PS1.1 | Lunar Science, Exploration & Utilisation
Lunar Science, Exploration & Utilisation
Co-organized by GI6
Convener: Chrysa Avdellidou | Co-conveners: Joana S. Oliveira, Ottaviano Ruesch, Bernard Foing
Orals
| Mon, 15 Apr, 14:00–15:45 (CEST)
 
Room 1.31/32
Posters on site
| Attendance Mon, 15 Apr, 16:15–18:00 (CEST) | Display Mon, 15 Apr, 14:00–18:00
 
Hall X3
Posters virtual
| Attendance Mon, 15 Apr, 14:00–15:45 (CEST) | Display Mon, 15 Apr, 08:30–18:00
 
vHall X3
Orals |
Mon, 14:00
Mon, 16:15
Mon, 14:00
The Lunar Science, Exploration & Utilisation Session will address the latest results from lunar missions, ground-based and satellite measurements, lunar meteorites research, terrestrial analogue studies, laboratory experiments, and modelling. The session aims to bring together contributions on theoretical models concerning the deep interior and subsurface structure and composition; observations of the surface morphology and composition; analyses of the atmospheric composition and dynamics; the interaction with the solar wind; analogue studies and future habitability of the Moon.
This session also aims at presenting highlights of results regarding the exploration and sustainable utilisation of the Moon through observations, modelling, and experiments. All past/current results as well as future exploration ideas and prospects are welcome.
In details, the topics of interest include:
- Lunar results: origins, geochemistry, geophysics in the context of open planetary science and exploration;
- Results from Clementine, Prospector, SMART-1, Kaguya, Chang’e programme, Chandrayaan-1, Chandrayaan-2, Chandrayaan-3 lander and rover, LCROSS, LADEE, Lunar Reconnaissance Orbiter, Artemis and GRAIL, JAXA SLIM lander, and missions using NASA commercial lunar payload services.
- Goals and Status of missions under preparation: orbiters, Luna25-27, SLIM, GLXP legacy, LRP, commercial landers, future landers, Lunar sample return missions;
- Precursor missions, instruments and investigations for landers, rovers, sample return, and human cis-lunar activities and human lunar surface sorties with Artemis and Intl Lunar Research Station;
- Preparation for International Lunar Decade: databases, instruments, missions, terrestrial field campaigns (e.g., EuroMoonMars), In-Situ Resources, ISRU, support studies;
- ILEWG and Global Exploration roadmaps towards a global robotic/human Moon village;
Note that this session is open to all branches of lunar science and exploration, and is intended as an open forum and discussion between diverse experts and Earth geoscientists and explorers at large. It is co-sponsored by ILEWG, COSPAR, IAF International Astronautical Federation, Space Renaissance International and MVA Moon Village Association.

Orals: Mon, 15 Apr | Room 1.31/32

Chairpersons: Chrysa Avdellidou, Joana S. Oliveira
14:00–14:01
Lunar Exploration & Utilisation
14:01–14:11
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EGU24-8916
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ECS
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On-site presentation
Peter Keresztes Schmidt, Nikita J. Boeren, Salome Gruchola, Marek Tulej, Andreas Riedo, and Peter Wurz

With NASA's emphasis on lunar exploration through the Artemis program, novel scientific objectives have been formulated to enhance our understanding of the Solar System's historical context, particularly the evolution of the Earth-Moon system. Simultaneously, the establishment of a permanent human presence on the Moon is proposed as a primary objective within the Artemis program, with the achievement of this goal hinging on in-situ resource utilization (ISRU) of lunar materials. Effective ISRU needs methodologies for chemical analysis and selecting appropriate lunar materials in-situ. To facilitate these tasks, the deployment of sensitive instrumentation capable of determining the element and isotope composition of lunar materials is imperative.

In this contribution, we present the current progress in developing a reflectron-type time-of-flight laser ablation ionisation mass spectrometer (RTOF-LIMS) to allow for direct sensitive chemical microanalysis of lunar regolith grains in-situ on the lunar surface. This LIMS system will operate in the lunar south pole region on a CLPS mission within NASA’s Artemis program.

The contribution will provide a general overview of the instrument and focus primarily on the design and operations of the sample handling system (SHS). Furthermore, we will discuss the results of experiments conducted on lunar regolith simulant. These experiments were performed using a prototype LIMS system to validate the feasibility of the SHS. This prototype system has capabilities representative of the flight instrument currently in development regarding the mass analyser and optical sub-system. The laboratory and flight optical sub-systems are based on a microchip Nd:YAG laser system (~ 1.5 ns pulse width, λ = 532 nm, 100 Hz laser pulse repetition rate, laser irradiance ~ 1 GW/cm2), and custom-made laser optics to achieve a focal spot on the sample surface of ~20 μm. Consequently, the conducted measurements can serve as a qualification baseline for the flight instrument during ground-based tests.

(1) P. Keresztes Schmidt et al., Sample handling concept for in-situ lunar regolith analysis by laser-based mass spectrometry, IEEE Aerospace Conference, 2024, submitted
(2) P. Wurz et al., In Situ Lunar Regolith Analysis by Laser-Based Mass Spectrometry, IEEE Aerospace Conference, 2023, 1-10
(3) P. Keresztes Schmidt, A. Riedo, P. Wurz, Chimia 2022, 76, 257
(4) A. Riedo, A. Bieler, M. Neuland, M. Tulej and P. Wurz, J. Mass Spectrom., 2013, 48, 1-15
(5) P. Wurz, M. Tulej, A. Riedo, V. Grimaudo, R. Lukmanov, and N. Thomas, IEEE Aerospace Conference, 2021, 50100, 1-15.

How to cite: Keresztes Schmidt, P., Boeren, N. J., Gruchola, S., Tulej, M., Riedo, A., and Wurz, P.: In-situ sample handling and chemical analysis of lunar regolith by laser ablation ionisation mass spectrometry, EGU General Assembly 2024, Vienna, Austria, 14–19 Apr 2024, EGU24-8916, https://doi.org/10.5194/egusphere-egu24-8916, 2024.

14:11–14:21
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EGU24-13507
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On-site presentation
F. Scott Anderson, Edward B. Bierhaus, Sarah E. Braden, Amy L. Fagan, Rico G. Fausch, James W. Head III, Katherine H. Joy, Jonathan Levine, Steve Osterman, John Pernet-Fisher, Romain Tartèse, Peter Wurz, and Marcella Yant

            The DIMPLE (Dating an Irregular Mare Patch with a Lunar Explorer) experiment has been selected by NASA for flight to the Moon later this decade. The objective is to date volcanic rocks from Ina, the largest known (3×2 km) irregular mare patch. Ina is remarkable for its scarcity of impact craters; taken at face value, the crater density implies a surface model age of 33 ± 2 Ma [1]. If the Moon was volcanically active this recently, it would require a profound reassessment of our understanding thermal evolution of the lunar interior. An alternative explanation for the anomalously low crater density posits that Ina is a chilled magmatic foam [2], the vesicularity of which favors crumbling rather than cratering during meteoroid impacts. If vesicularity can make a ~3000 Ma old terrane appear to be 100× younger, it begs the question of what other surface age estimates based on crater density, from anywhere in the inner Solar System, can also be wildly inaccurate.  

