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Launch Schedules

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   Artemis - Summary
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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)
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