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...

Täydet tiedot

Bibliografiset tiedot

Päätekijät:	Young-Joo Song, Jonghee Bae, Young-Rok Kim, Bang-Yeop Kim
Aineistotyyppi:	Artigo
Kieli:	Inglês
Julkaistu:	The Korean Space Science Society 2017-12-01
Sarja:	Journal of Astronomy and Space Sciences
Aiheet:	contingency trajectory design lunar orbit insertion failure direct recovery Korea pathfinder lunar orbiter
Linkit:	http://ocean.kisti.re.kr/downfile/volume/kosss/OJOOBS/2017/v34n4/OJOOBS_2017_v34n4_331.pdf
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