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Artemis will develop European
capabilities in satellite communications, testing new technologies
and acting as a relay platform to improve existing services to
other satellites and systems. As well as demonstrating new kinds
of mobile communications satellite services and providing direct
satellite-to-satellite communications, Artemis will support
development of a European satellite navigation system.
Artemis will
test communications between satellites and provide a practical
demonstration of the reception of data from other satellites in
orbit and their onward transmission to users in Europe. Satellites
in low Earth orbit (LEO) that are used to gather information about
the environment are restricted in their ability to communicate
with the ground, but Artemis will make it possible to replay data
from a LEO satellite to the same ground station in Europe while it
flies over a large portion of the globe.
Artemis has a data-relay payload
which comprises two complementary elements, both capable of
providing direct communications between satellites in orbit. It
can communicate with other spacecraft using either radio with a
laser beam. The laser communications terminal, known as SILEX
(Semiconductor Laser Inter-satellite Link Experiment), is a world
first. Developed by ESA, this technology is of prime interest for
future constellations of communications satellites in LEO that
will need to communicate with each other. Laser beam communication
offers very high data rates, less power consumption and
interference, and lightweight terminals compared to conventional
radio waves. The more advanced radio data-relay payload and laser
data-relay SILEX payload carried by Artemis will build on this.
Artemis will carry a payload known
as LLM (L-band Land Mobile) which will provide mobile
communications services throughout western Europe and neighbouring
regions, including the Mediterranean, the Middle East and parts of
Russia. The LLM payload has four coverage beams, one that will
extend over the entire area and three (known as spot beams) that
focus on specific parts. The versatility offered by the
three spot beams will be further enhanced by the LLM’s
capability to allocate bandwidth, power and frequencies across the
four beams in response to changing communications demands.
One
of the payloads on Artemis is designed to test satellite-based
navigation technology and ultimately it is envisaged this will
help in establishing a European system.
Artemis was originally scheduled for
launch on a Japanese H-IIA rocket under a cooperative agreement
with the Japanese space agency, NASDA. However, development delays
with the launcher caused ESA to review its launch options and
shift the launch to an Ariane rocket.

ARTEMIS
Advanced
Data Relay
and Technology
Mission
Satellite
|
|
SPACECRAFT
|
| Int'l Designation |
2001-029A
|
Launch
Failure
|
| Owner / Sponsor |
European
Space Agency (ESA)
|
| Mission |
Telecommunications
/ Experimental
|
| Manufacturer / Model |
Alenia
Spazio
|
|
| Launch Mass |
3100
kg (6832 lbm)
|
| Dimensions, stowed |
|
| Mission Orbit |
GSO
|
21.5°E
|
| Design Life |
10
years
|
| Power (EOL) |
2.500
kW
|
|
LAUNCH
|
| Launch Vehicle
Model |
Ariane
5 |
| Date / Time (UTC) |
2001
July 12
|
21:58
|
| Co-passenger(s) |
BSat
2B |
|
FINANCIAL
|
| Satellite cost |
US$
850 million (EUR
820 million)
|
| Web Links |
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