Chen, H., Kawakatsu, Y. and Hanada, T. (2014) Low-energy escape from the Sun-Earth L2 halo orbit utilizing unstable manifolds and lunar gravity assist. In Advances in the Astronautical Sciences: 24th AAS/AIAA Space Flight Mechanics Meeting, 2014; Mexico; United States; 26 January 2014 through 30 January 2014; Code 115949. vol. 152, Univelt, Inc. pp. 3679-3691 .
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Published date: 2014
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Local EPrints ID: 496645
URI: http://eprints.soton.ac.uk/id/eprint/496645
PURE UUID: 17ac9689-a700-441f-a132-b7449e2b9312
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Date deposited: 07 Jan 2025 18:43
Last modified: 10 Jan 2025 03:19
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Author:
H. Chen
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Y. Kawakatsu
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T. Hanada
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