Spectral Similarity in the Thermal Infrared between Sulfide-rich Carbonaceous Chondrite Meteorites, Jupiter Trojans, and Other D- and P-type Asteroids
The Planetary Science Journal American Astronomical Society 7:4 (2026) 90
Abstract:
Carbonaceous chondrite meteorites, which include the sulfide-rich âYamato-typeâ chondrites (CYs), have undergone a complex history of aqueous and thermal alteration and offer crucial insights into early outer solar system conditions. In this study, we evaluate thermal infrared (TIR) reflectance spectra of three CY chondrites. We observe a broad spectral plateau near 10 ÎŒm, a spectral signature that has been observed in remote observations of some primitive, low-albedo asteroids, including Jupiter Trojans. We compare our data to CY emissivity spectra, spectra of Fe-sulfide and olivine mixtures, and remote Jupiter Trojan observations and establish the plateau and low albedo are a result of a high content of fine-particulate Fe-sulfide of these meteorites. We therefore suggest that D- and P-type asteroids, like Jupiterâs Trojan asteroids, could have a high abundance of Fe sulfide on their surfaces as a potential result of aqueous alteration followed by dehydration, shedding light on the processes shaping the outer solar system.PANDOR-I: Preliminary vacuum chamber experimental set-up of dust layering, ice-regolith lunar analogues in reflectance (1.8 â 20 ”m)
(2026)
Abstract:
Targeting Intermittently Sunlit Areas With Thermal Stability for Buried Water Ice in the South Polar Region of the Moon
Journal of Geophysical Research Planets American Geophysical Union (AGU) 131:2 (2026)
Abstract:
Abstract Intermittently sunlit areas near the lunar south pole are estimated to harbor thermal conditions permitting longâterm stability of water ice and other volatiles. They are targets for future science and exploration missions due to the combination of sunlight availability for solar power generation, and the possibility for extraction of volatiles for scientific analysis and ISRU. We construct a geodatabase of spatially coâregistered remote sensing and thermal model results, and perform a probabilistic analysis to determine the likelihood of successfully landing and operating on such locations for a quadrangular study area that bounds the 80°S parallel. In addition to water ice thermal stability, we consider factors relevant for the operation of solarâpowered landed spacecraft: visibility to the Earth, visibility to the sun, and local slope. For two scenarios representing sets of mostâ and leastâconstrained landing site requirements, we find that circular landing ellipse diameters of âŒ0.9 and 2.6 km, respectively, would allow to target available compliant terrains with 100% success. We quantify the reduction in success probability with increasing landing ellipse size. Further, we explore the distributions of geometric properties of compliant areas, and identify three sites of interest that support large areas of compliant terrain: near De Gerlache crater, near Shackleton crater, and Mons Mouton (informally named as LeibnitzâÎČ massif). This study is provided to support planning for future lunar missions. Plain Language Summary Researchers have identified areas near the lunar poles that receive occasional sunlight and could keep water ice and other resources stable over a long period of time. These spots are valuable for future lunar missions since they could provide solar power and possibly resources such as water for scientific study and onâsite use. To assess potential landing sites in the south polar region, we created a database combining remote sensing and thermal data set, then used it to calculate the likelihood of successful landing on accessible terrains with stable water ice conditions from the 80°S to the South Pole. The study looked at factors critical for solarâpowered landers: the terrain's visibility to Earth (for communication), sunlight access, and the slope of the ground. We analyzed two scenarios with different landing precisions. We found that landing areas with diameters of about 0.9 and 2.6 km could ensure a 100% success rate under the mostâ and leastâconstrained scenarios, respectively. Larger landing areas decreased the success probability. We also mapped the physical characteristics of ideal areas and highlighted three promising locations near De Gerlache crater, Shackleton crater, and Mons Mouton. Key Points We identify intermittently sunlit areas that permit longâterm stability of subâsurface water ice, and accessible by landed missions âCompliant terrainsâ in two scenarios range from 13,071 kmÂČ (least constrained) to 290 kmÂČ (most constrained) in the south polar region For areas â„80°S, we recommend subâkm landing precision for missions with success criteria involving exploration of lunar polar water iceThe Lunar Trailblazer Lunar Thermal Mapper Instrument
(2025)
A Thermal Infrared Emission Spectral Morphology 51ÁÔÆæÈëżÚ of LizarditeÂ
(2025)