            The DIMPLE payload includes (i) the CODEX (Chemistry, Organics, and Dating Experiment) instrument, (ii) a sample-handling system including an arm for gripping rocks off the lunar surface, and (iii) a rover-mounted rake for collecting rock samples from farther afield. CODEX works by analyzing hundreds of 35 μm spots over rock samples 1.9-3.8 cm across, using laser-ablation mass spectrometry to measure the abundances of major elements and some trace elements, and using laser-ablation resonance-ionization mass spectrometry to measure the isotopic abundances of Rb and Sr. In this lunar context, the organics capability of CODEX will not be exploited.  The mass spectrometer for CODEX is a re-flight of the mass spectrometer designed for the Luna-Resurs mission, with an optimized ion source to collect resonantly excited ions in addition to ions produced directly by laser ablation. CODEX data will enable dating by the 87Rb-87Sr isochron technique and, by mapping elemental composition, will permit lithologic classification and petrologic interpretation of the analyzed rock samples from Ina.

 

References:        [1] Braden S.E. et al. (2014) Nature Geoscience 7, 787.

                             [2] Qiao L. et al. (2021) Planet. Sci. J. 2 66.

How to cite: Anderson, F. S., Bierhaus, E. B., Braden, S. E., Fagan, A. L., Fausch, R. G., Head III, J. W., Joy, K. H., Levine, J., Osterman, S., Pernet-Fisher, J., Tartèse, R., Wurz, P., and Yant, M.: The DIMPLE Experiment to Date Ina, a Young-Looking Volcanic Structure on the Moon, EGU General Assembly 2024, Vienna, Austria, 14–19 Apr 2024, EGU24-13507, https://doi.org/10.5194/egusphere-egu24-13507, 2024.

14:21–14:31
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EGU24-3294
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ECS
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Highlight
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On-site presentation
Honglei Lin

Water plays a crucial role in the Moon's evolution and holds significant implications for potential human activities on its surface. Previous studies, based on measurements of a limited number of lunar soil particles, have revealed evidence supporting various sources of lunar water, including its origin from the lunar interior, solar wind implantation, and impacts from comets or asteroids. Nevertheless, the limitation of these studies stems from the restricted number of particle samples, hindering the achievement of adequate statistical significance. As a result, the primary source of water on the Moon remains enigmatic. To address this critical question and advance our understanding of lunar water sources, we initiated new spectral measurements using lunar bulk soil collected by Chang'e-5 under controlled conditions. We observed variations in water content across different particle sizes. Our findings suggest that solar/ Earth wind implantation is likely the primary source of lunar surface water. The controlled experiments conducted on the lunar bulk soil samples provide valuable insights, offering statistical evidence for the origin of water in lunar soil. We also bridged the laboratory, in-situ, and orbital results, offering a cohesive understanding of lunar surface water characteristics as represented by Chang'e-5.

How to cite: Lin, H.: Primary Origin of Lunar Surface Water: Constraints from Observations of Chang'e-5, EGU General Assembly 2024, Vienna, Austria, 14–19 Apr 2024, EGU24-3294, https://doi.org/10.5194/egusphere-egu24-3294, 2024.

14:31–14:41
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EGU24-4876
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On-site presentation
Qin Zhou, Chunlai Li, Jianjun Liu, Weibin Wen, Yu Liu, Saihong Yang, Qiu-Li Li, Guangliang Zhang, Hongbo Zhang, Bin Liu, and Dawei Liu

Zircon is one of the most important U-bearing minerals in the lunar geochronological studies. Since the first lunar zircon grains were analyzed in the early 1980’s, the majority of lunar zircon U(Pb)-Pb ages obtained from the Apollo missions in the last decades were distributed between about 4.4 and 3.9 Ga. Although the crystallization age of Chang’e-5 (CE-5) basalts were obtained from baddeleyite, zirconolite and tranquillityite, we attempted to search for lunar zircon grains from the collected CE-5 lunar sample for comparison with the previous studies. We scanned almost all polished sections of the CE-5 powder sample to identify lunar zircon grains, most of which are isolated grains or mineral clast in agglutinates and impact melt breccias. In our study, only one zircon grain was preserved in the lithic clast of CE-5 basalts after the scanning of hundreds polished sections. This zircon records a precise Pb-Pb isochron age of 2036 ± 19 Ma, which is the youngest crystallization age ever reported for lunar zircon geochronology. Combined with the petrology, mineralogy and geochronology, we have demonstrated that this zircon grain is the extreme fractional product from a non-KREEP mantle source similar to CE-5 basalt. Compared to the zircon from Apollo mission, the sampling site of CE-5 provides a new case that lunar zircon can crystallize from a variety of magmatic compositions in addition to KREEP-related magma. In the future, we plan to perform the studies of zircon grains from CE-5 samples in different lithologies and try to find the origin of these zircons grains.

How to cite: Zhou, Q., Li, C., Liu, J., Wen, W., Liu, Y., Yang, S., Li, Q.-L., Zhang, G., Zhang, H., Liu, B., and Liu, D.: Lunar zircon from the Chang’e-5 landing site, EGU General Assembly 2024, Vienna, Austria, 14–19 Apr 2024, EGU24-4876, https://doi.org/10.5194/egusphere-egu24-4876, 2024.

14:41–14:51
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EGU24-6314
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solicited
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Highlight
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On-site presentation
Fabio Ferrari, Francesco Topputo, Carmine Buonagura, Carmine Giordano, Paolo Panicucci, Felice Piccolo, Antonio Rizza, Angelo Cervone, Detlef Koschny, Eleonora Ammannito, Richard Moissl, and Roger Walker

A large number of meteoroids and micrometeoroids enter the Earth–Moon system continuously, constituting a potential threat to our planet. Lunar meteoroid impacts have caused in the past a substantial change in the lunar surface and its properties. With no atmospheric shield, the Moon is subject to a large number of impacts from meteoroids, typically ranging from a few tens of grams to a few kilograms every day. The high impact rate on the lunar surface has important implications for future human and robotic assets that will inhabit the Moon for significant periods of time. Therefore, a better understanding of the meteoroid population in the cislunar environment is required for future exploration of the Moon. Moreover, refining current meteoroid models is of paramount importance for many applications, including planetary science investigations. For instance, since meteoroids may travel dispersed along the orbit of their parent body, understanding meteoroids and associated phenomena can be valuable for the study of asteroids and comets themselves, and their dynamical paths. Studying meteoroid impacts can help deepening the understanding of the spatial distribution of near-Earth objects in the Solar System. The study of dust particles is also relevant to the topic of space weather. The ability to predict impacts is therefore critical to many applications, both related to engineering aspects of space exploration, and to more scientific investigations regarding evolutional processes in the Solar System. Also, accurate impact flux models would be crucial to support planetary defense actions, as large meteoroids can cause severe damage to our communities.

In this context, the Lunar Meteoroid Impacts Observer (LUMIO) is a CubeSat mission to observe, quantify, and characterise lunar meteoroid impacts, by detecting their impact flashes on the far-side of the Moon. This complements the information available from Earth-based observatories, which are bounded to the lunar near-side, with the goal of synthesising a global recognition of the lunar meteoroid environment. LUMIO envisages a 12U CubeSat form-factor placed in a halo orbit at Earth-Moon L2. The detections are performed using the LUMIO-Cam, an optical instrument capable of detecting light flashes in the visible spectrum (450-950 nm). LUMIO has successfully passed Phases A and B and is currently moving towards Phase C.

