Abstract
The Thermal Infrared Sensor (TIRS), designed and built at NASA Goddard Space Flight Center (GSFC), is one half of the two-sensor Landsat Data Continuity Mission (LDCM) platform. TIRS data will extend the data record for thermal observations from the heritage Landsat sensors, dating back to the launch of Landsat 4 in 1982. The two-band (10.8 and 12.0 μm) pushbroom sensor with a 185 km wide swath and 100 m spatial resolution uses a staggered arrangement of quantum well infrared photodetector (QWIPs) arrays. Regular views of an on-board variable blackbody source and deep space via a rotating scene select mirror will be used to track the on-orbit performance of TIRS. During the instrument development stage, extensive thermal-vacuum chamber testing of the flight sensor was conducted using a custom-built calibration system with a NIST-traceable blackbody source. These measurements were used to calibrate and characterize the radiometric, spectral, and spatial performance of the instrument. Results of the pre-launch testing are presented in addition to the lessons learned.
Pre-launch Calibration of the Landsat Data Continuity Mission Thermal Infrared Sensor
The Thermal Infrared Sensor (TIRS), designed and built at NASA Goddard Space Flight Center (GSFC), is one half of the two-sensor Landsat Data Continuity Mission (LDCM) platform. TIRS data will extend the data record for thermal observations from the heritage Landsat sensors, dating back to the launch of Landsat 4 in 1982. The two-band (10.8 and 12.0 μm) pushbroom sensor with a 185 km wide swath and 100 m spatial resolution uses a staggered arrangement of quantum well infrared photodetector (QWIPs) arrays. Regular views of an on-board variable blackbody source and deep space via a rotating scene select mirror will be used to track the on-orbit performance of TIRS. During the instrument development stage, extensive thermal-vacuum chamber testing of the flight sensor was conducted using a custom-built calibration system with a NIST-traceable blackbody source. These measurements were used to calibrate and characterize the radiometric, spectral, and spatial performance of the instrument. Results of the pre-launch testing are presented in addition to the lessons learned.