On 3 February 1994, the small University satellite BREM-SAT was carrie
d into orbit by the Space Shuttle Discovery. The spacecraft waited six
days in its Get Away Special (GAS) Container before it was deployed i
n its initial 350 km high circular orbit. With 57 degrees inclination,
the operations from the ground station at the Drop Tower Bremen are p
ossible. BREM-SAT carries six experiments with different scientific ob
jectives. Experiments using the micro-g environment are operated as we
ll as experiments investigating the low earth orbital environment. Two
sensors measure the micrometeorite and dust flux and the atomic oxyge
n flux. In addition, re-entry experiments will be carried out during t
he last hours before re-entry, which is expected in January 1995. One
of these experiments determines the gas/surface interaction, the other
experiments uses deployable temperature and pressure sensors for meas
urements shortly before re-entry. The experience of operating a small,
but complex and versatile platform with ambitious objectives will be
described in detail. First results of the spacecraft operations are pr
esented.