QUOTE (RNeuhaus @ Dec 8 2005, 04:15 PM)
Some excellent points there. Does anyone know if (a) The MSL skycrane is likely to be a multi purpose design and ( what chance is there of Exomars considering it? The 2002 ExoMars\Netlander study specifies "inflatable technology" for the descent module, ie airbags.
Some further info on Exomars (also from the 2002 document available here so it maybe very out of date)
Total Rover landed mass 223kg.
Landing targets - 10-45deg latitudes (North or South).
Mission duration - 4months (main limiting factor appears to be Dust storm risk)
This proposal includes a relay orbiter and 4 netlander modules (stationary seismic\atmospheric probes with 0.5-1 year mission durations). I've seen no mention of the Netlanders in the current ESA announcements, do we know for certain that they have been canned?