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High precision astrometry mission for the detection and characterization of nearby habitable planetary systems with the Nearby Earth Astrometric Telescope (NEAT)

机译:使用邻近地球天体测量望远镜(NEaT)探测和表征附近可居住行星系统的高精度天体测量任务

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摘要

A complete census of planetary systems around a volume-limited sample of solar-type stars (FGK dwarfs) in the Solar neighborhood (d a parts per thousand currency signaEuro parts per thousand 15 pc) with uniform sensitivity down to Earth-mass planets within their Habitable Zones out to several AUs would be a major milestone in extrasolar planets astrophysics. This fundamental goal can be achieved with a mission concept such as NEAT-the Nearby Earth Astrometric Telescope. NEAT is designed to carry out space-borne extremely-high-precision astrometric measurements at the 0.05 mu as (1 sigma) accuracy level, sufficient to detect dynamical effects due to orbiting planets of mass even lower than Earth's around the nearest stars. Such a survey mission would provide the actual planetary masses and the full orbital geometry for all the components of the detected planetary systems down to the Earth-mass limit. The NEAT performance limits can be achieved by carrying out differential astrometry between the targets and a set of suitable reference stars in the field. The NEAT instrument design consists of an off-axis parabola single-mirror telescope (D = 1 m), a detector with a large field of view located 40 m away from the telescope and made of 8 small movable CCDs located around a fixed central CCD, and an interferometric calibration system monitoring dynamical Young's fringes originating from metrology fibers located at the primary mirror. The mission profile is driven by the fact that the two main modules of the payload, the telescope and the focal plane, must be located 40 m away leading to the choice of a formation flying option as the reference mission, and of a deployable boom option as an alternative choice. The proposed mission architecture relies on the use of two satellites, of about 700 kg each, operating at L2 for 5 years, flying in formation and offering a capability of more than 20,000 reconfigurations. The two satellites will be launched in a stacked configuration using a Soyuz ST launch vehicle. The NEAT primary science program will encompass an astrometric survey of our 200 closest F-, G- and K-type stellar neighbors, with an average of 50 visits each distributed over the nominal mission duration. The main survey operation will use approximately 70% of the mission lifetime. The remaining 30% of NEAT observing time might be allocated, for example, to improve the characterization of the architecture of selected planetary systems around nearby targets of specific interest (low-mass stars, young stars, etc.) discovered by Gaia, ground-based high-precision radial-velocity surveys, and other programs. With its exquisite, surgical astrometric precision, NEAT holds the promise to provide the first thorough census for Earth-mass planets around stars in the immediate vicinity of our Sun.
机译:围绕太阳系附近数量有限的太阳型恒星(FGK矮星)进行抽样的行星系统的全面普查(每千个货币符号da的分量每千个15 pc的欧元部分),其可居住范围内的地球质量行星具有统一的敏感性几个非盟区域的划定将是太阳系外行星天体物理学的一个重要里程碑。这个基本目标可以通过NEAT(附近的地球天文望远镜)等任务概念来实现。 NEAT旨在以0.05微米(1 sigma)的精确度执行太空超高精度天体测量,足以探测由于质量低于甚至更接近地球的恒星绕行轨道运行而产生的动力效应。这样的勘测任务将为所探测到的行星系统的所有组成部分(直至地球质量极限)提供实际的行星质量和完整的轨道几何形状。 NEAT的性能极限可以通过在目标和野外一组合适的参考恒星之间进行差分天文测量来实现。 NEAT仪器的设计包括离轴抛物线单镜望远镜(D = 1 m),距望远镜40 m的大视野探测器,由8个小型CCD固定在中央CCD周围组成,以及一种干涉仪校准系统,用于监测源自位于主反射镜的计量光纤的动态杨氏条纹。任务概况受以下事实的驱动:有效载荷的两个主要模块(望远镜和焦平面)必须位于40 m处,这导致选择编队飞行选项作为参考任务以及可部署的吊杆选项作为替代选择。拟议的任务架构依赖于使用两颗卫星,每颗卫星大约700公斤,在L2上运行5年,编队飞行并提供超过20,000种重新配置的能力。这两颗卫星将使用联盟号ST运载火箭以堆叠配置进行发射。 NEAT的主要科学计划将包括对我们200个最接近的F型,G型和K型恒星邻居的天文测量,在名义任务持续时间内平均进行50次造访。主要的勘测工作将使用任务寿命的70%。例如,可以分配剩余的30%NEAT观测时间,以改善Gaia发现的特定感兴趣的目标(低质量恒星,年轻恒星等)附近的选定行星系统的架构特征,基于高精度的径向速度测量和其他程序。 NEAT凭借其出色的外科手术天体测量精度,有望为我们太阳附近的恒星周围的地球质量行星提供首次彻底的普查。

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