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Rosetta (spacecraft)
Rosetta (spacecraft)
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Rosetta
Rosetta spacecraft
Artist's illustration of Rosetta
Mission typeComet orbiter/lander
OperatorESA
COSPAR ID2004-006A Edit this at Wikidata
SATCAT no.28169
Websiteesa.int/rosetta
Mission duration12 years, 6 months and 28 days
Spacecraft properties
ManufacturerAstrium
Launch massCombined: 3,000 kg (6,600 lb)
Orbiter: 2,900 kg (6,400 lb)
Lander: 100 kg (220 lb) [1]
Dry massOrbiter: 1,230 kg (2,710 lb)
Payload massOrbiter: 165 kg (364 lb)
Lander: 27 kg (60 lb)
Dimensions2.8 × 2.1 × 2 m (9.2 × 6.9 × 6.6 ft)
Power850 watts at 3.4 AU[2]
Start of mission
Launch date2 March 2004, 07:17:51 (2004-03-02UTC07:17:51) UTC[3]
RocketAriane 5G+ V-158
Launch siteKourou ELA-3
ContractorArianespace
End of mission
DisposalDeorbited
Last contact30 September 2016, 10:39:28 (2016-09-30UTC10:39:29) UTC SCET
Landing siteSais, Ma'at region[4]
2 years, 55 days of operations at the comet
Flyby of Earth
Closest approach4 March 2005
Distance1,954 km (1,214 mi)
Flyby of Mars
Closest approach25 February 2007
Distance250 km (160 mi)
Flyby of Earth
Closest approach13 November 2007
Distance5,700 km (3,500 mi)
Flyby of 2867 Šteins
Closest approach5 September 2008
Distance800 km (500 mi)
Flyby of Earth
Closest approach12 November 2009
Distance2,481 km (1,542 mi)
Flyby of 21 Lutetia
Closest approach10 July 2010
Distance3,162 km (1,965 mi)
67P/Churyumov–Gerasimenko orbiter
Spacecraft componentRosetta
Orbital insertion6 August 2014, 09:06 UTC[5]
Orbital parameters
Periapsis altitude29 km (18 mi)[6]
67P/Churyumov–Gerasimenko lander
Spacecraft componentPhilae
Landing date12 November 2014, 17:32 UTC
Landing siteAbydos
Transponders
BandS band (low gain antenna)
X band (high gain antenna)
Bandwidthfrom 7.8-bit/s (S band)[7]
up to 91 kbit/s (X band)[8]
Rosetta mission insignia
ESA Solar System insignia for Rosetta

Rosetta was a space probe built by the European Space Agency that launched on 2 March 2004. Along with Philae, its lander module, Rosetta performed a detailed study of comet 67P/Churyumov–Gerasimenko (67P).[9][10] During its journey to the comet, the spacecraft performed flybys of Earth, Mars, and the asteroids 21 Lutetia and 2867 Šteins.[11][12][13] It was launched as the third cornerstone mission of the ESA's Horizon 2000 programme, after SOHO / Cluster and XMM-Newton.[14] The total cost of the mission was about €1.3 billion (US$1.8 billion).[15]

On 6 August 2014, the spacecraft reached the comet and performed a series of manoeuvers to eventually orbit the comet at distances of 30 to 10 kilometres (19 to 6 mi).[16] On 12 November, its lander module Philae performed the first successful landing on a comet,[17] though its battery power ran out two days later.[18] Communications with Philae were briefly restored in June and July 2015, but due to diminishing solar power, Rosetta's communications module with the lander was turned off on 27 July 2016.[19] On 30 September 2016, the Rosetta spacecraft ended its mission by hard-landing on the comet in its Ma'at region.[20][21]

Name

[edit]

The probe was named after the Rosetta Stone,[22] a stele of Egyptian origin featuring a decree in three scripts. The lander was named after the Philae obelisk, which bears a bilingual Greek and Egyptian hieroglyphic inscription. A comparison of its hieroglyphs with those on the Rosetta Stone catalysed the deciphering of the Egyptian writing system. Similarly, it was hoped that these spacecraft would result in better understanding of comets and the early Solar System.[23][24] In a more direct analogy to its namesake, the Rosetta spacecraft also carried a micro-etched pure nickel prototype of the Rosetta disc donated by the Long Now Foundation. The disc was inscribed with 6,500 pages of language translations.[25][26]

Mission overview

[edit]
Comet Churyumov–Gerasimenko in March 2015 as imaged by Rosetta, enhanced colour

The spacecraft consisted of the Rosetta orbiter, which featured 12 instruments, and the Philae lander, with nine additional instruments.[27] The Rosetta mission orbited Comet Churyumov–Gerasimenko for 17 months and was designed to complete the most detailed study of a comet ever attempted.

Rosetta was launched on 2 March 2004 from the Guiana Space Centre in Kourou, French Guiana, on an Ariane 5 rocket. In 2007, Rosetta made a Mars gravity assist (flyby).[28] The spacecraft also performed two asteroid flybys:[29] of 2867 Šteins in September 2008 and of 21 Lutetia in July 2010.[30]

Rosetta reached Comet Churyumov–Gerasimenko in May 2014.[31] It performed a series of manoeuvres to enter orbit between then and 6 August 2014,[32] when it became the first spacecraft to orbit a comet.[33][31][34] Rosetta's Philae lander successfully made the first soft landing on a comet nucleus when it touched down on Comet Churyumov–Gerasimenko on 12 November 2014.[35][36][37]

Mission firsts

[edit]

The Rosetta mission achieved many historic firsts.[38] On its way to comet 67P, Rosetta passed through the main asteroid belt, and made the first European close encounter with several of these primitive objects. Rosetta was the first spacecraft to fly close to Jupiter's orbit using solar cells as its main power source.[39] Rosetta was the first spacecraft to orbit a comet nucleus,[40] and was the first spacecraft to fly alongside a comet as it headed towards the inner Solar System. Previous missions had conducted successful flybys of seven other comets.[41] It became the first spacecraft to examine at close proximity the activity of a frozen comet as it is warmed by the Sun. Shortly after its arrival at 67P, the Rosetta orbiter dispatched the Philae lander for the first controlled touchdown on a comet nucleus. The robotic lander's instruments obtained the first images from a comet's surface and made the first in situ analysis of its composition.

History

[edit]
Illustration of Rosetta and Philae at the comet

Background

[edit]

During the 1986 approach of Halley's Comet, international space probes were sent to explore the comet, most prominent among them being ESA's Giotto.[42] After the probes returned valuable scientific information, it became obvious that follow-ons were needed that would shed more light on cometary composition and answer new questions.[43]

Both ESA and NASA started cooperatively developing new probes. The NASA project was the Comet Rendezvous Asteroid Flyby (CRAF) mission.[44] The ESA project was the follow-on Comet Nucleus Sample Return (CNSR) mission.[45] Both missions were to share the Mariner Mark II spacecraft design, thus minimising costs. In 1992, after NASA cancelled CRAF due to budgetary limitations, ESA decided to develop a CRAF-style project on its own.[46] By 1993 it was evident that the ambitious sample return mission was infeasible with the existing ESA budget, so the mission was redesigned and subsequently approved by the ESA, with the final flight plan resembling the cancelled CRAF mission: an asteroid flyby followed by a comet rendezvous with in-situ examination, including a lander.[46] After the spacecraft launch, Gerhard Schwehm was named mission manager; he retired in March 2014.[47]

The Rosetta mission included generational team management; this allowed mission continuity over the long period of the mission and for special knowledge to be maintained and passed on to future team members. In particular, several younger scientists were brought on as principal science investigators, and regular training sessions were conducted.[16]

The spacecraft was controlled from the European Space Operations Centre (ESOC), in Darmstadt, Germany.[48] The planning for the operation of the scientific payload, together with the data retrieval, calibration, archiving and distribution, was performed from the European Space Astronomy Centre (ESAC), in Villanueva de la Cañada, near Madrid, Spain.[49] It has been estimated that in the decade preceding 2014, some 2,000 people assisted in the mission in some capacity.[47]

Rosetta was built in a clean room according to COSPAR rules, but "sterilisation [was] generally not crucial since comets are usually regarded as objects where you can find prebiotic molecules, that is, molecules that are precursors of life, but not living microorganisms", according to Gerhard Schwehm, Rosetta's project scientist.[50]

Rosetta was set to be launched on 12 January 2003 to rendezvous with the comet 46P/Wirtanen in 2011.[43] This plan was abandoned after the failure of an Ariane 5 ECA carrier rocket during Hot Bird 7's launch on 11 December 2002, grounding it until the cause of the failure could be determined.[51] In May 2003, a new plan was formed to target the comet 67P/Churyumov–Gerasimenko, with a revised launch date of 26 February 2004 and comet rendezvous in 2014.[52][53] The larger mass and the resulting increased impact velocity made modification of the landing gear necessary.[54]

Launch

[edit]

After two scrubbed launch attempts, Rosetta was launched on 2 March 2004 at 07:17 UTC from the Guiana Space Centre in French Guiana, using Ariane 5 G+ carrier rocket.[3] Aside from the changes made to launch time and target, the mission profile remained almost identical. Both co-discoverers of the comet, Klim Churyumov and Svetlana Gerasimenko, were present at the spaceport during the launch.[55][56]

Deep space manoeuvres

[edit]
Animation of Rosetta's trajectory from 2 March 2004 to 9 September 2016
  Rosetta ·   67P/Churyumov–Gerasimenko ·   Earth ·   Mars ·   21 Lutetia ·   2867 Šteins
Trajectory of the Rosetta space probe
Rosetta "selfie" at Mars
Enhanced image of asteroid Šteins by Rosetta

To achieve the required velocity to rendezvous with 67P, Rosetta used gravity assist manoeuvres to accelerate throughout the inner Solar System.[16] The comet's orbit was known before Rosetta's launch, from ground-based measurements, to an accuracy of approximately 100 km (62 mi). Information gathered by the onboard cameras beginning at a distance of 24 million kilometres (15,000,000 mi) were processed at ESA's Operation Centre to refine the position of the comet in its orbit to a few kilometres.[citation needed] The first Earth flyby was on 4 March 2005.[57]

On 4 July 2005, imaging instruments on board observed the collision between the comet Tempel 1 and the impactor of the Deep Impact mission.[58]

On 25 February 2007, the craft was scheduled for a low-altitude flyby of Mars, to correct the trajectory. This was not without risk, as the estimated altitude of the flyby was a mere 250 kilometres (160 mi).[59] During that encounter, the solar panels could not be used since the craft was in the planet's shadow, where it would not receive any solar light for 15 minutes, causing a dangerous shortage of power. The craft was therefore put into standby mode, with no possibility to communicate, flying on batteries that were originally not designed for this task.[60] This Mars manoeuvre was therefore nicknamed "The Billion Euro Gamble".[61] The flyby was successful, with Rosetta even returning detailed images of the surface and atmosphere of the planet, and the mission continued as planned.[11][28]

The second Earth flyby was on 13 November 2007 at a distance of 5,700 km (3,500 mi).[62][63] In observations made on 7 and 8 November, Rosetta was briefly mistaken for a near-Earth asteroid about 20 m (66 ft) in diameter by an astronomer of the Catalina Sky Survey and was given the provisional designation 2007 VN84.[64] Calculations showed that it would pass very close to Earth, which led to speculation that it could impact Earth.[65] However, astronomer Denis Denisenko recognised that the trajectory matched that of Rosetta, which the Minor Planet Center confirmed in an editorial release on 9 November.[66][67]

The spacecraft performed a close flyby of asteroid 2867 Šteins on 5 September 2008. Its onboard cameras were used to fine-tune the trajectory, achieving a minimum separation of less than 800 km (500 mi). Onboard instruments measured the asteroid from 4 August to 10 September. Maximum relative speed between the two objects during the flyby was 8.6 km/s (19,000 mph; 31,000 km/h).[68]

Rosetta's third and final flyby of Earth happened on 12 November 2009 at a distance of 2,481 km (1,542 mi).[69]

On 16 March 2010, Rosetta performed bservations of the dust tail of the object P/2010 A2. Together with observations by Hubble Space Telescope, it helped to confirm that P/2010 A2 is not a comet, but an asteroid, and that the tail most likely consists of particles from an impact by a smaller asteroid.[70]

Earth from Rosetta during final flyby
Joy from receiving first signals from Rosetta after waking up on 20 January 2014.

