvian Journal of Physics and Technical Sciences

The Journal of Institute of Physical Energetics

Journal Information

CiteScore 2017: 0.46

SCImago Journal Rank (SJR) 2017: 0.226
Source Normalized Impact per Paper (SNIP) 2017: 0.653

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