We present the latest results on the modelling of the meteoroid environment in the Earth-Moon system, including an estimate of LUMIO’s potential impact on our existing knowledge of meteoroids, supported by high-fidelity simulation data. An overview of the present-day LUMIO CubeSat design is also given, with a focus on the latest developments involving both the ongoing/planned scientific activities and the development of the payload.

How to cite: Ferrari, F., Topputo, F., Buonagura, C., Giordano, C., Panicucci, P., Piccolo, F., Rizza, A., Cervone, A., Koschny, D., Ammannito, E., Moissl, R., and Walker, R.: LUMIO: a CubseSat to detect meteoroid impacts on the lunar farside, EGU General Assembly 2024, Vienna, Austria, 14–19 Apr 2024, EGU24-6314, https://doi.org/10.5194/egusphere-egu24-6314, 2024.

14:51–14:53
Lunar Science
14:53–15:03
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EGU24-1216
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ECS
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Highlight
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On-site presentation
Daniel Sheward, Chrysa Avdellidou, Anthony Cook, and Marco Delbo

Impact craters have been identified on almost every type of celestial body, and are among the most destructive processes. The lunar surface is covered in craters ranging from 2500km in diameter, down to sub-millimetre scale, and >600 lunar impact flash (LIF) events have been observed by ground based telescopes, detecting the generated light. Despite this large volume of data, previously only three freshly formed craters had been both located within LROC imagery, and have the forming LIF documented.
Using PyNAPLE (Sheward et al., 2022) - software which locates fresh craters from the selenographic latitude, longitude, and epoch of a LIF - a search was performed upon the 22 most energetic LIFs within literature. For completeness, this included the three LIF events with already identified craters.

There were sufficient LROC images to locate six new freshly formed craters, in addition to the three already identified. For these nine events, the likely parent meteoroid stream for each event is identified to constrain the velocity, impact geometry, and impactor properties. From this, the pre-impact kinetic energy could be obtained from an estimation for the luminous efficiency, and the luminous energy released by the LIF.

Furthermore, using the crater scaling laws from Melosh (1989), both the predicted crater size from the kinetic energy, and the predicted energy from the observed crater size, could be calculated for each event.

From this, it was found that the predicted crater diameter was consistently larger than the observed crater. While there are several factors that could contribute to this, the single most likely factor is the poorly constrained luminous efficiency. Under this assumption, a more accurate value for the luminous efficiency can be calculated using the observed craters. Using a rearrangement of the crater scaling laws, with the kinetic energy equation, and luminous efficiency, η = Elum/Ekwhere Elum is the energy released by the LIF, and Ekis the kinetic energy. After outlier removal and meteoroid stream identification, this produces an average value of η=0.0171324. While this is slightly larger than the typically used values of between 102and 104, the difference is not drastic.

References

Melosh, H. J. (1989). Impact cratering : a geologic process.
Sheward, D. et al (2022). MNRAS, 514(3):4320–4328

How to cite: Sheward, D., Avdellidou, C., Cook, A., and Delbo, M.: Lunar Impact Flashes and their Resultant Craters , EGU General Assembly 2024, Vienna, Austria, 14–19 Apr 2024, EGU24-1216, https://doi.org/10.5194/egusphere-egu24-1216, 2024.

15:03–15:13
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EGU24-21481
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solicited
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On-site presentation
Foteini Vervelidou, Benjamin P. Weiss, Claire I. O. Nichols, Mary Murray, Jay Shah, France Lagroix, Helena McDonald, and Claire Carvallo

Spacecraft magnetic field measurements and paleomagnetic studies on Apollo lunar samples indicate that the Moon once sustained a core dynamo. However, strength and  duration of the dynamo field are key unknowns that may constrain the mechanism that powered it. Shedding light on these questions can improve our understanding about the generation of dynamos on small planetary bodies. Here, I will present new paleointensity measurements of the lunar magnetic field, based on alternating field and controlled atmosphere thermal demagnetization. In particular, we measured mare basalts and regolith breccias from the Apollo 16 and Apollo 17 missions, with ages ranging from 1.7 to 3.75 Gy old. I will discuss the results in the context of two issues surrounding lunar paleomagnetism. Firstly, I will show, through the example of an Apollo 17 mare basalt specimen carrying magnetizations acquired at two different epochs, that the magnetic record of these rocks is of lunar origin, as opposed to spacecraft or terrestrial contamination. Secondly, I will show results from the Apollo 16 regolith breccias suggesting that the lunar dynamo was fluctuating in intensity at least since 3.4 Ga. A fluctuating dynamo has been proposed as a possible resolution to the energy conundrum of the early phase of the lunar dynamo. Over a period of several hundred million years, extending up to 3.5 Gy ago, various paleomagnetic studies have inferred paleointensities that require an energy budget in excess of what numerical simulations, assuming a dynamo powered by thermochemical convection, estimate to have been available, given the Moon’s small metallic core. While our results do not directly address the energy budget conundrum during that time period, the fact that magnetic field fluctuations have occurred at least since 3.4 Gy ago, hints at the possibility that they could have occurred also at earlier times. If these fluctuations were large enough, they could allow for a reconciliation between paleomagnetic studies and numerical simulations, without the need to evoke alternative dynamo mechanisms.

How to cite: Vervelidou, F., Weiss, B. P., Nichols, C. I. O., Murray, M., Shah, J., Lagroix, F., McDonald, H., and Carvallo, C.: New paleointensity measurements of Apollo samples and implications for the lunar dynamo, EGU General Assembly 2024, Vienna, Austria, 14–19 Apr 2024, EGU24-21481, https://doi.org/10.5194/egusphere-egu24-21481, 2024.

15:13–15:15
15:15–15:25
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EGU24-6905
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Virtual presentation
Catherine Elder, Rebecca Ghent, James Haber, Paul Hayne, Gareth Morgan, Mark Robinson, Matt Siegler, and Jean-Pierre Williams

The surface rock abundance map derived from the Lunar Reconnaissance Orbiter (LRO) Diviner Lunar Radiometer Experiment (Diviner) revealed variability in the rock abundance across the surface of the lunar maria [1]. Rocks on the lunar surface break down quickly relative to lunar geologic history [2, 3], so surface rock abundance is likely to be strongly tied to subsurface rock content which could include both coherent layers of mare basalts or large boulders mixed in with regolith. Most of the Moon’s surface is now covered in fine grained regolith, and historically various authors have argued that each surface unit started as a flat coherent layer of rock which gradually broke down into a layer of regolith whose thickness is a function of its bombardment history [e.g. 4, 5]. However, recently Head and Wilson (2020) [6] argued that modern understanding of lunar volcanism suggests substantial variability in post eruption surface conditions (e.g. void space, pyroclastic deposits, etc.) which could affect subsequent regolith development possibly leading to surfaces of the same age having regolith layers of different thicknesses and/or suspended rock populations. We compare the Diviner rock abundance [1] in different maria units defined and dated by Hiesinger et al. (2011) [7] to investigate both the change in surface rock abundance with time, and possible regional variability in rock properties [8]. We find that surface rock abundance does decrease with unit age as expected for a thickening layer of regolith. However, there is significant scatter in this relationship. We calculate the best-fit linear relationship between the median rock abundance and age of the units defined by Hiesinger et al. (2011) [7]. Investigation of the residuals of this fit reveals that they are not random. For example, Mare Australe is similar in age to Mare Tranquillitatis, but nearly all units in Mare Tranquillitatis are rockier than those in Mare Australe. Mare Humorum is notable for being one of the rockiest regions in the maria despite its relatively ancient surface (>3 Ga). These observations support the hypothesis of Head and Wilson (2020) [6], and suggest that further investigation into the properties of present-day surface rocks may provide insight into the initial mare basalts before billions of years of communition. Specifically, future in situ missions across diverse mare locations could offer insights into the variability of basaltic eruption styles that may have formed the lunar maria.

