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ACCELERATION MEASUREMENT OPPORTUNITIES ON THE INTERNATIONAL SPACE STATION

机译:国际空间站上的加速测量机会

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Measurement of the microgravity acceleration environment on the International Space Station has been accomplished by two accelerometer systems since 2001. The Microgravity Acceleration Measurement System records the quasi-steady microgravity environment, including the influences of aerodynamic drag, vehicle rotation, and venting effects. Measurement of the vibratory/transient regime, comprised of vehicle, crew, and equipment disturbances, has been accomplished by the Space Acceleration Measurement System-II. Until the arrival of the Columbus Orbital Facility and the Japanese Experiment Module, the location of these sensors, and therefore, the measurement of the microgravity acceleration environment, has been limited to within the United States Laboratory.Japanese Aerospace Exploration Agency has developed a vibratory acceleration measurement system called the Microgravity Measurement Apparatus which will be deployed within the Japanese Experiment Module to make distributed measurements of the Japanese Experiment Module's vibratory acceleration environment. Two Space Acceleration Measurement System sensors from the United States Laboratory will be re-deployed to support vibratory acceleration data measurement within the Columbus Orbital Facility. The additional measurement opportunities resulting from the arrival of these new laboratories allows Principal Investigators with facilities located in these International Space Station research laboratories to obtain microgravity acceleration data in support of their sensitive experiments. The Principal Investigator Microgravity Services project, at NASA Glenn Research Center, in Cleveland, Ohio, has supported acceleration measurement systems and the microgravity scientific community through the processing, characterization, distribution, and archival of themicrogravity acceleration data obtained from the International Space Station acceleration measurement systems. This paper re-introduces the PIMS capabilities to the International Space Station scientific community and introduces plans for extending microgravity analysis results to the newly arrived scientific laboratories.
机译:自2001年以来,国际空间站上的微重力加速度环境的测量已由两个加速度计系统完成。微重力加速度测量系统记录了准稳定的微重力环境,包括气动阻力,车辆旋转和通风效果的影响。由车辆,机组人员和设备干扰组成的振动/瞬态状态的测量已通过“空间加速度测量系统-II”完成。在哥伦布轨道设施和日本实验模块到达之前,这些传感器的位置以及微重力加速度环境的测量仅限于美国实验室内。 日本航天探索局开发了一种称为“微重力测量装置”的振动加速度测量系统,该系统将部署在“日本实验模块”内,以对“日本实验模块”的振动加速度环境进行分布式测量。美国实验室将重新部署两个空间加速度测量系统传感器,以支持哥伦布轨道设施内的振动加速度数据测量。这些新实验室的到来带来了额外的测量机会,这些首席调查员在这些位于国际空间站研究实验室中的设施中获得了微重力加速度数据,以支持他们的敏感实验。位于俄亥俄州克利夫兰的美国宇航局格伦研究中心的首席研究员微重力服务项目已通过对加速度测量系统和微重力科学界的处理,表征,分配和存档,为该项目提供了支持 从国际空间站加速度测量系统获得的微重力加速度数据。本文将PIMS功能重新引入国际空间站科学界,并介绍了将微重力分析结果扩展到新近到达的科学实验室的计划。

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