On 10 July 2010, Rosetta flew by 21 Lutetia, a large main-belt asteroid, at a minimum distance of 3,168±7.5 km (1,969±4.7 mi) at a velocity of 15 kilometres per second (9.3 mi/s).[13] The flyby provided images of up to 60 metres (200 ft) per pixel resolution and covered about 50% of the surface, mostly in the northern hemisphere.[30][71] The 462 images were obtained in 21 narrow- and broad-band filters extending from 0.24 to 1 μm.[30] Lutetia was also observed by the visible–near-infrared imaging spectrometer VIRTIS, and measurements of the magnetic field and plasma environment were taken as well.[30][71]

On 8 June 2011, the spacecraft was transferred into a spin stabilised mode and all electronics except the onboard computer and the hibernation heaters were switched off for the planned 31 months of hibernation.[72] After leaving its hibernation mode in January 2014 and getting closer to the comet, Rosetta began a series of eight burns in May 2014. These reduced the relative velocity between the spacecraft and 67P from 775 to 7.9 m/s (2,543 to 26 ft/s).[32]

Reaction control system problems

[edit]

In 2006, Rosetta suffered a leak in its reaction control system (RCS).[16] The system, which consists of 24 bipropellant 10-newton thrusters,[32] was responsible for fine tuning the trajectory of Rosetta throughout its journey. The RCS operated at a lower pressure than designed due to the leak. While this may have caused the propellants to mix incompletely and burn 'dirtier' and less efficiently, ESA engineers were confident that the spacecraft would have sufficient fuel reserves to allow for the successful completion of the mission.[73]

Prior to Rosetta's deep space hibernation period, two of the spacecraft's four reaction wheels began exhibiting increased levels of "bearing friction noise". Increased friction levels in Reaction Wheel Assembly (RWA) B were noted after its September 2008 encounter with asteroid Šteins. Two attempts were made to relubricate the RWA using an on-board oil reservoir, but in each case noise levels were only temporarily lowered, and the RWA was turned off in mid-2010 after the flyby of asteroid Lutetia to avoid possible failure. Shortly after this, RWA C also began showing evidence of elevated friction. Relubrication was also performed on this RWA, and methods were found to temporarily increase its operating temperature to better improve the transfer of oil from its reservoir. In addition, the reaction wheel's speed range was decreased to limit lifetime accumulated rotations. These changes resulted in RWA C's performance stabilising.[74]

During the spacecraft's Deep Space Hibernation flight phase, engineers performed ground testing on a flight spare RWA at the European Space Operations Centre. After Rosetta exited hibernation in January 2014, lessons learned from the ground testing were applied to all four RWAs, such as increasing their operating temperatures and limiting their wheel speeds to below 1000 rpm. After these fixes, the RWAs showed nearly identical performance data.[74] Three RWAs were kept operational, while one of the malfunctioning RWAs was held in reserve. Additionally, new on-board software was developed to allow Rosetta to operate with only two active RWAs if necessary.[16][75] These changes allowed the four RWAs to operate throughout Rosetta's mission at 67P/Churyumov–Gerasimenko despite occasional anomalies in their friction plots and a heavy workload imposed by numerous orbital changes.[74]

Orbit around 67P

[edit]
Animation of Rosetta's trajectory around 67P from 1 August 2014 to 31 March 2015
  Rosetta ·   67P
Rosetta rendezvous with a comet
Comet 67P seen from 10 km (6 mi)

Starting on 7 May 2014, Rosetta began orbital correction manoeuvres to bring itself into orbit around 67P. At the time of the first deceleration burn Rosetta was approximately 2,000,000 km (1,200,000 mi) away from 67P and had a relative velocity of +775 m/s (2,540 ft/s); by the end of the last burn, which occurred on 23 July, the distance had been reduced to just over 4,000 km (2,500 mi) with a relative velocity of +7.9 m/s (18 mph).[32][76] In total eight burns were used to align the trajectories of Rosetta 67P with the majority of the deceleration occurring during three burns: Delta-v's of 291 m/s (650 mph) on 21 May, 271 m/s (610 mph) on 4 June, and 91 m/s (200 mph) on 18 June.[32]

In August 2014, Rosetta rendezvoused with the comet 67P/Churyumov–Gerasimenko (67P) and commenced a series of manoeuvres that took it on two successive triangular paths, averaging 100 and 50 kilometres (62 and 31 mi) from the nucleus, whose segments are hyperbolic escape trajectories alternating with thruster burns.[33][31] After closing to within about 30 km (19 mi) from the comet on 10 September, the spacecraft entered actual orbit about it.[33][31][34][needs update] This started the Global Mapping Phase.[6]

The surface layout of 67P was unknown before Rosetta's arrival. The orbiter mapped the comet in anticipation of detaching its lander.[77] On 14 July 2014, the OSIRIS on-board imaging system returned images of the comet which confirmed its irregular shape.[78][79] By 25 August 2014, five potential landing sites had been determined.[80] On 15 September 2014, ESA announced Site J, named Agilkia in honour of Agilkia Island by an ESA public contest and located on the "head" of the comet,[81] as the lander's destination.[82]

Philae lander

[edit]
Rosetta and Philae
The comet in January 2015 as seen by Rosetta's NAVCAM
Outbursting of the comet 67P/Churyumov–Gerasimenko on 12 September 2015 one of the most dramatic cliff collapses captured during the Rosetta mission.
Comet 67P with a tail of gas and dust, seen from 162 km (101 mi)

Philae detached from Rosetta on 12 November 2014 at 08:35 UTC, and approached 67P at a relative speed of about 1 m/s (3.6 km/h; 2.2 mph).[83] It initially landed on 67P at 15:33 UTC, but bounced twice, coming to rest at 17:33 UTC.[17][84] Confirmation of contact with 67P reached Earth at 16:03 UTC.[85]

On contact with the surface, two harpoons were to be fired into the comet to prevent the lander from bouncing off, as the comet's escape velocity is only around 1 m/s (3.6 km/h; 2.2 mph).[86] Analysis of telemetry indicated that the surface at the initial touchdown site is relatively soft, covered with a layer of granular material about 0.82 feet (0.25 meters) deep,[87] and that the harpoons had not fired upon landing. After landing on the comet, Philae had been scheduled to commence its science mission, which included:

  • Characterisation of the nucleus
  • Determination of the chemical compounds present, including amino acid enantiomers[88]
  • Study of comet activities and developments over time

After bouncing, Philae settled in the shadow of a cliff,[89] canted at an angle of around 30 degrees. This made it unable to adequately collect solar power, and it lost contact with Rosetta when its batteries ran out after three days, well before much of the planned science objectives could be attempted.[89][18] Contact was briefly and intermittently reestablished several months later at various times between 13 June and 9 July, before contact was lost once again. There was no communication afterwards,[90] and the transmitter to communicate with Philae was switched off in July 2016 to reduce power consumption of the probe.[19] The precise location of the lander was discovered in September 2016 when Rosetta came closer to the comet and took high-resolution pictures of its surface.[89] Knowing its exact location provides information needed to put Philae's two days of science into proper context.[89]

End of mission

[edit]

Between November 2014 and December 2015, Rosetta escorted the comet around the Sun and performed riskier investigations.[91] As the orbit of comet 67P took it farther from the Sun, the amount of sunlight reaching Rosetta's solar panels decreased. While it would have been possible to put Rosetta into a second hibernation phase during the comet's aphelion, there was no assurance that enough power would be available to run the spacecraft's heaters to keep it from freezing. To guarantee a maximum science return, mission managers made the decision to instead guide Rosetta down to the comet's surface and end the mission on impact, gathering photographs and instrument readings along the way.[92] On 23 June 2015, at the same time as a mission extension was confirmed, ESA announced that end of mission would occur at the end of September 2016 after two years of operations at the comet.[91]

All stations and the briefing room, we've just had loss of signal at the expected time. This is another outstanding performance by flight dynamics. So we'll be listening for the signal from Rosetta for another 24 hours, but we don't expect any. This is the end of the Rosetta mission. Thank you, and goodbye.
—Sylvain Lodiot, Rosetta Spacecraft Operations Manager, European Space Operations Centre[93]

Rosetta began a 19 km (12 mi) descent with a 208-second thruster burn executed on 29 September 2016 at approximately 20:50 UTC.[94][95][93] Its trajectory targeted a site in the Ma'at region near an area of dust- and gas-producing active pits.[96]

Impact on the comet's surface occurred 14.5 hours after its descent manoeuvre; the final data packet from Rosetta was transmitted at 10:39:28.895 UTC (SCET) by the OSIRIS instrument and was received at the European Space Operations Centre in Darmstadt, Germany, at 11:19:36.541 UTC.[94][95][97] The spacecraft's estimated speed at the time of impact was 3.2 km/h (2.0 mph; 89 cm/s),[21] and its touchdown location, named Sais by the operations team after the Rosetta Stone's original temple home, is believed to be only 40 m (130 ft) off-target.[96] The final complete image transmitted by the spacecraft of the comet was taken by its OSIRIS instrument at an altitude of 23.3–26.2 m (76–86 ft) about 10 seconds before impact, showing an area 0.96 m (3.1 ft) across.[96][98] Rosetta's computer included commands to send it into safe mode upon detecting that it had hit the comet's surface, turning off its radio transmitter and rendering it inert in accordance with International Telecommunication Union rules.[93]

On 28 September 2017, a previously unrecovered image taken by the spacecraft was reported. This image was recovered from three data packets discovered on a server after completion of the mission. While blurry due to data loss, it shows an area of the comet's surface approximately one square meter in size taken from an altitude of 17.9–21.0 m (58.7–68.9 ft), and represents Rosetta's closest image of the surface.[98][99]

Spacecraft

[edit]

The Rosetta bus was a 2.8 × 2.1 × 2.0 m (9.2 × 6.9 × 6.6 ft) central frame and aluminium honeycomb platform. Its total mass was approximately 3,000 kg (6,600 lb), which included the 100 kg (220 lb) Philae lander and 165 kg (364 lb) of science instruments.[100] The Payload Support Module was mounted on top of the spacecraft and housed the scientific instruments, while the Bus Support Module was on the bottom and contained spacecraft support subsystems. Heaters placed around the spacecraft kept its systems warm while it was distant from the Sun. Rosetta's communications suite included a 2.2 m (7.2 ft) steerable high-gain parabolic dish antenna, a 0.8 m (2.6 ft) fixed-position medium-gain antenna, and two omnidirectional low-gain antennas.[101]

Electrical power for the spacecraft came from two solar arrays totalling 64 square metres (690 sq ft).[102] Each solar array was subdivided into five solar panels, with each panel being 2.25 × 2.736 m (7.38 × 8.98 ft). The individual solar cells were made of silicon, 200 μm thick, and 61.95 × 37.75 mm (2.44 × 1.49 in).[103] The solar arrays generated a maximum of approximately 1,500 watts at perihelion,[103] a minimum of 400 watts in hibernation mode at 5.2 AU, and 850 watts when comet operations begin at 3.4 AU.[101] Spacecraft power was controlled by a redundant Terma power module also used in the Mars Express spacecraft,[104][105] and was stored in four 10-A·h [Li-ion] batteries supplying 28 volts to the bus.[101]

Main propulsion comprised 24 paired bipropellant 10 N thrusters,[102] with four pairs of thrusters being used for delta-v burns. The spacecraft carried 1,719.1 kg (3,790 lb) of propellant at launch: 659.6 kg (1,454 lb) of monomethylhydrazine fuel and 1,059.5 kg (2,336 lb) of dinitrogen tetroxide oxidiser, contained in two 1,108-litre (244 imp gal; 293 US gal) grade 5 titanium alloy tanks and providing delta-v of at least 2,300 metres per second (7,500 ft/s) over the course of the mission. Propellant pressurisation was provided by two 68-litre (15 imp gal; 18 US gal) high-pressure helium tanks.[106]

Instruments

[edit]
Rosetta instrument inventory

Nucleus

[edit]

