Journal
EARTH PLANETS AND SPACE
Volume 73, Issue 1, Pages -Publisher
SPRINGER
DOI: 10.1186/s40623-021-01537-7
Keywords
LIDAR; MMX; Phobos
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An altimeter is crucial in planetary missions for safety and scientific activities, and this study focuses on the required specifications and link budget calculations for using LIDAR on the MMX spacecraft. The LIDAR on MMX continuously measures distance between the spacecraft and its target to provide diagnostic information for safe operations and geomorphological studies. Changes to the optical system design were made to accommodate physical disturbances on the Martian satellite surface due to the nature of MMX being a sample return mission.
An altimeter is a critical instrument in planetary missions, for both safe operations and science activities. We present required specifications and link budget calculations for light detection and ranging (LIDAR) onboard the Martian Moons Exploration (MMX) spacecraft. During the mission phase, this LIDAR will continuously measure the distance between the spacecraft and its target. The time-series distance provides important diagnostic information for safe spacecraft operations and important information for geomorphological studies. Because MMX is a sample return mission, its LIDAR must accommodate physical disturbances on the Martian satellite surface. This resulted in changes to the optical system design.
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