Physics
Scientific paper
May 2001
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2001cosre..39..266y&link_type=abstract
Cosmic Research, v. 39, Issue 3, p. 266-274 (2001).
Physics
Scientific paper
An approximate technique for calculating the satellite orbit decay under
the aerodynamic drag effect for arbitrary values of the orbit
eccentricity and for the realistic model of the altitude dependence of
the atmospheric density is proposed.
Bobylev Alexander V.
Yaroshevskii V. A.
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