• 研究課題をさがす
  • 研究者をさがす
  • KAKENの使い方
  1. 課題ページに戻る

2022 年度 実績報告書

宇宙機の帯電シミュレーションで明らかにする彗星プラズマの真の姿

研究課題

研究課題/領域番号 22F22723
配分区分補助金
研究機関東京大学

研究代表者

笠原 慧  東京大学, 大学院理学系研究科(理学部), 准教授 (00550500)

研究分担者 BERGMAN SOFIA  東京大学, 理学(系)研究科(研究院), 外国人特別研究員
研究期間 (年度) 2022-11-16 – 2024-03-31
キーワードCometary plasma / spacecraft charging
研究実績の概要

In 2019, Comet Interceptor was selected by ESA as the first F-class mission. This mission will make a flyby of a long-period comet and for the first time make multi point measurements in the cometary environment using three spacecraft: Spacecraft A (ESA), Probe B1 (JAXA) and Probe B2 (ESA). All spacecraft will carry plasma instruments, allowing, for the first time, a threedimensional study of the cometary plasma environment. The plasma measurements are, however, expected to be affected by the spacecraft potential, as already observed by other cometary missions (e.g. the Rosetta mission, Bergman et al., 2020). Throughout the flyby, the spacecraft will pass by several plasma regions with different characteristics, and hence the spacecraft potential is expected to vary. In this study, we estimated the spacecraft potential of Probe B1 of Comet Interceptor throughout the cometary flyby using Particle-In-Cell (PIC) simulations and study the influence on the plasma measurements. The main results are as follows:
(1) At a low relative flyby velocity, a more effective cooling of the electrons in the inner coma results in less negative spacecraft potentials for a Halley-type comet.
(2) Secondary electron emissions from neutral impacts charge the spacecraft positive in most environments at a high relative flyby velocity.

現在までの達成度 (区分)
現在までの達成度 (区分)

2: おおむね順調に進展している

理由

The original plan is as follows:
November-December: Development of a spacecraft model to be used in the spacecraft Plasma Interaction Software (SPIS). A model of the ion sensor will be implemented in the model which will subsequently be used to trace low-energy ions in the simulations. The information about spacecraft B1 and the sensor needed to develop the model is available at the host institute in Japan, and an extended stay is hence necessary to carry out the proposed research.
January-March: Simulation running. The spacecraft model will be implemented in SPIS. A suitable model for the plasma environment around the spacecraft will be chosen based on available data and publications from previous comet missions (e.g., the Rosetta mission, the Giotto mission, and the Japanese Suisei/Sakigake missions).
We have successfully completed these items and have already got preliminary results.

今後の研究の推進方策

2022年度までに,複数の彗星環境中で探査機の帯電シミュレーションを実施し,結果を議論している.2023年度は,以下のような研究を実施予定である.

・これまで太陽電池パドルの表面を導体としていたが,探査機の設計進捗に伴い,コスト・スケジュールの制約から,表面に高抵抗部材・絶縁物が残る可能性が出てきた.このため,パドル表面を絶縁物とした場合のシミュレーションを実施し,帯電量を評価する.

・得られた電位分布に対して観測対象であるイオンの粒子軌道トレースを実施し,観測への影響を評価する.

  • 研究成果

    (1件)

すべて 2023

すべて 学会発表 (1件)

  • [学会発表] Estimating the spacecraft potential of Comet Interceptor - simulation results and implications for plasma measurements2023

    • 著者名/発表者名
      S. Bergman, S. Kasahara, Y. Miyake, F. L. Johansson
    • 学会等名
      Symposium on Planetary Sciences

URL: 

公開日: 2023-12-25  

サービス概要 検索マニュアル よくある質問 お知らせ 利用規程 科研費による研究の帰属

Powered by NII kakenhi