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Star Tracker Camera

Ultraviolet/Visible Camera

Near-Infared Camera

High-Resolution Camera

Laser Transmitter

Long-Wave Infared Camera

Near-Infrared Camera

The NIR camera used an indium antimonide (InSb), 256 x 256 pixel array mechanically cooled to 70 K and sensitive between 0.9 and 3.1 micrometers. Its field of view was 5.6 degrees x 5.6 degrees, with an IFOV of 396 microrad. As developed by Lawrence Livermore National Laboratory (LLNL), the NIR camera had a single pass band. At the request of the NASA Science Advisory Committee, a six-position filter wheel was added to the instrument. All except the longest-wavelength pass band were selected by the NASA Science Advisory Committee. Each of the six pass bands of the NIR camera were used to image the entire lunar surface. The NIR camera used on Clementine weighed 1920 g, including the Stirling-cycle cryocooler; this represents a significant decrease in mass when compared to similar sensors.

Specifications

Filter Wheel (6 Positions)

Mass 1920 grams A: 1100 nm (60 nm width)
Size 11.5 x 12 x 37 cm B: 1250 nm (60)
Avg. Power 21.5 W C: 1500 nm (60)
Wavelength 0.9-3.1 microns D: 2000 nm (60)
Field of View 5.6 x 5.6 degrees E: 2600 nm (60)
Pixel Format 256 x 256 F: 2690 nm (120)
Focal Plane Array InSb (Amber Eng.)


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