The investigation of the nucleus was done by three optical spectrometers, one microwave radio antenna and one radar:

  • Alice (an ultraviolet imaging spectrograph). The ultraviolet spectrograph searched for and quantified the noble gas content in the comet nucleus, from which the temperature during the comet creation could be estimated. The detection was done by an array of potassium bromide and caesium iodide photocathodes. The 3.1 kg (6.8 lb) instrument used 2.9 watts, with an improved version onboard New Horizons. It operated in the extreme and far ultraviolet spectrum, from 700–2,050 Å (70–205 nm).[107][108] ALICE was built and operated by the Southwest Research Institute for NASA's Jet Propulsion Laboratory.[109]
  • OSIRIS (Optical, Spectroscopic, and Infrared Remote Imaging System). The camera system had a narrow-angle lens (700 mm) and a wide-angle lens (140 mm), with a 2048×2048 pixel CCD chip. The instrument was constructed in Germany. Development and construction of the instrument was led by the Max Planck Institute for Solar System Research (MPS).[110]
  • VIRTIS (Visible and Infrared Thermal Imaging Spectrometer). The Visible and IR spectrometer was able to make pictures of the nucleus in the IR and also search for IR spectra of molecules in the coma. The detection was done by a mercury cadmium telluride array for IR and with a CCD chip for the visible wavelength range. The instrument was produced in Italy, and improved versions were used for Dawn and Venus Express.[111]
  • MIRO (Microwave Instrument for the Rosetta Orbiter). The abundance and temperature of volatile substances like water, ammonia and carbon dioxide could be detected by MIRO via their microwave emissions. The 30 cm (12 in) radio antenna along with the rest of the 18.5 kg (41 lb) instrument was built by NASA's Jet Propulsion Laboratory with international contributions by the Max Planck Institute for Solar System Research (MPS), among others.[112]
  • CONSERT (Comet Nucleus Sounding Experiment by Radiowave Transmission). The CONSERT experiment provided information about the deep interior of the comet using radar. The radar performed tomography of the nucleus by measuring electromagnetic wave propagation between the Philae lander and the Rosetta orbiter through the comet nucleus. This allowed it to determine the comet's internal structure and deduce information on its composition. The electronics were developed by France and both antennas were constructed in Germany. Development was led by the Laboratoire de Planétologie de Grenoble with contributions by the Ruhr-Universität Boch and the Max Planck Institute for Solar System Research (MPS).[113][114]
  • RSI (Radio Science Investigation). RSI made use of the probe's communication system for physical investigation of the nucleus and the inner coma of the comet.[115]

Gas and particles

[edit]
  • ROSINA (Rosetta Orbiter Spectrometer for Ion and Neutral Analysis). The instrument consisted of a double-focus magnetic mass spectrometer (DFMS) and a reflectron type time of flight mass spectrometer (RTOF). The DFMS had a high resolution (could resolve N2 from CO) for molecules up to 300 Da. The RTOF was highly sensitive for neutral molecules and for ions. The Max Planck Institute for Solar System Research (MPS) has contributed to the development and construction of the instrument.[116] ROSINA was developed at the University of Bern in Switzerland.
  • MIDAS (Micro-Imaging Dust Analysis System). The high-resolution atomic force microscope investigated several physical aspects of the dust particles which are deposited on a silicon plate.[117]
  • COSIMA (Cometary Secondary Ion Mass Analyser). COSIMA analysed the composition of dust particles by secondary ion mass spectrometry, using indium ions. It could detect ions up to a mass of 6500 amu. COSIMA was built by the Max Planck Institute for Extraterrestrial Physics (MPE, Germany) with international contributions. The COSIMA team is led by the Max Planck Institute for Solar System Research (MPS, Germany).[118]
  • GIADA (Grain Impact Analyser and Dust Accumulator). GIADA analysed the dust environment of the comet coma by measuring the optical cross section, momentum, speed and mass of each grain entering inside the instrument.[119][120]

Solar wind interaction

[edit]

Notable results

[edit]

Researchers expect the study of data gathered will continue for decades to come.[123][124]

Cometary activity

[edit]

On 2 July 2015, scientists report that active pits, related to sinkhole collapses and possibly associated with outbursts, have been found on the comet.[125][126] On 11 August 2015, scientists release images of a comet outburst that occurred on 29 July 2015.[127]

Magnetic field

[edit]

One of the first discoveries was that the magnetic field of 67P oscillated at 40–50 millihertz. A German composer and sound designer created an artistic rendition from the measured data to make it audible.[128] Although it is a natural phenomenon, it has been described as a "song"[129] and has been compared to Continuum for harpsichord by György Ligeti.[130] However, results from Philae's landing show that the comet's nucleus has no magnetic field, and that the field originally detected by Rosetta is likely caused by the solar wind.[131][132]

Inorganic chemistry

[edit]

New analysis of the original Rosetta data was published in November 2024 suggesting that the isotopic signature of water vapour from comet 67P is similar to that found on Earth, correcting early interpretations of data that showed a significant difference in isotopic composition between Earth's water and 67P's water.[133][134] That is, early results suggested the ratio of deuterium to hydrogen in the water from the comet was three times that found for terrestrial water; however, a re-analysis published in 2024 identified a significant measurement error that, when corrected, concluded that 67P's water isotopic composition is similar to Earth's. Thus it remains plausible that water found on Earth came from comets such as comet 67P, according to the scientists, and corroborates other deuterium-hydrogen ratio findings from Jupiter family comets.[135][136][137] On 22 January 2015, NASA reported that, between June and August 2014, the rate at which water vapour was released by the comet increased up to tenfold.[138]

On 2 June 2015, NASA reported that the Alice spectrograph on Rosetta determined that electrons within 1 km (0.6 mi) above the comet nucleus — produced from photoionization of water molecules, and not direct photons from the Sun as thought earlier — are responsible for the degradation of water and carbon dioxide molecules released from the comet nucleus into its coma.[139][140]

One of the most outstanding discoveries of the mission was the detection of large amounts of free molecular oxygen (O2) gas surrounding the comet.[141][142] A local abundance of oxygen was reported to be in range from 1% to 10% relative to H2O.[141][143]


Organic chemistry

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Previous observations have shown that comets contain complex organic compounds.[16][144][145][146] These are the elements that make up nucleic acids and amino acids, essential ingredients for life as we know it. Comets are thought to have delivered a vast quantity of water to Earth, and they may have also seeded Earth with organic molecules.[147] Rosetta and Philae searched for organic molecules, nucleic acids (the building blocks of DNA and RNA), and amino acids (the building blocks of proteins) by sampling and analysing the comet's nucleus and coma cloud of gas and dust,[147] helping assess the contribution comets made to the beginnings of life on Earth.[16]

The VIRTIS spectrometer has provided evidence of nonvolatile organic macromolecular compounds everywhere on the surface of comet 67P with little to no water ice visible.[148] Preliminary analyses strongly suggest the carbon is present as polyaromatic organic solids mixed with sulfides and iron-nickel alloys.[149][150]

Solid organic compounds were also found in the dust particles emitted by the comet; the carbon in this organic material is bound in "very large macromolecular compounds", analogous to those found in carbonaceous chondrite meteorites.[151] However, no hydrated minerals were detected, suggesting no link with carbonaceous chondrites.[150]

The Philae lander's COSAC instrument detected organic molecules in the comet's atmosphere as it descended to its surface.[152][153][154] Measurements by the COSAC and Ptolemy instruments on the Philae's lander revealed sixteen organic compounds, four of which were seen for the first time on a comet, including acetamide, acetone, methyl isocyanate and propionaldehyde.[155][156][157] The only amino acid detected thus far on the comet is glycine, along with the precursor molecules methylamine and ethylamine.[158]

Two enantiomers of a generic amino acid

One of the research tasks of Rosetta and Philae was to test hypotheses as to why essential amino acids used by terrestrial life are almost all "left-handed", which refers to their chirality, or how the atoms arrange in relation to the carbon core of the molecule.[159] Most asymmetrical molecules are oriented in approximately equal numbers of left- and right-handed configurations, and the primarily left-handed structure of essential amino acids used by living organisms is unique. One hypothesis was proposed in 1980s by William A. Bonner and Edward Rubenstein from Stanford University.[160] They conjectured that circularly polarised radiation generated by a supernova could destroy one type of chiral molecules. The other surviving molecules would then spread into space, where they could eventually end up on a planet.[161] However, the Rosetta mission couldn't contribute to this investigation, as the only amino acid it detected on the comet 67P was the non-chiral glycine.[162][163][164] Later asteroid sample return missions Hayabusa2 and OSIRIS-REx found mostly racemic (equally left- and right-handed) mixtures of amino acids on their target asteroids Ryugu and Bennu. This suggests that the selection of left-handed amino acids for life happened on Earth.[165][166][167]

Public image

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Once upon a time ... cartoon

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Cartoon versions of Rosetta and Philae as they appear in the ESA's Once upon a time... series

As part of the European Space Agency's media campaign in support of the Rosetta mission, both the Rosetta and Philae spacecraft were given anthropomorphic personalities in an animated web series titled Once upon a time.... The series depicts various stages in the Rosetta mission, involving the personified Rosetta and Philae on "a classic road trip story into the depths of our universe", complemented with various visual gags presented in an educational context.[168] Produced by animation studio Design & Data GmbH, the series was initially conceived by the ESA as a four-part fantasy-like series with a Sleeping Beauty theme that promoted community involvement in Rosetta's wake up from hibernation in January 2014. After the success of the series, however, the ESA commissioned the studio to continue producing new episodes in the series throughout the course of the mission.[168] A total of twelve videos in the series were produced from 2013 to 2016, with a 25-minute compilation of the series released in December 2016, after the end of the mission.[169] In 2019, Design & Data adapted the series into a 26-minute planetarium show that was commissioned by the Swiss Museum of Transport, and solicited to eighteen planetariums across Europe, with an aim "to inspire the young generation to explore the universe."[170]

The Rosetta and Philae characters featured in Once upon a time..., designed by ESA employee and cartoonist Carlo Palazzari, became a central part of public image of the Rosetta mission, appearing in promotional material for the mission such as posters and merchandise,[171] and often credited as a major factor in the popularity of the mission among the public.[168][172] ESA employees also role-played as the characters on Twitter throughout the course of the mission.[171][173] The characters were inspired by the JAXA's "kawaii" characters, who portrayed a number of their spacecraft, such as Hayabusa2 and Akatsuki, with distinct anime-like personalities.[174] The script for each episode of the series is written by science communicators at the European Space Research and Technology Centre, who kept close with mission operators and the producers at Design & Data.[174] Canonically, Rosetta and Philae are depicted as siblings, with Rosetta being the older sister, inspired by the spacecraft's feminine name, of Philae, her younger brother. The Giotto spacecraft is also depicted as the duo's grandfather, whereas others in the Halley Armada as well as NASA's Deep Impact and Stardust spacecraft are depicted as their cousins.[174]

Ambition

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To promote the spacecraft's arrival at comet 67P/Churyumov–Gerasimenko and the landing of Philae in 2014, a short film was produced by the European Space Agency with Polish visual effects production company Platige Image. Titled Ambition, the film, shot in Iceland, stars Irish actor Aidan Gillen, known for his roles in Game of Thrones and The Wire, and Irish actress Aisling Franciosi, also of Game of Thrones fame, and was directed by Oscar-nominated Polish director Tomasz Bagiński.[175][176] Set in the far future, Ambition centers around a discussion between a master, played by Gillen, discussing the importance of ambition with his apprentice, played by Franciosi, using the Rosetta mission as an example of such.[177][178] Ambition was premiered at the British Film Institute's Sci-Fi: Days of Fear and Wonder film festival in London on 24 October 2014, three weeks before the landing of Philae on 67P/Churyumov–Gerasimenko.[179] British science fiction author and former ESA employee Alastair Reynolds spoke about the film's message at the premiere, stating to the audience that "our distant descendants may look back to Rosetta with the same sense of admiration that we reserve for, say, Columbus or Magellan."[175] The film's conception was the result of the BFI's inquiry to the ESA for a contribution to their celebration of science fiction, with the ESA taking the opportunity to promote the Rosetta mission through the festival.[175][180]

