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Comparison of Dynamic Characteristics for an Inflatable Solar Concentrator in Atmospheric and Thermal Vacuum Conditions

机译:大气和热真空条件下充气式太阳能聚光器的动态特性比较

摘要

Dynamic testing of an inflatable solar concentrator structure in a thermal vacuum chamber as well as in ambient laboratory conditions is described in detail. Unique aspects of modal testing for the extremely lightweight inflatable are identified, including the use of a noncontacting laser vibrometer measurement system. For the thermal vacuum environment, mode shapes and frequency response functions are compared for three different test article inflation pressures at room temperature. Modes that persist through all the inflation pressure regimes are identified, as well as modes that are unique for each pressure. In atmospheric pressure and room temperature conditions, dynamic measurements were obtained for the expected operational inflation pressure of 0.5 psig. Experimental mode shapes and frequency response functions for ambient conditions are described and compared to the 0.5 psig results from the thermal vacuum tests. Only a few mode shapes were identified that occurred in both vacuum and atmospheric environments. This somewhat surprising result is discussed in detail, and attributed at least partly to 1.) large differences in modal damping, and 2.) significant differences in the mass of air contained by the structure, in the two environments. Results of this investigation point out the necessity of testing inflatable space structures in vacuum conditions before they can be launched. Ground testing in atmospheric pressure is not sufficient for predicting on-orbit dynamics of non-rigidized inflatable systems.
机译:详细介绍了在热真空室内以及环境实验室条件下对充气式太阳能集中器结构的动态测试。确定了用于超轻型充气车的模态测试的独特方面,包括使用非接触式激光测振仪测量系统。对于热真空环境,比较了室温下三种不同测试物品充气压力的模式形状和频率响应函数。确定了在所有通货膨胀压力状态下均能保持的模式,以及每种压力所独有的模式。在大气压和室温条件下,针对预期的0.5 psig的工作充气压力获得了动态测量结果。描述了环境条件下的实验模式形状和频率响应函数,并将其与热真空测试的0.5 psig结果进行比较。只能识别出在真空和大气环境中均会出现的几种模式形状。详细讨论了这个令人惊讶的结果,并且至少部分归因于以下两种情况:1。)模态阻尼的大差异; 2。)结构所包含的空气质量在两种环境中的显着差异。这项调查的结果指出了在发射可充气空间结构之前必须在真空条件下对其进行测试的必要性。在大气压力下进行地面测试不足以预测非刚性充气系统的在轨动力学。

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