小行星
离子推进器
天体生物学
航天器
航空航天工程
航空学
环境科学
工程类
物理
作者
S Hosoda,Kazutaka Nishiyama,Ryudo Tsukizaki
出处
期刊:Elsevier eBooks
[Elsevier]
日期:2022-01-01
卷期号:: 401-414
被引量:2
标识
DOI:10.1016/b978-0-323-99731-7.00020-9
摘要
Japan's second asteroid explorer Hayabusa2 successfully returned from asteroid 162173 Ryugu to Earth on December 6, 2020, with the asteroid samples. Four xenon ion thrusters based on electron cyclotron resonance discharge propelled the spacecraft for 9514 h during the round-trip journey between Earth and Ryugu asteroid. Ion engine system of Hayabusa2 was designed based on the Hayabusa ion engine system with minor improvement for the thrust performance and durability. Hayabusa2 ion engine system met no serious trouble during the round-trip journey, but some unexpected performance degradations due to carbon contamination. We summarize the operations of Hayabusa2 ion engine system.
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