 

[1] Bandfield+ (2011), JGR, 116, E00H02.

[2] Basilevsky+ (2013), PSS, 89, 118.

[3] Ghent+ (2014) Geology, 42, 1059.

[4] McKay+ (1991) Lunar Sourcebook, Cambridge Press, 285.

[5] Hörz (1977), PCE, 10, 3.

[6] Head+ (2020) GRL, 47.

[7] Hiesinger+ (2011), GSA Special Papers, 477.

[8] Elder+ (2023) PSJ, 4:244.

How to cite: Elder, C., Ghent, R., Haber, J., Hayne, P., Morgan, G., Robinson, M., Siegler, M., and Williams, J.-P.: The Variability of Lunar Mare Basalt Properties Inferred from Present-Day Surface Rock Abundance, EGU General Assembly 2024, Vienna, Austria, 14–19 Apr 2024, EGU24-6905, https://doi.org/10.5194/egusphere-egu24-6905, 2024.

15:25–15:35
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EGU24-20971
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On-site presentation
Iraklis Giannakis, Craig Warren, and Antonis Giannopoulos

The Chinese Lunar mission Chang'E-4 soft-landed on the far side of the Moon on January 2019 marking a significant milestone in space exploration. The mission's landing site is on the eastern floor of Von Kármán (VK) crater (45.4446°S, 177.5991°E), within the South Pole–Aitken (SPA) basin, one of the oldest and largest impact craters in the solar system.

Yutu-2 is the rover of the Chang;E-4 mission. Similar to its twin rover Yutu-1, amongst its scientific payloads Yutu-2 carries a set of ground-penetrating radar (GPR) systems. GPR is a well-established geophysical method and has been instrumental in the new era of planetary exploration. Chang’E-3 was the first mission incorporating in-situ planetary GPR, a trend continued by subsequent Lunar and Martian missions, including Chang'E-4, Perseverance, Chang'E-5 and Tianwen-1; with plans for future missions such as Chang'E-7 and ExoMars [1].

Existing Lunar GPR studies often assume that the dielectric properties of Lunar materials can be modelled via a constant electric permittivity and a conductive term. However, treating the electric permittivity as non-dispersive overlook the frequency-dependent complex electric permittivity of ilmenite. Ilmenite is a titanium mineral, particularly abundant in Lunar mare basalts and soils. Recent investigations [1] using a complex Cole-Cole function have shown that ilmenite-mixtures act as low-pass filters, causing a decrease in the pulse's central frequency as the wave propagates through an ilmenite formation. This frequency shift, proportional to the ilmenite content, serves as a basis for inferring the presence of basalts and approximating their ilmenite content.

In this study, we explore the frequency shift of signals received both from Channel-2B and Channel-1. Our analysis reveals a sequence of basaltic layers extending to approximately 300 m depth, displaying varying thickness and ilmenite content. Based on the estimated ilmenite content, the GPR data indicates three distinct phases of Lunar volcanism: an early phase with high-Ti basalts, followed by a low-Ti volcanic activity, and a final phase with high-Ti basalts. These findings align with generic models of Lunar lava emplacement [1]. According to these models, Lunar volcanic history includes an early "blue" titanium-rich volcanic event (~ 3.8-3.5 Ga), followed by low-Ti "red" basalts (~ 3.5-3 Ga), and a subsequent phase of "blue" high-Ti basalts (~3 Ga) [2].

References

[1]   Giannakis, I., Martin-Torres, J., Su, Y., Feng, J., Zhou, F., Zorzano, M-P., Warren, C., Giannopoulos, A., (2024). Evidence of Shallow Basaltic Lava Layers in Von Kármán Crater from Yutu-2 Lunar Penetrating Radar, Icarus, 2024.

 

[2] Cattermole, P. J., (1996). Planetary Volcanism: A Study of Volcanic Activity in the Solar System, Wiley, Chichester, 2ndEdition, 1996.

 

How to cite: Giannakis, I., Warren, C., and Giannopoulos, A.: Lunar Penetrating Radar Reveals Three Phases of Volcanism at Von Kármán Crater, EGU General Assembly 2024, Vienna, Austria, 14–19 Apr 2024, EGU24-20971, https://doi.org/10.5194/egusphere-egu24-20971, 2024.

15:35–15:45
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EGU24-17449
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ECS
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On-site presentation
Sabatino Santangelo, Ana-Catalina Plesa, Adrien Broquet, Doris Breuer, and Bart C. Root

High resolution gravity field measurements from GRAIL [1], in-situ heat flux [2] and seismic measurements from Apollo [3,4], surface composition from Clementine and Lunar Prospector [5,6], and the analysis of lunar samples have provided a wealth of information about the thermal evolution of the Moon [7].

Constraints on the present-day thermal state of the lunar interior come from the Apollo surface heat flux measurements: 21±3 mW m-2 at the Apollo 15 and 14±2 mW m-2 at the Apollo 17 landing sites [2]. A peak heat flux of ~180 mW m-2 was recently inferred by [8] from the Chang’E 1 and 2 data at the Compton-Belkovich location, a Thorium anomaly feature on the lunar farside. A lower bound for the lunar heat flux of only ~6 mW m-2 has been suggested, for the so-called Region 5, by measurements of the Diviner Lunar Radiometer Experiment onboard LRO [9]. Additionally, thermal expansion/contraction estimates [10] provide secondary constraints on the thermal state of the interior throughout lunar history.

Here, we model the interior dynamics of the Moon to infer plausible distributions of heat producing elements (HPEs) that, in turn, are directly linked to surface heat flux variations. To this end, we compare the present-day surface heat flux obtained in our models with the above constraints. Similar to [11], we combine global geodynamical models [12] with crustal thickness models derived from gravity and topography data [13]. We include higher HPEs abundances in the Procellarum KREEP Terrane (PKT) and crust compared to the mantle, and a mantle rheology similar to [14]. We test both constant and pressure/temperature dependent thermal conductivity scenarios. In addition to present-day heat flux, we compute the thermal expansion/contraction based on the interior thermal state obtained from our models at different times during lunar evolution and compare these values with available estimates to select best-fit models.

We find that variations in crustal thickness and the distribution of HPEs in the crust, mantle, and PKT region predominantly affect the convection pattern in the lunar interior and the surface heat flux. Models best compatible with the heat fluxes in the Apollo regions and Region 5 show an average Thorium abundance in the PKT region of ~2.4 ppm, smaller than the observed surface values [6], suggesting a strong Thorium enrichment close to the surface. These models have a crustal thermal conductivity of ~1.2 W/(mK), ~3 times lower than that of the mantle. None of our models matches the heat flux estimated at the Compton-Belkovich location, indicating either specific local processes [8] or large measurement uncertainties.

