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EFFICIENT MAIN BELT ASTEROID TOUR EXPLOITING SUN-EARTH LIBRATION POINT DEPARTURE

机译:高效的主腰带小行车旅游利用太阳地球自由点出发

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The exploration of small bodies and asteroids is a fundamental scientific objective, that helps understanding the origin of the universe and uncover novel celestial mechanics phenomena. In particular, the active asteroids of the Main Asteroid Belt (MAB) are of prominent scientific interest, as their volatiles and ejecta might shed light on the most primordial components on such bodies. Missions to selected targets in the MAB are particularly challenging, due to the phasing problem between the Earth and the target asteroid, as well as the unfavourable orbital inclination of some potential active asteroids, requiring expensive plane change manoeuvres. As a consequence, although attractive, these kinds of mission still belong to expensive exploration missions, asking for a large service module class. However, the question of technological feasibility with a small class spacecraft still needs an answer. The paper draws results from recent studies the proponents did, and discusses a mission scenario for a space segment, headed towards the MAB, that benefits of a departure from a Sun-Earth libration point (SEL2). Such scenario derives from the rising number of space mission headed towards SEL2, thus envisaging the possibility of a shared launch for a low-cost MAB mission, greatly reducing the launch cost and the platform mass as well. The departure from SEL2, towards the target asteroids, requires careful mission design and long coasting arcs to obtain an escape trajectory; the study presents the use of resonant Earth-Moon gravity assists, to boost the escape heliocentric velocity, and of a Mars gravity assist to change the plane of the spacecraft. Earth gravity assists are also considered to enable sample return mission scenarios. Different mission profiles are analysed, focusing on the active MAB bodies, but opening the possibility to visit other targets. The interplanetary trajectories are designed with a low thrust off the shelf engine, as the high specific impulse be
机译:小体和小行星的探索是一个基本的科学目标,有助于了解宇宙的起源,并揭示新的天体力学现象。特别地,主要的小行星带(MAB)的活性小行星具有突出的科学兴趣,因为它们的挥发物和喷射物可能会在这些体上最初的原始部件上脱光。由于地球和目标小行星之间的阶段问题以及一些潜在的活动小行星之间的阶段问题,因此,由于地球和目标小行星之间的相位问题以及一些潜在的活动小行星之间的阶段倾斜,因此需要普遍具有挑战性。结果,虽然有吸引力,但这些任务仍然属于昂贵的勘探任务,要求提供一个大型服务模块类。然而,与小级航天器的技术可行性问题仍需要答案。该论文提出了最近的研究表明的结果,并讨论了朝向MAB的空间段的使命场景,这对来自太阳地球自由点(SEL2)的偏离的益处。这种情景来自朝向SEL2的空间任务数量升高,因此设想为低成本MAB任务的共享发射的可能性,大大降低了发射成本和平台质量。从SEL2向目标小行星的出发需要仔细的使命设计和长沿海弧,以获得逃生轨迹;该研究呈现使用谐振地球 - 月球重力助攻,提高逃生皮层速度,并且火星重力有助于改变航天器的平面。地球重力辅助也被认为是启用样本返回任务方案。分析不同的使命概况,重点关注活跃的MAB体,但打开访问其他目标的可能性。由于高特定冲动,行星际轨迹采用架子发动机的低推力设计

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