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Precession rates for an artificial satellite.Long period component and secular component of satellite motion evaluated, using lagrange planetary equation
Document ID
19640042572
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Anderson, J.
Lorell, J.
Date Acquired
August 2, 2013
Publication Date
January 1, 1964
Subject Category
Space Radiation
Accession Number
64A28465
Distribution Limits
Public
Copyright
Other
Keywords
GRAVITATIONAL FIELD
LAGRANGE EQUATION
SATELLITE ORBIT

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