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SMILE (spacecraft)
SMILE (spacecraft)
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Solar wind Magnetosphere Ionosphere Link Explorer
Artist's impression of the SMILE spacecraft
Mission typeMagnetospheric mission
OperatorESA-CAS
Websitecosmos.esa.int/web/smile/
Mission duration3 years (nominal)[1]
Spacecraft properties
ManufacturerAirbus (payload module)
Launch mass2200 kg
Dry mass708 kg
Power850 W
Start of mission
Launch date2026 (planned)[2]
RocketVega-C
Launch siteKourou
ContractorArianespace
Orbital parameters
Reference systemGeocentric
RegimeHighly elliptical orbit
Perigee altitude5,000 km
Apogee altitude121,182 km
Inclination70° or 98°
SMILE mission logo
SMILE mission insigna
← JUICE
PLATO →

Solar wind Magnetosphere Ionosphere Link Explorer (SMILE) is a planned joint venture mission between the European Space Agency and the Chinese Academy of Sciences. SMILE will image for the first time the magnetosphere of the Sun in soft X-rays and UV during up to 40 hours per orbit, improving the understanding of the dynamic interaction between the solar wind and Earth's magnetosphere.[3][4] The prime science questions of the SMILE mission are: "What are the fundamental modes of the dayside solar wind/magnetosphere interaction? What defines the substorm cycle? How do coronal mass ejection-driven storms arise and what is their relationship to substorms?" As of September 2025, SMILE is expected to launch in 2026.[2]

Overview

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The mission will observe the solar wind interaction with the magnetosphere with its X-ray and ultraviolet cameras (SXI and UVI), gathering simultaneous images and videos of the dayside magnetopause (where Earth's magnetosphere meets the solar wind), the polar cusps (a region in each hemisphere where particles from the solar wind have direct access to Earth's ionosphere), and the auroral oval (the region around each geomagnetic pole where auroras most often occur). SMILE will also gather simultaneously in situ measurements with its two other instruments making up its payload – an ion analyser (LIA) and a magnetometer (MAG). These instruments will monitor the ions in the solar wind, magnetosheath and magnetosphere while detecting changes in the local DC magnetic field.

SMILE must reach a high enough altitude to view the outside edge of Earth's magnetopause and at the same time obtain good spatial resolution of the auroral oval. The chosen orbit is therefore highly elliptical and highly inclined (70 or 98 degrees depending on the launcher), and takes SMILE a third of the way to the Moon at apogee (an altitude of 121 182 km, i.e. 19 Earth radii or RE).

On 21 January 2025, engineers at ESA connected the two main parts of the Smile spacecraft, putting it into its final flight configuration.

This type of orbit enables SMILE to spend much of its time (about 80%, equivalent to nine months of the year) at high altitude, allowing the spacecraft to collect continuous observations for the first time during more than 40h. This orbit also limits the time spent in the high-radiation Van Allen belts, and in the two toroidal belts. SMILE will be injected into a low Earth orbit by a Vega-C launch vehicle from Kourou, French Guiana, and its propulsion module will bring the spacecraft to the nominal orbit with perigee altitude of around 5000 km.[1]

The SMILE spacecraft consists of a platform provided by the Chinese Academy of Sciences (CAS) attached below a payload module provided by ESA. The CAS platform is composed of a propulsion and a service module, together with the two detectors (or heads) of the ion instrument. The payload module hosts 3 of the 4 scientific instruments and an X-band communications system. It was built by Airbus.[5] The SMILE ground segment comprises the Chinese Academy of Sciences (CAS) ground segment and the European Space Agency (ESA) ground segment, which collaborate closely on this mission. The Ground Support System (GSS) and the Science and Application System (SAS) are two important components of the CAS ground segment. The SAS is tasked with fostering collaboration between CAS and ESA, designing effective frameworks to coordinate scientists in planning SMILE science operations.[6]

Instruments

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Key instruments on board the spacecraft include:[3][1]

