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How to Test the SME with Space Missions?In this communication, we focus on possibilities to constrain SME coefficients using Cassini and Messenger data. We present simulations of radio science observables within the framework of the SME, identify the linear combinations of SME coefficients the observations depend on and determine the sensitivity of these measurements to the SME coefficients. We show that these datasets are very powerful for constraining SME coefficients.
Document ID
20150008069
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
Authors
Hees, A.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Lamine, B.
(Centre National de la Recherche Scientifique Toulouse, France)
Le Poncin-Lafitte, C.
(Observatoire de Paris France)
Wolf, P.
(Observatoire de Paris France)
Date Acquired
May 13, 2015
Publication Date
June 17, 2013
Subject Category
Physics (General)
Meeting Information
Meeting: Meeting on CPT and Lorentz Symmetry
Location: Bloomington, IN
Country: United States
Start Date: June 17, 2013
End Date: June 21, 2013
Sponsors: Indiana Univ.
Distribution Limits
Public
Copyright
Other
Keywords
fi fth force search.
gravity
solar system
gravitation
parametrized post-newtonian (PPN) formalism

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