231 research outputs found

    Paper Session II-B - Phase I Lessons for the New Era

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    The Shuttle-Mir Program, officially known as the Phase 1 Program, was the premier international human space flight program. It involved 9 docking flights of the Space Shuttle to the Russian Mir Space Station, 7 long duration stays by US crew on the Mir, almost 1000 days of US crew occupancy of the Mir, and numerous scientific and engineering research activities. Phase 1 was also the source of numerous lessons learned that are being applied to the International Space Station to improve its safety, efficiency, and productivity as a research facility. These include learning to work with an international partner, improvements to experiment design and planning, hardware design risk mitigation, and first hand experience handling many of the most critical safety and operational issues confronting a space station. This paper will briefly cover the major contributions of the Phase 1 Program to ISS and subsequent cooperative space ventures

    An electrochemical and SEM study of the mechanism of formation, morphology, and composition of titanium or zirconium fluoride-based coatings

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    International audienceElectrochemical rest potential and cyclic voltametry were used to investigate the behaviour of the 6% Al magnesium alloy AM60 in various zirconium or titanium fluoride aqueous acid solutions. These solutions have a wide range of aggressiveness with respect to AM60 due largely to fluoride concentration and in some cases to their highly acidic nature. The morphology and composition of the resulting film have been determined by Scanning Electron Microscopy (SEM), and Energy Dispersive X-ray spectroscopy (EDX). The film nucleation is promoted by a pH increase due to water reduction and is thus more likely to occur on the cathodic parts of the surface. Correlatively, film formation on the anodic primary solid solution occurred in only one solution

    Monochromatized x-ray photoelectron spectroscopy of the AM60 magnesium alloy surface after treatments in fluoride-based Ti and Zr solutions

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    International audienceThe behaviour of the 6% aluminium-magnesium alloy (AM60) surface in zirconium or titanium fluoride aqueous acid solutions was studied. X-ray photoelectron spectroscopy was used to investigate modifications in the surface chemistry with respect to the composition of the surface treatment solution. The surface film is composed of magnesium hydroxide and hydroxyfluoride, zirconium oxide, oxyhydroxide or oxyfluoride, titanium oxide and structural and adsorbed water. Optimal parameters leading to the formation of a zirconium- or titanium-rich film were determined. A mechanism is proposed for the formation of zirconium- or titanium-based films

    The surface reactivity of a magnesium–aluminium alloy in acidic fluoride solutions studied by electrochemical techniques and XPS

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    International audienceThe behaviour of the 6% Al magnesium alloy AM60 in aqueous acid fluoride solutions was studied in situ by electrochemical techniques and the surface chemistry of the resulting film was examined by monochromatized XPS. The evolution of the corrosion potential and cyclic voltammograms showed that the aggressiveness of the solutions is mainly driven by their fluoride concentration, the pH having almost no detectable influence. The more concentrated and acidic fluoride solutions led to a higher degree of fluoride coverage of the surface. The surface film is composed of magnesium hydroxide and hydroxyfluoride Mg(OH)2−xFx which approaches MgF2 with increasing fluoride concentration in the film. The parameters governing the film evolution and their relation to surface reactions are discussed

    Analysis of In-Space Assembly of Modular Systems

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    Early system-level life cycle assessments facilitate cost effective optimization of system architectures to enable implementation of both modularity and in-space assembly, two key Exploration Systems Research & Technology (ESR&T) Strategic Challenges. Experiences with the International Space Station (ISS) demonstrate that the absence of this rigorous analysis can result in increased cost and operational risk. An effort is underway, called Analysis of In-Space Assembly of Modular Systems, to produce an innovative analytical methodology, including an evolved analysis toolset and proven processes in a collaborative engineering environment, to support the design and evaluation of proposed concepts. The unique aspect of this work is that it will produce the toolset, techniques and initial products to analyze and compare the detailed, life cycle costs and performance of different implementations of modularity for in-space assembly. A multi-Center team consisting of experienced personnel from the Langley Research Center, Johnson Space Center, Kennedy Space Center, and the Goddard Space Flight Center has been formed to bring their resources and experience to this development. At the end of this 30-month effort, the toolset will be ready to support the Exploration Program with an integrated assessment strateg
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