The dual-gain 10 μm back-thinned 3k×3k CMOS-APS detector of the solar orbiter extreme UV imager

The Extreme Ultraviolet Imager (EUI) on-board the Solar Orbiter mission will provide image sequences of the solar atmosphere at selected spectral emission lines in the extreme and vacuum ultraviolet. For the two Extreme Ultraviolet (EUV) channels of the EUI instrument, low noise and radiation tolerant detectors with low power consumption and high sensitivity in the 10-40 nm wavelength range are required to achieve the science objectives. In that frame, a dual-gain 10 μm pixel pitch back-thinned 1k x 1k Active Pixel Sensor (APS) CMOS prototype has been tested during the preliminary development phase of the instrument, to validate the pixel design, the expected EUV sensitivity and noise level, and the capability to withstand the mission radiation environment. Taking heritage of this prototype, the detector architecture has been improved and scaled up to the required 3k x 3k array. The dynamic range is increased, the readout architecture enhanced, the power consumption reduced, and the pixel design adapted to the required stitching. The detector packaging has also been customized to fit within the constraints imposed by the camera mechanical, thermal and electrical boundaries. The manufacturing process has also been adapted and back-thinning process improved. Once manufactured and packaged, a batch of sensors will undergo a characterization and calibration campaign to select the best candidates for integration into the instrument qualification and flight cameras. The flight devices, within their cameras, will then be embarked on the EUI instrument, and be the first scientific APSCMOS detectors for EUV observation of the Sun.

[1]  B. Giordanengo,et al.  Irradiation Damage Tests on Backside-Illuminated CMOS APS Prototypes for the Extreme Ultraviolet Imager On-Board Solar Orbiter , 2013, IEEE Transactions on Nuclear Science.

[2]  John D. Moses,et al.  HECOR: a HElium CORonagraphy aboard the Herschel sounding rocket , 2007, SPIE Optical Engineering + Applications.

[3]  Etienne Renotte,et al.  First light of SWAP on-board PROBA2 , 2010, Astronomical Telescopes + Instrumentation.

[4]  F. Auchère,et al.  The extreme UV imager of solar orbiter: from detailed design to flight model , 2014, Astronomical Telescopes and Instrumentation.

[5]  Laurence Rossi,et al.  The technical challenges of the Solar-Orbiter EUI instrument , 2010, Astronomical Telescopes + Instrumentation.

[6]  F. Auchère,et al.  The EUI instrument on board the Solar Orbiter mission: from breadboard and prototypes to instrument model validation , 2012, Other Conferences.

[7]  Luca Teriaca,et al.  The Lyman-alpha telescope of the extreme ultraviolet imager on Solar Orbiter , 2011, Optical Engineering + Applications.

[8]  B. Giordanengo,et al.  Developments, characterization and proton irradiation damage tests of AlN detectors for VUV solar observations , 2013 .

[9]  Richard A. Harrison,et al.  Summary of the Solar Orbiter payload working group activities , 2004, SPIE Optics + Photonics.

[10]  Frank Scholze,et al.  Characterization of Backside-Illuminated CMOS APS Prototypes for the Extreme Ultraviolet Imager On-Board Solar Orbiter , 2013, IEEE Transactions on Electron Devices.

[11]  Guy Meynants,et al.  A high-dynamic range (HDR) back-side illuminated (BSI) CMOS image sensor for extreme UV detection , 2012, Electronic Imaging.

[12]  Berend Winter,et al.  EUI, THE ULTRAVIOLET IMAGING TELESCOPES OF SOLAR ORBITER , 2007 .

[13]  Etienne Renotte,et al.  The Extreme Ultraviolet Imager (EUI) onboard the SOLAR ORBITER mission , 2009 .