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Design of an Extended Mission for GRAILThe GRAIL extended mission will extend the measurement of the lunar gravity field beyond what was achieved by the primary GRAIL mission this past spring (2012). By lowering the orbits of the two GRAIL spacecraft to less than half the altitude of the primary mission orbits on average, the resolution of the gravity field measurements will be improved by a factor of two, yielding a signicant improvement in our knowledge of the structure of the upper crust of the Moon. The challenges of flying so low and the design which will meet those challenges is presented here.
Document ID
20130000250
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
Authors
Sweetser, Theodore H.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Wallace, Mark S.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Hatch, Sara J.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Roncoli, Ralph B.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 27, 2013
Publication Date
August 13, 2012
Subject Category
Lunar And Planetary Science And Exploration
Meeting Information
Meeting: 2012 AIAA/AAS Astrodynamics Specialists Conference
Location: Minneapolis, MN
Country: United States
Start Date: August 13, 2012
End Date: August 16, 2012
Sponsors: American Astronautical Society, American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Other
Keywords
eccentricty vector
low lunar orbit
GRAIL
Moon
orbit control
formation flying
lunar mission
gravity

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