Flight model of the SMILE soft X-ray imager
Soft X-ray imager (flight model)
  • Soft X-ray Imager (SXI) – wide-field lobster-eye telescope using micropore optics to spectrally map the location, shape, and motion of Earth's magnetospheric boundaries, including the bow shock, magnetopause, and cusps, by observing emission from the [Solar Wind Charge eXchange (SWCX) process. The SXI is equipped with two large X-ray-sensitive Charge-coupled device (CCD) detectors covering the 0.2 keV to 2.5 keV energy band, and has an optic field of view spanning 15.5° × 26.5°. This telescope was developed, built, and calibrated at the University of Leicester, UK, and other institutions throughout Europe. CCDs have been procured from Teledyne e2v, UK, by ESA and calibrated by The Open University, UK.
Flight model of the SMILE Ultra-Violet imager
Ultra-Violet imager (flight model)
  • UV Imager (UVI) – an ultraviolet camera to image Earth's northern auroral regions. It will study the connection between the processes taking place at the magnetospheric boundaries – as seen by the SXI – and those acting on the charged particles precipitating into our ionosphere. UVI is a four mirror telescope imaging ultraviolet emissions with wavelengths from 160 to180 nm using a CCD detector. It is broken into three logical partitions: UVI-Camera (UVI-C) and UVI-Electronics (UVI-E) connected via a harness (UVI-H). The UVI optical design philosophy is based on an on-axis, 4-mirror system, optimized for the SMILE orbit and the required cadence and spatial resolution. UV filter technology coupled with the 4-mirror design provides orders of magnitude greater visible light suppression than previous auroral missions and is an enabling factor for the UVI science objectives. The detector module comprises a micro-channel plate (MCP) based image intensifier optically coupled to a CCD detector.[7] The UVI has a 10° × 10° field of view and will have a spatial image resolution at apogee of 150 km, using four thin film-coated mirrors to guide light into its detector. Temporal resolution will be up to 60s. UVI is built by NSSC with collaboration from Belgium Liège Space Center (CSL), ESA, Calgary University and the Polar Research Institute of China.
Flight model of one of the two Light Ion Analyzer (LIA) detector heads
Light Ion Analyzer (LIA) detector head and electronics box (flight model)
  • Light Ion Analyser (LIA) – will determine the properties and behaviour of the solar wind and magnetosheath ions under various conditions by measuring the three-dimensional velocity distribution of protons and alpha particles. It is made of two top-hat-type electrostatic analysers, each mounted on opposite side of the platform. It is capable of sampling the full 4 π three-dimensional distribution of the solar wind, and can measure ions in the energy range 0.05 to 20 keV at up 0.5 second time resolution. It is a joint venture between the Chinese National Space Science Centre, CAS, and University College London's Mullard Space Science Laboratory (UCL-MSSL), UK and LPP/CNRS/Ecole Polytechnique, France.
Flight model of SMILE MAGnetometer (MAG) on its folded boom
MAGnetometer (MAG) on its folded boom (flight model)
  • Magnetometer (MAG) – will be used to determine the orientation and magnitude of the magnetic field in the solar wind and magnetosheath, and to detect any solar wind shocks or discontinuities passing over the spacecraft. Two tri-axial sensors will be mounted away from the spacecraft on a 3-m-long boom some 80 cm apart, with a corresponding electronics unit mounted on SMILE's main body. This configuration will let the MAG act as a gradiometer, and allow SMILE's background magnetic field to be accurately determined and subtracted from any measurements. MAG will measure the three components of the magnetic field in the range +/- 12800 nT. It is joint venture between the Chinese National Space Science Centre, CAS, and the Space Research Institute, Austrian Academy of Sciences.

Working groups

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Several working groups have been set up to help preparing the SMILE mission including

[Top] Simulation of SMILE soft X-ray images during a 52-hour orbital period. Pink rectangular boxes show two field-of-view candidates of the SMILE soft X-ray imager. [Bottom] SMLE orbit (pink ellipse), location (pink dots), and look direction (blue line) projected on the XZ plane (left), XY plane (middle), and YZ plane (right). Color contour shows plasma density on each planes. The OpenGGCM global magnetosphere - ionosphere model and one of SMILE orbit candidates are used for this simulation.

In-situ science working group

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SMILE in-situ science working group is established to support the SMILE Team in ensuring that the mission science objectives are achieved and optimized, and in adding value to SMILE science. The in-situ SWG activity is centred on optimizing the design, the operations, calibrations planning, identifying the science objectives and opportunities of the in situ instrument package, including conjunctions with other magnetospheric space missions.

Modeling working group

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The SMILE modeling working group provides the following modeling supports for the upcoming SMILE mission

1. Grand modeling challenge: MHD model comparison and SXI requirements/goals -

  • unify the X-ray calculation method (same neutral density model, background, etc.),
  • check the model-to-model difference on Solar Wind Charge eXchange (SWCX) signals and on the boundary locations (bow shock, magnetopause, and cusp)
  • provide the MHD point of view on the range of X-ray signal strength.
  • provide the range of the expected boundary locations under various solar wind flux.
  • give a unified voice on the science requirements and goals (how high solar wind flux is needed to find the boundaries within 0.5RE resolution for 5 mins, or 0.2 RE resolution for 1 min?)

2. Boundary tracing from SXI data

  • select one exemplary simulation results to test the boundary tracing techniques.
  • test A. Jorgensen & T. Sun on magnetopause tracing method by using the SXI specification (orbit, field-of-view, backgrounds, noise, etc.)[8]
  • test M. Collier & H. Connor on magnetopause tracing method by using the same SXI specification[9] are visible in the soft X-rays.
  • develop new methods to derive plasma boundaries from X-ray image(s)
  • prepare a programing tool for the SXI data analysis
  • develop and validate the tracing methods for other boundaries (bow shock and cusps)

3. Other science projects

  • investigate if small magnetosheath signatures such as magnetosheath high speed jets are visible in the soft X-rays.
  • investigate the magnetosphere-ionosphere coupling using Soft X-ray and aurora images

Ground-based and additional science working group

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The SMILE Ground-based and Additional Science Working Group coordinates support for the mission in the solar-terrestrial physics community. Their aim is to maximise the uptake of SMILE data, and therefore maximise the science output of the mission. They will coordinate future observing campaigns with other experimental facilities, both on the ground and in space, for example by using high resolution modes for Super Dual Auroral Radar Network facilities, or with EISCAT 3D, and correlating with data from other missions flying at the time. The working group is also developing a set of tools and a visualisation facility to combine data from SMILE and supporting experiments.

