Ballute Aerocapture Trajectories at Neptune
Ballute Aerocapture Trajectories at Neptune
复制标题
海王星的巴鲁特航空捕获轨迹
DOI：
10.2514/6.2004-5181
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发表时间：
2004
期刊：
影响因子：
--
通讯作者：
W. Johnson
中科院分区：
文献类型：
--
作者：
D. Lyons;W. Johnson
在具有大气层的行星和卫星上使用可充气的气球系统进行空气捕获，不仅与传统的全推进捕获相比，而且与基于空气动力学壳体的空气捕获技术相比，具有提供显著性能益处的潜力。本文讨论了在海王星上进行降落伞空中捕获的进入轨道特性。这些轨迹是正在进行的更大的系统分析工作的第一步，以表征和优化未来任务的气球航空捕获系统的性能，不仅在海王星，而且在其他有大气层的天体。
Using an inflatable ballute system for aerocapture at planets and moons with atmospheres has the potential to provide significant performance benefits compared not only to traditional all propulsive capture, but also to aeroshell based aerocapture technologies. This paper discusses the characteristics of entry trajectories for ballute aerocapture at Neptune. These trajectories are the first steps in a larger systems analysis effort that is underway to characterize and optimize the performance of a ballute aerocapture system for future missions not only at Neptune, but also the other bodies with atmospheres.