Exploring the Moon gravity to escape from the Earth–Moon system

Escape trajectories from the Earth–Moon system can be obtained through a single gravity assist maneuver of a spacecraft with the Moon. This paper presents a semi-analytical study of variations in the semi-major axis and the eccentricity of a spacecraft for a geocentric frame—before and after a close...

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Veröffentlicht in:	Computational & applied mathematics 2016-10, Vol.35 (3), p.701-710
Hauptverfasser:	Santana, S. H. S., De Melo, C. F., Macau, E. E. N., Winter, O. C.
Format:	Artikel
Sprache:	eng
Schlagworte:	Applications of Mathematics Applied physics Computational mathematics Computational Mathematics and Numerical Analysis Earth orbits Earth-Moon system Initial conditions Mathematical Applications in Computer Science Mathematical Applications in the Physical Sciences Mathematics Mathematics and Statistics Parking orbits Spacecraft Spacecraft maneuvers Swingby technique
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