Review on abort trajectory for manned lunar landing mission

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XI XiaoNing HUANG WenDe WANG Wei College of Mechatronics Engineering and Automation National University of Defense Technology Changsha China College of Aerospace and Material Engineering National University of Defense Technology Changsha China School of Surveying and Spatial Information System University of New South Wales Sydney NSW Australia [1 ,2 ,2 ,3 ,1 ,410073 ,2 ,410073 ,3 ,2052 ]
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Science China(Technological Sciences). | 2010年 / 53卷 / 10期
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摘要：
Abort trajectory is a passage that ensures the astronauts to return safely to the earth when an emergency occurs. Firstly,the essential elements of mission abort are analyzed entirely based on summarizing the existing studies. Then,abort trajectory requirement and rational selection for different flight phases of typical manned lunar mission are discussed specifically. Considering a trade-off between the two primary constrains of an abort,the return time of flight and energy requirement,a general optimizing method for mission abort is proposed. Finally,some suggestions are given for China’s future manned lunar landing mission.
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