论文标题

Lyra项目:捕获1i/'Oumuamua- 2030年使用激光帆船

Project Lyra: Catching 1I/'Oumuamua -- Using Laser Sailcraft in 2030

论文作者

Hibberd, Adam, Hein, Andreas M.

论文摘要

在2017年10月发现的星际对象被指定为1i/'Oumuamua是第一个观察到穿越我们的太阳系的对象。 1i/'Oumuamua具有在天体中从未见过的其他特征,原地观察和测量值将具有非凡的科学价值。先前的研究表明,航天器轨迹的生存能力是使用化学推进的obuamua,在圆周上低至几个太阳半径的太阳能燃烧的化学推进力。除了化学推进外,还可能通过从地球上的激光器的激光束的辐射压力加速了涉及光帆的任务。基于缩放的突破性星际横梁基础设施,已经提出了使用0.001c的较低帆船速度放宽激光功率要求(3-30 GW,1-100 kg spacecraft)和其他各种任务约束。本文使用OITS轨迹仿真工具,该工具假设冲动$δ$ v增量,分析可能在2030年推出的帆船,然后推出,并假设它已经加速至最大速度,则最大速度为300 km/s(约0.001c)。发现2030年7月发布的最低飞行时间为440天。截距将发生在82 au之外。我们得出的结论是,启动大量航天器并达到1i的可能性要比化学推进快得多,这将避免以前提议的任务体系结构的几个缺点。

Discovered in October 2017, the interstellar object designated 1I/'Oumuamua was the first such object to be observed travelling through our solar system. 1I/'Oumuamua has other characteristics never seen before in a celestial body and in-situ observations and measurements would be of extraordinary scientific value. Previous studies have demonstrated the viability of spacecraft trajectories to 'Oumuamua using chemical propulsion with a Solar Oberth burn at a perihelion as low as a few solar radii. In addition to chemical propulsion, there is also the possibility of missions involving light sails accelerated by the radiation pressure of a laser beam from a laser located on Earth. Based on a scaled-down Breakthrough Starshot beaming infrastructure, interplanetary missions and missions to the outer solar system have been proposed using lower sailcraft speeds of 0.001c relaxing the laser power requirements (3-30 GW for 1-100 kg spacecraft) and various other mission constraints. This paper uses the OITS trajectory simulation tool, which assumes an impulsive $Δ$V increment, to analyze the trajectories which might be followed by a sailcraft to 'Oumuamua, with a launch in the year 2030 and assuming it has already been accelerated to a maximum speed of 300km/s (approx. 0.001c) by the laser. A minimum flight duration of 440 days for a launch in July 2030 is found. The intercept would take place beyond 82 AU. We conclude that the possibility of launching a large number of spacecraft and reaching 1I much faster than chemical propulsion would circumvent several disadvantages of previously proposed mission architectures.

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