CHEOPS

From Wikipedia, the free encyclopedia
Jump to navigation Jump to search
Characterising Exoplanets Satellite (CHEOPS)
CHEOPS spacecraft
Artist's impression of the CHEOPS space observatory
Mission typeExoplanetology, astrophysics
OperatorSwiss Space Office
ESA
COSPAR ID2019-092B
Websitecheops.unibe.ch
sci.esa.int/cheops
Mission durationPlanned: 3.5 years
Elapsed: 1 month and 4 days
Spacecraft properties
Spacecraft typeSpace observatory
BusSEOSAT platform[1]
ManufacturerAirbus Defence and Space
Launch mass≈300 kg (660 lb)[2]
Payload mass58 kg (128 lb)[3]
Dimensions1.5 m × 1.5 m × 1.5 m (4 ft 11 in × 4 ft 11 in × 4 ft 11 in)
Power64 watts[4]
Start of mission
Launch date18 December 2019 at 9:54 CET (08:54 GMT)[5]
RocketSoyuz VS23[6][7]
Launch siteGuiana Space Centre
(Ensemble de Lancement Soyouz)
ContractorArianespace[8][9]
Orbital parameters
Reference systemGeocentric
RegimeSun-synchronous 6 am/pm
Perigee altitude700 km (430 mi)[9]
Apogee altitude700 km (430 mi)[9]
RAAN6am
Main telescope
TypeRitchey–Chrétien
frame-transfer back-side illuminated CCD
Diameter32 cm (13 in)[9]
Focal lengthF/8
Wavelengths330 to 1100 nm
Transponders
Capacity1.2 GBit/day downlink[10]
Instruments
Photometer[11]
CHEOPS mission logo
Mission insignia  

CHEOPS (CHaracterising ExOPlanets Satellite) is a European space telescope to determine the size of known extrasolar planets, which will allow the estimation of their mass, density, composition and their formation. Launched on 18 December 2019, it is the first Small-class mission in ESA's Cosmic Vision science programme.[12]

The small satellite features an optical Ritchey–Chrétien telescope with an aperture of 30 cm, mounted on a standard small satellite platform. It was placed into a Sun-synchronous orbit of about 700 km (430 mi) altitude.

Science overview[edit]

Thousands of exoplanets have been discovered by the end of the 2010s;[13] some have minimum mass measurements from the radial velocity method while others that are seen to transit their parent stars have measures of their physical size. Few exoplanets to date have highly accurate measures for both mass and radius, limiting the ability to study the variety in bulk density that would provide clues as to what materials they are made of and their formation history.[14] For the planned mission duration of 3.5 years, CHEOPS is to measure the size of known transiting exoplanets orbiting bright and nearby stars[15] as well as search for transits of exoplanets previously discovered via radial velocity. Scientists behind the project expect these well-characterised transiting exoplanets to be prime targets for future observatories such as JWST or the extremely large telescopes.[16]

History[edit]

CHEOPS' mirror

Organized as a partnership between the European Space Agency (ESA) and the Swiss Space Office, CHEOPS was selected in October 2012 from among 26 proposals as the first S-class ("small") space mission in ESA's Cosmic Vision programme.[15] ESA is the mission architect and responsible for the spacecraft and launch opportunity procurement. The project is led by the Center for Space and Habitability at the University of Bern, Switzerland, with contributions from other Swiss and European universities. The Principal Investigator for the science instrument is Willy Benz at the University of Bern and the Principal Scientist from ESA is Kate Isaak. After a competition phase, Airbus Defence and Space in Spain was selected as the spacecraft builder.[6][17] The ESA mission cost is capped at €50 million.[6] Media Lario S.r.l. (Italy) was responsible for the optical finishing of the primary optical element[18].

