Early Phase Contingency Trajectory Design for the Failure of the First Lunar Orbit Insertion Maneuver: Direct Recovery Options

Early Phase Contingency Trajectory Design for the Failure of the First Lunar Orbit Insertion Maneuver: Direct Recovery Options

To ensure the successful launch of the Korea pathfinder lunar orbiter (KPLO) mission, the Korea Aerospace Research Institute (KARI) is now performing extensive trajectory design and analysis studies. From the trajectory design perspective, it is crucial to prepare contingency trajectory options for...

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Bibliographic Details
Main Authors: Young-Joo Song, Jonghee Bae, Young-Rok Kim, Bang-Yeop Kim
Format: Article
Language:English
Published: The Korean Space Science Society 2017-12-01
Series:Journal of Astronomy and Space Sciences
Subjects:
contingency trajectory design
lunar orbit insertion failure
direct recovery
Korea pathfinder lunar orbiter
Online Access:http://ocean.kisti.re.kr/downfile/volume/kosss/OJOOBS/2017/v34n4/OJOOBS_2017_v34n4_331.pdf

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