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|  |  |  |  | | | Rosetta overview
| | | | | | | | | | | |  | | Rosetta successfully lifted off from Europe's Spaceport at Kourou, French Guiana, at 04:17 local time (08:17 CET) on 2 March 2004. |  |  |  |  |
| | | |  | | An artist’s impression of Rosetta approaching the nucleus of Comet 67P/Churyumov-Gerasimenko.
Rosetta’s 11-year expedition began in March 2004, with an Ariane 5 launch from Kourou in French Guiana. Using three Earth-gravity assists (2004, 2007, 2009) and one at Mars (2007), the spacecraft was propelled towards the outer Solar System. It has encountered two asteroids, (2867)Steins in 2008 and (21)Lutetia in 2010, and is now cruising to its final destination.
Rosetta will reach the comet in 2014, and will be the first mission ever to orbit a comet’s nucleus and to deliver a lander, called Philae, on its surface.
Credits: ESA, image by AOES Medialab |  |  |  |  |
| | | |  | | An artist’s impression of Rosetta waking from deep-space hibernation to rendezvous with Comet 67P/Churyumov-Gerasimenko in 2014.
Rosetta’s 11-year expedition began in March 2004, with an Ariane 5 launch from Kourou in French Guiana, and the spacecraft was then sent towards the outer Solar System. The long journey includes three gravity assists at Earth (2004, 2007, 2009), one at Mars (2007), and two asteroid encounters: (2867) Steins (2008) and (21) Lutetia (2010).
After the third Earth-gravity assist and a large deep-space manoeuvre, the spacecraft will go into hibernation (July 2011 – January 2014). During this period, Rosetta will record its maximum distances from the Sun (about 800 million kilometres) and Earth (about 1 thousand million kilometres). The spacecraft will be reactivated prior to the comet-rendezvous manoeuvre, during which the thrusters will fire for several hours to slow the relative drift rate between the spacecraft and comet to about 25 m/s.
Credits: ESA, image by AOES Medialab |  |  |  |  |
| | | | | | | | Mission
 | The Rosetta orbiter - spacecraft design
Rosetta resembles a large aluminium box whose dimensions are 2.8 x 2.1 x 2.0 metres. The scientific instruments are mounted on the 'top' of the box – the Payload Support Module – while the subsystems are on the 'base' or Bus Support Module.
Credits: ESA/AOES Medialab |  |  |  |  |
| | | | Last update: 2 March 2004 | |
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