Abstract
The design, calibration, and performance of the Mars Orbiter Laser
Altimeter (MOLA) receiver are described. The MOLA measurements
include the range to the surface, which is determined by the
laser-pulse time of flight; the height variability within the footprint
determined by the laser echo pulse width; and the apparent surface
reflectivity determined by the ratio of the echo to transmitted pulse
energies.
© 2000 Optical Society of America
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