Sunday C, Murdoch N, Cherrier O, Morales Serrano S, Valeria Nardi C, Janin T, Avila Martinez I, Gourinat Y, Mimoun D
Département Electronique, Optronique et Signal (DEOS), Systèmes Spatiaux (SSPA), Institut Supérieur de l'Aéronautique et de l'Espace (ISAE-SUPAERO), Université de Toulouse, 31055 Toulouse, France.
Département Mécanique des Structures et Matériaux (DMSM), Institut Supérieur de l'Aéronautique et de l'Espace (ISAE-SUPAERO), Université de Toulouse, 31055 Toulouse, France.
Rev Sci Instrum. 2016 Aug;87(8):084504. doi: 10.1063/1.4961575.
This work presents an experimental design for studying low-velocity collisions into granular surfaces in low-gravity. In the experiment apparatus, reduced-gravity is simulated by releasing a free-falling projectile into a surface container with a downward acceleration less than that of Earth's gravity. The acceleration of the surface is controlled through the use of an Atwood machine, or a system of pulleys and counterweights. The starting height of the surface container and the initial separation distance between the projectile and surface are variable and chosen to accommodate collision velocities up to 20 cm/s and effective accelerations of ∼0.1 to 1.0 m/s(2). Accelerometers, placed on the surface container and inside the projectile, provide acceleration data, while high-speed cameras capture the collision and act as secondary data sources. The experiment is built into an existing 5.5 m drop tower frame and requires the custom design of all components, including the projectile, surface sample container, release mechanism, and deceleration system. Data from calibration tests verify the efficiency of the experiment's deceleration system and provide a quantitative understanding of the performance of the Atwood system.
这项工作展示了一种用于研究低重力环境下颗粒表面低速碰撞的实验设计。在实验装置中,通过将自由落体的抛射体释放到向下加速度小于地球重力加速度的表面容器中来模拟微重力。表面的加速度通过使用阿特伍德机或滑轮与配重系统来控制。表面容器的起始高度以及抛射体与表面之间的初始分离距离是可变的,其选择是为了适应高达20厘米/秒的碰撞速度以及约0.1至1.0米/秒²的有效加速度。放置在表面容器和抛射体内的加速度计提供加速度数据,而高速摄像机捕捉碰撞过程并作为辅助数据源。该实验构建在现有的5.5米落塔框架内,需要对所有组件进行定制设计,包括抛射体、表面样本容器、释放机构和减速系统。校准测试的数据验证了实验减速系统的效率,并对阿特伍德系统的性能提供了定量认识。