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Why Did NASA limit the use of Magnesium? Flammability and Corrosion Testing of Lightweight Magnesium Alloys for Space Flight Hardware Application

机译:为什么美国国家航空航天局限制使用镁? 轻质镁合金的易燃性和腐蚀试验,用于太空飞行硬件应用

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Magnesium (Mg) alloys are some of the lightest metals used in a myriad of applications across various industries such as automotive, medical, electronics, and aeronautics, yet have not been able to be adopted extensively in aerospace, particularly NASA, applications. Given that magnesium has 2/3 the density of aluminum (Al) and similar specific thickness, Mg components can either provide light weighting of a subsystem or enhance part stiffness by using a thicker part at a similar weight. An extensive literature search was carried out to determine when Mg alloys were used for NASA missions and a clear reason for the current lack of use. The authors additionally consulted with NASA Materials and Processes (M&P) subject matter experts, including the NASA-STD-6016 (Standard Materials and Processes Requirements for Spacecraft) primary author and the NASA Engineering Safety Center (NESC) M&P Technical Fellow, to determine the origin of apparent restrictions on Mg alloy use for spacecraft design. In asking these and many other agency technical experts, the (incorrect) beliefs that Mg alloys have not been adopted for aerospace use included flammability, corrosion, and fatigue life but there was no historical data to point towards the advantages or disadvantages of their use. Although advances in surface treatments and alloying additions are paving the way for adoption of Mg use in other industries, aerospace seems to fluctuate in its use. In fact, it appeared that the limited amount of data available in NASA databases for very specific NASA requirements might be the reason why a designer looking to use Mg alloys would be hindered. Information on corrosion behavior, stress corrosion cracking (SCC), flammability in high oxygen environments, and statistically-developed mechanical properties is needed. It became clear that Mg alloys, specifically those alloyed with rare earth metals which provide some beneficial characteristics, need a revamp in NASA test data to better represe
机译:镁(Mg)合金是各种行业的多数应用中使用的最轻的金属,尚未在航空航天,特别是美国宇航局,申请中广泛采用。鉴于镁具有2/3的铝(Al)和类似的比厚度,Mg组分可以通过使用在类似的重量的较厚部分提供子系统的轻度或增强部分刚度。进行了广泛的文献搜索,以确定镁合金用于NASA任务以及目前缺乏使用的明确原因。该作者还与美国宇航局材料和流程(M&P)主题专家咨询,包括NASA-STD-6016(航天器的标准材料和工艺要求)小学作者和美国宇航局工程安全中心(NESC)M&P技术研究员,以确定镁合金用于航天器设计的明显限制的起源。在询问这些和许多其他机构技术专家时(不正确)信念,即MG合金尚未用于航空航天使用,包括可燃性,腐蚀和疲劳生活,但没有历史数据以指向其使用的优缺点。尽管表面处理和合金化添加剂的进展正在为其他行业采用Mg使用的方式铺平了途径,但航空航天似乎在使用中波动。事实上,它似乎在NASA数据库中提供的有限数据,用于非常特定的美国国家航空航天局的要求可能是希望妨碍使用MG合金的设计者的原因。需要有关腐蚀行为,应力腐蚀开裂(SCC),高氧环境易燃性和统计发达的机械性能的信息。据此清楚的是,镁合金,特别是那些合金化的稀土金属,提供一些有益特征,需要在NASA测试数据中改造,更好地斥责

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