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Lunar Reconnaissance Orbiter (LRO): Observations for Lunar Exploration and Science

机译:月球侦察轨道器(LRO):月球探索和科学观测

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The Lunar Reconnaissance Orbiter (LRO) was implemented to facilitate scientific and engineering-driven mapping of the lunar surface at new spatial scales and with new remote sensing methods, identify safe landing sites, search for in situ resources, and measure the space radiation environment. After its successful launch on June 18, 2009, the LRO spacecraft and instruments were activated and calibrated in an eccentric polar lunar orbit until September 15, when LRO was moved to a circular polar orbit with a mean altitude of 50 km. LRO will operate for at least one year to support the goals of NASA’s Exploration Systems Mission Directorate (ESMD), and for at least two years of extended operations for additional lunar science measurements supported by NASA’s Science Mission Directorate (SMD). LRO carries six instruments with associated science and exploration investigations, and a telecommunications/radar technology demonstration. The LRO instruments are: Cosmic Ray Telescope for the Effects of Radiation (CRaTER), Diviner Lunar Radiometer Experiment (DLRE), Lyman-Alpha Mapping Project (LAMP), Lunar Exploration Neutron Detector (LEND), Lunar Orbiter Laser Altimeter (LOLA), and Lunar Reconnaissance Orbiter Camera (LROC). The technology demonstration is a compact, dual-frequency, hybrid polarity synthetic aperture radar instrument (Mini-RF). LRO observations also support the Lunar Crater Observation and Sensing Satellite (LCROSS), the lunar impact mission that was co-manifested with LRO on the Atlas V (401) launch vehicle. This paper describes the LRO objectives and measurements that support exploration of the Moon and that address the science objectives outlined by the National Academy of Science’s report on the Scientific Context for Exploration of the Moon (SCEM). We also describe data accessibility by the science and exploration community.
机译:实施“月球侦察轨道器”(LRO)是为了以新的空间尺度和新的遥感方法促进科学和工程驱动的月球表面制图,确定安全着陆点,寻找原地资源,并测量空间辐射环境。在2009年6月18日成功发射之后,LRO航天器和仪器在偏心极地月球轨道上被激活和校准,直到9月15日,LRO被移动到平均高度为50 km的圆极轨道。 LRO将至少运行一年以支持NASA探测系统任务局(ESMD)的目标,并至少延长两年的运行时间,以便获得NASA科学任务局(SMD)支持的其他月球测量。 LRO携带六种仪器,并进行相关的科学和勘探研究,并进行电信/雷达技术演示。 LRO仪器包括:辐射影响的宇宙射线望远镜(CRaTER),Diviner月球辐射计实验(DLRE),Lyman-Alpha制图项目(LAMP),月球探测中子探测器(LEND),月球轨道激光高度计(LOLA),和月球侦察轨道相机(LROC)。该技术演示是一种紧凑的双频混合极性合成孔径雷达仪器(Mini-RF)。 LRO观测还支持月球环形山观测和感知卫星(LCROSS),该月球撞击任务是与LRO在Atlas V(401)运载火箭上共同表现出来的。本文介绍了支持月球探索的LRO目标和测量结果,并解决了美国国家科学院关于月球探索的科学背景(SCEM)报告中概述的科学目标。我们还将描述科学和探索界的数据可访问性。

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