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http://dx.doi.org/10.5139/JKSAS.2010.38.10.998

Trans Lunar Injection (TLI) Maneuver Design and Analysis using Finite Thrust  

Song, Young-Joo (한국항공우주연구원)
Park, Sang-Young (연세대학교 천문우주학과)
Kim, Hae-Dong (한국항공우주연구원)
Lee, Joo-Hee (한국항공우주연구원)
Sim, Eun-Sup (한국항공우주연구원)
Publication Information
Journal of the Korean Society for Aeronautical & Space Sciences / v.38, no.10, 2010 , pp. 998-1011 More about this Journal
Abstract
For preparing Korean lunar missions, an Earth-Moon transfer trajectory is designed and analyzed using finite thrust. To be a more realistic scenario, kick motor's performance which is used for TLI (Trans Lunar Injection) maneuver is assumed to have a certain maximum capability. Under this assumption, optimal Earth-Moon transfer trajectory analysis is made from the beginning of Earth departure to the final lunar closest approach. As a results, optimal Earth-Moon transfer trajectory solutions with finite thrust are compared to those of designed with impulsive thrust in previous study. It is confirmed that if the trajectory solutions derived with impulsive burn is directly applied to estimate the finite burn trajectory solutions, careful consideration for finite burn losses must be paid as for TLI maneuver. Presented algorithm and various results will give numerous insights into the future Korea's Lunar missions using finite thrust engines.
Keywords
Lunar Transfer Trajectory Design; Optimal Trajectory; Finite Thrust;
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Times Cited By KSCI : 5  (Citation Analysis)
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