Spacecraft[edit]

The satellite has dimensions of approximately 1.5 × 1.5 × 1.5 m and a hexagonal base structure. The bus of the CHEOPS spacecraft is based on the SEOSat platform.[10]

Sunshield[edit]

A sunshield mounted on the platform protects the radiator and detector housing against the Sun, and it also features solar panels for the electrical power subsystem. The sunshield wraps around the hexagonal bus.[10]

Attitude and orbit control system (AOCS)[edit]

The control system is 3-axis stabilized, but nadir locked, ensuring that one of the spacecraft axes is always pointing towards the Earth. During each orbit, the spacecraft will slowly rotate around the telescope line-of-sight to keep the focal plane radiator oriented towards cold space, enabling passive cooling of the detector. The typical observation duration will be 48 hours. During a typical 48-hour observation CHEOPS will have a pointing stability of better than eight arcsec at 95% confidence.[10][19]

CHEOPS Instrument System (CIS)[edit]

The detector, support electronics, telescope, back-end optics, instrument computer and thermal regulation hardware are known collectively as the CHEOPS Instrument System (CIS). The required photometric precision will be achieved using a single frame-transfer, back-illuminated CCD detector from Teledyne e2v with 1024 × 1024 pixels and a pixel pitch of 13 µm. The CCD is mounted in the focal plane of the telescope, and will be passively cooled to 233 K (−40 °C; −40 °F), with a thermal stability of 10 mK. The telescope is a single medium-size f/8, on-axis Ritchey–Chrétien telescope with a 32 cm (13 in) aperture, mounted on a stiff optical bench.[20] The University of Geneva and the University of Bern provided the powerful photometer.[11]

Plaques[edit]

Two titanium plaques with thousands of miniaturised drawings by children have been fixed to CHEOPS. Each plaque measures nearly 18 cm × 24 cm (7.1 in × 9.4 in). The plaques, prepared by a team at the Bern University of Applied Sciences were unveiled in a dedicated ceremony at RUAG on 27 August 2018.[21] The individual drawings can be found at the website of CHEOPS by clicking on a map of Europe.[22]

Goals[edit]

The main goal of CHEOPS will be to accurately measure the size (radii) of the exoplanets for which ground-based spectroscopic surveys have already provided mass estimates. Knowing both the mass and the size of the exoplanets will allow scientists to determine the planets' density and thus their approximate composition, such as whether they are gaseous or rocky. CHEOPS will be the most efficient instrument to search for shallow transits and to determine accurate radii for known exoplanets in the super-Earth to Neptune mass range (1-6 Earth radius).[6]

CHEOPS will measure photometric signals with a precision limited by stellar photon noise of 150 ppm/min for a 9th magnitude star. This corresponds to the transit of an Earth-sized planet orbiting a star of 0.9 R in 60 days detected with a S/Ntransit >10 (100 ppm transit depth). For example, an Earth-size transit across a G star creates an 80 ppm depth.

The different science objectives require 500 separate target pointings. Assuming 1 hour per pointing the mission duration is estimated at 1175 days or 3.2 years. Together with the 20% of open time available for the community the total duration of the CHEOPS mission is estimated to be 3.5 years.[23]

The spacecraft is to be powered by solar panels that are also part of its sunshield. They will provide 60 W continuous power for instrument operations and allow for at least a 1.2 gigabit/day data downlink capacity.[10] The first data is expected at the beginning of 2020.[24]

Observation priorities[edit]

80% of the science observing time on CHEOPS is dedicated to the CHEOPS Guaranteed Time Observing (GTO) Programme, under the responsibility of the CHEOPS Science Team (chaired by Didier Queloz).[25] The majority of the GTO programme involves the characterization of known transiting exoplanets and improvement of known parameters. Part of the GTO programme is to find transits of known exoplanets that were confirmed by other techniques, such as radial-velocity, but not by the transit-method. Another part of the GTO programme includes exploration of multi-systems and search of additional planets in those systems, for example using the transit-timing-variation (TTV) method.[26]

