Journal
PLANETARY AND SPACE SCIENCE
Volume 62, Issue 1, Pages 1-9Publisher
PERGAMON-ELSEVIER SCIENCE LTD
DOI: 10.1016/j.pss.2011.11.010
Keywords
CEGM02; Chang'E-1; Lunar gravity field model; Lunar moments of inertia; Lunar potential Love number
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Funding
- National Natural Science Foundation of China [40904006, 40970404, 10973031]
- Chinese National High-tech Projects [2010AA122206]
- Grants-in-Aid for Scientific Research [20244073] Funding Source: KAKEN
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Using Chang'E-1 orbital tracking data, in combination with orbital tracking data of SELENE, Lunar Prospector, and historical spacecraft, a lunar gravity field model denoted CEGM02 is developed. Analyses show that due to its higher orbit altitude (200 km), tracking data of Chang'E-1 contribute to the long wavelengths of the lunar gravity field. When compared to SGM100h, formal error of CEGM02 coefficients below degree 5 is reduced by a factor of about 2. Lunar mean moment of inertia is found to be 0.393466 +/- 0.000065, which can be served as a strong constraint in lunar internal structure research. Lunar potential Love number k(2) is estimated to be 0.0242 +/- 0.0004 (ten times the formal error), which may provide better constraints on lunar interior by combination with lunar moments of inertia. (C) 2011 Elsevier Ltd. All rights reserved.
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