References:

[1] Zuber et al., 2013; [2] Langseth et al., 1976; [3] Garcia et al., 2019; [4] Nunn et al., 2020; [5] McEwen et al., 1997; [6] Lawrence at al., 2003; [7] Jaumann et al., 2012; [8] Siegler et al., 2023; [9] Paige & Siegler, 2016; [10] Andrews-Hanna et al. 2013; [11] Plesa et al., 2016; [12] Hüttig et al., 2013; [13] Broquet & Andrews-Hanna, 2023; [14] Laneuville et al., 2013.

How to cite: Santangelo, S., Plesa, A.-C., Broquet, A., Breuer, D., and Root, B. C.: Present-day surface heat flux variations on the Moon from global geodynamic and crustal thickness models, EGU General Assembly 2024, Vienna, Austria, 14–19 Apr 2024, EGU24-17449, https://doi.org/10.5194/egusphere-egu24-17449, 2024.

Posters on site: Mon, 15 Apr, 16:15–18:00 | Hall X3

Display time: Mon, 15 Apr, 14:00–Mon, 15 Apr, 18:00
Chairpersons: Chrysa Avdellidou, Joana S. Oliveira, Bernard Foing
Lunarphysics
X3.52
|
EGU24-4201
Full Moon Phase: Lunar Surface Charging in Plasma Sheet - PIC Simulation
(withdrawn after no-show)
Suleiman Baraka, Sona Hosseini, Guillaume Gronoff, and Robert Rankin
X3.53
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EGU24-4978
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ECS
Siqi Yi, Xiaojun Xu, Lianghai Xie, Xing Wang, Qi Xu, Zilu Zhou, Hengyan Man, Lei Luo, Peishan He, and Pu Yang

Comprehending the internal structure of the Moon is crucial for uncovering its formation and evolution. The existence of the lunar core can be proved by several pieces of evidence, including electromagnetic sounding analyses, mass and moment of inertia analyses, and seismic analyses. However, the precise size and composition of the lunar core are still unknown. In this study, the induced magnetic field generated by the lunar metallic core is illustrated through a three-dimensional MHD simulation. Several cases have been discussed in which the lunar core are set with different electrical conductivities and thicknesses. Compared to the hybrid model, our MHD model can calculate more accurate results with a more refined grid. Our simulation can capture the variations of parameters (plasma densities, temperature, and flow speed) in original and final conditions, while the hybrid model cannot.

How to cite: Yi, S., Xu, X., Xie, L., Wang, X., Xu, Q., Zhou, Z., Man, H., Luo, L., He, P., and Yang, P.: Three-dimensional MHD simulation of lunar induced magnetic field generated by lunar metallic core, EGU General Assembly 2024, Vienna, Austria, 14–19 Apr 2024, EGU24-4978, https://doi.org/10.5194/egusphere-egu24-4978, 2024.

X3.54
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EGU24-20166
Joana S. Oliveira, Foteini Vervelidou, Mark A. Wieczorek, and Marina Diaz Michelena

We know from spacecraft measurements that the crust of the Moon is heterogeneously magnetized. With the exception of a few magnetic anomalies related to craters and swirls, the origin of most of the lunar magnetic anomalies is not understood. Here we evaluate the performance of an inversion methodology, initially conceived to infer the direction of the underlying magnetization from magnetic field measurements, commonly referred to as Parker's method, to elucidate the origin of the magnetic sources by constraining the location and geometry of the underlying magnetization. We assess the performance of the method by conducting a variety of tests, using synthetic magnetized bodies of different geometries. These have been chosen such that they mimic  the main geological structures potentially magnetized within the lunar crust. Our test results show that the Parker method successfully localizes and delineates the two-dimensional surface projection of subsurface three-dimensional magnetized bodies, when certain conditions are fulfilled. In particular, the magnetization should be close to unidirectional, and the magnetic field data should have a higher spatial resolution than the smallest dimension of the magnetized body as well as a high signal-to-noise ratio. As an additional evaluation test, we applied this inversion methodology to two lunar magnetic anomalies that are associated with visible geological features, the Mendel-Rydberg impact basin and the Reiner Gamma swirl. For Mendel-Rydberg,  our analysis shows that the strongest magnetic sources are located within the basin's inner ring in agreement with previous studies showing that during an impact, the crust inside the newly formed crater undergoes demagnetization and potentially remagnetization (if an ambient magnetic field is present). For Reiner Gamma, we found the strongest magnetic sources form a narrow dike-like body that emanates from the center of the Marius Hills volcanic complex. The reason that only one such dike emanating from Marius Hills is magnetized could be linked to an atypical iron-metal composition or to the lunar ambient magnetic field being only intermittently present. Future applications of this method can focus on constraining the origin of the many lunar magnetic anomalies that are not associated with visible geological features.

How to cite: Oliveira, J. S., Vervelidou, F., Wieczorek, M. A., and Diaz Michelena, M.: Constraints on the spatial distribution of lunar crustal magnetic sources from orbital magnetic field data, EGU General Assembly 2024, Vienna, Austria, 14–19 Apr 2024, EGU24-20166, https://doi.org/10.5194/egusphere-egu24-20166, 2024.

X3.55
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EGU24-21717
Sarah Vines, George Ho, and David Blewett and the The Lunar Vertex Science Team

Lunar Vertex, selected as NASA’s first Payloads and Research Investigations on the Surface of the Moon (PRISM) delivery, will explore a portion of Reiner Gamma (7.585° N, 58.725° W) with instruments mounted on a lander and small rover. Reiner Gamma (RG) is home to a magnetic anomaly, a region of magnetized crustal rocks. The RG magnetic anomaly is co-located with the type example of a class of irregular high-reflectance markings known as lunar swirls. The Lunar Vertex payload was designed to address three science goals: (1) test hypotheses for the origin of the RG magnetic anomaly, (2) test hypotheses for the origin of the RG swirl, and (3) determine the structure of the RG mini-magnetosphere. The payload suite consists of three instruments on the lander, and two instruments on a small commercial rover.

The Lunar Vertex payload will be carried to the lunar surface on a commercial lander as part of NASA's Commercial Lunar Payload Services (CLPS) program. The lander and payload are designed for operation during one lunar daylight period (i.e., no night operations or survival). NASA selected Intuitive Machines as the CLPS provider for the Reiner Gamma delivery. At the time of this writing, the launch will be no earlier than June of 2024.

Lander Instruments: The three Lunar Vertex lander instruments were delivered to Intuitive Machines in June 2023. The Magnetic Anomaly Plasma Spectrometer (MAPS), built by the Southwest Research Institute, is capable of measuring the ion and electron velocity distribution over a 292.5° x 90° FOV from 8 eV/e to 17.5 keV/e. The Vector Magnetometer–Lander (VML) suite, built by APL, is comprised of a tetrahedral array of four commercial fluxgate magnetometers mounted on the bottom of a 0.5-meter mast, with a science-grade dual-ring core fluxgate magnetometer at the top of the mast. Together, MAPS and VML will characterize the magnetic field and surface plasma environment within RG. The Vertex Camera Array (VCA) suite, built by Redwire, is a set of three clusters of three RGB cameras. VCA images will be used to characterize the landing site geology and to understand the physical properties of the lunar regolith around the lander.