The other 20% of the science observing time on CHEOPS is made available to the scientific community in the form of an ESA-run Guest Observers' (GO) Programme. Researchers can submit proposals for observations with CHEOPS through an annual Announcements of Opportunity (AO) Program.[27] The approved AO-1 projects include observations of the hot jupiters HD 17156 b, Kelt-22A b,[28] warm jupiter K2-139b,[29] multi systems GJ 9827, K2-138, the exoplanet DS Tuc Ab,[30] 55 Cancri e (likely GTO),[31][32] and other exoplanet science related observations, such as planets around rapidly-rotating stars, planet material around white dwarfs and searching for transiting exocomets around 5 Vulpeculae.[33]

Launch[edit]

CHEOPS launched on board of a Soyuz-Fregat rocket on December 18, 2019 at 9:54 CET from Guiana Space Centre in Kourou, French Guiana.[5][34] The primary payload was the first satellite of ASI's Cosmo-SkyMed Second Generation constellation. The launcher also deployed three CubeSats, including ESA's OPS-SAT.[12]

See also[edit]

References[edit]

  1. ^ [https://directory.eoportal.org/web/eoportal/satellite-missions/c-missions/cheops CHEOPS (CHaracterizing ExOPlanets Satellite). EO Portal Directory. Accessed on 14 December 2019.
  2. ^ [https://en.wikipedia.org/w/index.php?title=CHEOPS&action=edit CHEOPS. Switzerland. Accessed on 14 December 2019.
  3. ^ The CHEOPS Payload: a single Telescope. CHEOPS Home Page. Accessed on December 18 2019.
  4. ^ CHEOPS - Executive Summary
  5. ^ a b "Flight VS23: Soyuz lifts off from the Spaceport in French Guiana". Arianespace. Retrieved 2019-12-18.
  6. ^ a b c d CHEOPS exoplanet mission meets key milestones en route to 2017 launch. ESA, 11 July 2014
  7. ^ CHEOPS has arrived in Kourou. Barbara Vonarburg. 16 October 2019.
  8. ^ "CHEOPS will ride on a Soyuz rocket". cheops.unibe.ch. 6 April 2017. Retrieved 19 September 2017.
  9. ^ a b c d CHEOPS - Mission Status & Summary
  10. ^ a b c d e Stettler, Ulrich. "Spacecraft". CHEOPS. Retrieved 2019-12-16.
  11. ^ a b [https://www.bbc.com/news/science-environment-50804258 Europe's Cheops telescope launches to study far-off worlds. Jonathan AMos, BBC News. 18 December 2019.
  12. ^ a b "Call for Media: Cheops launch to study exoplanets". www.esa.int. Retrieved 2019-12-13.
  13. ^ "ESA CHEOPS mission: Exoplanets in focus". dw.com. Retrieved 2019-12-16.
  14. ^ "ESA is about to launch a space telescope to study how planets are made". newscientist.com. Retrieved 2019-12-16.
  15. ^ a b "ESA Science Programme's new small satellite will study super-Earths". ESA press release. 19 October 2012. Retrieved 19 October 2012.
  16. ^ "ESA satellite set for launch to measure sizes of exoplanets". spaceflightnow.com. Retrieved 2019-12-16.
  17. ^ "Who is Who in CHEOPS - CHEOPS - Cosmos". www.cosmos.esa.int. Retrieved 2019-12-30.
  18. ^ "Cheops". ASI (in Italian). Retrieved 2019-12-18.
  19. ^ "ESA Science & Technology - Spacecraft". sci.esa.int. Retrieved 2019-12-16.
