Jump to content

SMILE (spacecraft)

From Wikipedia, the free encyclopedia

Solar wind Magnetosphere Ionosphere Link Explorer
Artist's impression of the SMILE spacecraft
Mission typeMagnetospheric mission
OperatorESA-CAS
Websitecosmos.esa.int/web/smile/links
Mission duration3 years (nominal)[1]
Spacecraft properties
ManufacturerAirbus (payload module)
Launch mass2200 kg
Dry mass708 kg
Power850 W
Start of mission
Launch dateQ3 2025 (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 our 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 April 2024, SMILE is expected to launch in late 2025.[2]

Overview

[edit]

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). 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 to a payload module containing nearly all of the scientific instruments and an X-band communications system, provided by ESA. The payload module will be built by Airbus.[5] The platform is composed of a propulsion and a service module, together with the two detectors (or heads) of the ion instrument. The Mission Operations Center will be run by CAS; both organizations will jointly operate the Science Operations Center.

Instruments

[edit]

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

  • 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 is being developed, built, and will be calibrated at the University of Leicester, UK, and other institutions throughout Europe. CCDs are being procured from Teledyne e2v, UK, by ESA and calibrated by The Open University, UK.
  • 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 155 to175 nm using a CMOS 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 CMOS detector.[6] 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.
  • 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.
  • 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

[edit]

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

[edit]

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

[edit]

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.)[7]
  • test M. Collier & H. Connor on magnetopause tracing method by using the same SXI specification[8] 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

[edit]

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

[edit]

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.

Space Lates at the National Space Centre
Jennifer Carter, University of Leicester, during her presentation

Result highlights

[edit]

2024

[edit]
  • January - Special Issue on Modeling and Data Analysis Methods for the SMILE mission with 21 refereed papers published in Earth and Planetary Physics journal, see preface[9]

2023

[edit]

2022

[edit]

2021

[edit]

2020

[edit]

2019

[edit]

2018

[edit]
  • December 17 - ESA SMILE definition study report [3]

Awards

[edit]

2020

[edit]

History

[edit]

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.[22] The SMILE mission proposal[23] 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.[24] The Mission System Requirements Review was completed in October 2018, and ESA Mission Adoption by the Science Programme Committee was granted in March 2019.[25] SMILE successfully completed the Spacecraft and Mission Critical Design Review (CDR) in June 2023 in Shanghai.[26]

