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The Design of a Lunar Farside Gravity Mapping Nanosatellite for the European Student Moon Orbiter Mission

机译:用于欧洲学生月亮轨道特派团的月球远程重力映射纳米卫星的设计

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The construction of a high-resolution map of the lunar gravity field would be very useful for studies of the lunar interior, and would be invaluable for accurately planning future lunar orbiter missions. Previous gravity-mapping missions have tracked the gravitational perturbations of lunar satellite orbits from Earth to construct nearside gravity maps, but have only been able to provide extrapolated measurements of the far side gravity field due to the lack of tracking data while the satellite's orbit is occluded by the Moon. Gravity-mapping payloads utilizing satellite-to-satellite range-rate tracking between a pair of lunar orbiters have been proposed on previous lunar missions, but have not yet flown. The University of Toronto Space Flight Laboratory, using expertise and design heritage from the CanX nanosatellite program, is in the process of developing a payload for the European Student Moon Orbiter (ESMO) called "Lunette," a gravity-mapping nanosatellite that will separate from a parent spacecraft and fly along track in a 100 km altitude circular polar lunar orbit. The Lunette nanosatellite is based on SFL's Generic Nanosatellite Bus and includes a coherent S-band radio transponder, three-axis attitude determination and control, and a 100 m/s propulsion system, allowing it to maintain an along-track orbital formation and measure the range-rate between itself and the parent spacecraft using Doppler tracking. These range-rate measurements will be used to construct a full-sphere lunar gravity map with an accuracy of 20 mGal or better, comparable to the current best-accuracy nearside gravity map from the Lunar Prospector mission data. Lunette has been selected as a payload for the ESMO project under the Student Space Exploration and Technology Initiative (SSETI) program of the European Space Agency. ESMO is currently in Phase A study, and is targeting a launch in 2011.
机译:农历生力场的高分辨率地图的构建对于农历内部的研究非常有用,并且对于准确规划未来的月球轨道特派团来说是非常有用的。以前的重力映射任务已经跟踪了来自地球的月球卫星轨道的引力扰动,以构造近乎重力图,但是只有能够由于缺乏跟踪数据而无法提供远侧重力场的外推测量,而卫星的轨道被遮挡。由月亮。在以前的农历任务上提出了利用一对月球轨道轨道之间的卫星到卫星范围跟踪的重力映射有效载荷,但尚未飞行。多伦多大学航天飞机实验室,使用Canx NanoSatellite计划的专业知识和设计遗产,是为欧洲学生月亮轨道(ESMO)的有效载荷而被称为“LONETER”的过程,该重力映射纳米卫星将分开父母航天器和沿着轨道飞行在100公里的高度圆极性月球轨道上。 Lunette NanoSatellite基于SFL的通用纳米卫星总线,包括相干的S频段无线电应答器,三轴姿态确定和控制,以及100米/秒的推进系统,使其能够保持轨道轨道地层并测量使用多普勒跟踪自身和父空间之间的范围率。这些范围测量将用于构造具有20mgal或更好的精度或更好的全球性月球重力图,可与来自Lunar ProSpector任务数据的当前最佳准确性相当。在欧洲航天局的学生空间探索和技术倡议(SSETI)计划下,已被选为ESMO项目的有效载荷。 ESMO目前在一项研究中,并在2011年的推出。

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