Critical reception of the film upon its premiere was mostly positive. Tim Reyes of Universe Today complimented the titular theme of ambition in the film, stating that it "shows us the forces at work in and around ESA", and that it "might accomplish more in 7 minutes than Gravity did in 90."[177] Ryan Wallace of The Science Times also gave praise to the film, writing, "whether you're a sci-fi fanatic, or simply an interested humble astronomer, the short clip will undoubtedly give you a new view of our solar system, and the research out there in space today."[181]

Media coverage

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The entire mission was featured heavily in social media, with a Facebook account for the mission and both the satellite and the lander having an official Twitter account portraying a personification of both spacecraft. The hashtag "#CometLanding" gained widespread traction. A live stream of the control centres was set up, as were multiple official and unofficial events around the world to follow Philae's landing on 67P.[182][183] On 23 September 2016, Vangelis released the studio album Rosetta in honour of the mission,[184][185] which was used on 30 September in the "Rosetta's final hour" streaming video of the ESA Livestream event "Rosetta Grand Finale".[186]

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See also

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References

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Revisions and contributorsEdit on WikipediaRead on Wikipedia
from Grokipedia
Rosetta was a robotic probe developed and operated by the (ESA) as part of its Horizon 2000 long-term scientific programme, designed to rendezvous with, , and land on the 67P/Churyumov–Gerasimenko to study its nucleus, , and surrounding environment. Launched on 2 March 2004 aboard an rocket from , , the 2.9-tonne spacecraft featured large solar arrays spanning 32 metres to power its operations far from the Sun, marking the first such mission to rely solely on solar cells beyond Mars' . Accompanied by the Philae lander, a 100 kg module equipped for in-situ analysis, Rosetta undertook a complex 10-year journey involving gravity assists from and Mars to reach its target, arriving on 6 August 2014 after awakening from a 31-month in January 2014. The mission's primary objectives included detailed observations of the comet's composition, structure, and activity as it approached perihelion in August 2015, providing insights into the early Solar System and the potential role of comets in delivering and organic materials to . 's orbiter carried 11 scientific instruments, such as the camera system for imaging, the ROSINA mass spectrometer for gas analysis, and the CONSERT radar for internal structure probing, while Philae featured tools like the COSAC and gas chromatographs for surface sampling. On 12 November 2014, Philae made history as the first probe to land on a , though it bounced due to low and shadowed terrain, limiting operations to about 60 hours before entering ; brief contact resumed in 2015 but ended permanently in 2016. Rosetta's observations revolutionized understanding of comets, revealing 67P's double-lobed, duck-like shape likely formed by slow collision of two bodies, the presence of molecular oxygen and nitrogen in its coma—unexpected for primitive bodies—and key prebiotic molecules including glycine and phosphorus, suggesting comets contributed life's building blocks. Initial analysis of Rosetta's data found the comet's water to have a deuterium-to-hydrogen ratio about five times higher than Earth's oceans, but a 2024 reanalysis indicates it is nearly identical to Earth's, supporting the potential role of comets in delivering water to Earth. After two years of close study, including flybys and orbital insertions as low as 20 km from the nucleus, Rosetta's mission concluded on 30 September 2016 with a controlled descent to the comet's surface for final measurements of gas, dust, and plasma near the nucleus. The data collected continues to yield discoveries, affirming Rosetta as a cornerstone in cometary science, with data analysis continuing to produce new insights as of 2024.

Mission Overview

Objectives and Significance

The Rosetta mission, conducted by the (ESA), had as its primary objectives to rendezvous with and enter orbit around comet 67P/Churyumov-Gerasimenko, escort the comet through its perihelion passage, and conduct detailed observations of its nucleus and surrounding . The spacecraft was tasked with mapping the comet's irregular nucleus to determine its shape, size, surface morphology, and internal structure, while analyzing the composition of both the solid nucleus and the gaseous through and in-situ measurements. Additionally, Rosetta aimed to deploy the Philae lander onto the comet's surface for direct sampling and to investigate the interactions between the comet and the , including how solar radiation and particles influence cometary activity. These goals encompassed studying the comet's evolution as it approached the Sun, from inactive to highly active states, to unravel physical and chemical processes driving and dust ejection. The mission held profound significance for cometary science and broader , marking the first time a orbited a comet's nucleus and successfully deployed a lander to its surface, thereby enabling unprecedented close-range data collection. By providing insights into the composition and formation of comets—considered pristine remnants from the early Solar System—Rosetta contributed to understanding planetary formation processes, the delivery of water and organic molecules to , and the potential role of comets in the origins of life. Among its pioneering achievements, the mission featured the longest interplanetary cruise phase to date, exceeding 10 years, and introduced the first use of a deep-space mode to conserve power during the extended journey. It also accomplished the first comprehensive study of a comet's full activity cycle, from distant inactivity to peak perihelion outbursts, revolutionizing knowledge of cometary behavior. In historical context, Rosetta built upon earlier cometary missions such as ESA's , which provided the first close-up images of a in 1986, and NASA's Deep Impact, which excavated subsurface material from comet in 2005 to reveal internal composition. These precursors offered flyby glimpses and impact data on primitive Solar System bodies, but Rosetta advanced the field by achieving sustained orbital observations and surface landing, thereby deepening comprehension of comets as key to unlocking the Solar System's formative history.

Key Parameters and Timeline Summary

The Rosetta spacecraft, comprising the orbiter and the Philae lander, had a total launch mass of approximately 3,000 kg, including about 1,670 kg of propellant, 165 kg of scientific instruments, and the 100 kg lander. The orbiter's main body measured 2.8 by 2.1 by 2.0 meters, with solar arrays spanning 32 meters in diameter to generate up to 850 watts of power at 3.4 astronomical units from the Sun, ensuring compatibility with the G+ launcher. Propulsion was provided by a bipropellant system featuring 24 paired 10 N thrusters for trajectory corrections and attitude control. Communications relied on a 2.2-meter high-gain antenna for data transmission to Earth, supported by the for enhanced tracking during distant phases. The mission targeted Comet 67P/Churyumov–Gerasimenko, a Jupiter-family comet approximately 4 km in diameter with an orbital period of 6.45 years around the Sun and a surface gravity of about 0.2 mm/s², creating a microgravity environment. Launched on 2 March 2004 from , , aboard an G+ rocket, Rosetta traveled a total distance of 7.9 billion kilometers over its 12-year duration, collecting 220 GB of data and capturing more than 100,000 images. Key mission phases unfolded as follows: after launch, Rosetta conducted its first Earth flyby in March 2005 for a , followed by a Mars flyby in February 2007 and a second Earth flyby in 2007. It then crossed the , encountering asteroid (2867) Steins in September 2008 and (21) Lutetia in July 2010 during a third Earth flyby in 2009. Entering deep-space from June 2011 to January 2014 to conserve power, the awoke and approached the , achieving insertion on 6 August 2014. Operations peaked at perihelion on 13 August 2015, when the was closest to the Sun at 186 million km, before the mission concluded with a controlled descent to the 's surface on 30 September 2016.

Development and Preparation

Background and Planning

The Rosetta mission originated in the late 1980s as a proposed follow-up to the European Space Agency's (ESA) Giotto spacecraft, which had conducted the first close-up observations of Comet 1P/Halley in 1986 and later flew by Comet 26P/Grigg-Skjellerup in 1992, revealing key insights into cometary nuclei but leaving many questions unanswered about their composition and evolution. Building on these successes, scientists advocated for a more ambitious rendezvous mission to orbit and land on a comet, enabling in-depth study over an extended period. In November 1993, ESA's Science Programme Committee selected Rosetta as the third cornerstone mission in its Horizon 2000 long-term scientific program, designating it as a flagship planetary exploration effort with an initial target of Comet 46P/Wirtanen and a planned launch in 2003. The scientific rationale for Rosetta centered on comets as pristine "time capsules" preserving material from the solar system's formation about 4.6 billion years ago, offering clues to the origins of , on , and the delivery of organic molecules potentially linked to the emergence of life. By rendezvous with a Jupiter-family , the mission aimed to investigate the nucleus's physical and chemical properties, plasma interactions, and outgassing processes, addressing debates on whether cometary impacts contributed significantly to Earth's oceans and prebiotic chemistry. Rosetta was led by ESA in collaboration with and contributions from more than 50 industrial contractors across 14 European countries, including major roles from , , , the , and the , with around 1,000 scientists and engineers involved overall. provided key instruments such as the Alice ultraviolet imager and the Microwave Instrument for the Orbiter (MIRO), while the total mission budget amounted to 1.4 billion euros, covering development, launch, operations, and science, with an additional 220 million euros allocated to the Philae lander. Project management was handled by ESA, with prime contractor responsibilities assigned to GmbH (now ) in for overall spacecraft design, and Alenia Spazio in overseeing assembly, integration, and verification. Key planning milestones included the 1993 selection, followed by formal approval and target confirmation for Comet 46P/Wirtanen in 1999, which solidified the mission's trajectory and instrumentation suite. The Philae lander, developed by a consortium led by the German Aerospace Center (DLR) with significant contributions from the French space agency CNES, was integrated into the orbiter design during the late 1990s and early 2000s to enable surface sampling and analysis. To enhance scientific return during the interplanetary cruise, asteroid flybys of 2867 Šteins and 21 Lutetia were added to the baseline plan shortly after the 2004 launch, leveraging the mission's trajectory for opportunistic observations of main-belt asteroids.

Design and Construction

The Rosetta orbiter featured a robust box-shaped structure measuring 2.8 m × 2.1 m × 2.0 m, designed to house the scientific instruments on its upper face while providing mounting points for the high-gain antenna and Philae lander on opposite sides. To ensure reliability over the 12-year mission duration, the incorporated redundant systems, including dual chains and multiple communication pathways. Thermal control was achieved through strategically placed radiators and louvres on the shaded sides and rear panels, protecting sensitive components from extreme deep-space temperatures and potential comet dust exposure while maintaining operational temperatures between -100°C and +100°C. Power was supplied by two deployable solar array wings, each comprising five panels for a total area of 64 m² and spanning 32 m tip-to-tip, generating approximately 12 kW at 1 from the Sun using cells; the arrays were rotatable up to 180° to optimize sunlight capture during the extended cruise phases. The utilized a bipropellant configuration with 1,670 kg of fuel and tetroxide oxidizer stored in two main tanks, enabling both major trajectory corrections and fine attitude adjustments. It included 24 redundant 10 N bipropellant thrusters arranged in clusters for reaction control and delta-v maneuvers, supplemented by a pair of larger 220 N main engines for primary burns. The Philae lander, with a total mass of 100 kg including 21 kg for instruments and subsystems, was integrated directly onto the orbiter's side panel during assembly, secured by a mechanical interface that allowed for ejection and deployment at the . Designed as a compact, battery-powered unit with a primary providing up to 60 hours of autonomy for surface operations, Philae featured a carbon fibre-reinforced structure with three foldable legs equipped with anchors and ice screws to secure it to the 's surface upon . Construction of the Rosetta spacecraft involved an international led by prime contractor in , , coordinating over 50 subcontractors from 14 European countries and the . Assembly and integration occurred primarily between 1996 and 2002 at facilities managed by Alenia Spazio in , , where the orbiter and lander were mated and subsystems verified. Final testing took place at the European Space Research and Technology Centre (ESTEC) in , , including rigorous vibration simulations to replicate launch loads and thermal tests to mimic deep-space conditions, ensuring the spacecraft's endurance for the long-duration mission.