Rover and Rover Instruments: The rover vehicle is from vendor Lunar Outpost. The rover instruments were integrated with the vehicle at APL, and environmental testing was carried out on the integrated system. The Vector Magnetometer–Rover (VMR), built by APL, is also comprised of a tetrahedral array of commercial fluxgate sensors, mounted on a 0.2-meter mast. With VML, VMR will characterize local spatial structuring of the magnetic field at RG. The Rover Multispectral Microscope (RMM), mounted inside the rover body, is a close-up imager that can provide information on soil texture, as well as active LED illumination at a set of UV to NIR wavelengths chosen for their utility in determining the composition and maturity state of the regolith. The rover will be delivered to Intuitive Machines in early January 2024.

How to cite: Vines, S., Ho, G., and Blewett, D. and the The Lunar Vertex Science Team: The Lunar Vertex PRISM Payload: Ready for the Moon, EGU General Assembly 2024, Vienna, Austria, 14–19 Apr 2024, EGU24-21717, https://doi.org/10.5194/egusphere-egu24-21717, 2024.

X3.56
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EGU24-9849
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ECS
Sabrina Keil, Heiner Igel, Felix Bernauer, Dmitriy Shutin, Ban-Sok Shin, Kai Nierula, Philipp Reiss, Rok Sesko, and Fabian Lindner

Ground motion observations on planetary objects are a prerequisite for a detailed understanding of their interior structure and evolution. The imaging of the near surface structure - in particular on the Moon - has strong practical implications. First, the race is on to detect ice-bearing rocks near the surface from which water could be extracted and used as a resource for crewed missions. Second, due to the substantial bombardment of the lunar surface with meteorites and the lack of an atmosphere, observatories or habitats may have to be built underground. It has been proposed that cavities from ancient lava flows below the lunar surface could be used to place infrastructure. Current mission plans for geophysical exploration focus on static seismic sensors/arrays that would be restricted to the area they can explore.      
With the NEPOS project we want to go beyond these restrictions and develop concepts for mobile seismic arrays that work in an autonomous way using robotic technology. The scientific challenges include the understanding of wavefield effects of icy rocks and caves in a strongly scattering environment, the provision of optimal source-receiver configurations to detect them, as well as an integrated data-processing workflow from observation to subsurface image including the quantification of uncertainties.   
In order to solve these challenges, we first developed a Digital Twin for wave propagation in the strongly heterogeneous lunar crust to generate synthetic seismic data using the spectral element code SALVUS. We compared the synthetic seismograms to data from the Apollo 17 Lunar Seismic Profiling Experiment (LPSE) and find that their main characteristics coincide. We further generated synthetic seismograms for a variety of network configurations and subsurface heterogeneities, which will be used to test appropriate imaging methods for the lunar subsurface structure. Due to the presence of strongly scattering media ambient noise tomography seems to be a promising method, as was already shown in previous studies. We apply seismic interferometry to LPSE data, as well as to our synthetic seismograms, to reconstruct Green’s functions, which give us information on the subsurface properties.

How to cite: Keil, S., Igel, H., Bernauer, F., Shutin, D., Shin, B.-S., Nierula, K., Reiss, P., Sesko, R., and Lindner, F.: The NEPOS Project: Near-Surface Seismic Exploration of Planetary Bodies with Adaptive Networks, EGU General Assembly 2024, Vienna, Austria, 14–19 Apr 2024, EGU24-9849, https://doi.org/10.5194/egusphere-egu24-9849, 2024.

X3.57
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EGU24-1694
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ECS
Keisuke Onodera

Seismic observation is a powerful tool to investigate the Earth’s geological activities and internal structure and has also been applied to the Moon and Mars [e.g., Latham et al., 1969; Banerdt et al., 2020]. For the Moon, a seismic network was constructed on the nearside during the Apollo missions, and nearly eight years of observation provided us with more than 13,000 seismic events [Nakamura et al., 1981]. These events have contributed to understanding the seismicity rate on the Moon and its internal structure [e.g., Garcia et al., 2019; Nunn et al., 2020], both of which are important to know the current geological activity level and trace back to the thermal evolution in the past.

In the Apollo lunar seismic observation, two types of seismometers were installed: Long-Period (LP) and Short-Period (SP) seismometers. While the LP sensor has sensitivity at 0.2 – 1.5 Hz, the SP is sensitive at 1 – 10 Hz [e.g., Nunn et al., 2020]. In previous studies, the LP data were mainly used. In fact, all the cataloged events were detected solely using the LP data [Nakamura et al., 1981]. On the other hand, because of numerous unnatural signals and/or spikey noises, the majority of SP data remained unanalyzed after the initial description of high-frequency quakes by Duennebier and Sutton (1974a, 1974b) [e.g., Frohlich and Nakamura, 2006; Knapmeyer-Endrun and Hammer, 2015]. This fact implies that there are potential seismic events only identifiable in the SP data, and the lunar seismicity might be underestimated.

Lately, Onodera (2023) denoised all the SP data and performed an automatic event detection. As a result, he discovered about 22,000 new seismic events, including thermally driven quakes (thermal moonquakes), impact-induced events, and tectonic-related quakes (shallow moonquakes). While the former two types are useful to understand the surface evolution or degradation processes, the latter type is closely related to the seismic activity level of the Moon. Here, I focus on shallow moonquakes. In the past, since only 28 shallow moonquakes were identified, it was difficult to give a detailed description of their source mechanism, regionality, and correlation with tidal force. In this study, using the newly discovered 46 shallow moonquakes, I’m trying to give new insights into this type of event.

In the presentation, I will describe the general characteristics of newly discovered shallow moonquakes (e.g., waveforms and spectral features) and summarize the estimated source parameters (such as energy release, seismic moment, and body wave magnitude).

 

References

  • Banerdt et al. (2020), Nat. Geosci., 13(3), 183-189.
  • Duennebier and Sutton (1974a), JGR, 79(29), 4365-4374.
  • Duennebier and Sutton (1974b), JGR, 79(29), 4351-4363.
  • Frohlich and Nakamura (2006), Icarus, 185(1), 21-28.
  • Garcia et al. (2019), Space Sci. Rev., 215(8), 50.
  • Knapmeyer-Endrun and Hammer (2015), JGR Planets, 120 (10), 1620-1645.
  • Latham et al. (1969), Science, 165(3890), 241-250.
  • Nakamura et al. (1981), UTIG Technical Report, No. 118.
  • Nunn et al. (2020), Space Sci. Rev., 216(5), 89.
  • Onodera (2023), ESSOAr, DOI: 22541/essoar.169841663.38914436/v1

How to cite: Onodera, K.: Newly Discovered Shallow Moonquakes: General Characteristics and Source Parameters, EGU General Assembly 2024, Vienna, Austria, 14–19 Apr 2024, EGU24-1694, https://doi.org/10.5194/egusphere-egu24-1694, 2024.

