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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:使用光学装置I(ASTROD I)进行相对论的天文空间测试-2015-2025年的M级基本视觉物理任务提案:20-20年:2010年更新

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摘要

ASTROD I is a planned interplanetary space mission with multiple goals. The primary aims are: to test General Relativity with an improvement in sensitivity of over 3 orders of magnitude, improving our understanding of gravity and aiding the development of a new quantum gravity theory; to measure key solar system parameters with increased accuracy, advancing solar physics and our knowledge of the solar system; and to measure the time rate of change of the gravitational constant with an order of magnitude improvement and the anomalous Pioneer acceleration, thereby probing dark matter and dark energy gravitationally. It is envisaged as the first in a series of ASTROD missions. ASTROD I will consist of one spacecraft carrying a telescope, four lasers, two event timers and a clock. Two-way, two-wavelength laser pulse ranging will be used between the spacecraft in a solar orbit and deep space laser stations on Earth, to achieve the ASTROD I goals.For this mission, accurate pulse timing with an ultra-stable clock, and a drag-free spacecraft with reliable inertial sensor are required. T2L2 has demonstrated the required accurate pulse timing; rubidium clock on board Galileo has mostly demonstrated the required clock stability; the accelerometer on board GOCE has paved the way for achieving the reliable inertial sensor; the demonstration of LISA Pathfinder will provide an excellent platform for the implementation of the ASTROD I drag-free spacecraft. These European activities comprise the pillars for building up the mission and make the technologies needed ready. A second mission, ASTROD or ASTROD-GW (depending on the results of ASTROD I), is envisaged as a three-spacecraft mission which, in the case of ASTROD, would test General Relativity to one part per billion, enable detection of solar g-modes, measure the solar Lense-Thirring effect to 10 parts per million, and probe gravitational waves at frequencies below the LISA bandwidth, or in the case of ASTROD-GW, would be dedicated to probe gravitational waves at frequencies below the LISA bandwidth to 100 nHz and to detect solar g-mode oscillations. In the third phase (Super-ASTROD), larger orbits could be implemented to map the outer solar system and to probe primordial gravitational-waves at frequencies below the ASTROD bandwidth. This paper on ASTROD I is based on our 2010 proposal submitted for the ESA call for class-M mission proposals, and is a sequel and an update to our previous paper (Appouchaux et al., Exp Astron 23:491–527, 2009; designated as Paper I) which was based on our last proposal submitted for the 2007 ESA call. In this paper, we present our orbit selection with one Venus swing-by together with orbit simulation. In Paper I, our orbit choice is with two Venus swing-bys. The present choice takes shorter time (about 250 days) to reach the opposite side of the Sun. We also present a preliminary design of the optical bench, and elaborate on the solar physics goals with the radiation monitor payload. We discuss telescope size, trade-offs of drag-free sensitivities, thermal issues and present an outlook.
机译:ASTROD I是一项计划中的具有多个目标的行星际太空任务。主要目的是:测试广义相对论,使其灵敏度提高3个数量级以上,增进我们对引力的理解,并协助开发新的量子引力理论;以更高的精度测量太阳系的关键参数,提高太阳物理学和我们对太阳系的了解;并测量引力常数的时间变化率,并提高一个数量级和反常的先驱加速度,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。为了实现ASTROD I目标,将在太阳轨道的航天器与地球上的深空激光站之间使用两向,两波长的激光脉冲测距,以实现ASTROD I的目标。需要具有可靠惯性传感器的无拖曳航天器。 T2L2证明了所需的准确脉冲时序;伽利略号上的id时钟已基本证明了所需的时钟稳定性; GOCE上的加速度计为实现可靠的惯性传感器铺平了道路。 LISA探路者的演示将为实施ASTROD I无阻力航天器提供一个极好的平台。这些欧洲活动构成了建立任务和使所需技术准备就绪的支柱。设想进行第二次飞行,即ASTROD或ASTROD-GW(取决于ASTROD I的结果),这是一次三飞船飞行任务,在ASTROD的情况下,它将测试广义相对论至十亿分之一,从而能够检测太阳g -模式,测量太阳Lens-Thirring效应至百万分之十,并且在LISA带宽以下的频率下探测引力波,或者在ASTROD-GW的情况下,专门用于探测LISA带宽以下的重力波。 100 nHz并检测太阳g模式振荡。在第三阶段(Super-ASTROD),可以实施更大的轨道以绘制外部太阳系的图并探测低于ASTROD带宽的原始引力波。这份有关ASTROD I的论文是基于我们为ESA提出的M级任务建议而提交的2010年提案,是对我们以前的论文的续集和更新(Appouchaux等,Exp Astron 23:491-527,2009;指定为论文I),这是基于我们为2007年ESA电话会议提交的最新建议。在本文中,我们将通过一个维纳斯绕行与轨道仿真一起介绍我们的轨道选择。在论文I中,我们的轨道选择是两个金星摆动。目前的选择需要较短的时间(约250天)才能到达太阳的另一侧。我们还介绍了光具座的初步设计,并详细说明了辐射监控器有效载荷对太阳物理学的目标。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。

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