BepiColombo

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Template:Italic titleTemplate:Short description Template:Use British English Template:Use dmy dates Template:Infobox spaceflight

BepiColombo is a joint mission of the European Space Agency (ESA) and the Japan Aerospace Exploration Agency (JAXA) to the planet Mercury.<ref name="Amos">Template:Cite news</ref> The mission comprises two satellites launched together: the Mercury Planetary Orbiter (MPO) and Mio (Mercury Magnetospheric Orbiter, MMO).<ref name="Miopressrelease">Template:Cite press release</ref> The mission will perform a comprehensive study of Mercury, including characterization of its magnetic field, magnetosphere, and both interior and surface structure. It was launched on an Ariane 5<ref name="ariane"/> rocket on 20 October 2018, with Mercury orbit insertion planned for November 2026, after a flyby of Earth, two flybys of Venus, and six flybys of Mercury.<ref name="FACTS"/><ref name="esa20161125">Template:Cite web</ref> The total cost of the mission was estimated in 2017 as US$2 billion.<ref>BepiColombo Mercury mission tested for journey into 'pizza oven' Stephen Clarke Spaceflight Now 17 July 2017</ref>

Names

BepiColombo is named after Giuseppe "Bepi" Colombo (1920–1984), a scientist, mathematician and engineer at the University of Padua, Italy, who first proposed the interplanetary gravity assist manoeuvre used by the 1974 Mariner 10 mission, a technique now used frequently by planetary probes.

Mio, the name of the Mercury Magnetospheric Orbiter, was selected from thousands of suggestions by the Japanese public. In Japanese, Mio means a waterway, and according to JAXA, it symbolizes the research and development milestones reached thus far, and wishes for safe travel ahead. JAXA said the spacecraft will travel through the solar wind just like a ship traveling through the ocean.<ref name="Miopressrelease"/> In Chinese and Japanese, Mercury is known as the "water star" (水星) according to wǔxíng.

Scientific objectives

The main objectives of the mission are:<ref name="ISAS homepage" /><ref name="FACTS2">Template:Cite web</ref>

Mercury is too small and hot for its gravity to retain any significant atmosphere over long periods of time, but it has a "tenuous surface-bounded exosphere"<ref>Template:Cite journal</ref> containing hydrogen, helium, oxygen, sodium, calcium, potassium and other trace elements. Its exosphere is not stable as atoms are continuously lost and replenished from a variety of sources. The mission will study the exosphere composition and dynamics, including generation and escape.

The orbiters are equipped with scientific instruments provided by various European countries and Japan. The mission will characterize the solid and liquid iron core (Template:Frac of the planet's radius) and determine the size of each.<ref>Science with BepiColombo ESA, Accessed: 23 October 2018</ref> The mission will also complete gravitational and magnetic field mappings. Russia provided gamma ray and neutron spectrometers to verify the existence of water ice in polar craters that are permanently in shadow from the Sun's rays.

Mission overview

The mission involves three components, which will separate into independent spacecraft upon arrival at Mercury.<ref>Template:Cite conference</ref>

  • Mercury Transfer Module (MTM) for propulsion, built by ESA.
  • Mercury Planetary Orbiter (MPO) built by ESA.
  • Mercury Magnetospheric Orbiter (MMO) or Mio built by JAXA.

During the launch and cruise phases, these three components are joined together (with the Magnetospheric Orbiter Sunshield and Interface or MOSIF between Mio and MPO)<ref name="MOSIF"/> to form the Mercury Cruise System (MCS).<ref name="Flyby 2018"/><ref name="Arrival 2018"/>

The stacked spacecraft will take eight years to position itself to enter Mercury orbit. During this time it uses solar-electric propulsion and nine gravity assists, flying past the Earth and Moon in April 2020, Venus in 2020 and 2021, and six Mercury flybys between 2021 and 2025.<ref name="FACTS" />

Expected to arrive in Mercury orbit in November 2026, the Mio and MPO satellites will separate and observe Mercury in collaboration for one year, with a possible one-year extension.<ref name="FACTS" /> Although originally expected to enter orbit in December 2025, thruster issues discovered in September 2024 before the fourth Mercury flyby resulted in a delayed arrival of November 2026.<ref>Template:Cite web</ref>

ESA is responsible for the overall mission, the design, development assembly and test of the propulsion and MPO modules, and the launch. The two orbiters are operated by mission controllers based in Darmstadt, Germany.<ref name="launched">Template:Cite news</ref> The spacecraft operations manager of BepiColombo was Elsa Montagnon until 2021,<ref>Template:Cite web</ref> and is now Ignacio Clerigo.<ref>Template:Cite web</ref> ESA's Cebreros, Spain Template:Convert ground station is the primary ground facility for communications during all mission phases.<ref>Template:Cite web</ref>

