Rosetta operations

Rosetta arrives at comet

The Rosetta mission was approved in November 1993 as the Planetary Cornerstone Mission in ESA's long-term space science programme. The mission goal was initially set for a rendezvous with Comet 46 P/Wirtanen. After postponement of the initial launch, a new target was set: Comet 67 P/Churyumov-Gerasimenko. On its 10-year journey to the comet, the spacecraft also passed by two asteroids.

The mission

Rosetta's main objective is to rendezvous with and enter orbit around Comet 67P/Churyumov-Gerasimenko, performing observations of the comet's nucleus and coma. During the period that Rosetta orbits the comet, 67P/Churyumov-Gerasimenko will reach the closest point to the Sun in its orbit. At the end of 2014, a lander, Philae, will be deployed and will attempt to make the first-ever controlled landing on a comet.

The Rosetta Mission Operations Centre (MOC) is located at ESOC, Darmstadt, Germany.

ROLEComet exploration/landing
LAUNCH DATE2 Mar 2004
LAUNCHER/LOCATIONAriane 5/Kourou, French Guiana
LAUNCH MASS3000 kg
ORBITHighly complex; 3 Earth & 1 Mars gravity assists en route; arrived at comet 67P/C-G on 6 Aug 2014
NOMINAL MISSIONto 2015
+ Rosetta now tracking 67P/C-G as it arcs toward the Sun and its lander Philae will make the first-ever controlled landing on a comet +
 

The Flight Control Team

Sylvain Lodiot, Rosetta Flight Control Team, ESA/ESOC
Sylvain Lodiot

The Flight Control Team (FCT) at ESOC operates from the same Dedicated Control Room (DCR) as Mars Express and Venus Express. Spacecraft Operations Manager (SOM) Sylvain Lodiot, from France, oversees a team of spacecraft operations engineers working full-time on Rosetta. The team is further augmented by analysts and SPACONs (spacecraft controllers), who support all three ESA interplanetary missions via integrated ground software and daily operations.

Other ESOC teams provide additional support in the areas of Flight Dynamics, Ground Facilities and Software Support.

Mission operations overview

Ariane 5 V158 lifts off 2 March 2004 with ESA's Rosetta spacecraft for a ten-year journey to comet 67P/C-G
Ariane 5 V158 lifts off 2 March 2004

During its 10-year journey to Comet 67P/Churyumov-Gerasimenko, Rosetta will circle the Sun almost four times. It will also cross the asteroid belt twice and gain velocity from gravitational 'kicks' provided by close swing-bys of Mars (2007) and Earth (2005, 2007 and 2009).

The launch and early orbit phase (LEOP)

The planned launch date for Rosetta was 07:36:49 UT on 26 February 2004. However, an initial delay due to adverse weather, and a subsequent delay due to a technical issue with the launch vehicle, pushed the launch date back by five days, to 2 March 2004.

After burn-out of the lower stage, the spacecraft and upper stage remained in Earth parking orbit (4000 x 200 km) for about two hours. Ariane's upper stage then ignited to boost Rosetta into its interplanetary trajectory, before separating from the spacecraft.

Earth swing-bys

Rosetta first travelled away from its home planet, before returning a year after launch, in March 2005. Rosetta then headed to Mars and returned to Earth in November 2007 for its second swing-by of our planet. In November 2009 Rosetta will fly past the Earth for the third and last time to receive the final boost required to reach its final target.

Rosetta alternates periods of active and passive phases during the cruise to Earth. The distance at closest approach is between 300 and 5300 km. Operations are mainly focused on orbit determination for the fundamental swing-by manoeuvres; however payload check-out, calibrations and scientific observations are also performed. If required, orbit correction manoeuvres take place before and after each swing-by.

Chasing a comet

Mars swing-by

Rosetta flew past Mars in February 2007 at a distance of about 250 km, phasing its trajectory for the next Earth swing-by and, as a spin-off, obtaining some science observations. During the swing-by, Rosetta had to survive an eclipse for which, due to the mission target change, the spacecraft was not specifically designed to handle. This operation required a significant effort by the FCT, but was entirely successful; during the swing-by itself, a communications black-out was also caused by an occultation as the spacecraft passed behind Mars with respect to the Earth.

