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Imaging Technique of the DISR Camera on the Huygens Lander J.R. Kramm 1, H.U. Keller 1, R. Bredthauer 2 and M. Tomasko 3 Imaging Technique of the DISR.

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Presentation on theme: "Imaging Technique of the DISR Camera on the Huygens Lander J.R. Kramm 1, H.U. Keller 1, R. Bredthauer 2 and M. Tomasko 3 Imaging Technique of the DISR."— Presentation transcript:

1 Imaging Technique of the DISR Camera on the Huygens Lander J.R. Kramm 1, H.U. Keller 1, R. Bredthauer 2 and M. Tomasko 3 Imaging Technique of the DISR Camera on the Huygens Lander J.R. Kramm 1, H.U. Keller 1, R. Bredthauer 2 and M. Tomasko 3 1 Max-Planck-Institut für Sonnensystemforschung Katlenburg-Lindau, Germany 2 Semiconductor Technology Associates, Inc. San Juan Capistrano, CA 3 Lunear and Planetary Laboratory, University of Arizona, Tucson, AZ MPS, June 20, 2005

2 Descent Imager/Spectral Radiometer (DISR) 14 optical apertures total 14 optical apertures total 9 optical apertures to 1 CCD detector 9 optical apertures to 1 CCD detector 1.1 Watt for the CCD, 512 x 256 pixels 1.1 Watt for the CCD, 512 x 256 pixels Date rate:8 kbit/s, ~ 1 bit per pixel Date rate:8 kbit/s, ~ 1 bit per pixel 6 years for design, production and calibr. 6 years for design, production and calibr. 7.5 years travel time to Titan, 1997-2005 7.5 years travel time to Titan, 1997-2005 150 min total operation time envisaged 150 min total operation time envisaged

3 Selection of MRI & HRI Images

4 DISR HRI, SLI and MRI Image Triplet after Landing on Titan


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