Ephemeris Model Optimization of Lunar Orbit Insertion from a Free Return Trajectory (AAS 11-452)
Astrodynamics 2011: proceedings of the AAS/AIAA Astrodynamics Specialist Conference held July 31-August 4, 2011, Girdwood, Alaska, U.S.A. / ; 2011 ; Girdwood, Alaska
2012-01-01
18 pages
Also held on attached CD-ROM. Includes bibliographical references and indexes.
Conference paper
English
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