Mission timeline

Before launch

The BepiColombo mission proposal was selected by ESA in 2000. A request for proposals for the science payload was issued in 2004.<ref name="Howell">BepiColombo: Joint Mission to Mercury Elizabeth Howell Space.com 21 October 2018</ref> In 2007, Astrium (now Airbus Defence and Space) was selected as the prime contractor,<ref name="sci.esa.int">Template:Cite web</ref> and Ariane 5 chosen as the launch vehicle.<ref name="Howell" /> The initial target launch of July 2014 was postponed several times, mostly because of delays on the development of the solar electric propulsion system.<ref name="Howell" /> The mission was approved in November 2009, after years in proposal and planning as part of the European Space Agency's Horizon 2000+ programme;<ref>Template:Cite web</ref> it is the last mission of the programme to be launched.<ref name="scaling back" />

Launch

The two orbiters were successfully launched together on 20 October 2018.<ref name="launched" /> The launch took place on Ariane flight VA245 from Europe’s Spaceport in Kourou, French Guiana.<ref>Template:Cite news</ref>

Gravity assist maneuvers

File:BepiColombo NBO 2020-04-10.webm
BepiColombo, imaged at Northolt Branch Observatories, 16 hours after the Earth flyby. The bright satellite passing by is INSAT-2D.

The stacked spacecraft left Earth with a hyperbolic excess velocity of Template:Cvt. Initially, the craft was placed in a heliocentric orbit similar to that of Earth. After both the spacecraft and Earth completed one and a half orbits, it returned to Earth to perform a gravity-assist maneuver and was deflected towards Venus.<ref name="mission design">Template:Cite web</ref>

Following its Earth flyby in April 2020, BepiColombo was briefly mistaken for a near-Earth asteroid, receiving the provisional designation Template:Mp.<ref name="2020GL2a">Template:Cite web</ref><ref name="2020GL2b">Template:Cite web</ref><ref name="2020GL2c">Template:Cite web</ref><ref>Template:Cite web</ref>

Two consecutive Venus flybys reduced the perihelion near to the Sun–Mercury distance with almost no need for thrust. A sequence of six Mercury flybys lowered the relative velocity to Template:Cvt. After the fourth Mercury flyby in 2024, the spacecraft is in an orbit similar to that of Mercury and remains in the general vicinity of the planet.<ref>Template:Cite web</ref>

Science during Venus flybys

After the potential biomarker phosphine has been tentatively discovered in the Venusian atmosphere in September 2020, ESA scientists suggested that BepiColombo might be able to detect the compound during its two Venus flybys in 2020 and 2021. However, it was not clear if the spacecraft's instruments were sufficiently sensitive<ref>Template:Cite news</ref> and there has been no announcement of such detection since.

During the first Venus flyby in October 2020, seven science instruments and a radiation monitor onboard the Mercury Planetary Orbiter, and three instruments onboard Mio, were active and gathering data. The observations were coordinated with JAXA's Akatsuki, the only active spacecraft orbiting Venus at that time, as well as Earth-based observatories.<ref>Template:Cite news</ref><ref name=":0" />

The second Venus flyby in August 2021 happened only 33 hours after another interplanetary spacecraft by ESA, Solar Orbiter, completed its gravity assist at the same planet. Both spacecraft used their science instruments to study the magnetic, plasma, and particle environment around Venus during their flybys, offering unique multipoint datasets. The MPO's MERTIS instrument captured high resolution spectra of the Venus atmosphere and the Mercury Transfer Module's three monitoring cameras (M-CAM) captured a series of black-and-white images of the planet, documenting the various phases of the flyby.<ref>Template:Cite web</ref>

Science during Mercury flybys

File:The search for volcanoes (annotated) ESA24328694.png
Photo of Mercury captured on 23 June 2022 during the second gravity assist at the planet.
File:BepiColombo says goodbye to Mercury for the fourth time (annotated) ESA501146.jpg
Photo of Mercury captured on 5 September 2024 during the fourth gravity assist at the planet.
File:Bepi, Mio and MTM complete their final Mercury flyby ESA505289.jpg
BepiColombo's cartoon characters during the sixth Mercury flyby