X3.58
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EGU24-8297
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ECS
Josipa Majstorović, Philippe Lognonné, Taichi Kawamura, and Mark Panning

NASA selected a new in-situ seismic experiment, Farside Seismic Suite (FSS), onboard CP-12 lander with the landing site at the farside of the Moon in Schrödinger Basin. This future mission should provide us with the data to further constrain lunar interior and the Moon seismicity. Due to the single-station nature of the mission, localisation of the newly detected events will be challenging. Therefore, in this study we develop a pipeline for the deep moonquake (DMQ) source region localisation on the legacy of the data acquired during the Apollo missions. We are interested into DMQs since their source regions, called nests, on the near side have been identified, and since their occurrence patterns follow specific spatial and temporal patterns. Spatial patterns are related to tsp=ts-tp travel time measurement. We can show that based on tsp measurements we can form group of nests, called sets, that share similar travel times within error bars and therefore we cannot distinguish between nests that belong to the same set just using the travel time information. Temporal patterns are related to the fact that occurrence of DMQs is closely related to the monthly motion of the Moon around the Earth. Different nests correspond differently to three lunar months: synodic, draconic, anomalistic. By combining the spatial and temporal patterns we try to characterise different nests and exploit this information for their prediction. For this purpose we develop a machine learning model for nets classification. An input data into model we use orbital parameters related to the monthly motion of the Moon around Earth, which we relate to different nests. The ML model is learned to classify between nests that belong to the sam set. We report that models are achieving an accuracy over 70% when those are trained to classify =< 4 nests within the set, and better than 90% when only two DMQ nests are in the same set. This approach opens up a new way to DMQ location estimate, on the near and farside of the Moon, when captured by the future FSS single-station seismometers or other seismic stations on the Moon. 

How to cite: Majstorović, J., Lognonné, P., Kawamura, T., and Panning, M.: Relating deep moonquake source regions from Apollo missions with their temporal and spatial patterns using machine learning, EGU General Assembly 2024, Vienna, Austria, 14–19 Apr 2024, EGU24-8297, https://doi.org/10.5194/egusphere-egu24-8297, 2024.

Lunar Subsurface
X3.59
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EGU24-21578
Anna Mittelholz, Simon C. Stähler, Hendrik Kolvenbach, Valentin Bickel, Joseph Church, Svein-Erik Hamran, Ozgur Karatekin, Birgit Ritter, Jordan Aaron, Barthélémy Anhorn, Sofia Coloma, Larissa de Palézieux dit Falconnet, Matthias Grott, Cristophe Ogier, Johan Robertsson, and Krzysrof Walas

We present LunarLeaper, a robotic explorer concept in response to the ESA 2023 Small Missions call. Pits, volcanic collapse features with near-vertical walls, have been identified across the lunar and Martian surface. These pits are high priority exploration destinations because some, referred to as skylights, might provide access to subsurface lava tube systems. Lava tubes are of particular interest for future human exploration as they offer protection from harmful radiation, micrometeorites and provide temperate and more stable thermal environments compared to the lunar surface. We propose to use a small legged robot (ETH SpaceHopper, <10 kg), to access and investigate the pit edge, using its ability to access complex and steep terrain more safely than a wheeled rover. LunarLeaper will land in Marius Hills within a few 100 m of the pit and traverse across the lateral extent of the hypothesized subsurface lava tube. On its traverse it will take measurements with a ground penetrating radar and a gravimeter, measurements that will allow us to survey the subsurface structure and detect and map lava tube geometry if present. The robot will approach the pit edges and acquire high resolution images of the pit walls containing uniquely exposed layers of the geophysically mapped lava flows and regolith layers. These images will allow not only scientific advances of lunar volcanism and regolith formation, but also enable assessment of the stability of the pit structure and its use as a possible lunar base. The mission is expected to last 1 lunar day. The robot could be delivered to the surface by a small lander, as they are currently developed and planned by various national and commercial agencies and hop off the landing platform without the need for a robotic arm. It is highly flexible in accommodation and can thus make full use of the new international lunar ecosystem.

How to cite: Mittelholz, A., Stähler, S. C., Kolvenbach, H., Bickel, V., Church, J., Hamran, S.-E., Karatekin, O., Ritter, B., Aaron, J., Anhorn, B., Coloma, S., de Palézieux dit Falconnet, L., Grott, M., Ogier, C., Robertsson, J., and Walas, K.: Lunarleaper – Unlocking a Subsurface World, EGU General Assembly 2024, Vienna, Austria, 14–19 Apr 2024, EGU24-21578, https://doi.org/10.5194/egusphere-egu24-21578, 2024.

X3.60
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EGU24-15979
Internal structure inference of lunar lave tubes with the MCMC approach
(withdrawn after no-show)
Wenrui Wang and Xingda Jiang
X3.61
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EGU24-7237
|
ECS
Parallel numerical simulation of impact crater with perfect matched layers
(withdrawn after no-show)
Huacheng Li, Nan Zhang, Zongyu Yue, Jinhai Zhang, and Zhongzheng Miao
X3.62
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EGU24-12084
Urs Mall, Yehor Surkov, and Peter Cadogan

The surfaces of planetary bodies reflect their evolution through primary surface shaping via their continuous evolvement over time. Surface formation and degradation processes need to be understood in detail to infer the timescales over which these processes operate.

Planetary surfaces which are heavily cratered offer the opportunity to investigate various aspects of the cratering processes which are initiated when an impactor strikes their surface and ejects rock fragments from the impact point upon the newly-formed crater cavity and its surroundings (e.g. Hörz, F. and Cintala, M., 1997). Among the ejecta material from the impact are boulders covering a wide range of sizes (e.g. Nagori,R. et al., 2024). Dependent on the planet’s environment and the size of the impact fragments, these boulders can form either secondary craters or simply become subject to the various environmental forces which ultimately add through different degradation processes to the formation of planetary regolith. To understand many of the aspects of the above processes, size distributions of both the impact-generated boulders and secondary craters need to be understood (e.g. Cadogan, P., 2024).

As many of the techniques to identify boulders and small craters on albedo images are using shadow-based identification methods one has to be aware that ambiguities can arise through complex topographies and overlapping surface features. These factors can modify the shape of the shadow and make the identification of its borders difficult, thereby preventing a precise determination of both it’s location and it’s radius.

To obtaining high-quality statistics for boulders and craters over large and varied planetary surfaces, machine learning and deep learning methods have been applied to automate the tedious human based detection work (e.g. DeLatte, D. et al, 2019). However, little attention has been paid to investigate the influence of the training sets on the success rates of these efforts (Mall, U. et al., 2023). We are investigating in this study the influence of crater training sets, originating from specifically chosen lunar areas on the resulting confusion matrices produced by specific convolution neural networks and compare these with the results found from traditional imaging methods.

Cadogan, P., (2024), Automated precision counting of small lunar craters - A broader view, Icarus, Volume 408, 2024,115796.

DeLatte, D.M., Crites, S.T., Guttenberg, N., Yairi, T. (2019), Automated crater detection algorithms from a machine learning perspective in the convolutional neural network era, Advances in Space Research, Volume 64, Issue 8, Pages 1615-1628.

Hörz, F. and Cintala, M. (1997), The Barringer Award Address Presented 1996 July 25, Berlin, Germany: Impact experiments related to the evolution of planetary regoliths. Meteoritics & Planetary Science, 32: 179-209. https://doi.org/10.1111/j.1945-5100.1997.tb01259.x.

Mall, U., Kloskowski, D., Laserstein, P., (2023), Artificial intelligence in remote sensing geomorphology—a critical study, Front. Astron. Space Sci., 30 November 2023, Sec. Planetary Science , Volume 10 – 2. https://doi.org/10.3389/fspas.2023.1176325.

