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Astrodynamical Space Test of Relativity using Optical Devices I (ASTROD I) - A class-M fundamental physics mission proposal for Cosmic Vision 2015-2025: 2010 Update

机译:使用光学器件I的相对论的天体动力学空间测试(asTROD   I) - 宇宙视觉的m级基础物理任务提案   2015-2025:2010年更新

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摘要

This paper on ASTROD I is based on our 2010 proposal submitted for the ESAcall for class-M mission proposals, and is a sequel and an update to ourprevious paper [Experimental Astronomy 23 (2009) 491-527; designated as PaperI] which was based on our last proposal submitted for the 2007 ESA call. Inthis paper, we present our orbit selection with one Venus swing-by togetherwith orbit simulation. In Paper I, our orbit choice is with two Venusswing-bys. The present choice takes shorter time (about 250 days) to reach theopposite side of the Sun. We also present a preliminary design of the opticalbench, and elaborate on the solar physics goals with the radiation monitorpayload. We discuss telescope size, trade-offs of drag-free sensitivities,thermal issues and present an outlook. ASTROD I is a planned interplanetaryspace mission with multiple goals. The primary aims are: to test GeneralRelativity with an improvement in sensitivity of over 3 orders of magnitude,improving our understanding of gravity and aiding the development of a newquantum gravity theory; to measure key solar system parameters with increasedaccuracy, advancing solar physics and our knowledge of the solar system; and tomeasure the time rate of change of the gravitational constant with an order ofmagnitude improvement and the anomalous Pioneer acceleration, thereby probingdark matter and dark energy gravitationally. It is envisaged as the first in aseries of ASTROD missions. ASTROD I will consist of one spacecraft carrying atelescope, four lasers, two event timers and a clock. Two-way, two-wavelengthlaser pulse ranging will be used between the spacecraft in a solar orbit anddeep space laser stations on Earth, to achieve the ASTROD I goals.
机译:这份关于ASTROD I的论文是基于我们为ESAcall提交的2010年M类任务建议而提出的,并且是我们先前论文的续集和更新[Experimental Astronomy 23(2009)491-527;指定为PaperI],这是基于我们为2007年ESA电话会议提交的最新提案。在本文中,我们将通过一个维纳斯摆动与轨道仿真一起介绍我们的轨道选择。在论文一中,我们的轨道选择是两个金星飞越。目前的选择需要更短的时间(约250天)才能到达太阳的对面。我们还介绍了光学平台的初步设计,并详细说明了具有辐射监视器有效载荷的太阳物理目标。我们讨论了望远镜的尺寸,无阻力灵敏度的权衡,热问题并提出了展望。 ASTROD I是一项计划中的具有多个目标的星际空间飞行任务。主要目的是:测试广义相对论,使灵敏度提高3个数量级以上,增进我们对引力的理解,并帮助发展新的量子引力理论;以更高的准确性测量关键的太阳系参数,提高太阳物理学和我们对太阳系的了解;并以一定的幅度提高和异常的先驱加速度测量引力常数的时间变化率,从而探测暗物质和暗能量的引力。设想它是一系列ASTROD任务中的第一个。 ASTROD I将由一架载有望远镜的航天器,四个激光器,两个事件计时器和一个时钟组成。在太阳轨道的航天器和地球上的深空激光站之间将使用两向,两波长激光脉冲测距,以实现ASTROD I目标。

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