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Measuring ejecta characteristics and momentum transfer in experimental simulation of kinetic impact

机译:在动力学冲击实验中测量喷射特性和动量传递

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摘要

The characteristics of ejecta are the crucial element in the concept of kinetic impact deflection of asteroids. The mass and velocity distribution of particles ejected from the impact site determine the enhancement of the momentum transferred by the kinetic impact spacecraft to the target body. Laboratory experiments provide an important means of investigating ejecta characteristics [1] and substantially contribute to the evaluation of deflection efficiency. Scaling laws derived from dimensional analysis and experiments, performed mainly in the context of cratering research [2], have been used to assess the kinetic impact deflection technique [3], [4]. In view of future real-scale deflection missions, like the planned NASA DART impact, more dedicated experiments at relevant impact conditions may substantially contribute to analyzing impact effects, validating numerical simulations and, finally, designing a mission.We performed scaled hypervelocity experiments with impact conditions similar to currently discussed full-scale kinetic impact demonstration missions like DART. In particular, we directly measured both the ejecta characteristics and the momentum transfer in these experiments. The objective of these initial experiments was to demonstrate a novel method for individual particle tracking in the context of asteroid deflection. By determining the size and the velocity of individual particles, we can directly study their influence on the momentum enhancement, the total amount of which we measured using a well-established ballistic pendulum.
机译:喷射的特性是小行星动力学碰撞偏转概念中的关键要素。从撞击点射出的粒子的质量和速度分布决定了由动力撞击航天器转移到目标物体的动量的增强。实验室实验提供了一种研究喷射特性的重要手段[1],并大大有助于评估偏转效率。从尺寸分析和实验中得出的缩放定律,主要是在缩孔研究的背景下进行的[2],已用于评估动力学冲击偏转技术[3],[4]。鉴于未来的实际偏转任务(如计划的NASA DART撞击),在相关撞击条件下进行更多专门的实验可能会极大地有助于分析撞击效果,验证数值模拟并最终设计任务。与目前讨论的全面动态影响演示任务(如DART)相似的条件。特别是,在这些实验中,我们直接测量了喷射特性和动量传递。这些初始实验的目的是证明在小行星偏转的情况下跟踪单个粒子的新方法。通过确定单个粒子的大小和速度,我们可以直接研究它们对动量增强的影响,我们使用完善的弹道摆来测量其总量。

著录项

  • 来源
    《Acta astronautica》 |2019年第3期|297-300|共4页
  • 作者单位

    EMI, Fraunhofer Inst High Speed Dynam, Eckerstr 4, D-79104 Freiburg, Germany;

    EMI, Fraunhofer Inst High Speed Dynam, Eckerstr 4, D-79104 Freiburg, Germany;

    EMI, Fraunhofer Inst High Speed Dynam, Eckerstr 4, D-79104 Freiburg, Germany;

    EMI, Fraunhofer Inst High Speed Dynam, Eckerstr 4, D-79104 Freiburg, Germany;

    EMI, Fraunhofer Inst High Speed Dynam, Eckerstr 4, D-79104 Freiburg, Germany;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Impact experiments; Momentum transfer; Ejecta dynamics; Kinetic impact;

    机译:冲击实验;动量传递;弹射动力学;运动冲击;

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