We investigate the feasibility of using an adaptive mirror for in-orbi
t aberration corrections. The advantage of an in situ aberration corre
ction of optical components in the space environment is that the mirro
r shape can be adjusted in an iterative fashion until the best image i
s obtained. Using the actuator spacing, corresponding to one half of t
he Nyquist frequency, the Strehl ratio of the corrected wave front imp
roves to 0.95 when the mirror is fabricated with 6.5 waves of spherica
l aberration. The Strehl ratio decreases to 0.86 when the number of ac
tuators is reduced by a factor of 4, ill a two-dimensional adaptive op
tics model.