References
- Huntress, W. T., Moroz, V. I., Shevalev, I. L, "Lunar and Planetary Robotic Exploration Missions in the 20th Century", Space Science Reviews, Vol. 107, 2003, pp. 541-649. https://doi.org/10.1023/A:1026172301375
- Kim, W.-S., Kim, S.-W., Hwang, D.-S., "Development Trend of Shock-Absorbing Landing Gear for Lunar Lander," Current Industrial and Technological Trends in Aerospace, Vol. 9, No. 1, 2011, pp. 119-129.
- Blanchard, U. J., "Evaluation of a Full-scale Lunar-gravity by Comparison of Landing-impact Tests of a Full-scale and a 1/6-scale Model", NASA Technical Note D-4474, 1968.
- Kim, H.-D., Lee, H.-H., Kim, S., Park, J.-S., "Design of the KAU Lunar Lander for Shock Absorption Structure Test," Proceeding of the 2010 KSAS Fall Conference, 2010, pp. 837-840.
- Kim, H.-D., Lee, H.-H., Hwang, D.-S., Park, J.-S., "Prediction to Shock Absorption Energy of an Aluminum Honeycomb", J. of The Korean Society for Aeronautical and Space Sciences, Vol. 38, No. 5, 2011, pp. 391-399. https://doi.org/10.5139/JKSAS.2011.39.5.391
- Oh, M. H., Cho, Y. M., Lee, H. J., Cho, J. Y., Hwang, D. S., "Sequential Approximate Optimization of Shock Absorption System for Lunar Lander by using Quadratic Polynomial Regression Meta-model", J. of The Korean Society for Aeronautical and Space Sciences, Vol. 39, No. 4, 2011, pp. 289-384. https://doi.org/10.5139/JKSAS.2011.39.4.314
- ESA-NEXT Team, "Next lunar lander with in-situ science and mobility: Lunar environment specification", ESA, 2008.
- Yang, S. S., Cho, J. Y., Kim, J. H., Lim, J. H., Kim, S. H., "Landing Behaviors of Lunar Lander considering the Effect of Lunar Regolith," Proceeding of the 2012 KSAS Fall Conference, 2012, pp. 1676-1681.
- Yang, S. S., Optimization for Shock Absorption System of Lunar Lander considering Characteristics of Lunar Regolith, Master Thesis, Inha University, 2013.
- Sun, Y., Hu, Y., Liy, P., Deng, Z. "Touchdown dynamics modeling and simulation of lunar lander", ISSCAA, 2010, pp. 1320-1324.
- Son, T.-J., Na, K.-S., Kim, J.-W., Lim, J. H., Kim, K.-W., "Design of a Structural Model for Korean Lunar Explorer", J. of The Korean Society for Aeronautical and Space Sciences, Vol. 41, No. 5, 2013, pp. 366-372. https://doi.org/10.5139/JKSAS.2013.41.5.366
- HEXCEL Composites, HexWebTM Honeycomb Attributes and Properties-A comprehensive guide to standard Hexcel honeycomb materials, configurations, and mechanical properties, 1999.
- Oh, M. H., Development of Sample-reusable Meta-model based Design Optimization Method and its Applications, Ph.D. Dissertation, Inha University, 2012.
- Lysmer, J., Kuhlemeyer, R. L., "Finite dynamic model for infinite media", J. Eng. Mech. Div., ASCE 95, 1969, pp. 859-877.
- Rao, A. S. R, Ranjan, G., Basic and Applied Soil Mechanics, 2nd Ed., New Age International, New Delhi, 2000, pp. 290-296.
- Kikendall Orr, Development of a finite element model to predict the behavior of a prototype wheel on lunar soil, Ph.D. Dissertation, Clemson University, 2010, pp. 62-63.
- Liu, Rongqiang, et al. "Design and selection of aluminum foam for impact damper of legged lunar Lander", Systems and Control in Aerospace and Astronautics, 2008. ISSCAA 2008. 2nd International Symposium on. IEEE, 2008. pp. 1-6.
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