Naming and Innovations

The Rosetta mission and its spacecraft were named after the ancient , an artifact discovered in that featured inscriptions in three languages and enabled the decipherment of , symbolizing the mission's goal to "decode" the origins of the Solar System through cometary analysis. The target comet, 67P/Churyumov–Gerasimenko, received its designation from astronomers Klim Ivanovich Churyumov and Svetlana Ivanovna Gerasimenko, who independently discovered it in 1969 while observing another comet at the Alma-Ata Astrophysical Institute. The lander, Philae, was named for the River island where a bilingual was found in the , providing key Greek and hieroglyphic texts that, alongside the Rosetta Stone, aided in hieroglyphic translation. In 2003, following a launch delay from 2003 to 2004 due to technical issues with the Ariane 5 rocket, ESA selected Comet 67P/Churyumov–Gerasimenko as Rosetta's target over the original choice, Comet 46P/Wirtanen, because the latter's orbital position would no longer align with the revised mission timeline for rendezvous. This switch ensured the spacecraft could achieve the necessary trajectory for orbiting and landing on the comet by 2014, maintaining the mission's scientific objectives despite the constraints. Rosetta pioneered the use of multiple gravity-assist maneuvers for comet rendezvous, employing three flybys and one Mars flyby between 2005 and 2009 to gain the velocity and trajectory adjustments needed for its long-duration journey beyond the main , powered entirely by solar cells. To conserve energy during the distant phase of its cruise, the entered a deep-space mode for approximately 2.5 years (957 days) from 8 2011 to 20 January 2014, during which most systems were powered down, with only a minimal heater and timer active to facilitate autonomous reactivation. Additionally, Rosetta incorporated advanced autonomous operations software, including failure detection, isolation, and recovery (FDIR) systems, enabling the to independently handle faults such as those during wake-up or landing emergencies without real-time ground intervention. Among its technological firsts, Rosetta achieved high-resolution imaging of a cometary nucleus using the instrument suite, capturing detailed surface features down to millimeter scales in the challenging dusty environment, which informed orbit planning and geological studies. The mission's Rosetta Plasma Consortium (RPC) instruments provided pioneering in-situ measurements of the comet's tail and plasma interactions with the , revealing dynamic processes like acceleration and tail disconnection events. The Philae lander featured innovative components such as a (SD2) for subsurface sampling and multiple spectrometers for analyzing surface composition, marking the first on a despite subsequent anchoring challenges.

Launch and Interplanetary Cruise

Launch Sequence

The Rosetta spacecraft lifted off on 2 March 2004 at 07:17:51 UTC from the in , , aboard an G+ rocket during flight V158. The launch proceeded nominally, with separation occurring 50 seconds after fairing jettison at approximately 07:20:50 UTC and at an altitude of about 100 km. Following separation from the upper stage, Rosetta entered a with an initial velocity of around 28,800 km/h relative to , setting the stage for its interplanetary trajectory. Immediate post-launch operations focused on stabilization and activation. The entered Sun Acquisition Mode shortly after separation, detecting the Sun within two minutes and deploying its solar panels by 10:11 UTC on 2 March, restoring power from the initial battery supply. The high-gain antenna was successfully deployed on 3 March at 00:34 UTC after three test rotations, enabling reliable communication with ground stations. The first trajectory correction maneuver (TCM-1), a brief 7-minute thruster burn delivering a delta-V of about 1 m/s, was executed on 3 March at 11:49 UTC to refine the orbit. Activation and checkout phases confirmed the health of subsystems during the Launch and Early Orbit Phase (LEOP). Instrument commissioning advanced rapidly due to nominal performance, with the Navigation Camera (NAVCAM) activated on 25 July 2004 for initial tests, capturing the first images of the Earth-Moon system from approximately 240,000 km away. Minor thermal issues with thrusters and power management components arose early on, but these were resolved through operational adjustments without impacting overall functionality. By April 2004, all systems were verified as nominal, transitioning Rosetta into routine cruise mode.

Deep Space Maneuvers

Rosetta's journey to 67P/Churyumov-Gerasimenko involved a series of maneuvers to achieve the necessary velocity and trajectory adjustments over its 10-year interplanetary cruise. These flybys utilized the gravitational pull of celestial bodies to the spacecraft, conserving propellant while altering its path. The primary gravity assists included three flybys, one Mars flyby, and encounters with two asteroids, each contributing to the overall through precise trajectory corrections. The first Earth gravity assist occurred on 4 March 2005, with passing at a closest approach of 1,954 km above the , providing an initial boost following launch. This maneuver was followed by the Mars flyby on 25 February 2007, where the approached within 250 km of the planet's surface, allowing for limited scientific observations of the Martian atmosphere and surface. The second Earth flyby took place on 13 November 2007 at a distance of 5,301 km, refining the trajectory toward the outer Solar System. Subsequent asteroid encounters served dual purposes as gravity assists and scientific targets: on 5 September 2008, flew by asteroid (2867) at 800 km, and on 10 July 2010, it passed asteroid (21) at 3,162 km. The final Earth gravity assist on 13 November 2009 occurred at 2,481 km, setting the on its approach to the comet. Throughout the cruise, trajectory correction maneuvers (TCMs) were essential to fine-tune the path, executed using the main 24 N bipropellant thruster for larger adjustments and the 10 N monopropellant (RCS) thrusters for precise attitude control and smaller corrections. A notable example was TCM-7 prior to the Mars flyby, delivering a delta-V of 31.8 m/s. The cumulative delta-V from these maneuvers, including deep space maneuvers like the initial 152.8 m/s adjustment post-launch, exceeded 1.7 km/s by rendezvous, with the total propulsion budget allocated up to approximately 2.2 km/s for the entire mission. relied on a of radio tracking from ground stations for Doppler and ranging data, supplemented by optical using the onboard Navigation Camera (NAVCAM) to visually track landmarks during flybys and correct for any deviations. The flybys yielded significant scientific bonuses beyond trajectory adjustments. During the Šteins encounter, instruments captured high-resolution images and spectral data, confirming its classification as a rare E-type with a high and enstatite-rich composition, providing insights into rare achondritic meteorites. The Lutetia flyby revealed a heavily cratered surface and primitive characteristics akin to C-type asteroids, indicating it as a remnant from the early Solar System formation, with no evidence of significant metallic content despite prior M-type suggestions. These observations enhanced understanding of asteroid diversity without dedicated mission resources. Power management during the varying heliocentric distances—reaching up to 5.3 —was critical, as solar intensity dropped to about 4% of Earth's levels. The 64 m² solar arrays, equipped with advanced cells, were oriented continuously toward the Sun via attitude control to maximize energy capture, with periodic adjustments ensuring optimal illumination despite the spacecraft's spin-stabilized cruise mode. This configuration supported essential and occasional instrument operations, culminating in a planned phase to conserve power at greater distances.

Early Operations and Hibernation

During the interplanetary cruise phase following its deep space maneuvers, the Rosetta spacecraft maintained operational health through periodic checkouts of its subsystems and instruments, as well as targeted software updates transmitted from ground control at the (ESOC). These activities, conducted roughly every six months, involved activating select payloads for performance verification and anomaly resolution without full system engagement, helping to preserve the limited power available from solar arrays at increasing distances from the Sun. Fuel conservation was a primary objective, with thruster firings minimized to reserve —estimated at around 160 kg remaining by —for the demanding comet rendezvous and orbiting phases ahead. To further optimize power usage as Rosetta ventured beyond 4 AU from the Sun, where solar illumination dropped to less than 5% of Earth's levels, the spacecraft entered deep-space mode on 8 June 2011, at approximately 3.7 AU (549 million km) heliocentric distance. In this mode, nearly all systems were powered down, including scientific instruments, communication transponders, and most heaters, leaving only the main computer clock, a minimal control setup, and the solar arrays active to prevent battery degradation and structural damage from extreme cold (down to -150°C). The hibernation period lasted 957 days, allowing Rosetta to coast silently toward its target while reaching an aphelion of 5.3 AU in 2012, the farthest solar-powered mission to date. The wakeup sequence was autonomously initiated by an onboard timer on 20 January 2014, as Rosetta approached 4.5 AU (673 million km) from the Sun and sufficient became available. Ground controllers at ESOC received the confirmation signal about 45 minutes later, from a distance of about 800 million km to , verifying that the had successfully reactivated its telecommand receiver and begun warming up. Over the following weeks, systems were progressively brought online: by late January, entered for initial diagnostics; full checkouts and instrument commissioning occurred through and , restoring nominal operations by early 2014. Post-hibernation trajectory corrections, including four mid-course maneuvers starting in , fine-tuned the path for comet arrival, adjusting velocity by about 0.6 m/s total. Hibernation carried inherent risks, including potential failure of the autonomous wakeup due to , on electronics, or unrecoverable faults in the power subsystem, which could have ended the mission prematurely without real-time ground intervention possible. To mitigate these, pre-hibernation testing in May-June 2011 validated the onboard software, enabling self-diagnostic and recovery sequences in case of partial failures during reactivation; redundancies like dual computers and backup timers were also confirmed operational. No major issues arose, but the 31-month silence heightened tension at ESOC, as a failed wakeup would preclude the rendezvous.

Arrival and Operations at Comet 67P

Approach and Orbit Insertion

Rosetta's approach phase to Comet 67P/Churyumov-Gerasimenko began following its reactivation from on 20 January 2014, with the spacecraft gradually reducing its distance from the target over several months. By May 2014, Rosetta was approximately 1 million km from the comet, executing a series of thruster burns to match the comet's and slow its relative velocity from hundreds of meters per second to near zero. The final leg of the approach, from about 9 million km in January 2014 to rendezvous, involved precise corrections to account for the comet's orbit and increasing outgassing activity, culminating in arrival on 6 August 2014 at a distance of 100 km. During this phase, initial revealed the comet's unexpectedly irregular, bilobate structure, with the first detailed images from the instrument on 25 July 2014 clearly showing its distinctive "rubber duck" shape, consisting of two lobes connected by a narrow . Navigation during the approach presented significant challenges due to the comet's faint radio signal at large distances, necessitating reliance on optical using the spacecraft's navigation camera (NAVCAM) for trajectory updates and landmark tracking. As Rosetta closed in, the growing of dust and gas posed risks of collision with unseen particles, requiring real-time monitoring and contingency maneuvers to maintain safe separation while refining the comet's . These efforts ensured the could safely transition to proximity operations without impacting the fragile nucleus. On 10 September 2014, Rosetta achieved the historic milestone of insertion around Comet 67P, becoming the first spacecraft to establish a around a . The insertion maneuver involved a main burn delivering a delta-V of approximately 0.9 m/s, placing the orbiter at an initial altitude of 29 km above the surface. This low-energy insertion minimized fuel use while allowing close-range observations, marking the start of extended orbital studies. Initial mapping efforts immediately followed insertion, utilizing the wide-angle camera (WAC) for contextual views of the coma and narrow-angle camera (NAC) for high-resolution surface imaging. These observations confirmed the nucleus's rotation period of 12.4 hours and detected localized patterns, with (H₂O) first identified on 6 June 2014 during the approach, indicating active sublimation even at 3.6 AU from the Sun. The data provided essential context for subsequent safe orbital adjustments and instrument calibration.

Mapping and Orbiting Phases

Following its arrival at Comet 67P/Churyumov-Gerasimenko in August 2014, the orbiter executed a series of orbital strategies designed to balance scientific with operational amid increasing cometary activity. These included close orbits at altitudes of 10–30 km to enable detailed and in-situ measurements, bound elliptical orbits that allowed repeated passes over specific surface regions, and targeted fly-throughs that brought the within 5 km of the nucleus for high-resolution . To mitigate risks from dust particles and thermal stresses, also adopted safe "terminator" orbits, positioned along the day-night boundary plane at distances of 100–140 km, which minimized exposure to high-velocity and solar heating. The mission's mapping campaigns progressed in phases to systematically characterize the comet's irregular, bilobate nucleus, spanning approximately 4 km in length. Initial global mapping occurred from orbital heights of around 50 km, providing broad coverage of the entire surface and identifying major geological boundaries. Subsequent regional mapping at 20 km focused on key areas like the and regions, revealing diverse terrains such as smooth plains and pitted surfaces. High-resolution campaigns at 5 km or closer achieved detailed imaging of about 90% of the nucleus, delineating 26 distinct regions named after Egyptian deities and enabling the creation of 3D shape models with resolutions down to meter-scale features. As Comet 67P approached perihelion from 3.6 AU in March 2014 to 1.24 AU on 13 August 2015, Rosetta's orbits facilitated continuous monitoring of cometary activity, including the mapping of gas and dust jets emanating from active regions like Hapi and Anhur. The spacecraft observed multiple outburst events—sudden, intense releases of material—such as those on 29 July 2015 and 19 February 2016, which were characterized by rapid expansions of dust plumes traveling at speeds up to 10 m/s. These observations tracked the evolution of jet sources and their with surface features, providing insights into sublimation-driven processes without delving into specific compositional analyses. Throughout the escort phase, Rosetta performed over 100 trajectory adjustment maneuvers using its bipropellant thruster system to maintain desired orbits and respond to the comet's variable gravity field and torques. These operations, including delta-V corrections of up to 1 m/s per , were carefully planned to conserve , with onboard monitoring ensuring sufficient reserves—approximately 170 kg at arrival—for the extended mission until 2016. Fuel usage was tracked via gauges and data, allowing extensions to closer approaches in the low-activity tail phase.