  20. ^ "ESA Science & Technology - Instrument". sci.esa.int. Retrieved 2019-12-16.
  21. ^ "Cheops plaques". www.esa.int. Retrieved 2019-12-16.
  22. ^ Jungo, Janine (2016-03-31). "CHEOPS-Children's Drawings". CHEOPS. Retrieved 2019-12-18.
  23. ^ Broeg, C.; Fortier, A.; Ehrenreich, D.; Alibert, Y.; Baumjohann, W.; Benz, W.; Deleuil, M.; Gillon, M.; Ivanov, A.; Liseau, R.; Meyer, M.; Oloffson, G.; Pagano, I.; Piotto, G.; Pollacco, D.; Queloz, D.; Ragazzoni, R.; Renotte, E.; Steller, M.; Thomas, N. (April 2013). "CHEOPS: A transit photometry mission for ESA's small mission programme". EPJWC. 47: 03005. arXiv:1305.2270. Bibcode:2013EPJWC..4703005B. doi:10.1051/epjconf/20134703005.
  24. ^ "Planned launch of the CHEOPS satellite on December 17 - Communiqués de presse - UNIGE". www.unige.ch. 2019-12-06. Retrieved 2019-12-18.
  25. ^ "The CHEOPS Guaranteed Time Observing Programme - CHEOPS - Cosmos". www.cosmos.esa.int. Retrieved 2019-11-15.
  26. ^ "CHEOPS GTO program: GTO v1.4". 2019-03-19.
  27. ^ "CHEOPS Guest Observers Programme - CHEOPS Guest Observers Programme - Cosmos". www.cosmos.esa.int. Retrieved 2019-11-15.
  28. ^ Labadie-Bartz, Jonathan; Rodriguez, Joseph E.; Stassun, Keivan G.; Ciardi, David R.; Penev, Kaloyan; Johnson, Marshall C.; Gaudi, B. Scott; Colón, Knicole D.; Bieryla, Allyson; Latham, David W.; Pepper, Joshua (2019-01-21). "KELT-22Ab: A Massive, Short-Period Hot Jupiter Transiting a Near-solar Twin". The Astrophysical Journal Supplement Series. 240 (1): 13. arXiv:1803.07559. Bibcode:2019ApJS..240...13L. doi:10.3847/1538-4365/aaee7e. ISSN 1538-4365.
  29. ^ Barragán, O.; Gandolfi, D.; Smith, A. M. S.; Deeg, H. J.; Fridlund, M. C. V.; Persson, C. M.; Donati, P.; Endl, M.; Csizmadia, Sz; Grziwa, S.; Nespral, D. (2018-04-01). "K2-139 b: a low-mass warm Jupiter on a 29-d orbit transiting an active K0 V star". Monthly Notices of the Royal Astronomical Society. 475 (2): 1765–1776. arXiv:1702.00691. Bibcode:2018MNRAS.475.1765B. doi:10.1093/mnras/stx3207. hdl:10486/684205. ISSN 0035-8711.
  30. ^ Newton, Elisabeth R.; Mann, Andrew W.; Tofflemire, Benjamin M.; Pearce, Logan; Rizzuto, Aaron C.; Vanderburg, Andrew; Martinez, Raquel A.; Wang, Jason J.; Ruffio, Jean-Baptiste; Kraus, Adam L.; Johnson, Marshall C. (2019-07-23). "TESS Hunt for Young and Maturing Exoplanets (THYME): A Planet in the 45 Myr Tucana–Horologium Association". The Astrophysical Journal. 880 (1): L17. arXiv:1906.10703. Bibcode:2019ApJ...880L..17N. doi:10.3847/2041-8213/ab2988. ISSN 2041-8213.
  31. ^ "Atmosphere, Not Lava Flows, for Exoplanet 55 Cancri e". Sky & Telescope. 2017-11-27. Retrieved 2019-12-18.
  32. ^ Grass, Alexandra. ""Cheops"-Start wegen Softwareproblems verschoben". Natur - Wiener Zeitung Online (in German). Retrieved 2019-12-18.
  33. ^ "AO-1 Programmes - CHEOPS Guest Observers Programme - Cosmos". www.cosmos.esa.int. Retrieved 2019-11-15.
  34. ^ "Flight VS23: Launch rescheduled to December 18". Arianespace. Retrieved 2019-12-17.

External links[edit]