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Endogenous Lunar Volatiles
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Erosion of Volatiles by Micro-Meteoroid Bombardment on Ceres, and Comparison to the Moon and Mercury
Ceres, the largest reservoir of water in the main-belt, was recently visited by the Dawn spacecraft that revealed several areas bearing H2O-ice features. Independent telescopic observations showed a water exosphere of currently unknown origin. We explore the effects of meteoroid impacts on Ceres considering the topography obtained from the Dawn mission using a (Replaced: full-fledged replaced with: widely-used) micro-meteoroid model and ray-tracing techniques. Meteoroid populations with 0.01-2 mm diameters are considered. We analyze the short-term effects Ceres experiences during its current orbit as well as long-term effects over the entire precession cycle. We find the entire surface is subject to meteoroid bombardment leaving no areas in permanent shadow with respect to meteoroid influx. The equatorial parts of Ceres produce 80% more ejecta than the polar regions due to the large impact velocity of long-period comets. Mass flux, energy flux, and ejecta production vary seasonally by a factor of (Replaced: a few replaced with: 3–7) due to the inclined eccentric orbit. Compared to Mercury and the Moon, Ceres experiences significantly smaller effects of micro-meteoroid bombardment, with a total mass flux of 4.5±1.2×10(exp −17)kg m(exp −2)s(exp −1). On average Mercury is subjected to a 50× larger mass flux and generates 700× more ejecta than Ceres, while the lunar mass flux is 10× larger, and the ejecta generation is 30× larger than on Ceres. For these reasons, we find that meteoroid impacts are an unlikely candidate for the production of a water exosphere or significant excavation of surface features. The surface turnover rate from the micro-meteoroid populations considered is estimated to be 1.25 Myr on Ceres.
High-resolution Volatiles and Minerals Mapper (HVM³) Measurement Sensitivity
UNKNOWN
VIPER: Volatiles Investigating Polar Exploration Rover
We will review the technical components of the NASA lunar rover mission, VIPER, with a focus on software components that rely on ROS 2 and Gazebo. We’ll start with an overview of the hardware and software components. Next, we’ll explore some of the custom Gazebo plugins for simulating the rover and the lunar surface. We’ll describe a fault injection framework that was built on ROS 2 parameters and how it is used to simulate hardware faults. Finally, we’ll see how ROS 2 is used as part of the rover ground software.
Submillimeter Solar Observation Lunar Volatiles Experiment (SSOLVE) Optics and Receivers
Power point presentation
Halogen Geochemistry of Unopened Angsa and Conventional Apollo Materials: The ‘End-Member’ of Volatile Processing?
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Volatiles Investigating Polar Exploration Rover (VIPER)
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New Constraints on Prokofiev's Volatile Deposit
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Capture, Accumulation, Concentration and Transfer of Unknown Volatile Species (CACTUS) for Mass Spectrometry Instruments
No abstract provided
R-Hope: Development Approach to Extreme Non-volatile Memory Reuse Onboard the Curiosity Rover
No abstract provided
R-Hope: Development approach to extreme non-volatile memory reuse onboard the Curiosity Rover
No abstract provided