
NASA’s Mars Reconnaissance Orbiter (MRO) is currently on Mars using the probe’s High Resolution Imaging Science Experiment (HiRISE) instrument to gather data on the planet’s climate, composition, and surface features. On May 25, 2008, e2v CCD image sensors incorporated into the HiRISE captured an image of NASA’s Phoenix Mars Lander suspended from its parachute, as the lander successfully arrived on Mars. This is the first time a spacecraft has captured an image of another spacecraft landing on a planetary body. HiRISE normally points downwards, but the whole orbiter was tilted up in order to capture the image of the lander as it approached Mars.
The CCD sensor includes a two-phase serial readout structure with two output amplifiers located at the center of the readout register. The parallel CCD register has a charge capacity of 200 Ke- and incorporates a four-phase architecture. A light shield ensures that incident photons only strike the photosensitive pixels on the sensor. Also included is a vertical injection structure that may be used to pre-flush the entire photoactive area or pre-fill select portions only. The CCD sensors operate in the back-illumination mode to yield high quantum efficiency over the 400 to 900-nm wavelength range.
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