The ESA Huygens probe is due for launch as part of the NASA/ESA Cassin
i mission in 1997, to arrive at Titan in late 2004, and will make a 2-
2.5 h exploratory descent to the surface. Huygens is designed to enter
and,brake in Titan's atmosphere in order to parachute a fully-instrum
ented robotic laboratory. The main scientific measurements will take p
lace during that parachute descent, but some will also be performed du
ring the atmospheric entry and the probe resources are sized to allow
measurements after it has impacted Titan's surface for at least a few
minutes. This paper describes the optimization process which has been
implemented,to build that mission, taking into account the scientific
requirements and the environmental and technical constraints imposed o
n both Cassini orbiter and Huygens probe.