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Mars environment and magnetic orbiter model payload

机译:火星环境和电磁轨道器模型的有效载荷

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Mars Environment and Magnetic Orbiter was proposed as an answer to the Cosmic Vision Call of Opportunity as a M-class mission. The MEMO mission is designed to study the strong interconnections between the planetary interior, atmosphere and solar conditions essential to understand planetary evolution, the appearance of life and its sustainability. MEMO provides a high-resolution, complete, mapping of the magnetic field (below an altitude of about 250 km), with an yet unachieved full global coverage. This is combined with an in situ characterization of the high atmosphere and remote sensing of the middle and lower atmospheres, with an unmatched accuracy. These measurements are completed by an improved detection of the gravity field signatures associated with carbon dioxide cycle and to the tidal deformation. In addition the solar wind, solar EUV/UV and energetic particle fluxes are simultaneously and continuously monitored. The challenging scientific objectives of the MEMO mission proposal are fulfilled with the appropriate scientific instruments and orbit strategy. MEMO is composed of a main platform, placed on a elliptical (130 x 1,000 km), non polar (77A degrees inclination) orbit, and of an independent, higher apoapsis (10,000 km) and low periapsis (300 km) micro-satellite. These orbital parameters are designed so that the scientific return of MEMO is maximized, in terms of measurement altitude, local time, season and geographical coverage. MEMO carry several suites of instruments, made of an 'exospheric-upper atmosphere' package, a 'magnetic field' package, and a 'low-middle atmosphere' package. Nominal mission duration is one Martian year.
机译:提出将“火星环境与电磁轨道器”作为对M级任务的“宇宙展望”号召的答案。 MEMO任务旨在研究行星内部,大气和太阳条件之间的紧密联系,这对于理解行星的进化,生命的外观及其可持续性至关重要。 MEMO提供了磁场的高分辨率,完整的映射(低于约250 km的高度),但尚未实现完整的全球覆盖。这与高气压的原位表征和中低气压的遥感功能相结合,具有无与伦比的精度。这些测量通过对与二氧化碳循环和潮汐变形有关的重力场特征的改进检测来完成。此外,太阳风,太阳EUV / UV和高能粒子通量会被同时连续监测。 MEMO任务建议书具有挑战性的科学目标可以通过适当的科学仪器和轨道策略来实现。 MEMO由放置在椭圆形(130 x 1,000 km),非极性(77A度倾斜)轨道上的主平台以及独立的较高顶点(10,000 km)和低边缘(300 km)微卫星组成。这些轨道参数的设计使MEMO在测量高度,当地时间,季节和地理覆盖范围方面的科学回报最大化。 MEMO装有几套仪器,由“大气层-高空”包装,“磁场”包装和“中低气压”包装制成。标称任务持续时间为火星年。

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