The Public Engagement working group

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Space Lates at the National Space Centre

The SMILE Public Engagement working group aims to promote SMILE and its science among the general public, amateur science societies and school pupils of any age. Members of the group are active in giving presentations illustrating the science which SMILE will produce and the impact it will have on our knowledge of solar-terrestrial interactions. They generate contacts with organisations promoting science in primary and secondary schools, particularly in socio-economical deprived areas, hold hands-on workshops and promote careers in science. The group is focusing on SMILE as a practical example of how space projects are developed, and encouraging pupils to follow its progress to launch and beyond. It also promotes international exchanges, a good example of which is the translation of the book 'Aurora and Spotty' for children (and maybe for some adults too), originally in Spanish, into Chinese.

Publications

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2025

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  • May 20 - Connor, H.K.; Sun, T.; Samsonov, A. (2025). "Modeling Working Group: Modeling and Analysis of X-ray and Ultraviolet Images of Solar Wind – Earth Interactions". Space Sci. Rev. 221 (4): 46. doi:10.1007/s11214-025-01172-8. PMC 12092568. PMID 40405899.
  • March 18 - Zhang, XX.; Wang, YM.; He, F. (2025). "Ultraviolet Imager (UVI) for the SMILE Mission". Space Sci. Rev. 221 (3): 31. Bibcode:2025SSRv..221...31Z. doi:10.1007/s11214-025-01160-y.
  • February 07 - Ma, F.; Dai, L.; Zhang, Y.C. (2025). "SMILE Ground Support System and Science Application System". Space Sci. Rev. 221. Bibcode:2025SSRv..221...15M. doi:10.1007/s11214-025-01141-1.
  • January 27 - Wang, C.; Branduardi-Raymont, G.; Escoubet, C.P.; Forsyth, C. (2025). "Solar Wind Magnetosphere Ionosphere Link Explorer (SMILE): Science and Mission Overview". Space Sci. Rev. 221 (1): 9. Bibcode:2025SSRv..221....9W. doi:10.1007/s11214-024-01126-6. PMC 11772532. PMID 39882204.

2024

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2023

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2022

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2021

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2020

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2019

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Awards

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2020

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Mission timeline

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  • Following the success of the Double Star mission, the ESA and CAS decided to jointly select, design, implement, launch and exploit the results of a space mission together for the first time. After initial workshops, a call for proposals was announced in January 2015. After a joint peer review of mission proposals, SMILE was selected as the top candidate out of 13 proposed.[10] The SMILE mission proposal[11] was jointly led by the University College London and the Chinese National Space Science Center.
  • From June to November 2015, the mission entered initial studies for concept readiness, and final approval was given for the mission by the ESA Science Programme Committee in November 2015.
  • A Request For Information (RFI) on provisions for the payload module was announced on 18 December 2015. The objective was to collect information from potential providers to assess low risk payload module requirements given stated interest in the mission, in preparation for the Invitation to Tender in 2016.[12]
  • The Mission System Requirements Review was completed in October 2018, and ESA Mission Adoption by the Science Programme Committee was granted in March 2019.[13]
  • SMILE successfully completed the Spacecraft and Mission Critical Design Review (CDR) in June 2023 in Shanghai.[14]
  • SMILE's payload module, built by Airbus in Spain, arrived at ESTEC in September 2024 followed by the Chinese-built platform which arrived at ESTEC on a dedicated flight from Shanghai on 9 December 2024. The two parts were connected on 21 January 2025.[15] In April 2025, the spacecraft was moved into the Maxwell Test Chamber at ESTEC for space environment testing[16] and later it underwent measurements of mass properties[17] and vibration testing.[18]

See also

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References

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Revisions and contributorsEdit on WikipediaRead on Wikipedia
from Grokipedia
Solar wind Magnetosphere Ionosphere Link Explorer (SMILE) is a space science mission developed jointly by the (ESA) and the (CAS), designed to study the dynamic interaction between the and Earth's through global imaging in soft X-rays and light. As the first collaborative space mission between ESA and CAS, SMILE aims to provide unprecedented simultaneous observations of the , the , and the -thermosphere system, enabling a comprehensive understanding of Sun-Earth connections and processes. The , with a dry mass of approximately 700 kg (total mass approximately 2300 kg including propellant), carries four key instruments: the Soft X-ray Imager (SXI) for imaging the magnetosheath and ; the Imager (UVI) for auroral observations; the Light Ion Analyser (LIA) for in-situ measurements; and the (MAG) for data. SMILE will operate in a (HEO) with an apogee of up to 121,000 km over the and a perigee of about 5000 km, allowing for over 40 hours of continuous imaging per orbit during its nominal three-year mission lifetime. Launched aboard an ESA Vega-C rocket from Europe's Spaceport in , , SMILE is scheduled for liftoff in 2026, following successful assembly and environmental testing of the at ESA's ESTEC facility in the , completed in September 2025. As of November 2025, the has completed all pre-launch testing and is in final preparations for launch. The mission's platform is provided by CAS, while ESA contributes the module, the SXI instrument, launch services, and ground operations, with science data processed through working groups. By revealing how drives magnetospheric responses, such as cusp precipitation and dynamics, SMILE will enhance predictions of impacts on Earth, including satellite operations and power grids.

