Ballute aerocapture trajectories at Titan

被引：0
|
作者：
Lyons, DT [1 ]
Johnson, W [1 ]
机构：
[1] CALTECH, Jet Prop Lab, Pasadena, CA 91109 USA
来源：
ASTRODYNAMICS 2003, PTS 1-3 | 2003年 / 116卷
关键词：
D O I：
暂无
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
Aerocapture at planets and moons with atmospheres using a towed, inflatable ballute system has the potential to provide significant performance benefits compared to traditional all propulsive and aeroshell based aerocapture technologies. This paper discusses the characteristics of entry trajectories for ballute aerocapture at Titan. 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 to Titan.
引用
收藏
页码：2275 / 2294
页数：20
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