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Trajectory Design Considerations for Exploration Mission 1

机译:勘探任务1的轨迹设计注意事项

摘要

Exploration Mission 1 (EM-1) will be the first mission to send an uncrewed Orion vehicle to cislunar space in 2018, targeted to a Distant Retrograde Orbit (DRO). Analysis of EM-1 DRO mission opportunities in 2018 help characterize mission parameters that are of interest to other subsystems (e.g., power, thermal, communications, flight operations, etc). Subsystems request mission design trades which include: landing lighting, addition of an Orion main engine checkout burn, and use of auxiliary thruster only cases. This paper examines the evolving trade studies that incorporate subsystem feedback and demonstrate the feasibility of these constrained mission trajectory designs and contingencies.
机译:探索任务1(EM-1)将是2018年将无人猎户座飞船送入月球空间的第一个任务,目标是遥远的逆行轨道(DRO)。对2018年EM-1 DRO任务机会的分析有助于表征其他子系统感兴趣的任务参数(例如,功率,热力,通信,飞行操作等)。子系统要求执行任务的设计交易,包括:着陆照明,增加Orion主引擎检查燃烧以及仅使用辅助推进器的情况。本文研究了结合子系统反馈的不断发展的贸易研究,并证明了这些受约束的任务轨迹设计和突发事件的可行性。

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