Key Facts
- NASA Earth Observing System Facility Instrument : Geoscience Laser Altimeter System (GLAS)
- Nadir-pointed laser altimeter; spacecraft enables off-nadir pointing capability
- Measures polar ice-sheet topography and temporal changes in topography; cloud heights, planetary boundary heights, and aerosol vertical structure; and land and water topography
- NASA/Goddard Space Flight Center in-house development of GLAS
- Laser is diode pumped, Q-switched Nd:YAG laser with 40 Hz pulse repetition; 75 mJ at 1064 nm and 35 mJ at 532 nm
- Receiver telescope is 1 meter diameter
- Heritage: airborne and spaceborne laser altimetry and lidar systems; satellite laser ranging systems
- GLAS completed Preliminary Design Review; Critical Design Review completed in March 1999
- GLAS will be carried on ICESat (Ice, Cloud and land Elevation Satellite)
- ICESat spacecraft delivery order signed February 1998, with Ball Aerospace, Boulder, CO; ICESat completed Mission Design Review in December, 1998
- Orbit altitude is 600 km, near circular (frozen), 94 degree inclination
- Verification orbit uses 8 day repeat pattern during first 120 days after launch
- Mission orbit (post-verification) uses 183 day repeat pattern
- Global Positioning System receiver provides 5 cm (radial) orbit position; ground-based laser ranging provides validation and backup
- On-board star cameras and gyros provide spacecraft orientation and laser pointing direction
- Launch no earlier than December 19, 2002, 16:45-17:30 PST
- 3 year lifetime with 5 year goal
Last Update: March 27, 1999