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The Comet Nucleus Tour
(CONTOUR), a NASA Discovery mission will visit and study at least
two comets.
CONTOUR’s two
baseline targets, the comets Encke and Schwassmann–Wachmann 3.
Encke, CONTOUR’s first target, Encke, has the shortest orbital
period of any known comet. CONTOUR will visit Encke in November
2003. CONTOUR plans to fly by Schwassmann–Wachmann 3 in June
2006. The CONTOUR mission uses Earth-gravity assist maneuvers to
accomplish the multiple encounters. Three Earth gravity-assist
maneuvers are used to accomplish the two comet encounters over a
3-year period
.
The sequence begins with a 1-year
Earth-return loop that positions the spacecraft for an encounter
with Encke in November 2003. Three Earth-swingby maneuvers are
then used to retarget the spacecraft for an encounter with
Schwassmann Wachmann-3 in June 2006.
CONTOUR will fly by
each comet at the peak of its activity, close to the Sun. During
each encounter, the target comet will also be well situated in the
night sky for astronomers worldwide to make concurrent
observations from the ground. Protected by its dust shield, the
CONTOUR spacecraft will fly by each comet at a distance of about
100 km (54 nmi). The most intensive data taking will occur within
a day or so of each encounter.
The spacecraft design
is simple. CONTOUR has few articulated mechanisms; the solar array
is body mounted and does not require drive motors. The mission
geometry allows CONTOUR to use fixed, passive, existing antenna
designs. With the exception of a long-track pointing of CRISP, all
instrument pointing and antenna pointing is controlled by moving
the spacecraft. A dust shield made of Nextel and Kelvar protects
against impacts for the dust sizes and densities expected at the
three encounters.
The mass spectrometer
and dust analyzer will be mounted to look in the direction of
flight at closest approach. NGIMS will be provided by NASA Goddard
Space Flight Center. It will be placed on the spacecraft within
the dust shield as far forward as possible
CONTOUR's mission
design is flexible so that the spacecraft can be retargeted to
intercept an unexpected comet. The appearance of such a comet
cannot be predicted in time to plan a space mission, but CONTOUR
can take advantage of the opportunity if a "new" comet
passes close enough to Earth's orbit. To identify suitable
candidates for a CONTOUR intercept as early as possible, the
CONTOUR project supports a worldwide early warning search program
for comets approaching from the edge of the solar system.

CONTOUR
Comet
Nucleus
Tour
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SPACECRAFT
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| Int'l Designation |
2002 034A
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Launched
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| Owner / Sponsor |
NASA
/ Cornell University
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| Mission |
Science
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| Satellite Bus |
Johns
Hopkins Univ APL
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|
| Launch Mass |
970 kg (2138
lbm)
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| Mission Orbit |
Earth
Escape
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|
| Design Life |
28
months
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| Power (EOL) |
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LAUNCH
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| Launch Vehicle
Model |
Delta
2 7425 |
| Launch Date / Time |
3 July 2002
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0647:41
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FINANCIAL
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| Satellite cost |
US$159
million
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| Web Links |
CONTOUR
Website
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