Session
Session IV: Science/Mission Payloads
Location
Utah State University, Logan, UT
Abstract
The European Space Agency (ESA) Science Programme Committee (SPC) selected CHEOPS (Characterizing Exoplanets Satellite) in October 2012 as the first Small-class mission (S1) within the Agency’s Scientific Programme. It is considered as a pilot case for implementing “small science missions” in the agency with the following requirements: science driven mission selected through an open Call; an implementation cycle, from the Call to launch, drastically shorter than for Medium-class (M) and Large-class (L) missions; a strict cost-cap to ESA, with possibly higher Member States involvement than for M or L missions.
The CHEOPS mission is devoted to the characterization of known exoplanets orbiting bright stars, achieved through the precise measurement of exoplanet radii using the technique of transit photometry. It was adopted for implementation in February 2014 as a partnership between the ESA Science Programme and Switzerland, with a number of other Member States delivering significant contributions to the instrument development and to operations.
The CHEOPS instrument is an optical Ritchey-Chrétien telescope with 300 mm effective aperture diameter and a large external baffle to minimize straylight. The compact CHEOPS spacecraft (approx. 300 kg, 1.5 m size), based on a flight-proven platform, will orbit the Earth in a dawn-dusk Sun Synchronous Orbit at 700 km altitude. CHEOPS completed the Preliminary Design Review at the end of September 2014, and passed the Critical Design Review in May 2016. In the course of 2017, flight platform and payload have been integrated and tested, and then followed by satellite level activities, targeting flight readiness by the end of year 2019. Implementation and validation of the ground segment, which is composed of the MOC (Mission Operations Centre), located in Torrejón (Madrid, Spain) and the SOC (Science Operations Centre), located at the University of Geneva (Switzerland) was achieved in parallel. CHEOPS will be launched as a secondary passenger on a Soyuz from Kourou by end of 2019.
The paper describes the latest CHEOPS development status, focusing on the activities for verification and validation of the satellite and the system at large, including the ground segment and the activities in preparation for S/C launch and its operations. Additional details can be found on the ESA and UBE websites referred in [8].
CHEOPS: The ESA Mission for Exo-Planets Characterization Ready for Launch
Utah State University, Logan, UT
The European Space Agency (ESA) Science Programme Committee (SPC) selected CHEOPS (Characterizing Exoplanets Satellite) in October 2012 as the first Small-class mission (S1) within the Agency’s Scientific Programme. It is considered as a pilot case for implementing “small science missions” in the agency with the following requirements: science driven mission selected through an open Call; an implementation cycle, from the Call to launch, drastically shorter than for Medium-class (M) and Large-class (L) missions; a strict cost-cap to ESA, with possibly higher Member States involvement than for M or L missions.
The CHEOPS mission is devoted to the characterization of known exoplanets orbiting bright stars, achieved through the precise measurement of exoplanet radii using the technique of transit photometry. It was adopted for implementation in February 2014 as a partnership between the ESA Science Programme and Switzerland, with a number of other Member States delivering significant contributions to the instrument development and to operations.
The CHEOPS instrument is an optical Ritchey-Chrétien telescope with 300 mm effective aperture diameter and a large external baffle to minimize straylight. The compact CHEOPS spacecraft (approx. 300 kg, 1.5 m size), based on a flight-proven platform, will orbit the Earth in a dawn-dusk Sun Synchronous Orbit at 700 km altitude. CHEOPS completed the Preliminary Design Review at the end of September 2014, and passed the Critical Design Review in May 2016. In the course of 2017, flight platform and payload have been integrated and tested, and then followed by satellite level activities, targeting flight readiness by the end of year 2019. Implementation and validation of the ground segment, which is composed of the MOC (Mission Operations Centre), located in Torrejón (Madrid, Spain) and the SOC (Science Operations Centre), located at the University of Geneva (Switzerland) was achieved in parallel. CHEOPS will be launched as a secondary passenger on a Soyuz from Kourou by end of 2019.
The paper describes the latest CHEOPS development status, focusing on the activities for verification and validation of the satellite and the system at large, including the ground segment and the activities in preparation for S/C launch and its operations. Additional details can be found on the ESA and UBE websites referred in [8].
