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Mathematical Problems in Engineering
Volume 2015, Article ID 681901, 16 pages
http://dx.doi.org/10.1155/2015/681901
Research Article

Lunar CubeSat Impact Trajectory Characteristics as a Function of Its Release Conditions

1Satellite Ground System Development Team, Satellite Operation Division, Korea Aerospace Research Institute, 169-84 Gwahagno, Yuseong-Gu, Daejeon 305-806, Republic of Korea
2School of Space Research, Kyung Hee University, 1 Seocheon-dong, Giheung-gu, Yongin-si, Gyeonggi-do 446-701, Republic of Korea
3Department of Earth and Planetary Sciences, University of California, Santa Cruz, 1156 High Street, Santa Cruz, CA 95064, USA

Received 26 October 2014; Revised 25 February 2015; Accepted 1 March 2015

Academic Editor: Gongnan Xie

Copyright © 2015 Young-Joo Song et al. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.

How to Cite this Article

Young-Joo Song, Ho Jin, and Ian Garick-Bethell, “Lunar CubeSat Impact Trajectory Characteristics as a Function of Its Release Conditions,” Mathematical Problems in Engineering, vol. 2015, Article ID 681901, 16 pages, 2015. https://doi.org/10.1155/2015/681901.