Reaction Control System Challenges

The Reaction Control System (RCS) of the Rosetta spacecraft comprised 24 bipropellant thrusters, each delivering 10 N of thrust, arranged in two redundant branches of 12 thrusters each for three-axis attitude control and precise trajectory corrections essential to maintaining spacecraft orientation and orbital stability during interplanetary cruise and comet operations. The system utilized monomethylhydrazine (MMH) as fuel and dinitrogen tetroxide (N₂O₄) as oxidizer, stored in separate tanks and pressurized by helium gas to ensure reliable propellant delivery across the mission's demanding thermal and dynamic environments. A significant anomaly emerged in August 2006, when a transducer (PT2) in the RCS helium pressurization line registered an unexpected drop to 0 bar, signaling a leak likely originating in the segment, possibly due to a pyrovalve malfunction though not definitively confirmed. This issue persisted and was further verified during a dedicated RCS test on 9 2010, which pinpointed the leak in an unisolable section of the helium plumbing, preventing isolation or repair. By the spacecraft's arrival at Comet 67P in August 2014, the cumulative effect of the ongoing leak had reduced helium to approximately 6.7–7.5 bar—well below the nominal 17 bar operational range—necessitating a shift to blow-down mode, where thrusters relied solely on residual without active repressurization. The degraded RCS performance manifested in several operational challenges, particularly during the close-proximity phases at the , where er output became noisy and inconsistent in pulsed mode, leading to attitude drifts that compromised precise for scientific instruments and heightened collision risks during low-altitude orbits as low as 20 km. These drifts occasionally resulted in unplanned rotational excursions, reducing available time for observations and increasing power consumption as reaction wheels and auxiliary systems compensated for the unreliable . Additionally, anomalous in the associated reaction wheels exacerbated steering difficulties, further straining the system's ability to maintain stability amid the comet's variable and torques. To mitigate these issues, the European Space Agency's (ESA) ground team conducted extensive simulations and thruster tests to characterize performance at low pressures, enabling the development of updated software models and control algorithms that optimized durations and firing sequences for blow-down conditions. Planned repressurization in January 2011 was canceled to avoid exacerbating the leak, with operations instead adapted to conserve by delaying the post-hibernation rendezvous maneuver by about one week and repurposing unspent fuel from earlier phases for thermal regulation of the tanks. Thrust usage was minimized through refined trajectory planning, prioritizing larger continuous burns over frequent small corrections to enhance efficiency despite the 20–30% reduction in . These interventions ensured the RCS remained functional without compromising core mission objectives, including safe Philae lander deployment and extended mapping. By mid-2016, confirmed the leak had stabilized with no additional degradation, supporting the decision to extend operations beyond the original December 2015 endpoint until the controlled end-of-mission descent in September.

Philae Lander Mission

Lander Design and Instruments

The Philae lander featured a compact, box-shaped measuring approximately 1 m × 0.8 m × 0.8 m, with a total mass of 100 kg, including 21 kg for its scientific . Its structure consisted of a rigid baseplate, an instrument platform, and a polygonal sandwich of carbon fiber reinforced plastic panels, protected by a deployable aluminum hood covered in solar cells for power generation. The lander was powered primarily by a 21 Ah non-rechargeable battery for initial operations, supplemented by solar panels capable of recharging a secondary battery during extended surface activities. For secure attachment to the comet surface, it incorporated three foldable landing legs equipped with ice screws at the feet and a pair of harpoons fired from the base to embed into the subsurface. Philae carried ten scientific instrument packages to investigate the comet's surface composition, structure, and environment. Key among these were the Cometary Sampling and Composition (COSAC) experiment, a gas chromatograph and mass spectrometer for analyzing volatile and organic compounds in surface and subsurface samples; the Ptolemy instrument, an evolved gas analyzer using mass spectrometry to measure isotopic ratios of light elements like hydrogen and oxygen; the Multi-Purpose Sensors for Surface and Sub-Surface Science (MUPUS), a probe for probing thermal and mechanical properties through penetration and temperature measurements; the Rosetta Lander Magnetometer and Plasma Monitor (ROMAP), combining a magnetometer and accelerometer to study magnetic fields, plasma, and acceleration during landing; the Comet Infrared and Visible Analyser (CIVA), providing panoramic imaging, microscopic analysis, and infrared spectroscopy of the surface; and the Rosetta Lander Imaging System (ROLIS), a descent camera for high-resolution optical imaging to characterize surface morphology. Additional instruments included the Alpha Particle X-ray Spectrometer (APXS) for elemental analysis, the Comet Nucleus Sounding Experiment by Radiowave Transmission (CONSERT) for internal structure mapping, the Surface Electrical, Seismic and Acoustic Monitoring Experiment (SESAME) for subsurface sounding and dust detection, and the Sampling, Drilling, and Distribution (SD2) subsystem. Design innovations enabled Philae to operate semi-autonomously on the comet's low-gravity surface, with onboard for execution and fault recovery in the absence of real-time control from . The SD2 system represented a core innovation, capable of extracting samples up to 20 cm deep and distributing them via a mechanism to ovens in COSAC, , and CIVA for thermal desorption and analysis, allowing in-situ study of subsurface materials without human intervention. Communication occurred exclusively through a UHF radio link with the Rosetta orbiter, which relayed data to at rates up to 16 kbit/s, ensuring all operations depended on the parent spacecraft's proximity and visibility. The lander was developed by an international consortium led by the (DLR) and the French space agency (), with contributions from institutions in (ASI), the , and other European countries. Integration with the Rosetta orbiter occurred in 2003 at the facility in , , where Philae was mounted on the orbiter's side panel using a deployment mechanism tested for microgravity conditions. Pre-launch testing included vibration simulations, thermal vacuum chamber runs, and pyrotechnic separation trials to verify the lander's readiness for the 10-year cruise and comet rendezvous.

Deployment and Landing Sequence

On 12 November 2014, the Philae lander separated from the Rosetta orbiter at 08:35 UTC while the spacecraft was positioned approximately 22.5 km above the center of 67P/Churyumov–Gerasimenko, initiating a passive, unpowered descent expected to last about seven hours. The separation was confirmed shortly after by ground stations, marking the start of the first-ever attempt to soft-land on a . During the descent, Philae's instruments actively monitored the comet's environment, with the CIVA (Comet Infrared and Visible Analyser) camera capturing a series of images of the approaching surface at the planned Agilkia landing site, starting from an altitude of about 67 m and resolving down to 9 m. Simultaneously, the CONSERT (Comet Nucleus Sounding Experiment by Radiowave Transmission) instrument on both Philae and provided ranging data to track the lander's position until roughly 50 minutes before touchdown, while 's navigation cameras also imaged Philae's trajectory. These observations revealed a rugged, uneven with slopes steeper than anticipated, confirming deviations from pre-mission models. Philae made first contact with the comet's surface at 15:34:04 UTC at the Agilkia site, slightly offset from the target by about 112 m, but the anchoring harpoons failed to deploy, and a intended to press the lander down malfunctioned, causing an immediate rebound estimated at up to 1 km in height. The lander then traveled for approximately two hours before a second brief touchdown around 17:26 UTC at a site later identified as Abydos, followed by a short additional bounce and final settling at 17:31:17 UTC in a tilted orientation within a shadowed crevice. Sensors on Philae's feet recorded the initial impact vibrations, indicating a hard, icy surface with variable texture, while post-contact CONSERT signals from helped triangulate the unexpected final location. In the immediate aftermath, Philae's battery levels remained nominal, allowing initiation of surface science activities, but the anchoring failure resulted in an unstable position—tilted at about 30 degrees with one leg elevated and the solar panels partially obscured by shadows—which limited power generation and orientation for instruments. Confirmation of the bounces and terrain challenges came from real-time telemetry and later analysis of descent images, highlighting the lander's resilience despite the unplanned trajectory.

Surface Operations and Contact Loss

Following its final touchdown on 12 November 2014 at the Abydos site on Comet 67P/Churyumov–Gerasimenko, the Philae lander initiated its primary 60-hour science mission, known as the First Science Sequence (FSS), which lasted approximately 56 hours and 28 minutes despite the unexpected orientation and limited sunlight exposure. The lander activated several instruments, including the CIVA camera system, which captured panoramic images of the shadowed, uneven terrain revealing a mix of dust, rocks, and ice particles. The MUPUS probe attempted to penetrate the surface with its hammer mechanism to measure subsurface thermal and mechanical properties, but the deployment failed due to the unexpectedly hard icy crust just a few centimeters below the soft upper layer, limiting penetration to only about 9 cm via the rod alone. Meanwhile, the COSAC instrument operated in sniffing mode to analyze ambient volatiles, detecting confirmed organic compounds such as acetaldehyde, along with others including methylamine and acetone, hints of water ice in the porous surface material. Data from these operations, totaling around 13.88 MB, was relayed to the Rosetta orbiter via short UHF bursts during the limited communication windows when the lander was in view, achieving approximately 80% of the planned first science sequence goals despite the challenges. Eight of Philae's ten instruments successfully collected data on surface composition, , and magnetic properties, providing initial insights into the comet's heterogeneous structure before the primary battery depleted. Contact with Philae was lost on 15 November 2014 at 00:02 UTC when the primary batteries ran out after just over two days of operations, forcing the lander into or hibernation due to insufficient from its tilted panels in the shaded location. Intermittent communication resumed in 2015 as the approached perihelion and increased; signals were received from 13 to 9 July, allowing brief data transmissions and attempts to reactivate instruments, though limited by the lander's orientation. Efforts to re-establish contact continued through January , including commands relayed via the orbiter to activate the for potential repositioning, but no further responses were obtained after the final loss in July 2015, attributed to overheating near perihelion and the lander's awkward pose. In , 's camera imaged Philae's approximate location in a dark crevice on the 's surface, confirming its wedged position but ruling out further recovery.

Scientific Instruments

Orbiter Instruments by Category

The Rosetta orbiter carried 11 scientific instruments, plus the NavCam, grouped into categories based on their primary roles in investigating the comet's nucleus, gaseous and particulate environment, interactions with the , and shared multi-purpose functions. These instruments enabled , in-situ analysis, and plasma measurements to elucidate the comet's physical structure, composition, and dynamic processes.

Nucleus Category

Instruments dedicated to the nucleus provided high-resolution imaging, spectroscopic mapping, and thermal profiling to characterize the comet's surface morphology, , and subsurface properties. The Optical, Spectroscopic, and Infrared Remote Imaging System () consisted of narrow- and wide-angle cameras that captured detailed optical images of the nucleus, revealing its shape, craters, and dust features at resolutions down to centimeters per pixel. The Visible and InfraRed Thermal Imaging Spectrometer (VIRTIS) performed visible and near-infrared mapping to identify surface compositions, including ices and organics, while also measuring thermal emissions for temperature distribution analysis. The Ultraviolet Imaging Spectrometer measured ultraviolet emissions (70–205 nm) from the nucleus and to assess and surface volatiles. The Microwave Instrument for the Rosetta Orbiter (MIRO) used millimeter- and submillimeter-wave to detect , , and subsurface temperatures, aiding in understanding heat transport and activity drivers.

Gas and Particles Category

This category encompassed instruments for analyzing the coma’s neutral gases, ions, and grains to quantify rates, chemical abundances, and particle dynamics. The Rosetta Orbiter Spectrometer for Ion and Neutral Analysis (ROSINA) featured double-focusing mass spectrometers and a pressure sensor to identify and quantify neutral and ionic species, such as , , and complex organics, in . The Cometary Secondary Ion Mass Analyser (COSIMA) collected and analyzed particles via secondary ion mass spectrometry, determining their mineral and organic content at the molecular level. The Grain Impact Analyser and Dust Accumulator (GIADA) measured the size, speed, and momentum of grains using light-scattering and impact detection, tracking flux variations with comet activity. The Micro-Imaging Dust Analysis System () employed to image individual particles at nanometer resolution, examining their microtexture and aggregation states.

