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Designing of the Optimal Energy Escaping Orbit from Moon L2 Point in Elliptical Three-body Problem
JING Wuxing, LIU Yue
ACTA AERONAUTICAET ASTRONAUTICA SINICA . 2014, (6): 1496 -1504 .  DOI: 10.7527/S1000-6893.2013.0433

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All copyright © editorial office of Chinese Journal of Aeronautics

Total visits: 6658907 Today visits: 1341