Thermal IRCCDS For Space Applications

P. Nothaft; H. RoBeiBl-Urban; J. Ziegler; J. Vermeiren; B. Dierixcks; M. Fabbricotti

doi:10.1117/12.948313

7 December 1988 Thermal IRCCDS For Space Applications

P. Nothaft, H. RoBeiBl-Urban, J. Ziegler, J. Vermeiren, B. Dierixcks, M. Fabbricotti

Proceedings Volume 0972, Infrared Technology XIV; (1988) https://doi.org/10.1117/12.948313
Event: 32nd Annual International Technical Symposium on Optical and Optoelectronic Applied Science and Engineering, 1988, San Diego, CA, United States

Abstract

Earth observation satellites will use linear arrays of a few thousands of pv-CMT-detectors combined with CCDs to scan the surface in the (8-12) μm spectral range in the pushbroom principle. The hybrid approach of large CMT-IRCCDs is based on butting small entities of CMT-submodules with CCD-signalprocessors. According to the high photon background charge suppression techniques have to be implemented in the detector-CCD coupling circuit. CMT-IRCCD engineering models are manufactured, electro-optical results are presented.

Citation Download Citation

P. Nothaft, H. RoBeiBl-Urban, J. Ziegler, J. Vermeiren, B. Dierixcks, and M. Fabbricotti "Thermal IRCCDS For Space Applications", Proc. SPIE 0972, Infrared Technology XIV, (7 December 1988); https://doi.org/10.1117/12.948313

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