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MISSION AND OPTIMAL TRAJECTORY DESIGN FOR THE KOREAN LUNAR EXPLORATION MISSION

원문정보

초록

영어

This paper covers the design of the mission and the trajectory for the Korean lunar exploration program. For this research, previous lunar missions carried out by other countries were benchmarked. Korean experts who are involved in the lunar exploration program were interviewed so that various perspectives on Korean lunar program can be collected. Using the space exploration simulation program STK (Satellite Tool Kit), we designed three Korean lunar exploration missions, called Boreum1, Boreum2, and Boreum3. Boreum1 mission is a lunar orbiter mission using direct injection trajectory. Boreum2 mission is a lunar landing and sample return mission. Boreum3 mission is a Earth-Moon lagrange point (L1) exploration mission. We expect that the results of this research will contribute to the future Korean lunar exploration program.

목차

ABSTRACT
 1. INSTRUCTION
  1. 1. Research Background
 2. RESEARCH METHOD
  2. 1. Investigation and analysis of precedent lunar exploration mission
  2. 2. Interviewing with experts for Korean lunar exploration mission
  2. 3. Designing trajectories for Korean Lunar exploration mission based on the STK
 3. RESULT
  3. 1. Boreum 1
  3. 2. Boreum 2
  3. 3. Boreum 3
  3. 4. Boreum Project Profile
 4. CONCLUSION
 5. ACKNOWLEDGEMENTS
 6. REFERENCES

저자정보

  • So Hyung Kim Korea Science Academy of KAIST, Busan 614-822, Republic of Korea
  • Kwang Ho Ahn Korea Science Academy of KAIST, Busan 614-822, Republic of Korea
  • Ho Jin Park Korea Science Academy of KAIST, Busan 614-822, Republic of Korea
  • Heekun Roh Korea Science Academy of KAIST, Busan 614-822, Republic of Korea
  • Jaemyung Ahn Department of Aerospace Engineering, Korea Advanced Institute of Science and Technology, Daejeon 305-701, Republic of Korea

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