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Lunar gravity derived from long-period satellite motion, a proposed methodA method was devised to determine the spherical harmonic coefficients of the lunar gravity field. The method consists of a two-step data reduction and estimation process. Pseudo-Doppler data were generated simulating two different lunar orbits. The analysis included the perturbing effects of the L1 lunar gravity field, the earth, the sun, and solar radiation pressure. Orbit determinations were performed on these data and long-period orbital elements were obtained. The Kepler element rates from these solutions were used to recover L1 lunar gravity coefficients. Overall results of the experiment show that lunar gravity coefficients can be accurately determined and that the method is dynamically consistent with long-period perturbation theory.
Document ID
19720007190
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Ferrari, A. J.
(Bellcomm, Inc. Washington, DC, United States)
Date Acquired
August 6, 2013
Publication Date
November 29, 1971
Subject Category
Space Sciences
Report/Patent Number
NASA-CR-124759
CASE-310
TM-71-2014-6
Report Number: NASA-CR-124759
Report Number: CASE-310
Report Number: TM-71-2014-6
Accession Number
72N14840
Funding Number(s)
CONTRACT_GRANT: NASW-417
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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