VERTECS: thermal modeling and analysis to enhance mission efficiency through temperature control strategies of a 6U CubeSat with visible light telescope
This study focuses on optimizing the thermal performance of the Visible Extragalactic background RadiaTion Exploration by CubeSat (VERTECS), a 6U CubeSat with a 3U telescope for observing Extragalactic Background Light. Aside from dealing with satellite survivability in the space environment, the payload includes a CMOS sensor which requires operational temperatures of less than 0°C to minimize the noise due to temperature dependent dark current in observation data. The payload telescope lens optical system is designed to operate within a temperature range of -10°C to 35°C. The thermal analysis considers solar radiation, internal heat dissipation, and external factors in various orbital scenarios. The investigation identifies potential temperature fluctuations and proposes passive thermal control strategies, including enhanced coatings and radiators. By implementing tailored strategies, this research enhances the reliability and longevity of 6U CubeSat missions, advancing small satellite technology in space exploration and scientific research.
Authors
- Kei Sano (ORCID: https://orcid.org/0000-0002-6468-8532)
- Hirokazu Masui (ORCID: https://orcid.org/0000-0001-8596-6119)
- Mengu Cho (ORCID: https://orcid.org/0000-0001-6024-2667)
- Marco Rosa (ORCID: https://orcid.org/0000-0002-4591-8216)
- Shuji Matsuura (ORCID: https://orcid.org/0000-0002-5698-9634)
- Keenan Chatar (ORCID: https://orcid.org/0000-0002-1542-4362)
- Yuki Hirose (ORCID: https://orcid.org/0000-0001-6879-7886)
- Takao Nakagawa (ORCID: https://orcid.org/0000-0002-6660-9375)
- Shohei Karaki
- Ezra Fielding
- Hisataka Kawasaki
- Reynel Josué Galindo Rosales
Institutions
- Kwansei Gakuin University (JP)
- Kyushu Institute of Technology (JP)
- Institute of Space and Astronautical Science (JP)
Publication Details
- Published
- 2024-08-23
- DOI
- https://doi.org/10.1117/12.3018823
- Citations
- 1
- Primary Topic
- Spacecraft Design and Technology
- Type
- article
- Field-Weighted Citation Impact
- 1.30