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Space Suit Joint Torque Measurement Method Validation

机译:航天服关节扭矩测量方法验证

摘要

In 2009 and early 2010, a test method was developed and performed to quantify the torque required to manipulate joints in several existing operational and prototype space suits. This was done in an effort to develop joint torque requirements appropriate for a new Constellation Program space suit system. The same test method was levied on the Constellation space suit contractors to verify that their suit design met the requirements. However, because the original test was set up and conducted by a single test operator there was some question as to whether this method was repeatable enough to be considered a standard verification method for Constellation or other future development programs. In order to validate the method itself, a representative subset of the previous test was repeated, using the same information that would be available to space suit contractors, but set up and conducted by someone not familiar with the previous test. The resultant data was compared using graphical and statistical analysis; the results indicated a significant variance in values reported for a subset of the re-tested joints. Potential variables that could have affected the data were identified and a third round of testing was conducted in an attempt to eliminate and/or quantify the effects of these variables. The results of the third test effort will be used to determine whether or not the proposed joint torque methodology can be applied to future space suit development contracts.
机译:在2009年和2010年初,开发并执行了一种测试方法,以量化在几种现有的作战服和原型太空服中操纵关节所需的扭矩。这样做是为了制定适合新星座计划太空服系统的联合扭矩要求。对星座宇航服承包商也采用了相同的测试方法,以验证其宇航服设计符合要求。但是,由于最初的测试是由单个测试操作员设置并进行的,因此存在一个问题,即该方法是否可重复,足以被视为Constellation或其他未来开发程序的标准验证方法。为了验证方法本身,使用与航天服承包商相同但由不熟悉先前测试的人员进行设置的信息,重复了先前测试的代表性子集。使用图形和统计分析比较所得数据;结果表明,对于部分重新测试的关节,报告的值存在显着差异。确定了可能影响数据的潜在变量,并进行了第三轮测试,以试图消除和/或量化这些变量的影响。第三次测试的结果将用于确定建议的联合扭矩方法是否可以应用于未来的太空服开发合同。

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