Mission Background

Development History

The SMILE (Solar wind Magnetosphere Ionosphere Link Explorer) mission was proposed in 2015 under a joint call between the (ESA) and the (CAS), as part of ESA's F-class small missions. It was selected in June 2015 from 13 competing concepts by a joint ESA-CAS committee, entering Phase A feasibility studies shortly thereafter. The Chinese component received formal adoption by CAS in November 2016, securing funding and committing to development responsibilities. Phase A and B studies, focusing on mission definition and preliminary design, spanned from early 2016 to late 2018, involving ESA, CAS, and European industrial partners like . These phases culminated in the Mission System Requirements Review in October 2018, paving the way for full implementation. ESA's Science Programme Committee adopted the mission in March 2019, approving a budget of approximately €46 million for the European contributions (ESA's share of the total €92 million mission cost) and targeting a 2026 launch. The project advanced through detailed design and prototyping in Phase C/D, achieving a key milestone with the joint spacecraft and mission Critical Design Review (CDR) passed in June 2023 in . This review confirmed the maturity of the spacecraft design, including the platform and integration, and reaffirmed the 2026 launch timeline under the collaborative ESA-CAS framework. Assembly and integration progressed in 2024–2025, with the payload module—built by in —arriving at ESA's ESTEC facility in the in September 2024, followed by the spacecraft platform from Institute of Satellite Engineering in December 2024. On 21 January 2025, the two modules were successfully connected using 120 bolts in a cleanroom environment, forming the complete flight model. Pre-launch environmental testing commenced in March 2025 at ESTEC, encompassing vibration simulations, thermal vacuum cycles, and checks to verify performance under space conditions. These phases were completed in July 2025. Following the environmental tests, final instrument re-checks and software validations were conducted in July–August 2025. As of November 2025, the spacecraft is in the final integration phase at ESTEC, preparing for shipment to Europe's Spaceport in for the 2026 launch.

International Collaboration

The SMILE mission represents a pioneering collaboration between the (ESA) and the (CAS), marking the first fully joint science mission from concept to operations between the two agencies. ESA leads the scientific aspects and development of the payload module, while CAS is responsible for the spacecraft bus, , and mission operations. This partnership builds on prior ESA-CAS collaborations, such as the Cluster-Double Star mission, and was formalized through a joint mission call issued in January 2015, with SMILE selected from 13 proposals. Key institutions play specialized roles in the mission's implementation. In , leads the payload module assembly on behalf of ESA, integrating the European instruments at facilities like ESTEC in the . The Soft X-ray Imager (SXI) is led by the , with scientific oversight from (UCL), supported by funding totaling over £13.5 million for instrument development and team roles. In , the National Space Science Center (NSSC) under CAS handles integration, testing, and overall mission coordination in . The Centre Spatial de in contributes critical components, including optical elements for the Imager (UVI). Funding is shared equally, with ESA's contribution estimated at approximately €46 million for its share of the total €92 million mission cost, covering payload and launch elements like the Vega-C rocket. Broader international involvement enhances SMILE's scientific reach. Canada participates through the Canadian Space Agency, providing expertise and funding (nearly CAD $11 million) for the UVI instrument design via . NASA's contributions include a guest investigator program to support analysis of SMILE data alongside missions like Cluster, fostering global data sharing for studies. Over 250 scientists from multiple countries, including contributions from institutions like the Max Planck Institute for Solar System Research in and IRAP in , form the international science team.

Scientific Objectives

Core Research Questions

The Solar wind Magnetosphere Ionosphere Link Explorer (SMILE) mission addresses the central scientific challenge of understanding how solar wind energy, momentum, and mass enter and dissipate within the Earth's magnetosphere-ionosphere system. This inquiry seeks to elucidate the pathways through which influences geomagnetic activity, providing insights into the transfer of plasma and energy across magnetospheric boundaries and their subsequent effects on ionospheric dynamics. Key sub-questions guiding SMILE's investigations include the dominant modes of solar wind-magnetosphere coupling, particularly the fundamental processes at the dayside interaction where facilitates energy influx. Another focuses on how dayside reconnection events and nightside reconnection processes interconnect with ionospheric responses, such as auroral and electrodynamic coupling. Additionally, the mission probes the role of coronal mass ejections (CMEs) in driving substorms, examining how these intense structures trigger global magnetospheric reconfiguration and substorm cycles. These questions address critical gaps in , especially during when enhanced solar activity amplifies magnetospheric dynamics and risks. By targeting these interactions, contributes to broader models of solar-terrestrial coupling, linking dayside plasma entry to ionospheric phenomena like auroral ovals.

