Back-illuminated, fully-depleted CCD image sensors for use in optical and near-IR astronomy

Author(s):  
D.E Groom ◽  
S.E Holland ◽  
M.E Levi ◽  
N.P Palaio ◽  
S Perlmutter ◽  
...  
2014 ◽  
Author(s):  
Peter E. Doherty ◽  
Pierre Antilogus ◽  
Pierre Astier ◽  
James Chiang ◽  
D. Kirk Gilmore ◽  
...  

2004 ◽  
pp. 33-40
Author(s):  
Morley M. Blouke ◽  
Denis L. Heidtmann ◽  
James Eriksen ◽  
Archibald Barter

2007 ◽  
Author(s):  
Koji Kikuchi ◽  
Shinji Miyazawa ◽  
Yoshinori Uchida ◽  
Hiroe Kamata ◽  
Teruo Hirayama
Keyword(s):  

1998 ◽  
Author(s):  
Hiromitsu Aoki ◽  
Kenji Yokozawa ◽  
Nobuyuki Waga ◽  
Tomoko Ohtagaki ◽  
Yoshiaki Nishi ◽  
...  

2007 ◽  
Vol 364-366 ◽  
pp. 104-107
Author(s):  
Jong Myoung Lee ◽  
Un Chung Cho

A new dry cleaning methodology named laser shock cleaning and optical inspection technique has been applied not only to remove the particles from the surfaces of image sensors but also to inspect the surfaces automatically before or after the cleaning. In the packaging of CMOS and CCD image sensing modules, the particles generated during the assembly process should be removed from the surfaces of image sensors in order to ensure clear image as well as to enhance the yield. The different kinds of particles were removed from the surfaces by the laser shock cleaning technique which utilizes the airborne shock wave induced by intense laser pulse. For the quantitative evaluation of cleaning performance, number, shape and size of the particles on the surfaces of image sensors were measured by vision inspection technique before and after cleaning. It was found that most particles on the surfaces were successfully removed after the treatment of laser-induced shock waves. The average removal efficiency of the particles was over 95 %. It is interestingly found that the remaining particles after the cleaning are based on organics, which are probably attached during the bonding process.


2007 ◽  
Vol 3 (S248) ◽  
pp. 296-297 ◽  
Author(s):  
T. Yano ◽  
N. Gouda ◽  
Y. Kobayashi ◽  
Y. Yamada ◽  
T. Tsujimoto ◽  
...  

AbstractJASMINE is the acronym of the Japan Astrometry Satellite Mission for INfrared (z-band: 0.9 micron) Exploration, and is planned to be launched around 2017. The main objective of JASMINE is to study the fundamental structure and evolution of the Milky Way bulge components. In order to accomplish these objectives, JASMINE will measure trigonometric parallaxes, positions and proper motions of about ten million stars in the Galactic bulge with a precision of 10 microarcsec at z = 14mag.The primary mirror for the telescope has a diameter of 75cm with a focal length of 22.5m. The back-illuminated CCD is fabricated on a 300 micron thick substrate which is fully depleted. These thick devices have extended near infrared response. The size of the detector for z-band is 3cm×3cm with 2048×2048 pixels. The size of the field of view is about 0.6deg×0.6deg by using 64 detectors on the focal plane. The telescope is designed to have only one field of view, which is different from the designs of other astrometric satellites. JASMINE will observe overlapping fields without gaps to survey a total area of about 20deg×10 deg around the Galactic bulge. Accordingly we make a “large frame” of 20deg×10 deg by linking the small frames using stars in overlapping regions. JASMINE will observe the Galactic bulge repeatedly during the mission life of about 5 years.


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