During the first Mercury flyby in October 2021, the spacecraft captured its first images of the target planet using the M-CAM monitoring cameras on the Mercury Transfer Module.<ref>Template:Cite web</ref><ref>Template:Cite web</ref> Some of the scientific instruments on both orbiters were also active during the flyby, exploring the magnetic and particle environment around Mercury and measuring the planet's gravity.<ref>Template:Cite web</ref>

During the second flyby in June 2022, the M-CAM cameras imaged, among other targets, the crater Heaney with a candidate volcano, an important target for the spacecraft's primary mission. This crater has been recently named after Seamus Heaney following a request from the M-CAM team. Some of the scientific instruments have been again active, measuring the magnetic, plasma, and particle environment around the spacecraft.<ref>Template:Cite web</ref>

During the third flyby in June 2023, the MPPE suite of instruments on Mio was used to map the magnetosphere of Mercury.<ref>Template:Cite web</ref> Based on these data, scientists described various expected features of the magnetosphere, but also made new discoveries: 1) a low latitude layer containing particles with much broader energy range than ever observed on Mercury, 2) energetic hydrogen ions trapped at low latitude and near the equator, and 3) cold plasma ions of oxygen and sodium, as well as signatures of potassium, which were probably ejected from the planet's surface by micrometeorites or the solar wind.<ref>Template:Cite web</ref><ref>Template:Cite journal</ref>

In May 2024, computers on BepiColombo (as well as on another ESA mission, Mars Express) reported a sharp increase in the number of memory errors, coinciding with a massive solar flare from the active region AR3664, at that time facing away from Earth. The event was also observed in detail by ESA's Solar Orbiter.<ref>Template:Cite web</ref>

During the fourth flyby in September 2024, the spacecraft had, for the first time, a clear view of Mercury's south pole. The M-CAM 2 and 3 cameras provided images of the polar region, as well as the Vivaldi crater and a crater newly named Stoddart after Margaret Olrog Stoddart following a request from the M-CAM team.<ref>Template:Cite web</ref>

During the fifth flyby in December 2024, using the MERTIS instrument, BepiColombo became the first spacecraft ever to observe Mercury in mid-infrared light.<ref>Template:Cite web</ref> During the sixth and final Mercury flyby in January 2025, the M-CAM 1 camera imaged the permanently shadowed craters Prokofiev, Kandinsky, Tolkien, and Gordimer near the planet's north pole.<ref>Template:Cite web</ref>

Thruster issues

On 15 May 2024, ESA reported an issue preventing the spacecraft's thrusters from operating at full power during a scheduled manoeuvre on 26 April 2024.<ref name="x457">Template:Cite web</ref> On 2 September 2024, ESA reported that to compensate for the reduced available thrust, a revised trajectory had been developed that would add 11 months to the cruise, delaying the expected arrival date from 5 December 2025 to November 2026.<ref>Template:Cite web</ref>

Future

Four final thrust arcs will reduce the relative velocity to the point where Mercury will "weakly" capture the spacecraft in November 2026 into polar orbit. Only a small maneuver is needed to bring the craft into an orbit around Mercury with an apocentre of Template:Convert. The orbiters then separate and will adjust their orbits using chemical thrusters.<ref name="Data Center">Template:Cite web Template:PD-notice</ref><ref name="mission design" />

Trajectory

Template:Asof, the mission schedule is:<ref>Template:Cite web</ref>Template:Clear