Targeted Phenomena

The mission targets the dayside magnetospheric boundaries, including the magnetosheath, , , and magnetospheric cusps—the regions separating Earth's from the —where soft emissions arise from charge exchange interactions between ions and neutral atoms in the . These emissions enable remote imaging of their positions and dynamics, including inward erosion of the during periods of enhanced pressure and subsequent outward expansion, providing insights into rates and plasma flux transport across these interfaces. SMILE will also characterize the auroral ovals, particularly in the , through ultraviolet emissions produced by energetic particle precipitation into the . These ovals mark regions of magnetosphere-ionosphere coupling, with observations revealing global distributions, poleward boundary movements, and equatorward expansions that correlate with magnetotail flux loading and unloading. Additionally, the mission focuses on substorm cycles, involving nightside that releases stored energy, driving plasma flows toward the and enhancing currents that power auroral brightenings. By tracking these sequences from growth phase to expansion and recovery, SMILE aims to delineate triggers such as auroral beads and the linkage between tail dynamics and ionospheric responses. For (CME) impacts, SMILE will observe global magnetospheric responses, including compression of the , enhancements in the ring current, and the onset of geomagnetic storms driven by prolonged southward interplanetary . These events amplify energy transfer into the inner , leading to intensified auroral activity and prolonged substorm-like disturbances. The ionospheric cusp, a key region of direct entry, will be targeted to study particle acceleration and where open lines connect to the dayside , manifesting as latitudinal shifts in response to reconnection and cusp funnels. Such observations will directly inform core research questions on the modes of energy transfer across the solar wind--ionosphere system.

Spacecraft Design

Technical Specifications

The SMILE spacecraft features a launch mass of 2,300 kg, including , and a dry mass of 707 kg without . Its power system generates 850 from two deployable solar arrays with a combined area of 4.1 , supported by lithium-ion batteries with 60 Ah capacity. The structure comprises a platform developed by the and an ESA payload module constructed by , with stowed dimensions of 2.8 m × 2.8 m × 3.5 m and deployed dimensions of 4.8 m × 9.8 m × 3.5 m. Attitude and control employs three-axis stabilization via four reaction wheels, two trackers, three fiber optic gyroscopes, and twelve 10 N thrusters, achieving an absolute pointing accuracy of ≤ 0.02° (3σ). The communication subsystem utilizes S-band frequencies for , telecommands, and at rates of 2–16 kbps, while X-band handles downlink, transmitting an average of 32–40 Gbit per during 10–15 minute passes.

Orbital and Operational Parameters

The SMILE spacecraft will be launched on a Vega-C rocket from Europe's in , , with a targeted liftoff in 2026. Following initial injection into a parking trajectory, the spacecraft's onboard propulsion module will perform a series of burns to transfer it to the nominal over approximately one month. The operational orbit is a highly elliptical, Molniya-type trajectory designed to optimize observations of Earth's and auroral regions. It features a perigee altitude of 5,000 km, an apogee altitude of 121,182 km (approximately 19 radii), an inclination of 73° to enable views of the northern auroral oval, and an of about 51 hours. This configuration allows the to spend roughly 80% of its time—equivalent to nine months per year—at high altitudes beyond the Van Allen radiation belts, minimizing exposure while providing extended viewing opportunities toward the Sun and dayside . The nominal mission duration is three years, during which SMILE will conduct continuous science operations, with potential for an extended phase subject to spacecraft health and fuel reserves. Operational modes are tailored to the : at apogee, the spacecraft will dwell for up to 40 hours per orbit, enabling remote-sensing imaging of the magnetosheath and auroras; near perigee, it will perform in-situ measurements of plasma and . Attitude control will maintain the desired pointing using star trackers, gyroscopes, and reaction wheels, supported by the spacecraft's power system. Data acquisition will generate up to 40 Gbit per orbit, downlinked via X-band to primary ground stations including the Sanya station in (operated by the ) and the O'Higgins Antarctic station (operated by the for ESA). At end-of-life, the spacecraft will execute a deorbit maneuver using remaining propellant to lower perigee into the atmosphere for controlled reentry, complying with international space debris mitigation guidelines that require removal from protected orbits within 25 years.

Instruments

Soft X-ray Imager (SXI)

The Soft X-ray Imager (SXI) is the primary instrument on the SMILE spacecraft for capturing wide-field soft X-ray emissions from Earth's magnetosphere. Developed by the University of Leicester in the United Kingdom, it utilizes lobster-eye optics based on microchannel plate technology to focus incoming X-rays onto a focal plane assembly of two custom charge-coupled device (CCD) detectors. This design enables a rectangular field of view of 15.5° × 26°, allowing the instrument to survey large-scale structures in the dayside magnetosphere from the spacecraft's highly elliptical orbit. The SXI is optimized for the energy range of 0.2–2.5 keV, with a detectable range up to 5.0 keV, and particular sensitivity to characteristic emission lines from oxygen (such as O VII at ~0.57 keV and O VIII at ~0.65 keV) and (He-like lines around 0.7 keV) produced through charge exchange interactions with exospheric neutrals. These emissions trace plasma distributions at key magnetospheric boundaries, enabling the instrument to produce global images of the dayside and polar cusps. With an of approximately 11–15 arcminutes (FWHM across 60% of the detector plane), effective resolution down to 1.5 arcminutes under optimal conditions for boundary mapping, and of 50 eV (FWHM), the SXI supports detailed mapping of boundary dynamics, operating at a of up to one image per minute during visibility periods. Over the nominal three-year mission lifetime, it is projected to generate approximately 10,000 such images, offering unprecedented temporal coverage of responses to variations. Ground calibration of the flight model SXI, including optic alignment, detector quantum efficiency, and effective area measurements, was completed in 2024 at facilities in the UK and , verifying performance ahead of spacecraft integration. The flight model was integrated into the by early 2025, with environmental testing completed by mid-2025. The SXI's plasma imaging will complement simultaneous observations from the Ultraviolet Imager (UVI) to provide multi-wavelength context for magnetospheric processes.

