Dynamic soaring as a means to exceed the solar wind speed

Mathias N. Larrouturou, A. Higgins, J. Greason
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引用次数: 2

Abstract

A technique by which a spacecraft can interact with flows of ionized gas in space (the solar wind or interstellar medium) in order to be accelerated to velocities greater than the flow velocity is explored. Inspired by the dynamic soaring maneuvers performed by sea birds and gliders in which differences in wind speed are exploited to gain velocity, in the proposed technique a lift-generating spacecraft circles between regions of the heliosphere that have different wind speeds, gaining energy in the process without the use of propellant and only modest onboard power requirements. In the simplest analysis, the spacecraft motion can be modeled as a series of elastic collisions between regions of the medium moving at different speeds. More detailed models of the spacecraft trajectory are developed to predict the potential velocity gains and the maximum velocity that may be achieved in terms of the lift-to-drag ratio of the vehicle. A lift-generating mechanism is proposed in which power is extracted from the flow over the vehicle in the flight direction and then used to accelerate the surrounding medium in the transverse direction, generating lift (i.e., a force perpendicular to the flow). Large values of lift-to-drag ratio are shown to be possible in the case where a small transverse velocity is imparted over a large area of interaction. The requirement for a large interaction area in the extremely low density of the heliosphere precludes the use of a physical wing, but the use of plasma waves generated by a compact, directional antenna to impart momentum on the surrounding medium is feasible, with the excitation of R-waves, X-waves, Alfven waves, and magnetosonic waves appearing as promising candidates. A conceptual mission is defined in which dynamic soaring is performed on the termination shock of the heliosphere, enabling a spacecraft to reach speeds approaching 2% of c within two and a half years of launch without the expenditure of propellant. The technique may comprise the first stage for a multistage mission to achieve true interstellar flight to other solar systems.
动态飙升作为一种手段,以超过太阳风的速度
探索了一种航天器与空间中电离气体(太阳风或星际介质)流动相互作用以加速到大于流动速度的技术。受到海鸟和滑翔机的动态飞行的启发,利用不同的风速来获得速度,在提出的技术中,产生升力的航天器在具有不同风速的日光层区域之间旋转,在不使用推进剂的情况下获得能量,只需要适度的机载功率。在最简单的分析中,航天器的运动可以被建模为以不同速度运动的介质区域之间的一系列弹性碰撞。开发了更详细的航天器轨道模型,以根据飞行器的升阻比预测潜在的速度增益和可能达到的最大速度。提出了一种升力产生机构,该机构从飞行器飞行方向上的气流中提取能量,然后用于在横向上加速周围介质,产生升力(即垂直于气流的力)。大的升阻比值显示在一个小的横向速度在一个大的相互作用区域的情况下是可能的。在极低密度的日球层中,对大的相互作用区域的要求排除了物理机翼的使用,但是使用由紧凑的定向天线产生的等离子体波向周围介质传递动量是可行的,激发r波、x波、阿尔芬波和磁声波似乎是有希望的候选国。一个概念性的任务是在日球层的末端激波上进行动态飙升,使航天器在发射后的两年半内达到接近2% c的速度,而不消耗推进剂。这项技术可能包括多级任务的第一阶段,以实现真正的星际飞行到其他太阳系。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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