探空火箭上的电生理记录:利用非洲爪蟾卵母细胞的首次尝试报告

Simon L. Wuest, T. Plüss, Christoph Hardegger, M. Felder, A. Kunz, Benno Fleischli, Carlos Komotar, Lukas Rüdlinger, Andreas Albisser, T. Gisler, D. Frauchiger, M. Egli
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引用次数: 1

摘要

细胞如何检测外部机械力尚不完全清楚,但机械敏感离子通道在检测物理力并将其转化为生物反应(机械转导)方面发挥着重要作用。利用“OoClamp”装置,我们开发了一种工具来研究电生理过程,包括不同重力条件下离子通道的门控特性。“OoClamp”设备使用膜片钳技术和运营期间抛物线飞行和离心20 g。在REXUS/BEXUS计划的框架下,我们进一步开发了“OoClamp”装置,目标是在飞行的探空火箭上进行电生理实验。这样一个实验的目的是首先评估非洲爪蟾卵母细胞的电生理测量是否可以在探空火箭飞行中进行,这是以前从未做过的。其次,我们旨在研究微重力条件下离子通道的门控特性。该实验于2016年3月在REXUS 20火箭上进行。飞行后分析显示,当火箭进入微重力阶段时,所有的记录室都是空的。对飞行数据的进一步分析显示,卵母细胞在火箭发射后几秒钟就被撕裂了。因此,使用探空火箭作为电生理记录研究平台的首次尝试受到了限制。我们改进的“OoClamp”硬件能够在探空火箭上执行困难的电生理记录的必要任务;然而,发射过程中的物理应力(加速度和振动)不支持爪蟾卵母细胞的生存能力。
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Electrophysiological Recordings on a Sounding Rocket: Report of a First Attempt Using Xenopus laevis Oocytes
Abstract It is not fully understood how cells detect external mechanical forces, but mechanosensitive ion channels play important roles in detecting and translating physical forces into biological responses (mechanotransduction). With the “OoClamp” device, we developed a tool to study electrophysiological processes, including the gating properties of ion channels under various gravity conditions. The “OoClamp” device uses an adapted patch clamp technique and is operational during parabolic flight and centrifugation up to 20 g. In the framework of the REXUS/BEXUS program, we have further developed the “OoClamp” device with the goal of conducting electrophysiological experiments aboard a flying sounding rocket. The aim of such an experiment was first to assess whether electrophysiological measurements of Xenopus laevis oocytes can be performed on sounding rocket flights, something that has never been done before. Second, we aimed to examine the gating properties of ion channels under microgravity conditions. The experiment was conducted in March 2016 on the REXUS 20 rocket. The post-flight analysis showed that all recording chambers were empty as the rocket reached the microgravity phase. A closer analysis of the flight data revealed that the oocytes were ripped apart a few seconds after the rocket launch. This first attempt at using sounding rockets as a research platform for electrophysiological recordings was therefore limited. Our modified “OoClamp” hardware was able to perform the necessary tasks for difficult electrophysiological recordings aboard a sounding rocket; however, the physical stresses during launch (acceleration and vibrations) did not support viability of Xenopus oocytes.
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