Date Event Comment
20 October 2018, 01:45 UTC Launch
10 April 2020,
04:25 UTC 		Earth flyby 1.5 years after launch
15 October 2020, 03:58 UTC First Venus flyby On 15 October 2020, the ESA reported the flyby was a success. Closest approach at a distance of about 10 720 km from the planet's surface.<ref name=":0">Template:Cite web</ref>
10 August 2021,
13:51 UTC 		Second Venus flyby 1.35 Venus years after first Venus flyby. Flyby was a success, and saw BepiColombo come within Template:Convert of Venus's surface.<ref>Template:Cite web</ref><ref>Template:Cite news</ref>
1 October 2021,
23:34:41 UTC 		First Mercury flyby Passed Template:Convert from Mercury's surface.<ref>Template:Cite tweet</ref> Occurred on what would have been the 101st birthday of Giuseppe Colombo.
23 June 2022,
09:44 UTC 		Second Mercury flyby ~2 orbits (3 Mercury years) after 1st Mercury flyby. Closest approach of about Template:Convert altitude.<ref>Template:Cite web</ref>
19 June 2023,
19:34 UTC 		Third Mercury flyby ~3 orbits (4.1 Mercury years) after 2nd Mercury flyby. Closest approach of about Template:Convert altitude.<ref>Template:Cite web</ref><ref>Template:Cite news</ref>
Template:Nowrap, 21:48 UTC Fourth Mercury flyby ~4 orbits (5.0 Mercury years) after 3rd Mercury flyby. Closest approach of about Template:Convert altitude.<ref>Template:Cite web</ref>
1 December 2024, 14:23 UTC Fifth Mercury flyby 1 orbit (1.0 Mercury year) after 4th Mercury flyby. Closest approach about Template:Convert altitude.<ref>Template:Cite web</ref>
8 January 2025, 05:58:52 UTC Sixth Mercury flyby ~0.4 orbits (0.4 Mercury years) after 5th Mercury flyby. Closest approach about Template:Convert altitude.<ref>Template:Cite web</ref><ref>Template:Cite web</ref>
21 November 2026 Mercury orbit insertion 7.8 Mercury years after 6th Mercury flyby. 60-hour orbital period
December 2026 Template:Nowrap, detaches from MPO 9.3-hour orbital period
4 Mars 2027 Template:Nowrap 2.36-hour orbital period
April 2028 End of nominal mission
April 2029 End of planned extended mission
File:Timeline of BepiColombo.svg
Timeline of BepiColombo from 20 October 2018 to 2 November 2025. Red circle indicates flybys.

Template:-

Mission components

Mercury Transfer Module

QinetiQ T6 Performance <ref>Qualification of the T6 Thruster for BepiColombo Template:Webarchive R. A. Lewis, J. Pérez Luna, N. Coombs. 30th International Symposium on Space Technology and Science 34th International Electric Propulsion Conference and 6th Nano-satellite Symposium, Hyogo-Kobe, Japan, 4–10 July 2015</ref><ref>QinetiQ's T6 and T5 Ion Thruster Electric Propulsion System Architectures and Performances Template:Webarchive Mark Hutchins, Huw Simpson. 30th International Symposium on Space Technology and Science 34th International Electric Propulsion Conference and 6th Nano-satellite Symposium, Hyogo-Kobe, Japan, 4–10 July 2015</ref>
Type Kaufman Ion Engine
Units on board 4 <ref>Template:Cite web</ref><ref>Template:Cite web</ref>
Diameter Template:Cvt
Max. thrust 145 mN each
Specific impulse
(Isp)		 4300 seconds
Propellant Xenon
Total power 4628 W

The Mercury Transfer Module (MTM) has a mass of Template:Cvt, including Template:Cvt of xenon propellant, and is located at the base of the stack. Its role is to carry the two science orbiters to Mercury and to support them during the cruise.

The MTM is equipped with a solar electric propulsion system as the main spacecraft propulsion. Its four QinetiQ-T6 ion thrusters operate singly or in pairs for a maximum combined thrust of 290 mN,<ref>Template:Cite conference</ref> making it the most powerful ion engine array ever operated in space. The MTM supplies electrical power for the two hibernating orbiters as well as for its solar electric propulsion system thanks to two Template:Convert solar panels.<ref name="MPO page">Template:Cite web</ref> Depending on the probe's distance to the Sun, the generated power will range between 7 and 14 kW, each T6 requiring between 2.5 and 4.5 kW according to the desired thrust level.

The solar electric propulsion system has typically very high specific impulse and low thrust. This leads to a flight profile with months-long continuous low-thrust braking phases, interrupted by planetary gravity assists, to gradually reduce the velocity of the spacecraft. Moments before Mercury orbit insertion, the MTM will be jettisoned from the spacecraft stack. After separation from the MTM, the MPO will provide Mio all necessary power and data resources until Mio is delivered to its mission orbit.<ref>Template:Cite web</ref> Separation of Mio from MPO will be accomplished by spin-ejection.<ref>Template:Cite journal</ref>

Mercury Planetary Orbiter

The Mercury Planetary Orbiter (MPO) has a mass of Template:Cvt and uses a single-sided solar array capable of providing up to 1000 watts and featuring Optical Solar Reflectors to keep its temperature below Template:Cvt. The solar array requires continuous rotation keeping the Sun at a low incidence angle in order to generate adequate power while at the same time limiting the temperature.<ref name="MPO page"/>

The MPO carries a payload of 11 instruments, comprising cameras, spectrometers (IR, UV, X-ray, γ-ray, neutron), a radiometer, a laser altimeter, a magnetometer, particle analysers, a Ka-band transponder, and an accelerometer. The payload components are mounted on the nadir side of the spacecraft to achieve low detector temperatures, apart from the MERTIS and PHEBUS spectrometers located directly at the main radiator to provide a better field of view.<ref name="MPO page"/>

