Passive Temperature Stabilization System for MEMS Sensors Performance Maintenance

Author:

MIYATA Kikuko1,NAGANO Hosei2,HARA Susumu1

Affiliation:

1. Department of Aerospace Engineering, Nagoya University

2. Department of Mechanical System Engineering, Nagoya University

Publisher

Japan Society for Aeronautical and Space Sciences

Reference14 articles.

1. 1) SpaceWorks, 2019 Nano/Microsatellite Market Forecast, https://www.spaceworks.aero/wp-content/uploads/Nano-Microsatellite-Market-Forecast-9th-Edition-2019.pdf, 2019. (accessed Jan. 30, 2019).

2. 2) Shea, H. R.: MEMS for pico-to micro-satellites, Proc. SPIE, 7208, (2009), 72080M.

3. 3) Patel, C. and McCluskey, P.: Modeling and simulation of the MEMS vibratory gyroscope, 13th InterSociety Conference on Thermal and Thermomechanical Phenomena in Electronic Systems, San Diego, CA, 2012, pp. 928-933.

4. 4) Totani, T., Ogawa, H., Wakita, M., Nagata, H., Kuramoto, Y., and Miyashita, N.: Verification of Rapid Thermal Design Approach using Design and Flight Data of Hodoyoshi-1 Microsatellite, Proceeding of 46th International Conference on Environmental Systems, ICES-2016-116, 2016.

5. 5) Miyata, K., Kim, J., Aoyanagi, Y., Matsumoto, T., and Nakasuka, S.: Thermal Design and On-Orbit Data Evaluation of the 3U-class CubeSat TRICOM-1, Proceedings of the 62nd Space Sciences and Technology Conference, JSASS-2018-4608, 2018 (in Japanese).

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