...
首页> 外文期刊>Earth, planets and space: EPS >Japanese contribution to in-situ meteoroid and debris measurement in the near Earth space
【24h】

Japanese contribution to in-situ meteoroid and debris measurement in the near Earth space

机译:日本对近地空间流星体和碎片测量的贡献

获取原文
获取原文并翻译 | 示例
           

摘要

This paper reviews major results of present studies and recent developments for future missions in the Japanese space program regarding in-situ measurement and collection of micrometeoroids and orbital debris in the near Earth space. Japan's contribution in this area began with the post flight impact analysis of the Space Flyer Unit (SFU) satellite which was returned to Earth in 1996 after 10-month exposure in space. Despite a decade later than similar efforts first conducted in the USA and Europe, it resulted in a record of over 700 hypervelocity impact signatures, which now forms the nation's first database of real space impacts being open to public in the Internet. Together with laboratory impact tests, both morphological and elemental analyses of the impact craters yielded new insights of the meteoroid to debris ratio as well as flux variation compared with the previous spacecraft. The next step was a passive aerogel exposure in the STS-85 shuttle mission in 1997. No hypervelocity impact was found there but its experience has been incorporated for designing a microparticle collector to be on-board the Japan Experiment Module-Exposed Facility of the International Space Station. All of such "passive" collection of micro-impact features, however, still leave the significant uncertainty in the quest of their origins. Therefore an aerogel-based "hybrid" dust collector and detector (HD-CAD) is currently under the development. It measures time of impact and deduces impactors' orbital and physical parameters by detecting impact flash while still capturing them intact. The system is suitable for both (1) sample return missions in LEO as well as to parent bodies of meteoroids, i.e., comets and asteroids, and (2) one-way mission to where the thermal and plasma environment is such that impact induced plasma detectors may suffer from significant noise, e.g., a Mercury orbiter and a solar probe. Together with unambiguous dust samples from a comet by STARDUST and an asteroid by MUSES-C as references, the HD-CAD in the LEO will be able to deduce the accretion rates of the cometary and asteroidal dust grains on the Earth.
机译:本文回顾了当前研究的主要成果以及日本太空计划中有关近地空间中微流星体和轨道碎片的现场测量和收集的未来飞行任务的最新进展。日本在这一领域的贡献始于对太空飞行器(SFU)卫星的飞行后影响分析,该卫星在太空中暴露了10个月后于1996年返回地球。尽管比在美国和欧洲首次进行类似的努力晚了十年,但它还是创造了700多个超高速撞击特征的记录,现已成为美国第一个在互联网上向公众开放的真实空间撞击数据库。与实验室撞击测试一起,对撞击坑的形态和元素分析都产生了与以前的航天器相比流星体与碎片比以及通量变化的新见解。下一步是在1997年的STS-85航天飞机任务中被动暴露气凝胶。在那里没有发现超高速影响,但其经验已被用于设计微粒收集器,该微粒收集器将用于国际实验的日本实验组件暴露设施。空间站。然而,所有这些“被动”的微冲击特征的集合,在寻找其起源方面仍然存在很大的不确定性。因此,目前正在开发基于气凝胶的“混合”集尘器和检测器(HD-CAD)。它可以测量撞击时间并通过检测撞击闪光来推断撞击者的轨道和物理参数,同时仍将其完整捕获。该系统既适用于(1)LEO中的样品返回任务,也适用于流星体的母体(即彗星和小行星),以及(2)单向任务,用于热和等离子环境导致撞击诱发的等离子体探测器可能遭受很大的噪音,例如水星轨道器和太阳探测器。加上来自STARDUST彗星的明确尘埃样本和MUSES-C的小行星的尘埃样本作为参考,LEO中的HD-CAD将能够推断出地球上的彗星和小行星尘埃颗粒的积聚率。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号