Ultraviolet Imager (UVI)

The Imager (UVI) is a far- camera aboard the SMILE spacecraft, designed to capture images of Earth's northern auroral regions and monitor dynamic ionospheric responses to forcing. It employs a co-axial four-mirror all-reflective with specialized thin-film coatings to focus light onto an intensified (ICCD) detector, enabling high-sensitivity observations in the low-light environment of . The instrument's development is led by the National Space Science Center (NSSC) in , with key contributions from the in for detector integration and the Centre Spatial de Liège (CSL) in for precision optical components such as the mirrors. The flight model was integrated into the spacecraft by early 2025, with environmental testing completed by mid-2025. UVI targets emissions in the 160–180 nm wavelength range, specifically the N₂ Lyman-Birge-Hopfield (LBH) bands, which are prominent in auroral precipitation and minimally contaminated by daytime glow. The instrument provides a circular of 9.97°, sufficient to encompass the entire auroral oval from the spacecraft's , with a of approximately 80 km at apogee. Equipped with a 512×512 ICCD featuring a CsI photocathode and photon-counting mode for enhanced signal-to-noise in faint emissions, UVI acquires full-frame images every 60 seconds under nominal conditions, with the option to increase cadence to 30 seconds during intense substorms. In the SMILE mission, UVI plays a central role in mapping the morphology and of the northern auroral , including substorm onset and expansion, to reveal how magnetospheric processes drive ionospheric patterns. By providing contextual UV imagery alongside wide-field X-ray views of magnetospheric boundaries from the Soft X-ray Imager (SXI), UVI facilitates correlative studies of dayside reconnection and its propagation to auroral displays. This dual-imaging approach elucidates energy transfer across the solar wind-magnetosphere-ionosphere system, addressing key questions on global coupling dynamics. Ground of UVI was conducted extensively prior to spacecraft integration, encompassing geometric assessments to correct optical distortions and establish a of 77.91 mm, as well as photometric evaluations to measure sensitivity (down to 61.8 Rayleighs per ) and ensure flat-field uniformity across the detector. These tests, performed in vacuum UV facilities, validated the instrument's performance for in-orbit auroral monitoring and included simulations of expected LBH emission profiles.

Light Ion Analyser (LIA)

The Light Ion Analyser (LIA) is an in-situ plasma instrument aboard the SMILE spacecraft, developed by the National Space Science Center (NSSC) of the (CAS) to measure key properties of and magnetosheath ions. It utilizes a top-hat electrostatic analyzer design, consisting of two identical units mounted on opposite sides of the spacecraft to achieve full 4π steradian coverage for detecting incoming particles from all directions. Each unit incorporates electrostatic deflectors and microchannel plate detectors to analyze ion trajectories, enabling the determination of three-dimensional velocity distributions. The flight model was integrated into the spacecraft by early 2025, with environmental testing completed by mid-2025. The LIA operates across an energy range of 0.05 to 20 keV/q, targeting protons and alpha particles, with time-of-flight mass resolution to differentiate species such as H⁺ and He²⁺. It provides an energy resolution of 7% (FWHM) and ranging from 5.625° to 22.5° in and 7.5° to 30° in , depending on operation mode, supporting a sampling rate of 1 spectrum per second in , with burst modes capable of 0.5-second for high-cadence events. These specifications allow for precise derivation of plasma moments, including , , bulk , and , under varying conditions. In the context of the SMILE mission, the plays a critical role in monitoring upstream conditions to provide contemporaneous plasma data that correlates with remote observations from the Soft Imager (SXI) and Imager (UVI), facilitating studies of magnetosphere-ionosphere coupling and dynamic responses to variations. The 's ion measurements are briefly contextualized with data from the onboard (MAG) to characterize the full plasma environment. Comprehensive ground , including particle beam tests performed in 2024, has verified the instrument's performance, achieving measurement accuracies better than 20% for key .

Magnetometer (MAG)

The Magnetometer (MAG) instrument on the SMILE spacecraft is a digital fluxgate designed to provide in-situ measurements of the in the solar wind, magnetosheath, and . It consists of two tri-axial fluxgate sensor heads mounted on a deployable boom approximately 3 meters long, with one sensor at the boom tip and the other positioned 80 cm inboard to minimize interference and enable error correction through differential measurements. This dual-sensor configuration offers , including backup power supplies and communication interfaces, ensuring reliable operation throughout the mission. The instrument was developed by the National Space Science Center (NSSC) of the (CAS), in collaboration with international partners including contributions from . The flight model was integrated into the by early 2025, with environmental testing completed by mid-2025. The MAG provides vector measurements of the magnetic field, capturing both direction and magnitude across three orthogonal components. Its measurement range spans ±12,800 nT, suitable for the expected fields in the mission's operational environment, with a sensitivity of approximately 0.1 nT resolution and absolute accuracy goals of 0.5 nT. Sampling rates reach up to 40 Hz, allowing detection of dynamic phenomena on timescales relevant to solar-terrestrial interactions. These capabilities enable the instrument to monitor interplanetary orientation and strength simultaneously with observations. In the context of SMILE's science goals, the MAG plays a key role in detecting signatures of magnetospheric currents, at the , and substorm onsets by tracking field variations and fluctuations. It complements plasma measurements from the Light Ion Analyser (), such as correlating ion flux enhancements with perturbations during reconnection events. Post-launch, will involve boom deployment verification and periodic spacecraft rolls in low-variability regions like the magnetospheric lobes to correct for offsets and thermal drifts.

