QUOTE (edstrick @ Jan 18 2008, 03:16 AM)

If Cassini had retained a simple 1-degree of freedom (fore-and-aft) scan platform, a roll maneuver and platform slew could have permitted imaging while the antenna was on Earth for the RSS occultation. Another victim of NASA and JPL's total failure to contain costs during the "Mariner Mark II" development of a new "low cost" multi-mission outer solar system vehicle.
RSS occs are pretty power-consuming. Even if there were a scan platform there might not be power
to run it and its instruments as well as all the RF downlinks near the end of the nominal mission as the RTGs
run down
I don't disagree scan platforms add enormously to flexibility during the fleeting geometric opportunities
that present themselves on a mission like Cassini, but
a) 'simple..scan platform' may define the null set

as future outer solar system Flagships are being considered and costed, people are wondering how
Cassini was as cheap as it (apparently) was
MMII would have been a bargain if implemented as originally intended - a platform designed once and
re-used for multiple missions - 2 missions for the price of 1.5, 3 missions for the price of 2 maybe.... but
as so often happens with multiple missions (remember how Pathfinder was Mesur Pathfinder....?)
budget got squeezed, CRAF got killed, and Cassini is what it is.