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Atomic Oxygen Durability Testing of an International Space Station Solar Array Validation Coupon

机译:国际空间站太阳能电池阵列验证优惠券的原子氧耐久性测试

摘要

An International Space Station solar array validation coupon was exposed in a directed atomic oxygen beam for space environment durability testing at the NASA Lewis Research Center. Exposure to atomic oxygen and intermittent tensioning of the solar array were conducted to verify the solar array#s durability to low Earth orbital atomic oxygen and to the docking threat of plume loading both of which are anticipated over its expected mission life of fifteen years. The validation coupon was mounted on a specially designed rotisserie. The rotisserie mounting enabled the solar and anti-solar facing side of the array to be exposed to directed atomic oxygen in a sweeping arrival process replicating space exposure. The rotisserie mounting also enabled tensioning, in order to examine the durability of the array and its hinge to simulated plume loads. Flash testing to verify electrical performance of the solar array was performed with a solar simulator before and after the exposure to atomic oxygen and tensile loading. Results of the flash testing indicated little or no degradation in the solar array#s performance. Photographs were also taken of the array before and after the durability testing and are included along with comparisons and discussions in this report. The amount of atomic oxygen damage appeared minor with the exception of a very few isolated defects. There were also no indications that the simulated plume loadings had weakened or damaged the array, even though there was some erosion of Kapton due to atomic oxygen attack. Based on the results of this testing, it is apparent that the International Space Station#s solar arrays should survive the low Earth orbital atomic oxygen environment and docking threats which are anticipated over its expected mission life.
机译:在NASA Lewis研究中心,将国际空间站太阳能电池阵列验证试样暴露在定向原子氧束中,以进行太空环境耐久性测试。进行了原子氧暴露和太阳能电池阵列的间歇张紧测试,以验证太阳能电池阵列对低地球轨道原子氧的耐受性以及烟羽对接的威胁,预计这两者在其预期的十五年任务寿命内都可以预期。验证券安装在专门设计的烤肉店上。烤肉架可以使阵列的面向太阳和反太阳的一面在扫描到达过程中暴露于定向原子氧,从而复制空间暴露。烤肉架还可以张紧,以便检查阵列及其铰链对模拟羽流载荷的耐久性。在暴露于原子氧和拉伸载荷之前和之后,使用太阳能模拟器进行了闪光测试以验证太阳能电池阵列的电性能。闪蒸测试的结果表明太阳能电池阵列的性能几乎没有下降。在耐久性测试之前和之后,还拍摄了阵列的照片,并在本报告中包括了比较和讨论。除极少数孤立缺陷外,原子氧损伤的程度似乎很小。也没有迹象表明,模拟的羽流载荷削弱或损坏了阵列,即使由于原子氧攻击而使Kapton受到了一些侵蚀。根据该测试的结果,很明显,国际空间站的太阳能电池板应能够在预计的任务寿命内在低地球轨道原子氧环境和对接威胁中生存。

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