Ground Operations

Working Groups

The SMILE mission is supported by a network of specialized working groups that coordinate international scientific efforts, ensuring effective data utilization and mission operations. These groups, established under the joint ESA-Chinese Academy of Sciences (CAS) framework, facilitate collaboration among global researchers to address the mission's goals of studying solar wind-magnetosphere-ionosphere interactions. The In-Situ Science Working Group (ISWG) focuses on the interpretation of data from the and instruments, optimizing their design, operational modes, calibration, and data products to capture plasma and measurements within the . Led by Lei Dai at the National Space Science Center (NSSC) under CAS, the ISWG discusses pointing accuracy requirements and in-situ observation strategies to maximize scientific return during SMILE's . The Modeling Working Group (MWG) develops advanced simulations to model magnetosphere-ionosphere coupling, including the generation of synthetic soft X-ray and ultraviolet images for comparison with observations. Co-chaired by Hyunju Connor at NASA Goddard Space Flight Center, Tianran Sun at NSSC/CAS, and Andrey Samsonov at , the group includes contributions from institutions such as the , where Connor previously advanced modeling techniques for forecasting. The MWG conducts regular teleconferences and joint meetings to refine global magnetohydrodynamic models and support instrument validation. The Ground-Based and Additional Science Working Group (GBASWG) integrates complementary data from ground-based and other space-based assets, such as radar and optical observations from the mission array and SuperDARN network, to provide multi-scale context for SMILE's . Chaired by Jenny Carter at the , this international group develops community tools, visualization software, and coordinated observation campaigns to enhance the analysis of auroral dynamics and substorms. The Public Engagement Working Group (PEWG) coordinates outreach and educational initiatives to promote SMILE's science objectives, including workshops, programs, and online resources that highlight the mission's role in understanding . Chaired by Colin Forsyth at the Mullard Space Science Laboratory () and led by ESA with global partners, the group fosters public awareness through multimedia content and collaborative events. Overall coordination of these working groups occurs through the Science Operations Center at NSSC/CAS, which manages mission-level planning and data handling, complemented by ESA's advisory structure and Science Operations Centre at the European Space Astronomy Centre for European contributions and data formats standardization.

Data Processing and Analysis

The data flow for begins with raw received via ground stations such as the Sanya X-band station in and the O’Higgins station in , which downlink data approximately every two days over the planned five-year operational phase. This is processed at the Ground Support System (GSS) in Huairou, , to generate Level 0 products, including uncalibrated packets. These are then transferred to the ESA Science Operations Centre (SOC) via secure protocols like SFTP and GFTS for higher-level processing, yielding Level 1 calibrated data (e.g., instrument-specific corrections applied to raw counts), Level 2 products (e.g., geolocated images), and Level 3 derived parameters (e.g., background-subtracted soft images and plasma boundary maps). pipelines, utilizing Docker-based tools from instrument teams, enable rapid generation of preliminary products for initial assessment shortly after each orbital pass. Archiving of SMILE data is managed dually by the (CAS) Space Science Data Center (SSDC) and ESA's SMILE Archive at the European Space Astronomy Centre (ESAC), ensuring redundancy and long-term preservation in an Open Archival Information System (OAIS)-compliant framework. The SSDC handles raw , auxiliary files, and metadata with over 5.6 PB of online storage and a 1500-slot tape library for offline retention, while ESA's archive integrates all processing levels into the broader HelioPhysics Archive for unified access via graphical user interfaces and Table Access Protocol (TAP) queries. Data become openly accessible to the scientific community after a proprietary period, typically 12 months for guest investigators, in accordance with ESA's Data Rights Policy. Analysis of SMILE data employs custom software pipelines for co-registering soft (SXI) and ultraviolet (UVI) images, such as end-to-end simulators that align 2D projections with 3D magnetospheric models to reconstruct plasma boundaries. These tools integrate magnetohydrodynamic (MHD) simulations from models like OpenGGCM and BATS-R-US to forward-model emissions based on plasma density and velocity, enabling inversion techniques for deriving shapes. Advanced methods, including AI-driven approaches like OESA-UNet and DeepLabV3+, facilitate automated detection and restoration of features in limited-field-of-view images, supporting the Modeling Working Group's efforts in event selection and health monitoring. Validation of processed data involves cross-checks with ground-based observations, such as auroral emissions from SuperDARN radars and field-aligned currents from , alongside space-based datasets from missions like DMSP/SSUSI for UV comparisons and for exospheric density benchmarks. The Quick Look Analysis (QLA) tool at ESA SOC provides graphical interfaces for verifying data consistency, syntax, and instrument performance against the Master Science Plan, with feedback loops to the GSS for workflow optimization. Data Quality Assessment and Assurance Systems (DQAAS) further ensure integrity across processing levels through automated checks on format compliance and metadata accuracy. Expected scientific outputs include global 2D maps of locations from SXI-derived boundaries and 3D reconstructions linking UVI-observed open-closed field lines to magnetosheath plasma distributions, refined via field-line tracing in models like Tsyganenko T96. These products, combined with in-situ measurements from and MAG, aim to provide continuous monitoring of magnetospheric responses to variations, enhancing empirical models of subsolar distances and flaring angles.

