Session
Technical Session IX: Instrumentation and Sensors
Abstract
Advances in several key sensor technologies make it possible now to build a high performance, very compact and low cost imaging spectrometer for spacebourne terrestrial remote sensing. We describe an instrument based on a highly innovative optical design that incorporates state of the art focal plane arrays, electronics, focal plane cooling and dimensionally stable ceramics for the optical elements and structure. The instrument is optimized for viewing the earth's solid surface and adjacent coastal oceans. It has very high signal-to-noise performance over the full spectral range covered, from 400 to 2450 nanometers (nm). Spectral sampling is in 200 10-nm wide, contiguous bands. The instrument combines a high spatial resolution panchromatic imaging system with a modest spatial resolution imaging spectrometer. It weighs 25 kg, requires less than 100 watts of power, and is approximately 30 by 20 by 10 cm in dimension, fitting well within the capacity of Pegasus-class small spacecraft missions. The instrument is well suited to support studies in earth system science as well as commercial remote sensing. Several applications in these areas will be highlighted to set in context the performance requirements that were used to define the sensor design and choice of sensor technologies.
Small Earth Imaging Spectrometer
Advances in several key sensor technologies make it possible now to build a high performance, very compact and low cost imaging spectrometer for spacebourne terrestrial remote sensing. We describe an instrument based on a highly innovative optical design that incorporates state of the art focal plane arrays, electronics, focal plane cooling and dimensionally stable ceramics for the optical elements and structure. The instrument is optimized for viewing the earth's solid surface and adjacent coastal oceans. It has very high signal-to-noise performance over the full spectral range covered, from 400 to 2450 nanometers (nm). Spectral sampling is in 200 10-nm wide, contiguous bands. The instrument combines a high spatial resolution panchromatic imaging system with a modest spatial resolution imaging spectrometer. It weighs 25 kg, requires less than 100 watts of power, and is approximately 30 by 20 by 10 cm in dimension, fitting well within the capacity of Pegasus-class small spacecraft missions. The instrument is well suited to support studies in earth system science as well as commercial remote sensing. Several applications in these areas will be highlighted to set in context the performance requirements that were used to define the sensor design and choice of sensor technologies.
