Hyperspectral Thermal Emissions Spectrometer

Status

Status
In Development
Operated By
PI

The Hyperspectral Thermal Emissions Spectrometer (HyTES) instrument has 512 pixels across track with pixel sizes in the range of 5 to 50 m depending on aircraft flying height and 256 spectral channels between 7.5 and 12 µm. The HyTES design is built upon a Quantum Well Infrared Photodetector (QWIP) focal plane array (FPA) , a cryo-cooled Dyson Spectrometer and a high-efficiency, concave blazed grating, produced using E-beam lithography.

HyTES will be useful for a number of applications, including high-resolution surface temperature and emissivity measurements and volcano observations. HyTES measurements will also be used to help determine scientifically optimal band locations for the thermal infrared (TIR) instrument for the Decadal HyspIRI mission.

Instrument Type
Measurements
Recent Missions
(Gulfstream V - JSC)
Point(s) of Contact
(Co-I),
(POC; PI)
Range of Measurement
Ground
Instrument Pointing
Nadir (directly downwards)
Swath Width
3590.00 m (at 4 km)
Horizontal Resolution
7.00 m (at 4 km)
Measurement Wavelengths
7.5-12 µm
Notes
First science flights were in 2012. Since then HyTES has flown on Twin Otter aircraft from Twin Otter International and the British Antarctic Survey, NASA ER-2 and NASA Gulfstream V.
TRL
6

 

Disclaimer: This material is being kept online for historical purposes. Though accurate at the time of publication, it is no longer being updated. The page may contain broken links or outdated information, and parts may not function in current web browsers. Visit https://espo.nasa.gov for information about our current projects.