Interplanetary small mission studies

J. Owens, M. Johnson
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引用次数: 3

Abstract

Small missions can play a large role in future robotic space exploration. While these missions cannot accomplish the vast scope of science objectives achieved by large missions such as Mars Sample Return or Cassini, they offer opportunities to explore smaller, but pertinent, science goals for significantly reduced total mission cost. The Jet Propulsion Laboratory's Advanced Projects Design Team (Team X) has conducted several mission studies to explore the feasibility of scientifically significant small interplanetary missions. These mission studies encompassed various targets (Mars, Earth's Moon, Venus, the Sun) using several scientific payloads (radar, imagers, radiometers). These missions can also perform other functions such as probe/balloon delivery or communications relay for landed missions. The studies considered a range of secondary payload launch vehicle options. This paper will highlight the results from these studies and discuss how the concurrent engineering environment of Team X lends itself to pre-phase A concept investigations.
行星际小型任务研究
小型任务可以在未来的机器人太空探索中发挥重要作用。虽然这些任务无法完成像“火星样本返回”或“卡西尼”这样的大型任务所实现的广泛科学目标,但它们提供了探索较小但相关的科学目标的机会,从而大大降低了任务的总成本。喷气推进实验室的高级项目设计团队(Team X)已经进行了几项任务研究,以探索具有科学意义的小型行星际任务的可行性。这些任务研究包括不同的目标(火星、地球的月球、金星、太阳),使用几个科学有效载荷(雷达、成像仪、辐射计)。这些任务还可以执行其他功能,例如探测器/气球交付或着陆任务的通信中继。这些研究考虑了一系列次级有效载荷运载火箭的选择。本文将重点介绍这些研究的结果,并讨论X团队的并行工程环境如何有助于前期A阶段概念调查。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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