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TIRCIS: A Thermal Infrared, Compact Imaging Spectrometer for Small Satellite Applications (TIRCIS)
Completed
TRL 6
Description
This project will demonstrate how hyperspectral thermal infrared (TIR; 8-14 microns) image data, with a spectral resolution of up to 8 wavenumbers, can be acquired by an instrument of sufficiently low mass, volume, and power consumption that it could be cost effectively deployed on small- or micro-satellites. This would constitute a new earth science measurement as there are currently no operational hyperspectral sensors acquiring TIR data with the spatial resolution needed to perform imaging spectroscopy for earth science applications, although these are many (mineral exploration; wildfire characterization; volcanic hazards; soil moisture/drought characterization). The University of Hawaii has developed a breadboard that uses uncooled microbolometers and a Fabry-Perot interferometer to acquire image cubes of 52 TIR spectral bands. This project will mature this technology towards spaceborne deployment. The proposed work involves, 1) optimizing the optical and mechanical design and calibration system; 2) incorporating new microbolometers with surface coatings that increase sensitivity and flatten responsiveness between 8-14 microns, 3) conducting a system level characterization of the instrument using NIST-traceable standards (SNR, spectral and spatial resolution, saturation radiances, radiometric linearity/response; 4) producing integrated instrument control and interferometric processing software; and 5) demonstrating science data collection from an airborne platform. The spatial resolution of the proposed microbolometer-based instrument would be ~120 m from an orbit of 480 km. Performance period is 36 months. Entry TRL is 4 and exit TRL is 6.
Benefits
Enabling lower cost innovative remote sensing instrument development from concept through breadboard and demonstration
Details
| Technology area | Sensors and Instruments > Remote Sensing Instruments and Sensors > Optical Components |
| Program | Instrument Incubator (IIP) |
| Lead organization | NASA Headquarters, Washington, DC |
| Start date | 2014-04-01 |
| End date | 2018-03-31 |
Project contacts
Listed on TechPort itself — the most direct way to ask about this specific project.
- Robert B Wright
- Kathleen S Yoshinaga
How to get involved
This is early/mid-stage (TRL 6) — the most realistic path in is NASA SBIR/STTR, which funds small businesses and research institutions to develop technology aligned with NASA's needs (equity-free, phased funding). Check whether a current SBIR/STTR solicitation topic overlaps with this project's technology area, or contact the project directly (above) to ask.
None of these are guaranteed paths for this specific project — TechPort itself doesn't have an "apply" button. Reaching out to the contact(s) above with a specific question is usually the fastest way to find out what's actually open.