The acceleration of a material interface by a shock wave generates an
interface instability known as the Richtmyer-Meshkov instability. Prev
ious attempts to model the growth rate of the instability have produce
d values that are almost twice that of the experimental measurements.
This Letter presents numerical simulations using front tracking that f
or the first time are in quantitative agreement with experiments of a
shocked air-SF6 interface. Moreover, the failure of the impulsive mode
l, and the linear theory from which it is derived, to model experiment
s correctly is understood in terms of time limits on the validity of t
he linear model.