Asteroid fly-bys

During the cruise phase, Rosetta alternates between phases of passive and active operation, depending on mission needs. As a secondary scientific objective, Rosetta has observed asteroid Steins in 2008 from a distance of 800 km. In July 2010 only 3160 km will separate Rosetta from asteroid Lutetia when it will fly past. Science data recorded onboard will be transmitted to Earth afterwards.

Deep-space hibernation

Following a planned deep-space manoeuvre using the engine to achieve a change in speed of approximately 800 m/s, the spacecraft went into hibernation between 8 June 2011 and 20 January 2014, due to the very limited power that was available – which did not allow safe spacecraft operations. Almost all electrical systems were switched off, except for the thermal subsystem, on-board computer, radio receivers, command decoders and power supply.

During this period, Rosetta recorded its maximum distance from the Sun, approximately 780 000 000 km, and Earth, approximately 880 000 000 km.

Wake up

On 20 January 2014, still approximately 9 million km from the comet, Rosetta’s pre-programmed internal alarm clock woke up the spacecraft. After warming up its key navigation instruments, coming out of a stabilising spin, and aiming its main radio antenna at Earth, Rosetta sent a signal to let mission operators know it had survived the most distant part of its journey.

The signal was received by both NASA’s Goldstone and Canberra ground stations at 18:18 GMT/ 19:18 CET, during the first window of opportunity the spacecraft had to communicate with Earth. It was immediately confirmed in ESA’s space operations centre in Darmstadt and the successful wake-up announced via the @ESA_Rosetta twitter account, which tweeted: “Hello, World!”

How to orbit a comet

Comet approach

During May-August 2014, Rosetta conducted a series of ten orbit correction manoeuvres to phase its orbit with that of the comet and bring it closer to the point of arrival. One of these thruster burns, conducted on 21 May 2014, was one of the longest-ever burns carried out by an ESA spacecraft.

Arrival

On 6 August 2014, when Rosetta was just 100 km from the comet’s surface, it conducted an orbit manoeuvre that kicked the spacecraft onto the first leg of a pair of triangular-shaped trajectories passing in front of the comet, first at a distance of 100 km and then at 50 km. In the following weeks, Rosetta is attempting to achieve a close, near-circular orbit at 30 km and, depending on the activity of the comet, perhaps come even closer.

Landing sites

On 25 August, using detailed information collected by Rosetta during its first two weeks at Comet 67P/Churyumov-Gerasimenko, five locations were identified as candidate sites to set down the Philae lander in November 2014. Final site selection (a prime and backup) will be made mid-September 2014. 

The ground station - New Norcia

ESA's New Norcia station (DSA-1) is designed to communicate with deep-space missions, typically at ranges in excess of 2 million km
New Norcia station

Since launch, the Rosetta mission has been controlled from a single control centre, the Rosetta Mission Operations Centre (MOC) at ESOC, Darmstadt, using ESA's DSA 1 deep-space ground station at New Norcia.

During critical mission phases (launch, planet swing-bys, etc.) it is supported for tracking, telemetry and command by other ESA ground stations at Kourou, Malargüe and Cebreros, and by the NASA Deep Space Network (DSN) stations at Madrid, Spain, and Goldstone, USA.

Ground segment & mission control system

SIGNAL RECEIVED #AOS European Space Agency has reestablished contact with @ESA_Rosetta 807 million km from Earth #Rosetta @esaoperations
Rosetta teams at ESOC

The Rosetta ground segment is designed to meet both the scientific objectives and the challenges imposed by a deep-space mission. These challenges include long turnaround times for signals (up to 100 minutes), low bit rates for data (8 bps), low power availability (it is the first spacecraft ever to fly with solar power generators beyond 3.1 AU from the Sun) and very precise navigation during planetary swing-bys (Rosetta made use of gravity-assist manoeuvres with Mars and Earth to achieve its final orbit around the Sun).