Solar Wind Interaction Category

Instruments in this group monitored plasma, , and energetic particles to investigate how the comet's environment interacts with incoming . The Rosetta Plasma Consortium (RPC) suite, comprising multiple sensors including the Ion Composition Analyser (ICA), (MAG), and Ion and Electron Sensor (IES), characterized low-energy , fluctuations, and energetic particles in the plasma, distinguishing from cometary to map interaction boundaries and the induced .

Shared Category

Multi-purpose instruments supported nucleus interior probing and overall navigation with scientific utility. The Comet Nucleus Sounding Experiment by Radiowave Transmission (CONSERT) transmitted radio signals through the between orbiter and lander to perform , estimating constants and internal structure. The Radio Science Investigation (RSI) utilized the spacecraft's radio telecommunication system to measure the comet's mass and gravity field, infer internal structure, and analyze coma density through signal propagation effects. The Navigation Camera (NavCam) provided wide-field black-and-white images for spacecraft orientation but also contributed to scientific imaging of the surface, enabling studies of morphology and outbursts.

Instrument Operations and Calibration

The instruments aboard the Rosetta orbiter were calibrated through a combination of pre-launch ground testing and in-flight procedures to ensure precise measurements of the comet's environment. Pre-launch calibrations involved comprehensive ground tests for each instrument, including spectral, geometric, radiometric, and flat-field assessments; for instance, the Visible and InfraRed Thermal Imaging Spectrometer (VIRTIS-M) underwent testing with monochromators, Hg and QTH lamps, and blackbodies at temperatures from 350–690 K to derive responsivity matrices and central wavelengths, achieving spectral sampling intervals of 1.884 nm per band in the visible channel and 9.448 nm per band in the infrared channel. In-flight calibrations utilized known celestial sources such as stars and asteroids to monitor and adjust instrument performance; the Optical, Spectroscopic, and Infrared Remote Imaging System () narrow-angle camera, for example, achieved radiometric accuracy of approximately 1–1.7% in visible and near-infrared wavelengths through observations of asteroid Vesta and internal cross-camera comparisons. Cross-calibration between instruments further refined data consistency, as demonstrated by the alignment of radiometric factors between the Navigation Camera and OSIRIS narrow-angle camera using overlapping stellar fields, which yielded multiplicative correction factors with uncertainties below 5%. Instrument operations were tailored to the mission's progression, employing diverse modes to optimize data collection across phases. During initial flybys of asteroids and , remote sensing modes dominated, with instruments like and VIRTIS capturing wide-field spectral and imaging data from distances exceeding 1000 km to characterize surface compositions and photometry. Upon rendezvous with comet 67P/Churyumov-Gerasimenko in 2014, operations shifted to close-range configurations during orbiting phases, enabling high-resolution in-situ sampling by instruments such as the Grain Impact Analyzer and Dust Accumulator (GIADA) and the Rosetta Orbiter Spectrometer for Ion and Neutral Analysis (ROSINA) at altitudes as low as 20 km. Specialized burst modes were activated for transient events like cometary outbursts, allowing coordinated, high-cadence observations; for example, during the February 19, 2016, outburst, nine instruments simultaneously recorded elevated gas and dust fluxes in short-duration sequences to capture the rapid evolution of activity. Following pressure anomalies detected in mid-2014, power prioritization was implemented, favoring essential and plasma instruments while cycling others to conserve the spacecraft's limited energy margins during extended low-activity periods. Mission adaptations ensured instrument reliability amid evolving cometary conditions, incorporating software refinements and operational constraints. Software updates were uploaded to address dust accumulation on optical surfaces, particularly for , by enhancing image processing algorithms to correct for and in observations. Near perihelion in August 2015, when solar distances reached 1.24 AU and dust activity peaked, instrument operations were scaled back—such as limiting exposure times for VIRTIS and safing heat-sensitive sensors—to mitigate risks from elevated temperatures and particle fluxes exceeding 10 particles per cubic meter. Data management included onboard compression techniques, reducing raw science volumes through lossless algorithms to facilitate downlink of key datasets via the 8 cm high-gain antenna, with daily dumps ranging from 2 to 6 Gbit during active phases. Operational challenges necessitated proactive responses to maintain , including anomaly handling and environmental interferences. Instruments were routinely safed—powered down or placed in protective modes—during spacecraft anomalies, such as unexpected attitude drifts or solar conjunctions, to prevent ; this procedure was invoked over a dozen times between 2014 and 2016, restoring full operations within hours via ground commands. For GIADA, dust flux measurements were particularly challenged by particle variability, with impacts ranging from compact grains (speeds up to 50 m/s) to fluffy aggregates, leading to intermittent detector saturation and requiring post-processing corrections based on velocity distributions derived from complementary RPC plasma data. These adaptations and mitigations ultimately enabled the suite to deliver coherent, calibrated datasets spanning the comet's inbound and outbound orbits.

Scientific Discoveries

Comet Nucleus Characterization

The nucleus of comet 67P/Churyumov-Gerasimenko, as revealed by Rosetta's imaging system, exhibits a distinctive bilobate structure resembling a , consisting of a larger "body" lobe and a smaller "head" lobe connected by a narrow neck region known as Hapi. The overall dimensions along the principal axes measure approximately 4.3 km × 2.6 km × 2.1 km, with the body lobe spanning 4.1 km × 3.5 km × 1.6 km and the head lobe 2.5 km × 2.1 km × 1.6 km. High-resolution shape models derived from stereophotogrammetry yielded a total volume of 18.8 ± 0.3 km³, with the body comprising about 66% and the head 27%, while the neck contributes roughly 7%. Combined with mass measurements from the Rosetta radio science experiment, this volume implies a of 532 ± 7 kg/m³, indicating a highly porous interior consistent with primordial formation processes. Surface features mapped across the nucleus highlight a complex geological history, including steep cliffs, expansive pits, scattered boulders, and layered terrains suggestive of subl layered deposition or . Notable examples include the cliff in the region, a 900 m-high with rectilinear lineations and alcoves indicating fracturing and ; the region's 210 m-diameter, 170 m-deep pit, which exhibits brittle failure and dust emission activity; and the depression on the body lobe, an irregular basin of ~0.12 km³ volume strewn with boulders up to 30 m in size. The Hapi neck features smoother, dust-covered plains with seasonal thickness variations, while consolidated terrains like Aker show angular fractures exceeding 200 m and smooth patches 50–100 m across, pointing to tectonic-like stresses from rotation or . Boulders ≥7 m follow a power-law size distribution with index -3.6, and pinnacles 10–200 m high in regions like suggest sublimation-driven . Layered structures in areas such as indicate episodic deposition, with polygonal fractures on a 650 m-wide mesa. The surface composition is dominated by a dark, dust mantle covering most of the nucleus, with a of 4–6% at visible wavelengths (6.5 ± 0.2% at 649 nm globally, rising to ~16% in ice-rich Hapi). This low arises from a mix of ~45% organic-rich (including aliphatic hydrocarbons and polyaromatic compounds) and ~55% minerals (silicates and iron sulfides like ), forming a porous up to several meters thick in plains like , where impact craters reveal underlying layers. Water ice exposures are rare and localized, comprising less than 1% of the surface area, often appearing as bright patches or boulders in scarps (e.g., 1–3 μm grains in Hapi, up to 48% abundance in small Anhur-Bes exposures) with no detection of crystalline ice phases. These icy features, observed via and VIRTIS, show diurnal cycles and long-term stability in shadowed areas, but are quickly obscured by redeposition. Interior probing by the CONSERT radar experiment, using bistatic signals between Rosetta and the Philae lander, revealed a low constant with real of 1.27 ± 0.05, implying 75–85% and a dust-to-ice of 0.4–2.6 by . This suggests a homogeneous of porous -dust aggregates (6–12% ice, 16–21% refractories) at scales of ~3 m, with no significant scattering or contrasts exceeding 0.25, excluding large voids or dense inclusions larger than a few meters. Refinements to the rotation axis (obliquity ~52°) and period (12.4041 ± 0.0004 hours) from and RSI data further support a low-density, elongated body with minimal mass concentration.

Gas, Dust, and Activity Analysis

The Rosetta mission's analysis of gas emissions from comet 67P/Churyumov-Gerasimenko revealed a dominated by (H₂O), which constituted approximately 80% of the total gas production, alongside (CO₂) at 10–15% and (CO) at 3–6%, with the remainder comprising complex organics and other volatiles. The ROSINA instrument detected over 40 distinct molecules in the , including hints of , the simplest , alongside precursors like and , indicating a diverse volatile inventory driven by sublimation from the nucleus surface. These compositions exhibited strong spatial and temporal heterogeneities, with CO₂ often peaking in the due to its lower sublimation temperature compared to H₂O. Dust particles in ranged from submicron sizes (around 1 μm) to several centimeters, characterized as porous, fluffy aggregates with low densities, facilitating their entrainment into the gas flow. The total dust-to-gas mass ratio was estimated at approximately 4, reflecting a dust-rich environment where larger grains dominated the . Ejection velocities reached up to 50 m/s, primarily influenced by gas drag from sublimating ices, with GIADA and observations confirming that smaller particles accelerated more rapidly near active regions. Cometary activity manifested through localized outbursts and collimated jets, notably from the region on the comet's large lobe, where sudden increases in gas and production were observed, such as the prominent July 29, 2015, event that altered the coma composition temporarily. Overall activity peaked at perihelion (1.24 AU in August 2015), with gas production rates scaling inversely with heliocentric distance, showing seasonal variations as different facets rotated into sunlight; for instance, water production surged by factors of 100 from 3 AU inbound to perihelion. Models of particle entrainment emphasized sublimation-driven lift-off of from the nucleus, with no for cryovolcanism; a thin mantle, estimated at 10–20 cm thick in active areas, regulated by insulating underlying ices.

Organic Compounds and Astrobiological Implications

The Rosetta mission's instruments, particularly the Rosetta Orbiter Spectrometer for Ion and Neutral Analysis (ROSINA) and the Cometary Sampling and Composition (COSAC) experiment on the Philae lander, identified over 20 carbon-bearing molecules in the coma and surface of comet 67P/Churyumov-Gerasimenko. ROSINA detected volatile organics such as glycine—the simplest amino acid—along with methylamine, ethylamine, and various hydrocarbons, through repeated measurements in the comet's atmosphere during perihelion passages. COSAC, during Philae's brief surface operations in November 2014, confirmed the presence of organics at the landing site in the Abydos region, identifying 16 compounds including methyl isocyanate (a precursor to amino acid synthesis), propionaldehyde, and acetone via gas chromatography-mass spectrometry of ambient gases. These detections highlighted a diverse inventory of simple and complex carbon-based species, with hydrocarbons comprising aliphatic chains and aromatics. A 2025 untargeted investigation of ROSINA data revealed additional nitrogen- and nitrogen-oxygen-bearing complex organic molecules (e.g., of general formulae C_n H_m N and C_n H_m NO), further enriching the comet's organic repertoire. Analysis of dust grains by the Comet Microscopic Imager (COSIMA) and other instruments revealed that organics constitute 25–45% of the comet's nucleus mass, forming a significant portion of the non-volatile material alongside silicates and oxides. These insoluble organic macromolecules exhibit spectral and compositional similarities to the insoluble in carbonaceous chondrites, such as those in the , including high carbon content and hydrogen-to-carbon ratios around 1.0–1.2, suggestive of formation through ultraviolet irradiation of interstellar precursors in the protosolar disk. The fraction's dominance underscores the comet's role as a preserved of primitive solar system organics, with minimal aqueous alteration compared to meteorites. From an astrobiological perspective, the presence of prebiotic molecules like and in 67P supports hypotheses of cometary delivery of organics to the during the , potentially seeding hydrothermal vents or oceans with building blocks for . However, the low abundance of appearing at levels below 1% relative to in —indicates that comets may have played a supplementary rather than primary role in 's origins, with endogenous synthesis on likely more significant. Initial detections in 2014–2015 from Philae's landing provided tentative evidence of surface organics, but subsequent analyses from 2016–2020, including reprocessed ROSINA spectra, confirmed the inventory without evidence of chiral bias in ; , being achiral, showed no enantiomeric preference, and no other chiral were unambiguously identified, consistent with abiotic synthesis pathways.

