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Mission scenario

Mission profile


To reach its target, Rosetta will complete several revolutions of the Sun, using the gravitational pull of other planets to "bounce off" and modify its trajectory while consuming a minimum of fuel. In all, it will require four fuel-saving gravity assists

The first was round the Earth in March 2005, one year after launch. On 25 February 2007, the probe made a close approach to Mars, acquiring remarkable pictures of the planet’s surface.

The second Earth swing-by took place on 13 November 2007.

On 5 September 2008, Rosetta encountered asteroid Steins, approaching to within 802.6 km. The data from its instruments allowed scientists to precisely determine the asteroid’s composition. An Earth flyby is then scheduled in November 2009. Lastly, a close flyby of asteroid Lutetia is planned in July 2010.

Rosetta's trajectory. Crédits : CNES, Sébastien Rouquette

Rosetta's trajectory. Crédits : CNES, Sébastien Rouquette

This strategy involves a long cruise phase lasting 10 years. Outside a so-called hibernation period when the probe is at its furthest point from the Sun, and remains out of contact with Earth to save power, mission controllers will be continuously uplinking commands during the planned planetary flybys and 2 asteriod flybys to calibrate its instruments and acquire the first science data.

Rosetta will begin observing the comet in mid-2014 for about 18 months, until it passes perihelion. It will drop the lander onto the comet’s surface after a few months in orbit. The Philae lander will conduct measurements for at least five days, then will embark on an extended, higher-risk mission.

A new target


Rosetta initially planned to encounter comet 46/P Wirtanen in 2011, landing on its surface in 2012. But because the Ariane 5 launcher was not available, the launch was be postponed early in 2003 and, a new mission profile was defined. In May 2003, ESA’s Science Programme Committee selected Churyumov-Gerasimenko as the new target, a comet whose nucleus dimensions, activity, orbit and other characteristics met the mission requirements.

Churyumov Gerasimenko comet's model, as seen by Hubble Space  Telescope in 2003. Crédits : NASA, ESA et Philippe Lamy

Churyumov Gerasimenko comet's model, as seen by Hubble Space Telescope in 2003. Crédits : NASA, ESA et Philippe Lamy

The LAM astrophysics laboratory in Marseille, attached to the French national scientific research centre CNRS, also more accurately determined the size of Churyumov-Gerasimenko using the Hubble Space Telescope.

CNES did a new feasibility analysis for the lander mission, as the larger nucleus compared to comet Wirtanen will induce higher levels of gravity.

The mission eventually launched on 2 March 2004 atop an Ariane 5 and the more-than-3-tonne spacecraft began its long voyage around the Sun.



Comet 67P/Churyumov Gerasimenko
Discovery 1969 by Klim Churyumov and Svetlana Gerasimenko
Aphelion 858 million kilometres
Perihelion 194 million kilometres
Diameter of nucleus 1.980 metres


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