Title :
Microbolometer instrument payload design for a microsatellite mission
Author :
Payne, W.F. ; Gore, J.V. ; Pope, T.D. ; Phong, Linh Ngo ; Zheng, Wanping
Author_Institution :
Routes AstroEngineering, Ottawa, Ont., Canada
Abstract :
This paper describes the design of the mission and the instrument. It compares the use of microsatellites, ground and air based platforms. An Earth observation microsatellite mission is based on microbolometer technology. The detectors are linear arrays, filtered to be sensitive in five bands: 3 bands between 8.5 and 12.5 microns, and 2 bands between 3.0 and 4.5 microns. It is expected that this Earth observation satellite will produce useful dates like ice-shelf formation/melt, cloud monitoring, oil spills, forest fire tracking and damage assessment, Kyoto Accord compliance monitoring, city heat bloom, temperatures of oceans, land, and ice with the focus on northern coastal waters, Arctic and sub-Arctic land areas. Hence, satellite-based sensors have more advantages over terrestrial or airborne sensors.
Keywords :
artificial satellites; bolometers; remote sensing; 3.0 to 4.5 micron; 8.5 to 12.5 micron; Arctic land areas; Earth observation microsatellite mission; air based platform; airborne sensors; city heat bloom; cloud monitoring; forest damage assessment; forest fire tracking; ground based platform; ice temperatures; ice-shelf formation-melt; land temperatures; microbolometer detectors; microbolometer technology; microsatellites mission design; multiband linear arrays; northern coastal waters; ocean temperatures; oil spills; satellite-based sensors; subarctic land areas; terrestrial sensors; Artificial satellites; Clouds; Detectors; Earth; Instruments; Lubricating oils; Monitoring; Nonlinear filters; Payloads; Sensor arrays;
Conference_Titel :
MEMS, NANO and Smart Systems, 2005. Proceedings. 2005 International Conference on
Print_ISBN :
0-7695-2398-6
DOI :
10.1109/ICMENS.2005.69