更深入:探索降低卡西尼号最终轨道的可行性

Erick J. Sturm
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引用次数: 1

摘要

在卡西尼号任务的最后五个轨道上,飞船将比以往任何时候都更接近土星。这五个轨道被设计成卡西尼号能够安全飞行的最深处的大气层;然而,最近土星大气层的掩星数据表明它正在收缩。鉴于这种收缩,在这些轨道运行期间,主要关注的问题已经从航天器的健康和安全转移到科学价值的丧失。这篇论文探讨了一种修改卡西尼号航天器轨道的方案,在这些最后的轨道上,这样它就能更深入地进入土星的大气层。本方案描述了原位探测土星大气状态的方法、降低最终近心高度的机动的位置和规模、此类机动对剩余轨道的影响以及所涉及的风险。结果是,在卡西尼号的最后轨道上,“弹出”的降低近日点的机动是可行的。在最后五次轨道的前三次大气过境中,使用姿态控制推进器作为密度探测器,将航天器的风险降至最低。如果这些过境显示出足够低的密度和足够的推进剂,那么卡西尼项目将考虑执行机动。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Diving deeper: Exploring the feasibility of lowering Cassini's final orbits
During the final five orbits of Cassini's mission, the spacecraft will get closer to Saturn than it has ever been. These five orbits were designed to be as deep in the atmosphere as Cassini could safely fly; however, recent occultation data of Saturn's atmosphere suggest that it is contracting. Given this contraction, the primary concern during these orbits has shifted from spacecraft health and safety to loss of science value. This paper explores a scenario for modifying the Cassini spacecraft's trajectory, during these final orbits, such that it dips deeper into Saturn's atmosphere. This scenario describes the method for in-situ detection of Saturn's atmospheric state, the locations and sizes of maneuvers that would reduce the final periapsis altitudes, the effects of such maneuvers on the remaining trajectory, and the risks involved. The result is that a periapsis-lowering, “pop-down” maneuver is feasible during Cassini's final orbits. Risk to the spacecraft is minimized by using the attitude control thrusters as density detectors during the first three atmospheric transits of the final five orbits. Should these transits reveal sufficiently low density and should sufficient propellant remain, then the Cassini project will consider performing the maneuver.
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