[논문]CONCEPTUAL STRUCTURAL DESIGN AND COMPARATIVE POWER SYSTEM ANALYSIS OF OZONE DYNAMICS INVESTIGATION NANO-SATELLITE (ODIN)

Park, Nuri; Hwang, Euidong; Kim, Yeonju; Park, Yeongju; Kang, Deokhun; Kim, Jonghoon; Hong, Ik-seon; Jo, Gyeongbok; Song, Hosub; Min, Kyoung Wook; Yi, Yu

doi:10.5303/jkas.2021.54.1.9

[국내논문] CONCEPTUAL STRUCTURAL DESIGN AND COMPARATIVE POWER SYSTEM ANALYSIS OF OZONE DYNAMICS INVESTIGATION NANO-SATELLITE (ODIN) 원문보기

Journal of the Korean astronomical society = 천문학회지, v.54 no.1, 2021년, pp.9 - 16

Park, Nuri (Department of Astronomy and Space Science, Chungnam National University) , Hwang, Euidong (Department of Astronomy and Space Science, Chungnam National University) , Kim, Yeonju (Department of Astronomy and Space Science, Chungnam National University) , Park, Yeongju (Department of Astronomy and Space Science, Chungnam National University) , Kang, Deokhun (Department of Electrical Engineering, Chungnam National University) , Kim, Jonghoon (Department of Electrical Engineering, Chungnam National University) , Hong, Ik-seon (Department of Astronomy and Space Science, Chungnam National University) , Jo, Gyeongbok (Department of Astronomy and Space Science, Chungnam National University) , Song, Hosub (Department of Astronomy and Space Science, Chungnam National University) , Min, Kyoung Wook (Department of Physics, Korea Advanced Institute of Science and Technology) , Yi, Yu (Department of Astronomy and Space Science, Chungnam National University)

Abstract ▼ AI-Helper

The Ozone Dynamics Investigation Nano-Satellite (ODIN) is a CubeSat design proposed by Chungnam National University as contribution to the CubeSat Competition 2019 sponsored by the Korean Aerospace Research Institute (KARI). The main objectives of ODIN are (1) to observe the polar ozone column density (latitude range of 60° to 80° in both hemispheres) and (2) to investigate the chemical dynamics between stratospheric ozone and ozone depleting substances (ODSs) through spectroscopy of the terrestrial atmosphere. For the operation of ODIN, a highly efficient power system designed for the specific orbit is required. We present the conceptual structural design of ODIN and an analysis of power generation in a sun synchronous orbit (SSO) using two different configurations of 3U solar panels (a deployed model and a non-deployed model). The deployed solar panel model generates 189.7 W through one day which consists of 14 orbit cycles, while the non-deployed solar panel model generates 152.6 W. Both models generate enough power for ODIN and the calculation suggests that the deployed solar panel model can generate slightly more power than the non-deployed solar panel model in a single orbit cycle. We eventually selected the non-deployed solar panel model for our design because of its robustness against vibration during the launch sequence and the capability of stable power generation through a whole day cycle.

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표/그림 (18)

그림 Figure 1. Overall design of ODIN.
표 Table 1 Overall requirements of ODIN
표 Table 2 Compartments used in conceptual structural design
표 Table 3 Length of ODIN avionics bus components
표 Table 4 Mass budget of ODIN
표 Table 5 Instrument operation as function of flight mode
그림 Figure 2. Configuration of ODIN.
표 Table 6 Power margins for the deployed solar panel design in nadir observation mode
표 Table 7 Power margins for the non-deployed solar panel design in nadir observation mode
그림 Figure 3. Avionics bus system of ODIN.
그림 Figure 4. Structural frame of ODIN.
그림 Figure 5. Non-deployed solar panel model of ODIN.
그림 Figure 6. Deployed solar panel model of ODIN.
그림 Figure 7. Simulation of power generation in nadir observation mode for the deployed solar panel model.
그림 Figure 8. Simulation of power generation in Sun pointing mode (charging mode) for the deployed solar panel model.
그림 Figure 9. Simulation of power generation in nadir observation mode for the non-deployed solar panel model.
그림 Figure 10. Simulation of power generation in Sun pointing mode (charging mode) for the non-deployed solar panel model.
그림 Figure 11. Power budget table of ODIN.

참고문헌 (11)

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