References

[edit]
  1. ^ a b c "SMILE Mission Overview". Chinese Academy of Sciences. Retrieved 14 February 2023.
  2. ^ a b "Smiles all round: Vega-C to launch ESA solar wind mission". ESA. 30 April 2024. Retrieved 27 June 2024.
  3. ^ a b c Branduardi-Raymont, G.; Wang, C.; Escoubet, C.P.; et al. (2018). ESA SMILE definition study report (PDF) (Technical report). European Space Agency. pp. 1–84. doi:10.5270/esa.smile.definition_study_report-2018-12. S2CID 239612452. ESA/SCI(2018)1. Archived (PDF) from the original on 22 April 2023.
  4. ^ "SMILE: Summary". UCL Mullard Space Science Laboratory. Retrieved 19 December 2018.
  5. ^ "Airbus brings a SMILE to ESA". Airbus. Retrieved 31 July 2019.
  6. ^ "SMILE instruments". National Space Science Center. Retrieved 9 October 2024.
  7. ^ Jorgensen, A.M.; T. Sun; C. Wang; L. Dai; S. Sembay; F. Wei; Y. Guo; R. Xu (2019). "Boundary Detection in Three Dimensions With Application to the SMILE Mission: the Effect of Photon Noise". Journal of Geophysical Research: Space Physics. 124 (6): 4365. Bibcode:2019JGRA..124.4365J. doi:10.1029/2018JA025919. hdl:2381/45334. S2CID 204266610.
  8. ^ Collier, M.R.; Connor, H.K. (2018). "Magnetopause Surface Reconstruction from Tangent Vector Observations". Journal of Geophysical Research: Space Physics. 123 (12): 9022–9034. Bibcode:2018JGRA..12310189C. doi:10.1029/2018JA025763. hdl:2060/20180008652.
  9. ^ Sun, T.R.; Connor, H.; Samsonov, A. (2024). "Preface to the Special Issue on Modeling and Data Analysis Methods for the SMILE mission". Earth and Planetary Physics. 8 (1): 1–4. Bibcode:2024E&PP....8....1S. doi:10.26464/epp2023089.
  10. ^ Dai, L.; Han, Y.; Wang, C.; Yao, S.; Gonzalez, W.; Duan, S.; Lavraud, B.; Ren, Y.; Guo, Z. (2023). "Geoeffectiveness of Interplanetary Alfvén Waves. I. Magnetopause Magnetic Reconnection and Directly Driven Substorms". The Astrophysical Journal. 945 (47): 47. Bibcode:2023ApJ...945...47D. doi:10.3847/1538-4357/acb267.
  11. ^ Samsonov, A.; Carter, J.A.; Read, A.; Sembay, S.; Branduardi-Raymont, G.; Sibeck, D.; Escoubet, P. (2022). "Finding magnetopause standoff distance using a soft X-ray imager: 1. Magnetospheric masking". Journal of Geophysical Research: Space Physics. 127 (12). Bibcode:2022JGRA..12730848S. doi:10.1029/2022JA030848.
  12. ^ Samsonov, A.; Sembay, S.; Read, A.; Carter, J. A.; Branduardi-Raymont, G.; Sibeck, D.; Escoubet, P. (2022). "Finding magnetopause standoff distance using a Soft X-ray Imager: 2. Methods to analyze 2-D X-ray images". Journal of Geophysical Research: Space Physics. 127 (12). Bibcode:2022JGRA..12730850S. doi:10.1029/2022JA030850.
  13. ^ Guo, Y.; Sun, T.; Wang, C.; Sembay, S. (2022). "Deriving the magnetopause position from wide field-of-view soft X-ray imager simulation". Sci. China Earth Sci. 65 (8): 1601–1611. Bibcode:2022ScChD..65.1601G. doi:10.1007/s11430-021-9937-y. S2CID 250065345.
  14. ^ Huang, Y.; Dai, L.; Wang, C.; Xu, R.L.; Li, L. (2021). "A new inversion method for reconstruction of plasmaspheric He+ density from EUV images". Earth Planet. Phys. 5 (2): 218–222. Bibcode:2021E&PP....5..218H. doi:10.26464/epp2021020 (inactive 1 November 2024).{{cite journal}}: CS1 maint: DOI inactive as of November 2024 (link)
  15. ^ Su, B.; Kong, L.G.; Zhang, A.B.; Klecker, B.; Escoubet, C.P.; Kataria, D.O.; Dai, L. (2021). "Performance and simulated moment uncertainties of an ion spectrometer with asymmetric 2π field of view for ion measurements in space". Review of Scientific Instruments. 92 (2): 024501. doi:10.1063/5.0028866. PMID 33648106.
  16. ^ Connor, H. K.; Sibeck, D. G.; Collier, M. R.; et al. (2021). "Soft X-ray and ENA imaging of the Earth's dayside magnetosphere". Journal of Geophysical Research: Space Physics. 126 (3): e2020JA028816. Bibcode:2021JGRA..12628816C. doi:10.1029/2020JA028816. PMC 7988574. PMID 33777610.
  17. ^ Tian, C.-J.; Du, H.-D.; Yang, P.-L.; Zhou, Z.-M.; Zhao, X.-F.; Zhou, S. (2020). "Automatic auroral boundary determination algorithm with deep feature and dual level set". Journal of Geophysical Research: Space Physics. 125 (10). Bibcode:2020JGRA..12527833T. doi:10.1029/2020JA027833. S2CID 224859541.
  18. ^ Sun, T.; Wang, C.; Connor, H.K.; Jorgensen, A.M.; Sembay, S. (2020). "Deriving the magnetopause position from the soft X-ray image by using the tangent fitting approach". Journal of Geophysical Research: Space Physics. 125 (9). Bibcode:2020JGRA..12528169S. doi:10.1029/2020JA028169. S2CID 225422666.
  19. ^ Samsonov, A.A.; et al. (2020). "Is the relation between the solar wind dynamic pressure and the magnetopause standoff distance so straightforward?". Geophys. Res. Lett. 47 (8). Bibcode:2020GeoRL..4786474S. doi:10.1029/2019GL086474. hdl:2027.42/154966.
  20. ^ Connor, H.K.; Carter, J.A. (2019). "Exospheric neutral hydrogen density at the nominal 10 RE subsolar point deduced from XMM-Newton X-ray observations". Journal of Geophysical Research: Space Physics. 124 (3): 1612–1624. Bibcode:2019JGRA..124.1612C. doi:10.1029/2018JA026187.
  21. ^ Jorgensen, A.M.; Sun, T.; Wang, C.; Dai, L.; Sembay, S.; Zheng, J.; Yu, X. (2019). "Boundary Detection in Three Dimensions With Application to the SMILE Mission: the Effect of Model-fitting Noise". Journal of Geophysical Research: Space Physics. 124 (6): 4341–4355. Bibcode:2019JGRA..124.4341J. doi:10.1029/2018JA026124. hdl:2381/45333.
  22. ^ "ESA and Chinese Academy of Sciences to study Smile as joint mission". ESA. 22 June 2015. Retrieved 5 October 2015.
  23. ^ Branduardi-Raymont, Graziella; Wang, Chi. "Joint Scientific Space Mission Chinese Academy of Science (CAS) - European Space Agency (ESA) PROPOSAL SMILE: Solar wind Magnetosphere Ionosphere Link Explorer" (PDF). Retrieved 4 June 2015.
  24. ^ "Request for Information (RFI) for the provision of the payload module for the joint ESA-China SMILE mission". ESA. 18 December 2015. Retrieved 8 January 2016.
  25. ^ "SMILE mission summary". ESA. 22 April 2021. Retrieved 22 April 2021.
  26. ^ "Sino-European joint space mission enters flight model phase". Space Daily. 11 July 2023. Retrieved 15 September 2023.
[edit]


Retrieved from "https://en.wikipedia.org/w/index.php?title=SMILE_(spacecraft)&oldid=1261447341"