ESOC teams must cope with the long mission duration and the related problems in scheduling expertise and experienced FCT personnel, while minimising overall cost. The central element of the Rosetta ground segment, the Mission Control System, is based on SCOS-2000.

The Rosetta Science Operations Centre (RSOC) located at ESAC, near Madrid, produces detailed scientific mission planning requests, which are submitted to the MOC in the form of operation requests. The RSOC makes pre-processed scientific data and the scientific data archive available to the scientific community.

A Rosetta Lander Ground Segment (RLGS) will control the Philae lander. This will be coordinated through the Lander Control Centre at the German Aerospace Research Centre (DLR) establishment in Cologne, Germany, and the scientific control centre of CNES, France's space agency, in Toulouse.

The platform and payload

Rosetta’s instruments
The platform

Rosetta is a large aluminium box, 2.8 x 2.1 x 2.0 metres in size. The scientific instruments are mounted on the 'top' of the box (the Payload Support Module) while the subsystems are on the 'base' (Bus Support Module).

On one side of the orbiter is a 2.2m-diameter communications dish antenna – the steerable high-gain antenna; the lander is attached to the opposite face. Two enormous solar panels extend from the other sides. These 'wings', each 32 square metres in area, have a total span of about 32m tip-to-tip. Each comprises five panels, and both may be rotated through +/-180° to track the Sun in every attitude assumed by the spacecraft.

Orbiter instruments

In order to investigate the comet nucleus and the gas and dust ejected from the nucleus as the comet approaches the Sun, Rosetta carries a suite of eleven instruments on-board the orbiter; the lander, Philae, is equipped with a further ten instruments to perform surface measurements.

The orbiter instruments combine remote sensing techniques, such as cameras and radio science measurements, with direct sensing systems such as dust and particle analysers. The instruments are provided by collaborative efforts between scientific institutes in ESA member states and the USA. Principal investigators in several European countries and America lead the nationally funded science teams.

Instrument

Name

ALICE

Ultraviolet Imaging Spectrometer

CONSERT

Comet Nucleus Sounding Experiment by Radiowave Transmission

COSIMA

Cometary Secondary Ion Mass Analyser

GIADA

Grain Impact Analyser and Dust Accumulator

MIDAS

Micro-Imaging Dust Analysis System

MIRO

Microwave Instrument for the Rosetta Orbiter

OSIRIS

Optical, Spectroscopic, and Infrared Remote Imaging System

ROSINA

Rosetta Orbiter Spectrometer for Ion and Neutral Analysis

RPC

Rosetta Plasma Consortium

RSI

Radio Science Investigation

VIRTIS

Visible and Infrared Thermal Imaging Spectrometer

Philae’s instruments
Lander instruments

The ~100-kg Philae lander will be the first spacecraft ever to make a soft landing on the surface of a comet nucleus. The lander is provided by a European consortium under the leadership of the German Aerospace Centre (DLR); other members include ESA, CNES and institutes from Austria, Finland, France, Hungary, Ireland, Italy and the UK. The Philae Lander Control Centre is located at the DLR facility in Cologne, Germany.

The lander structure consists of a baseplate and an instrument platform made in a polygonal sandwich construction, all made of carbon fibre. Some of the instruments and subsystems are beneath a hood that is covered with solar cells.

The lander experiments will study the composition and structure of Comet 67P/Churyumov-Gerasimenko's nucleus.

Instrument

Name

APXS

Alpha-p-X-ray spectrometer

CIVA

Panoramic and microscopic imaging system

CONSERT

Radio sounding, nucleus tomography

COSAC

Evolved gas analyser - elemental and molecular composition

MODULUS Ptolemy

Evolved gas analyser - isotopic composition

MUPUS

Measurements of surface and subsurface properties

ROLIS

Imaging

ROMAP

Magnetometer and plasma monitor

Sampling, Drilling and Distribution Subsystem (SD2)

Drilling and sample retrieval

SESAME

Surface electrical, acoustic and dust impact monitoring

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