A high-temperature-resistant Template:Cvt diameter high-gain antenna is mounted on a short boom on the zenith side of the spacecraft. Communications will be on the X-band and Ka-band with an average bit rate of 50 kbit/s and a total data volume of 1550 Gbit/year. ESA's Cebreros, Spain Template:Convert ground station is planned to be the primary ground facility for communications during all mission phases.<ref name="MPO page"/>

Science payload of MPO

File:MPO’s science instruments ESA17050215.jpeg
MPO's science instruments

The science payload of the Mercury Planetary Orbiter consists of eleven instruments:<ref name="MMO objectives"/><ref name="MPO Instruments 2008">Template:Cite web</ref>

Mio (Mercury Magnetospheric Orbiter)

Mio, or the Mercury Magnetospheric Orbiter (MMO), developed and built mostly by Japan, has the shape of a short octagonal prism, Template:Cvt long from face to face and Template:Cvt high.<ref name='ISAS homepage'/><ref>Template:Cite journal</ref> It has a mass of Template:Cvt, including a Template:Cvt scientific payload consisting of 5 instrument groups, 4 for plasma and dust measuring run by investigators from Japan, and one magnetometer from Austria.<ref name='ISAS homepage'/><ref name="MMO brochure 2015">Template:Cite web</ref><ref>Template:Cite web</ref>

Mio will be spin stabilized at 15 rpm with the spin axis perpendicular to the equator of Mercury. It will enter a polar orbit at an altitude of Template:Cvt, outside of MPO's orbit.<ref name="MMO brochure 2015"/> The top and bottom of the octagon act as radiators with louvers for active temperature control. The sides are covered with solar cells which provide 90 watts. Communications with Earth will be through a Template:Cvt diameter X-band phased array high-gain antenna and two medium-gain antennas operating in the X-band. Telemetry will return 160 Gb/year, about 5 kbit/s over the lifetime of the spacecraft, which is expected to be greater than one year. The reaction and control system is based on cold gas thrusters. After its release in Mercury orbit, Mio will be operated by Sagamihara Space Operation Center using Usuda Deep Space CenterTemplate:'s Template:Cvt antenna located in Nagano, Japan.<ref name="MMO objectives">Template:Cite web</ref>

Science payload of Mio

Mio carries five groups of science instruments with a total mass of Template:Cvt:<ref name='ISAS homepage'/><ref name='MMO objectives'/>

Magnetospheric Orbiter Sunshield and Interface

File:BepiColombo stack with sunshield.jpg
Full stack with sunshield on top

The Mio orbiter requires additional thermal control on the cruise to Mercury, in addition to umbilicals to the MPO. The European Space Agency thus provided the Magnetospheric Orbiter Sunshield and Interface (MOSIF), a white shroud that is shaped like a conical frustrum to provide clearance, as Mio is spun up during its separation in 2026, before being ejected from the MPO.<ref name="MOSIF">Template:Cite web</ref><ref name="Flyby 2018">Template:Cite web</ref><ref name="Arrival 2018">Template:Cite web</ref>

Mercury Surface Element (cancelled)

The Mercury Surface Element (MSE) was cancelled in 2003 due to budgetary constraints.<ref name="scaling back">Template:Cite press release</ref> At the time of cancellation, MSE was meant to be a small, Template:Cvt, lander designed to operate for about one week on the surface of Mercury.<ref name="Data Center"/> Shaped as a Template:Cvt diameter disc, it was designed to land at a latitude of 85° near the terminator region. Braking manoeuvres would bring the lander to zero velocity at an altitude of Template:Cvt at which point the propulsion unit would be ejected, airbags inflated, and the module would fall to the surface with a maximum impact velocity of Template:Cvt. Scientific data would be stored onboard and relayed via a cross-dipole UHF antenna to either the MPO or Mio. The MSE would have carried a Template:Cvt payload consisting of an imaging system (a descent camera and a surface camera), a heat flow and physical properties package, an alpha particle X-ray spectrometer, a magnetometer, a seismometer, a soil penetrating device (mole), and a micro-rover.<ref>Template:Cite web</ref>

See also

References

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Template:Portal bar Template:Mercury (planet) Template:Mercury spacecraft Template:Venus spacecraft Template:ESA projects Template:Japanese space program Template:Planetary Missions Program Office Template:Solar System probes Template:Orbital launches in 2018 Template:2018 in space

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