日本地球惑星科学連合2021年大会

講演情報

[E] 口頭発表

セッション記号 P (宇宙惑星科学) » P-CG 宇宙惑星科学複合領域・一般

[P-CG17] 宇宙・惑星探査の将来計画および関連する機器開発の展望

2021年6月4日(金) 10:45 〜 12:15 Ch.02 (Zoom会場02)

コンビーナ:小川 和律(宇宙航空研究開発機構)、尾崎 光紀(金沢大学理工研究域電子情報学系)、坂谷 尚哉(立教大学 理学部 物理学科)、吉岡 和夫(東京大学大学院新領域創成科学研究科)、座長:小川 和律(宇宙航空研究開発機構)、坂谷 尚哉(立教大学 理学部 物理学科)

10:45 〜 11:00

[PCG17-09] Microsatellite development and Eduaction of Space Science and Technology at Kanazawa University

*井町 智彦1、八木谷 聡1、米徳 大輔1、笠原 禎也1、澤野 達哉1、有本 誠1、尾崎 光紀1、藤本 龍一1 (1.金沢大学)

キーワード:超小型衛星、重力波、金沢、先端宇宙理工学研究センター

At Kanazawa University, a microsatellite is being developed. This satellite is selected to be an onboard satellite for JAXA's "Innovative Satellite Technology Demonstration-3" project and planned to be launched by Epsilon rocket in 2022.
The satellite is developed as an activity of ARC-SAT (Advanced Research Center for Space Science and Technology) and Kanazawa-SAT3 (Study and Training in Space Science and Technology for Kanazawa Cube-Satellites) project. ARC-SAT is a research center of Kanazawa University, established on July 1, 2019. ARC-SAT has 3 research divisions: Satellite Development Division, Astronomy & Astrophysics Division and Solar-Terrestrial Science Division. And ARC-SAT is concluding "Kanazawa University Satellite Project (Kanazawa-SAT3)". In this project, a space science and engineering course has been established in the Graduate School of Natural Sciences in April 2018. This course is based on the 'satellite development by students', and students are actually involved in the design, fabrication, ground tests, and operation of scientific satellites, aiming to train personnel who are familiar with space science and space engineering, with satellite-development skills.
The satellite being developed in Kanazawa University is a scientific satellite which will contribute to the elucidation of the mechanism of gravitational wave generation by identifying the source of gravitational wave by detecting the arrival direction of gamma rays and X rays radiated at the same time when gravitational waves are generated by collision of astronomical objects. It is a microsatellite with a total weight of 50 kg or less, and its size is cubic with a side of 50 cm, and will be inserted into a solar synchronous orbit at about 500 or 560 km altitude. The satellite is on the stage of flight model assembly. And for the ground station, we have installed a parabolic antenna (2.4 m is diameter) and a crossed Yagi antenna (14 elements) in Kanazawa university.
In the presentation, we will report the details of ARC-SAT and Kanazawa-SAT3 project, and the development status of our satellite.