Timeline and Status

Key Milestones

The development of the spacecraft has progressed through several key phases since its initial selection, marked by international collaboration between the (ESA) and the (CAS). Below is a chronological summary of major achievements and decisions.
  • 2015: was selected by ESA's Science Programme Committee as the F1 mission candidate in early , initiating the joint European-Chinese effort to study solar wind-magnetosphere interactions.
  • 2016–2019: The mission was adopted by CAS in 2016 and by ESA in March 2019, with Phase B (preliminary design) completed by early 2019, including the Payload Module Preliminary Design Review and the start of Phase B2 implementation.
  • 2023: The Mission Critical Design Review was successfully passed in June in , confirming the spacecraft's design readiness for production and integration.
  • 2024: Key instrument deliveries included the Soft Imager flight model in August and the Imager flight model in , alongside completion of platform flight model integration and subsystem environmental tests by September.
  • 2025: Full spacecraft assembly was achieved in January by joining the payload and platform modules; environmental testing, including thermal vacuum and vibration campaigns, occurred from February to September at ESA's ESTEC facility.
  • 2026: The planned launch is scheduled for early 2026 aboard a Vega-C from Europe's in , with projections targeting April.

Current Developments (as of 2025)

In January 2025, the SMILE spacecraft achieved a major milestone with the successful integration of its European payload module and Chinese service platform (bus) at the National Space Science Center (NSSC) in , , followed by final assembly at ESA's ESTEC facility in the on January 21. This step united the spacecraft's core components, enabling subsequent system-level testing to verify interfaces and overall functionality. Testing progressed steadily throughout the first half of 2025, with vibration and acoustic environmental tests completed by the end of April at ESTEC, simulating launch stresses to confirm structural integrity. Thermal vacuum testing, which replicates space conditions including extreme temperatures and vacuum, began in June and continued through early September in ESA's Large Space Simulator, with all phases concluding successfully by September 2025. These tests validated the spacecraft's resilience, paving the way for pre-launch preparations. The mission's launch, originally targeted for late , has been rescheduled to early —specifically —primarily due to Vega-C launcher scheduling constraints at Europe's Spaceport in and to optimize observations during the solar cycle's peak activity phase. Earlier supply chain disruptions, stemming from global impacts like the , have been fully resolved, and as of June 2025, all subsystems—including the instruments and platform—were verified as fully functional following integrated checks. In the third quarter of 2025, preparations advanced with rehearsals, highlighted by the China-Europe Operation Validation Test conducted August 4–8, which confirmed network connectivity, data exchange protocols, and operational readiness between international teams. Concurrently, science team training sessions focused on mission operations and data handling, ensuring coordinated support for the upcoming launch and initial phase. In October 2025, the mission passed the China-Europe Joint Qualification and Flight Acceptance Review (QFAR) on October 28 at ESA's ESTEC in , , confirming the spacecraft's readiness following assembly, integration, and environmental testing. As of November 2025, has advanced to the launch phase, with final preparations underway for the 2026 liftoff.

Outreach and Recognition

Public Engagement Efforts

The (ESA) and its partners have implemented various outreach programs to engage schools and educators with the mission. A key initiative is the SMILE for Schools program, integrated into the ORBYTS (Open University Research BY Targeted Students) project, which involves 14-year-old students in analyzing real mission-related data on and magnetospheric interactions, with the goal of producing peer-reviewed publications co-authored by participants. This program includes workshops tailored for disadvantaged pupils in locations such as and , fostering hands-on learning about solar-terrestrial physics. Additionally, videos providing insights into the mission's assembly process at ESA's ESTEC site have been released as part of the "Let's Smile" series. Media and events play a central role in broadening awareness of SMILE's focus on aurora science and magnetospheric dynamics. The mission team has organized webinars and participated in exhibits at science fairs, such as the British Science Festival and the Royal Society Summer Exhibition, highlighting the spacecraft's instruments and their role in observing interactions. campaigns, coordinated through ESA platforms and project-specific channels, feature updates on auroral phenomena and mission progress to engage global audiences, often tying into real-time events like the 2024 solar storms to explain impacts. Citizen science efforts aim to complement SMILE's Ultraviolet Imager (UVI) data by involving the public in ground-based observations. Potential applications for reporting auroral sightings are under development, drawing inspiration from existing projects like the Space Weather UnderGround magnetometer network and NASA's Aurorasaurus, to create a crowdsourced for validating . Educational resources further support these initiatives, including animations depicting magnetosphere-solar wind interactions produced by ESA, as well as partnerships with universities for student-led projects on aurora modeling. The Public Engagement (PE) working group, which reports to the broader Science Working Team, coordinates these activities and oversees a dedicated team responsible for global events, including China-ESA workshops that promote on the mission's collaborative aspects. This group also develops accessible materials, such as the children's book Aurora and Spotty and the Tactile Space project for visually impaired and neurodiverse communities, ensuring inclusive participation in SMILE's scientific narrative.

Awards and Honors

The SMILE mission was selected in November 2015 as ESA's second S-class mission under the programme (2015-2025), honouring its innovative proposal for imaging interactions with Earth's using soft and techniques from a joint ESA-Chinese Academy of Sciences collaboration.

References

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