You have requested a machine translation of selected content from our databases. This functionality is provided solely for your convenience and is in no way intended to replace human translation. Neither SPIE nor the owners and publishers of the content make, and they explicitly disclaim, any express or implied representations or warranties of any kind, including, without limitation, representations and warranties as to the functionality of the translation feature or the accuracy or completeness of the translations.
Translations are not retained in our system. Your use of this feature and the translations is subject to all use restrictions contained in the Terms and Conditions of Use of the SPIE website.
3 May 2007The lunar orbiter laser altimeter (LOLA) on NASA's lunar reconnaissance orbiter (LRO) mission
The Lunar Orbiter Laser Altimeter (LOLA) instrument on NASA's Lunar Reconnaissance Orbiter (LRO) mission,
scheduled to launch in October 2008, will provide a precise global lunar topographic map using laser altimetry. LOLA
uses short pulses from a single laser through a Diffractive Optical Element (DOE) to produce a five-beam pattern that
illuminates the lunar surface. For each beam, LOLA measures the time of flight (range), pulse spreading (surface
roughness), and transmit/return energy (surface reflectance). LOLA will produce a high-resolution global topographic
model and global geodetic framework that enables precise targeting, safe landing, and surface mobility to carry out
exploratory activities. In addition, it will characterize the polar illumination environment, and image permanently
shadowed polar regions of the lunar surface to identify possible locations of surface ice crystals in shadowed polar
craters.
The alert did not successfully save. Please try again later.
Haris Riris, Xiaoli Sun, John F. Cavanaugh, Glenn B. Jackson, Luis Ramos-Izquierdo, David E. Smith, Maria Zuber, "The lunar orbiter laser altimeter (LOLA) on NASA's Lunar Reconnaissance Orbiter (LRO) mission," Proc. SPIE 6555, Sensors and Systems for Space Applications, 65550I (3 May 2007); https://doi.org/10.1117/12.719266