Title :
Thermal emission imaging system (THEMIS) for Mars 2001 using an uncooled microbolometer array
Author :
Silverman, Steven H. ; Blasius, Karl R. ; Ferry, Stephen J. ; Christensen, Philip R.
Author_Institution :
Remote Sensing Lab., Raytheon Syst. Co., Goleta, CA, USA
fDate :
6/21/1905 12:00:00 AM
Abstract :
THEMIS is a 13 kg 14 W pushbroom imager being built for NASA´s Mars 2001 orbiter to acquire 9 IR bands (6.5-15.5 μm) of 100 m resolution images to map mineralogy and search for hydrothermal activity. A 20 m resolution multispectral visible sensor, from Malin Space Science Systems, is also integrated into THEMIS. THEMIS data will support selection of landing sites for sample collection and return missions. Optics and detector designs are keys to meeting the low-cost mission requirements. THEMIS´ telescope is a compact 3-mirror f/1.6 diamond-turned design. Spectral selection is via stripe filters fixed above the focal planes. The IR focal plane incorporates a 2D array of Si microbolometer detectors, based on a Honeywell patent and further developed by Raytheon. These uncooled detectors relieve the instrument design from accommodating the bulk/weight/power of an active/passive cryocooler. The detector high responsivity range is being extended down from 8 to 6 μm to image carbonate absorption bands
Keywords :
Mars; aerospace instrumentation; astronomical telescopes; bolometers; focal planes; infrared detectors; microsensors; remote sensing; space vehicles; 13 kg; 14 W; 3-mirror diamond-turned design; 6.5 to 15.5 muHz; IR bands; IR focal plane; LWIR; Malin Space Science Systems; Mars 2001 orbiter; NASA; Si; Si microbolometer detectors; THEMIS; THEMIS´ telescope; hydrothermal activity; multispectral visible sensor; pushbroom imager; spectral selection; stripe filters; thermal emission imaging; uncooled microbolometer array; Image resolution; Mars; Optical design; Optical detectors; Optical filters; Optical imaging; Optical sensors; Sensor arrays; Sensor systems; Telescopes;
Conference_Titel :
Aerospace Conference, 1999. Proceedings. 1999 IEEE
Print_ISBN :
0-7803-5425-7
DOI :
10.1109/AERO.1999.789797