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In 1990 EUMETSAT
decided that a second generation Meteosat system should be
established to ensure continuity and to upgrade the performance of
meteorological observations from Geostationary orbit. The MSG
system consists of a space segment and a ground segment. It is
designed to provide data, products and services over a system
lifetime of, at least, 12 years, based on a series of three
satellites called MSG-1, -2 and -3. The
MSG satellites will be placed in orbit at 0 degrees longitude, but
can be moved up to 50 degrees east or west as required.
MSG
will generate multi-spectral imagery of the Earth's surface and
cloud systems every 15 minutes, for twelve spectral channels. with
1 km geometrical resolution for the high-resolution visible
channel and 3 km for the others. Eight of the channels will be in
the thermal infrared, providing among other information, permanent
data about the temperatures of clouds, land and sea surfaces.
Using channels that absorb ozone, water vapor and carbon dioxide,
MSG will enable meteorologists to analyze the characteristics of
atmospheric air masses making it possible to reconstruct a
three-dimensional view of the atmosphere.
The
MSG body is a cylindrical-shaped solar drum, 3.2 m in diameter and
2.4 m high. The satellite is modular, built around three main
sub-assemblies. The satellite uses a bi-propellant system, both
for its initial boost into geostationary orbit, as well as for
station keeping. This includes small thrusters, which will also be
used for attitude control. The MSG solar array, built from eight
curved panels is wrapped around the satellite body. When operating
in geostationary orbit, the satellite will spin counter-clockwise
at 100 rpm around its longitudinal axis, which will be aligned
with the Earth's rotational axis.

MSG
1
Meteosat
Second
Generation
Program
|
|
SPACECRAFT
|
| Int'l Designation |
2002 040B
|
Launched
|
| Owner / Sponsor |
EUMETSAT
|
| Mission |
Weather
|
| Satellite Bus |
Alcatel
Space Industries
|
|
| Launch Mass |
2000 kg (4408
lbm)
|
| Mission Orbit |
GSO
|
0°
|
| Design Life |
7
years
|
| Power (EOL) |
0.700
kW
|
|
LAUNCH
|
| Launch Vehicle
Model |
Ariane
5 |
| Launch Date / Time |
28
August 2002
|
22:45
|
| Co-passenger(s) |
Atlantic
Bird 1 |
|
FINANCIAL
|
| Satellite cost |
|
| Web Links |
MSG
Website
|
|