Fig. 1.
The time t=τ50, when
(M/L)obs(t)≥50,
is plotted against orbital eccentricity for a number of simulations with
Msat=107 Msun and
RPl=300 pc, as defined in the key
Fig. 2.
Initial satellite mass as a function of initial characteristic satellite
radius
Links (back/forward) to:
First version: | 14th | July, | 1998
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Last update: | 28th | September, | 1998
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Jochen M. Braun &
Tom Richtler
(E-Mail: jbraun|richtler@astro.uni-bonn.de)