Solar Wind and Plasma Interactions

The Rosetta Plasma Consortium (RPC) suite of instruments on the orbiter provided detailed in-situ measurements of the plasma environment surrounding 67P/Churyumov-Gerasimenko, capturing densities on the order of 10–100 per cubic centimeter near the nucleus and flows influenced by and pickup processes. These observations revealed a dynamic plasma tail extending thousands of kilometers, with cold cometary dominating the inner and protons penetrating closer to the nucleus during low activity phases. A key feature identified was the formation of a weak approximately 80 km from the nucleus during periods of enhanced at heliocentric distances near 2 AU, marking the boundary where plasma slows and compresses due to mass loading from newly ionized cometary neutrals. Magnetic field measurements from the RPC-Magnetometer (MAG) demonstrated the draping of the interplanetary lines around the comet's induced , with field strengths increasing from typical values of 20–50 nT to up to 100 nT in draped regions due to pile-up effects. No intrinsic was detected within the nucleus, confirming the absence of a permanent ; instead, transient induced fields were generated by the expansion of outgassing neutrals, which diamagnetically expel and create cavity-like structures up to several hundred kilometers in scale. These draping patterns evolved with the comet's orientation relative to the flow, forming nested field lines that guide plasma transport. Theoretical models of the comet-solar wind interaction, informed by RPC data, describe the pickup of water-group ions (primarily H₂O⁺) by the convective in the comet's frame, where exospheric neutrals are ionized and accelerated to speeds, leading to mass loading and deflection of the incoming flow. This process transfers momentum and energy from the to the cometary plasma, resulting in heating of pickup ions to keV energies and the generation of emissions through charge exchange reactions between highly charged ions (e.g., O⁶⁺, O⁷⁺) and neutral cometary atoms, producing soft s in the 0.3–1 keV range observable from Earth-based telescopes. Hybrid particle-in-cell simulations validated these mechanisms, reproducing observed asymmetries in ion distributions and field perturbations by treating ions kinetically while modeling electrons as a . The nature of these interactions varied significantly over the mission: pre-perihelion, at heliocentric distances greater than 2 AU, weak led to diffuse plasma boundaries and minimal deflection of the , with pickup ions forming ring-like velocity distributions. Post-perihelion, as the comet approached 1.2 AU in August 2015, intensified activity created a more pronounced with stronger draping and occasional current sheets, where hybrid models showed enhanced mass loading slowing the by up to 50% within 100 km of the nucleus. These temporal changes highlighted the comet's response to solar proximity, with comparisons to hybrid simulations confirming the role of neutral density gradients in shaping the plasma boundaries.

Mission Conclusion and Legacy

End of Mission Descent

The decision to conclude the Rosetta mission with a controlled descent was driven by the achievement of primary scientific objectives following the comet's perihelion passage in August 2015, combined with the spacecraft's approaching fuel depletion after over 12 years of operations, including extensive exposure to the comet's dusty environment that posed ongoing hazards to the orbiter's systems. By September 2016, Rosetta had depleted most of its propellant, limiting further orbital maneuvers, while cumulative dust accumulation had aged instruments and solar panels, increasing operational risks even as cometary activity waned post-perihelion. Additionally, the impending solar conjunction in October 2016 would interrupt communications for weeks, and the comet's increasing distance from the Sun was reducing available solar power. ESA selected 30 September 2016 as the optimal end date to maximize final science returns without endangering the spacecraft in uncontrolled orbits. The descent began on 29 September 2016 at 20:50 UTC, when , orbiting at approximately 20 km altitude, executed its final collision course maneuver using the last of its fuel to set a toward the Ma'at on the comet's small lobe. Over the next 14 hours, the spacecraft entered a free-fall phase without additional thruster firings to avoid contaminating scientific measurements, allowing all operational instruments—except COSIMA, , and VIRTIS—to collect data on the comet's surface, gas, dust, and plasma environment during the approach. The targeted impact site was a 700 by 500 meter near active pits in Ma'at, selected for its scientific value in observing dust jet sources. During the final minutes, the narrow-angle camera captured high-resolution images of the rugged terrain, with the last image acquired at an altitude of 23–26 meters above the surface (initially estimated at 51 meters based on predicted timing). Concurrently, the ROSINA instrument recorded the final in-situ measurements of cometary gases, providing a snapshot of the local environment just before contact at 11:19 UTC on 30 September 2016. No thrusters were fired during to preserve pure scientific data, ensuring the orbiter's impact remained around 0.9 meters per second. Signal loss was confirmed at ESA's in , , at 11:19 UTC, as the spacecraft's antenna tilted away from upon surface contact, marking the mission's end after transmitting 220 GB of data overall. Ground teams monitored the final telemetry in real-time, celebrating the successful closure with applause as the signal flatlined on displays. Immediately afterward, operations transitioned to archiving the complete dataset at the European Space Astronomy Centre, ensuring long-term accessibility for ongoing analysis.

Data Legacy and Ongoing Analysis

The Rosetta mission generated approximately 220 GB of scientific data, which is publicly accessible via the European Space Agency's (ESA) Planetary Science Archive (PSA). This archive encompasses raw , calibrated instrument measurements, and derived products from the orbiter's 11 scientific instruments as well as the Philae lander, supporting long-term research into 67P/Churyumov-Gerasimenko's composition, activity, and environment. By the mission's conclusion in 2016, Rosetta data had spurred over 100 peer-reviewed publications, with the total exceeding 800 by the early as researchers continue to mine the dataset, and further papers published into 2025. Ongoing analyses in the employ advanced techniques, such as for automated detection of dust plumes in OSIRIS images and refined geophysical models to simulate surface evolution, yielding new insights into cometary outbursts and material transport. For example, reexaminations using updated plasma interaction models have clarified deflection events observed in 2016. Comparisons with datasets from and missions highlight 67P's unique volatile inventory relative to carbonaceous asteroids, informing hybrid comet-asteroid formation theories. In , ESA marked the 10th anniversary of 's arrival at the comet and Philae's landing with public exhibitions and outreach events, highlighting the mission's enduring inspiration. Rosetta's legacy extends to revised comet models emphasizing their role as volatile-rich planetesimal remnants, while isotopic data from ROSINA confirmed that such s contributed minimally to Earth's water supply, redirecting astrobiological focus toward asteroidal delivery of prebiotic materials. These findings directly shape future missions like ESA's , providing calibration standards for and amid unpredictable . The open archive also enables educational applications, including student-led simulations of 67P's seasonal activity using public datasets to explore gravitational and thermal dynamics.

Public Engagement and Cultural Impact

Outreach Programs and Media

The (ESA) implemented a comprehensive outreach strategy for the Rosetta mission, featuring the official Rosetta on ESA's , which delivered real-time updates, diaries, and behind-the-scenes insights from mission control in , . Live webcasts of pivotal events, including the spacecraft's wakeup from hibernation in January 2014 and the Philae lander's deployment, engaged a global audience through ESA's streaming platform, with the November 2014 comet landing broadcast drawing widespread viewership and real-time commentary from mission teams. These streams highlighted the mission's drama, such as the Philae lander's unexpected bounce upon touchdown due to failed harpoons, which ESA communicated transparently to balance public excitement with operational realities. Social media played a central role in amplifying engagement, with ESA's @ESA_Rosetta Twitter account and the associated @Philae Twitter handle amassing over 670,000 followers combined by late 2014 through targeted campaigns using hashtags like #WakeUpRosetta, #CometLanding, and #Rosetta. Viral content, including the animated video of Rosetta's wakeup call and Philae's descent, garnered millions of views and shares, fostering a sense of communal anticipation among followers worldwide. ESA also released social media kits with profile images and graphics tied to mission milestones, encouraging user-generated content and broadening the narrative beyond technical updates. Media coverage was extensive, with major outlets like and providing in-depth features, live reports, and interviews with Rosetta scientists during key phases such as the spacecraft's arrival at Comet 67P in August 2014 and the Philae landing, often ranking the event among the top space achievements of the year. ESA supported this through detailed press kits containing mission overviews, imagery, and expert contacts, distributed ahead of events like the grand finale in September 2016. Interviews with principal investigators and project managers, such as those conducted at mission briefings in ESOC, emphasized the human element of the decade-long endeavor, helping to demystify complex science for broad audiences. Outreach efforts extended to education via the Teach with Rosetta program, which supplied multilingual classroom resources, lesson plans, and activities on comets and for primary and secondary schools across ESA member states. Through networks like the European Space Education Resource Office (ESERO), space education ambassadors delivered workshops and materials to thousands of institutions, integrating Rosetta data into curricula to inspire the next generation of scientists. These initiatives navigated challenges like coordinating communications in up to 22 languages to reach diverse European audiences, ensuring accessibility while managing expectations around mission uncertainties, such as Philae's partial success.

Educational and Artistic Representations

The Rosetta mission inspired a variety of animated content aimed at engaging younger audiences with . The (ESA) produced a series of short cartoons titled "Once Upon a Time... Rosetta," which narrate the spacecraft's journey to Comet 67P/Churyumov-Gerasimenko in a whimsical, storybook style, covering key events like the rendezvous and Philae lander's deployment. These animations, including episodes such as "The Amazing Adventures of and Philae," depict the orbiter and lander as anthropomorphic characters facing challenges like hibernation and landing bounces, making complex accessible through humor and adventure. Additionally, ESA's Paxi animations feature the agency's mascot exploring the mission's science, such as comet composition and solar system origins, to foster curiosity in children. Musical and artistic works drew directly from the mission's imagery and themes, transforming scientific data into cultural expressions. In 2014, ESA collaborated on the short film "Ambition," which inspired the album "Ambition: Original Soundtrack From & Inspired by Ambition – The Rosetta Mission" by composer Atanas Valkov, featuring electronic and cinematic tracks evoking the spacecraft's decade-long voyage and comet encounter. The Philae lander became a , commemorated with a special by the British marking the 2014 landing. Artists responded to Comet 67P's detailed images with tributes, such as Ekaterina Smirnova's series of large-scale watercolor paintings that interpret the comet's rubber-duck-like lobes and rugged terrain using pigments mimicking its icy, dusty composition. Other works include public installations like STUDIOKCA's LED-lit comet pavilion in , which replicated 67P's shape to symbolize the mission's success. Educational media extended the mission's reach through books, virtual reality (VR) experiences, and STEM curricula tailored for students. Children's books such as "Rosetta Probe: A Robot's Mission to Catch a " by Robert Snedden detail the spacecraft's design, journey, and discoveries in simple language, accompanied by illustrations of the orbiter's instruments and the comet's activity. VR simulations allow immersive exploration of 67P, including ESA-supported 360-degree videos from the that recreate 's approach and Philae's landing, enabling users to "fly" around the comet's surface features. STEM programs incorporate mission data into classroom activities; for instance, ESA's "Teach with " resources provide lesson plans on topics like simulations during Philae's descent and comet , used in to teach and astronomy. Similarly, the STEM Learning platform offers primary and secondary curricula using images to explore solar system formation and engineering challenges. Public icons emerging from the mission captured widespread imagination, particularly among younger demographics. The comet's bilobed, duck-like shape, revealed in early Rosetta images, spawned affectionate nicknames and visual comparisons, with media outlets dubbing it the "space rubber duck" and inspiring lighthearted illustrations in coverage. ESA ran a naming contest for Philae's landing site, open to European and U.S. residents, culminating in the selection of "Agilkia" after over 8,000 submissions, which highlighted public involvement in the mission. The 2014 Philae landing significantly boosted interest in space, with physicist Brian Cox highlighting the mission's potential to inspire children to pursue careers in science and , as the event's live broadcasts and dramatic bounces mirrored the excitement of historic milestones like the . In 2024, marking the 10th anniversary of Philae's landing on 12 November, ESA launched exhibitions and initiatives to relive the mission's historic moments, continuing to engage public interest in space exploration and its cultural legacy.

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