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SYSTEM DESIGN OF HAYABUSA2 –ASTEROID SAMPLE RETURN MISSION TO 1999JU3

机译:HAYABUSA2 – 1999JU3类星型样品返回系统的系统设计

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The Japan Aerospace Exploration Agency is now developing the second asteroid sample return mission"Hayabusa2." Following the successful return back of Hayabusa from the asteroid Itokawa, Hayabusa2 aims at around trip mission to the asteroid 1999JU3.1999JU3 is a C-type asteroid, which is supposed to contain organicmatters and hydrated minerals. Thus it is expected that, after the successful sample collection, we could acquire moreknowledge on the origin and evolution of the planets, especially the origin of water and organic matters. The currentmission scenario enables the spacecraft to reach 1999JU3 in the middle of 2018, and performs an asteroid proximityoperation for 1.5 years. Three touch downs for sampling and one 2m class-crater generation by a high-speed impactoperation are planned during the asteroid proximity operation. The sample is to be brought back to the Earth by there-entry capsule. This paper describes the system design of Hayabusa2, some key technical challenges of the missionand the development status.
机译:日本宇航局目前正在开展第二次小行星样本返回任务 “ Hayabusa2。”继Hay鸟号成功从小行星丝川号返回后,ab鸟号2的目标是 小行星的往返飞行任务1999JU3.1999JU3是C型小行星,应该包含有机物 物质和水合矿物质。因此,可以预期的是,在成功收集样本之后,我们可以获得更多 有关行星起源和演化的知识,尤其是水和有机物质的起源。目前 任务情景使航天器能够在2018年中期达到1999JU3,并执行小行星近距离飞行 运行1。5年。 3次降落进行采样,高速撞击产生2m级陨石坑 计划在小行星近距离操作中进行操作。样品将被带回地球。 重新进入胶囊。本文介绍了Hayabusa2的系统设计,任务的一些关键技术挑战 以及发展状况。

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