Artemis ready for launch this summer
ESA’s
newest communication satellite Artemis
(Advance Relay and TEchnology
MISsion) has undergone its final testing at ESA’s Technology centre
ESTEC in Noordwijk the Netherlands.
Originally the satellite was scheduled to be shipped to Tanegashima space centre
in Japan last
October, for its launch by a Japanese H-IIA rocket
on February 01, 2001. But
problems with that launcher kept Artemis
in Europe several extra months. In
March Artemis
left ESTEC for this summer’s launch by an Ariane-5 rocket.
The Artemis satellite
The 800 million Euro project-contract to built Artemis
was awarded by ESA to a consortium of companies led by Alenia Aerospazio of
Italy. Artemis has a height of 4.5 meters and a length of 24.7 meters. The launch
mass of the satellite will be 3.1 tons. Ones in orbit, 36.000 km above the
Earth, at a position of 21.5 degrees East, Artemis can be in constant
communication with satellites in Low-Earth Orbit (LEO) for long periods of each
orbit, and can beam the data from those satellites directly to the end user on
the ground in Europe and North Africa.
Artemis is a satellite for testing and operating new
telecommunications services. Communications is one sector of space activity
that has a truly commercial nature. The Artemis spacecraft will herald the
start of a new generation of technology and communications services. Artemis
is not the conventional type of communication satellite. In particular it
differs in one very important aspect: none of its payloads connects a fixed
point on the Earth with other fixed points on the Earth. Instead:
* Artemis will connect users on the ground with satellites in orbit via
its radio frequency data relay payload. This dramatically increases
communication time with spacecraft in low-Earth orbit.
* With Artemis, a mobile user will be able to link up from anywhere in
Europe, North Africa or the Middle East to any fixed user in the same area at
very competitive prices. Large ocean areas are included in Artemis’ coverage
zone, allowing voice or data connections to land from the Mediterranean, the
North Sea or the eastern part of the Atlantic Ocean.
*The navigation payload will enable users to determine their position
with higher accuracy and 24-hour availability. Artemis will add corrections and
health checks to the existing GPS signals, thus supporting the first phase of
Galileo, Europe’s new navigation programme.
*Via its optical data relay payload, SILEX, Artemis can receive and
re-transmit in real time.
SILEX
The laser communications terminal aboard Artemis,
known as SILEX (Semiconductor Laser Inter-satellite Link Experiment) is the
worlds first inter-satellite communications data relay system using lasers as
carriers for the signal transmission. There are two SILEX terminals built, one
of them was launched on the French SPOT-4 satellite in 1998, the other will fly
with Artemis. With Artemis in orbit the two terminals will transmit the image
data of the SPOT-4 at a rate of 50 megabits per second (Mbps) to the ground
station near Toulouse. In addition to this data transmission, SILEX will also
support an experiment between OICETS (Optical Inter-orbit Communications
Engineering Test Satellite), a Japanese satellite due for launch also in 2001,
and Artemis. During this experiment the data rate from OICETS to Artemis will
be 50 Mbps, but there will be an optical link between the two satellites also.
Via this optical link a data stream of 2 Mbps can be sent from the ground to
OICETS via Artemis. The advantage of SILEX is very high data rates, less power
consumption and interference, and a saving of weight compared to conventional
radio beam terminals.
ION propulsion Subsystem
(IPS)
Artemis will be the first ESA satellite to fly with
electric propulsion technology operationally. It will be used for inclination
control during the 10-year lifetime of Artemis. The IPS consists of two
thruster assemblies one on the north and one on the south side of the
satellite. Each assembly comprises an Ion Thruster Alignment Mechanism upon
which two redundant thrusters are mounted, a Radio-frequency Ion Thruster (RIT)
and an Electro-bombardment Ion Thruster (EIT). Each of these thrusters has its
own control equipment and power supply and also its own flow control/propellant
monitoring units. Xenon is the propellant used; 40 kg are loaded on board
Artemis. If they didn’t use IPS, the propellant needed would be 400 Kg. So it
is a big weight saver. When the IPS is working it needs about 600 W power,
which comes directly from the solar arrays and later in life from the onboard
batteries.
Satellite users
As mentioned above, Japan will use 40 % of the Artemis
satellite. The OICETS, and Adeos-II, satellites will transmit data via Artemis.
Also the Japanese JEM Module of the International Space Station will use
Artemis to give scientist a chance to monitor the status of experiments that
astronauts perform in on board the station in real time and it gives them an
opportunity to actively intervene. The
European Envisat and SPOT-4 as well as the Italian David satellites will also
transmit data via Artemis.
Thanks to: Leo van Holtz (Artemis project manager) and
Heidi Graf (ESTEC Public Relations)
Notes:
[1] AFP news release, September 26, 2000
[2] ESA press release (09.01) February 15, 2001
[3] Arianespace press release, February 15, 2001