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The 2001 Mars Odyssey
Orbiter is scheduled for launch on April 7, 2001with a planned
arrival at Mars on Oct. 20, 2001. After a propulsive maneuver into
a 25-hour capture orbit, aerobraking will be used during 273
orbits taking 76 days to achieve the science orbit. The satellite
will be placed in an orbit with an altitude of 400 kilometers (216
nmi) in a near-polar Sun-synchronous orbit, with a period of 2
hours. Its orbit will bring it over targets in late afternoon on
the day side of the planet and shortly before dawn on the night
side of the planet.
The spacecraft is
designed to orbit Mars for three years, conducting a detailed
analysis of the planet's surface from orbit and measuring the
radiation environment. The orbiter will also act as a
communications relay for future missions to Mars.
The spacecraft will
study the kinds of minerals on the surface and measure the amount
of hydrogen in the shallow subsurfaces of the planet, which will
give scientists clues about the presence of water, either past or
present. It will also provide information on the structure of the
Martian surface and on the geological processes that may have
caused it. The orbiter will also take measurements of the planet's
radiation environment so potential health risks to future human
explorers can be evaluated. To do this, the spacecraft carries
three science instruments: The Thermal Emission Imaging System (THEMIS),
the Gamma Ray Spectrometer (GRS), and the Mars Radiation
Environment Experiment (MARIE).

| Mars
Odyssey Orbiter
|
|
SATELLITE
|
| Int'l Designation |
2001 014A
|
Launched
|
| Owner / Sponsor |
NASA
/ Jet Propulsion Laboratory (JPL)
|
| Mission |
Science
|
| Satellite Bus |
Lockheed
Martin
|
|
| Launch Mass |
758
kg (1668 lbm)
|
| Mission Orbit |
Earth
Escape
|
Mars
|
| Design Life |
3
years
|
| Power (EOL) |
|
|
LAUNCH
|
| Launch Vehicle
Model |
Delta
2 |
| Launch Date / Time |
2001
April 7
|
15:02
|
|
FINANCIAL
|
| Satellite cost |
US$305
million
|
| Web Links |
Mars
Odyssey Orbiter Home Page
|
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