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CHEOPS (CHaracterising ExOPlanet Satellite)

CHEOPS – Characterising ExOPlanet Satellite is a small photometric observatory to be launched into low Earth orbit to measure transits of Exo-planets. CHEOPS is the first Small mission from ESA and was selected in October 2012 with a launch target for 2017. ESA is the Mission Architect and in charge of the spacecraft development and launcher procurement. The Member States contribution is led by University of Bern (UBE). The mission's main science goal is to search for transits by means of ultrahigh precision photometry on bright stars already known to host planets. By being able to point at nearly any location on the sky, it will provide the unique capability of determining accurate radii for a subset of those planets for which the mass has already been  estimated  from  ground-based spectroscopic surveys. It will also provide precision radii for new planets discovered by the next generation ground-based transits surveys (Neptune-size and smaller). The   mission  is flying  a  single  medium-size telescope  (30 cm aperture, 1.2 m length including baffle). All platform requirements  are  aimed  at supporting the functionality of the telescope and its ultrahigh photometric precision. The main  implications for  the platform are related  to  pointing capabilities and thermal environment for the payload.

TECHNICAL OBJECTIVE is to develop two radiator assemblies for the scientific instrument of the CHEOPS satellite. Proper thermal control at instrument and spacecraft level is one of the key components   to  mission  success.  The  Focal  Plane  Array  (FPA) requires 10mK and Front-end Electronics (FEE) 50 mK temperature stability with -55 °C and -10 °C operational temperatures. FPA radiator and the  associated FEE   radiator   are  responsible  to   keep   these equipment at optimum  working  temperature  in  all mission  phases  while  the  operational temperature  range  of  spacecraft  is  between  -70  and  +40  °C. ADMATIS  is responsible  for the Structural and Thermal Model (STM) and Proto Flight Model (FPM) delivery. Design activity included thermal and structural FE analysis to optimize mechanical and thermal properties. Raw material of radiators is aluminium alloy, baseline machining processes are NC milling and turning. Radiators will be chromate conversion coated to improve corrosion resistance and adhesion to paints and glues. Radiative areas will be coated with thermal  control   system    (white paint or  secondary surface mirror, SSM)   to   ensure   the  proper  heat   rejecting. Vacuum  bake-out  will be performed to remove organic contaminants and residues of solvents or other volatiles. Verification included the mechanical and thermal tests. Large number of MGSE tools has been developed for environmental tests which were also managed by ADMATIS.

STATUS: In december 2014 ADMATIS successfully deliverered the radiator Structural and Thermal Models (STM). At the time ADMATIS runs the project third qualification phase. Project webpage: cheops.unibe.ch

THE SCIENCE BEHIND CHEOPS: An exoplanet or extrasolar planet is a planet that orbits a star other than the Sun, a stellar remnant, or a brown dwarf. CHEOPS satellite will be investigate exoplanets with Transit photometry method. This method can determine the radius of a planet. If a planet crosses (transits) in front of the disk of its parent star, then the observed visual brightness of the star drops a small amount (shown on the right picture). The amount the star dims depends on the relative sizes of the star and the planet. When combine this method with the radial-velocity method (wich determines the planet’s mass) one can determine the density of the planet and learns something about the planet’s physical structure. The transit method also makes it possible  to study  the atmosphere of a planet.

 

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Downloadable media:

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s Project flyer CHEOPS visualization CHEOPS introduction Testing of CHEOPS STM
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