GLAS Sensor

3-D Assembly Drawing of GLAS Sensor The Geoscience Laser Altimeter System (GLAS) includes a laser system to measure distance, a Global Positioning System (GPS) receiver, and a star-tracker attitude determination system. The laser will transmit short pulses (4 nano seconds) of infrared light (1064 nanometers wavelength) and visible green light (532 nanometers). Photons reflected back to the spacecraft from the surface of the Earth and from the atmosphere, including the inside of clouds, will be collected in a 1 meter diameter telescope. Laser pulses at 40 times per second will illuminate spots (footprints) 70 meters in diameter, spaced at 170-meter intervals along Earth's surface.
GLAS is being developed by a partnership of NASA, industry, and university teams. The smallest of the new Med-LiLe class of rockets, the Taurus, will launch GLAS into an orbit at 590 km altitude and 94 degrees inclination to the equator. GLAS utilizes advanced laser detection and ranging, attitude sensing, and orbital-position-sensing technologies. The spacecraft provides a highly autonomous, inertially stabilized platform with advanced power, guidance, and propulsion systems to maintain the critical performance required for repeated Earth observations. Its designed lifetime is for 3 years of operation with a 5-year goal. Successive spacecraft will acquire the 10 to 15 year data set planned for ESE.

GLAS Specifications
532nm 1064nm
Laser Pulse Energy 36 mJ 74 mJ
Laser PRF 40 Hz 40 Hz
Telescope Diameter 1.0 m 1.0 m
Reciever FOV 0.15 mrad 0.475 mrad
Optical Bandwidth < 25 pm < 1.4 nm
Detector Quantum Efficency 0.6 0.3
Detection Scheme Photon Counting Analog
Surface Ranging Accuracy - 10 cm
Pointing Knowledge - 3 arsec