Astronomy and Astrophysics – Astronomy
Scientific paper
Jun 1974
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1974jansc..21..252d&link_type=abstract
Journal of the Astronautical Sciences, vol. 21, Mar.-June 1974, p. 252-254.
Astronomy and Astrophysics
Astronomy
Eccentricity, Elliptical Orbits, Planetary Systems, Two Body Problem, Deposition, Iterative Solution, Orbit Calculation, Orbital Mechanics, Solar System
Scientific paper
Use of an iterative solution of Kepler's equation shows how the semimajor axis and the eccentricity of the orbit of a particle moving around a massive body are affected when mass is added to the body incrementally, as by accretion. The net effect of numerous small discrete mass additions is to reduce the semimajor axis; the eccentricity, however, remains substantially unchanged.
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