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question is asked, why didn't they do the probe
launch closer to Jupiter - 80,000 kilometers
seems like a pretty far distance? Well, the
Orbiter itself had to be aimed right at Jupiter,
that is, flying straight toward the spot where
the Probe would enter the atmosphere: that's how
the Probe was going to be aimed. The idea was to
impart the axial spin of the spacecraft to the
Probe. Obviously, after launching the Probe the
Orbiter was going to have change its trajectory,
it didn't want to follow the Probe into Jupiter,
rather swing around the outside of Jupiter so
that it could achieve an orbital pattern. Remember, they could only send so much
propellant fuel with the spacecraft and there was
going to be a terrific "burn" when it
got to Jupiter, to slough off velocity so that
Jupiter's gravity could capture it and turn it
into an artificial moonlet. They didn't have the
luxury of getting up close to the target and then
blow propellant to do a major course correction
and remember, the closer they would get to the
target entry point, the greater the angle to have
to course correct. Not to mention fighting the
monstrous Jupiter gravity well. No, there wasn't
any way around it - it was just going to have to
be a terrific aim.
Orbit Deflection Maneuver
The early release of the Probe
saved Orbiter propellant, and saving
propellant--a limited resource for Galileo--was
important. Remember that the Probe had no
trajectory control of its own. That means that at
the time that the Probe was released, the Orbiter
was also on a collision course with Jupiter! So,
shortly after the Probe release, the Orbiter
changed its trajectory (by firing its main
engine) to avoid sharing the Probe's fate. Since
the Orbiter was still a long distance from
Jupiter, a small trajectory change--and,
consequently, a small amount of propellant--was
all that was needed to properly "aim"
the Orbiter. If Galileo's navigators waited to
release the Probe until the spacecraft was much
closer to Jupiter, the Orbiter would have had to
use much more propellant to carry out the Orbital
Deflection Maneuver.
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