Nagori,R., Dagar, A. K., Rajasekhar, R.P., (2024),  Age estimation and boulder population analysis of the West crater at Apollo 11 landing site using Orbiter High Resolution Camera on board Chandrayaan-2 mission, Planetary and Space Science, Volume 240, 2024, 105828.

How to cite: Mall, U., Surkov, Y., and Cadogan, P.: How do training sets influence crater and boulder detection in machine learning?, EGU General Assembly 2024, Vienna, Austria, 14–19 Apr 2024, EGU24-12084, https://doi.org/10.5194/egusphere-egu24-12084, 2024.

X3.63
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EGU24-10730
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Highlight
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Werner Grandl

Space stations on the lunar surface are exposed to cosmic rays, solar flares, micrometeorites and huge temperature variations. Therefore human outposts on the lunar surface have to be covered by huge layers of regolith. In 2009 the Japanese lunar orbiter SELENE (Selenological and Engineering Explorer) has detected three giant lunar holes: Mare Tranquilitatis Hole (MTH), Marius Hills Hole and Mare Ingenii Hole. The holes differ from normal impact craters and may be the entrances to underground lave tubes. The deepest one is MTH with 107 m and 98 x 84 m in diameter. According to Haruyama et al. the soil of lunar holes could contain water resources (protons from solar-wind hydrogen flux or even water molecules). Lunar holes reduce the effects of cosmic rays because of their limited field of view from the bottom. They provide also milder temperatures than the lunar surface. In the shadowed areas the temperature  ranges from -20°C to +30°C during the lunar day. These benefits make lunar holes become favourite locations to establish initial lunar stations. In a first step we propose to build an initial base on the lunar surface at the edge of MTH. It can be used for storage and as a "site hut" for astronauts to supervise the following work. In a second step the initial base is enlarged by a modular structure down to the bottom of MTH. Robotic and semi-robotic machinery is used to erect the modular structures. Lunar regolith is used for protection against cosmic rays and meteorites (ISRU In Situ Resource Utilization). Finally MTH could be  closed by a transparent dome and filled with air to create a "green" habitat for human settlers.

 

How to cite: Grandl, W.: Mare Tranquilitatis Hole - a habitable place for a first lunar settlement, EGU General Assembly 2024, Vienna, Austria, 14–19 Apr 2024, EGU24-10730, https://doi.org/10.5194/egusphere-egu24-10730, 2024.

Lunar Surface
X3.64
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EGU24-3166
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ECS
Jing Yang and Lianghui Guo

As an important physical property of the Moon, the lunar crustal density provides evidence for the early evolution process of the Moon, such as the asymmetry of its nearside and farside. The apparent density is the average value of the bulk density at a certain depth. The gravity inversion method is an effective tool of determining the apparent density distribution of the lunar crust. Benefiting from the lunar GRAIL mission's high-precision gravity field models, it is theoretically possible to establish a global high-resolution apparent density model through the gravity inversion. However, there are two major problems, namely, the accuracy and efficiency of the inversion. To solve these problems, different from the admittance methods, we develop a high-precision apparent density mapping method in the spherical coordinate. The improved 2D Gauss-Legende formula and adaptive subdivision algorithm are adopted to calculate the high-precision gravity anomalies of the Tesseroid cells. The parallel algorithm based on OpenMP is involved to improve the calculation efficiency of the global data. And the Cordell iterative algorithm is utilized to derive the apparent density model fitting the real gravity anomalies. The synthetic data tests verify the accuracy and efficiency of our method. Subsequently, we use LOLA topographic data to correct the gravity anomalies obtained from GRAIL and derive the global lunar Bouguer gravity anomalies. The lunar crust thickness model given by Wieczorek et al (2013) is chosen as the bottom interface of the density layer. As a result, we obtain a global high-resolution lunar crust apparent density model with a resolution of about 20 km by the presented mapping method. Our model shows that the apparent density of the lunar crust ranges from about 2200 - 2900 kg/m3 with a mean value of about 2600 kg/m3. The Procellarum KREEP Terrane (PKT) and the large impact basins present higher apparent density, while the Feldspathic Highlands Terrane (FHT) varies around the mean apparent density, and there is a significant variation within the South Pole-Aiken Basin Terrane (SPAT). Our apparent density distribution around the PKT and FHT is significantly relevant to the surface grain density model derived from the current FeO and TiO2 abundance map. However, our apparent density distribution around the SPAT differs from the surface grain density, suggesting a more complex density structure in this region.

How to cite: Yang, J. and Guo, L.: The apparent density distribution of the lunar crust revealed by the spherical coordinate-based mapping method, EGU General Assembly 2024, Vienna, Austria, 14–19 Apr 2024, EGU24-3166, https://doi.org/10.5194/egusphere-egu24-3166, 2024.

X3.65
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EGU24-17062
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ECS
Dung Tri Nguyen, Stéphane Jacquemoud, Antoine Lucas, Sylvain Douté, Cécile Ferrari, Sophie Coustance, Sébastien Marcq, and Aimé Meygret

Understanding the physical characteristics of terrestrial and planetary surfaces is imperative for unraveling the complexity of landscape formation and evolution, and to develop strategies for future planetary rover missions. Photometry is one of the most widely used methods for studying these characteristics. The light scattered by a surface is quantified by the bidirectional reflectance distribution function (BRDF), providing a uniquely detailed optical measurement for each target observed. Hapke model inversion, an approach widely used over the past decades, reveals complex surface attributes, including roughness, porosity, grain size and shape, micro-texture, mineral composition, and more.

Although the challenges of restrictive data conditions and limited computational capabilities impeded the inversion of the Hapke model for large-scale surface analysis, we’ve addressed these issues with appropriate data and a comprehensive framework. Extracting multiangular surface data requires optical sensors with pointing capabilities and, by extension, images captured from different illumination directions. Earth observation satellites such as the Pleiades constellation managed by the Centre National d’Études Spatiales (CNES), have demonstrated their agility in extracting large-scale BRDF data on the Moon for optical sensor calibration. The processing chain involves geometric correction using digital elevation models supplied by NASA, and inversion of the Hapke model on each pixel, which is facilitated by a fast Bayesian inversion framework (Kugler et al., 2022). Inversion of the Hapke model on the BRDF extracted from each pixel generates maps of the six model parameters for the areas studied on the near side of the lunar surface, primarily the Apollo landing sites.

The BRDFs extracted from Pleiades images over the Apollo 17 landing site are consistent with prior knowledge of the photometric behavior of the Moon's surface. The quality of these BRDFs prompted us to extend our analysis to a 10° x 10° region around the mentioned site. Given the 1.5 km ground sampling distance of Pleiades images, the map size is 200 x 200 pixels (approximately 300 x 300 km). The distribution of the parameter values reflects the topography of the region, with a notable contrast between flat and steeply sloping areas. Optimal fits with an acceptable level of error are obtained on flat terrain, while the algorithm encounters difficulties in steeply sloping areas due to the complexity of the terrain within the large ground sampling distance.  In the current state, the application of the framework is extending to cover the near side of the Moon. The parameters obtained for each terrain unit will be compared with previous works (Souchon et al., 2013; Sato et al., 2014; Gimar et al., 2022; Marshal et al., 2023; Nagori et al., 2023) and correlated with a geological map (Fortezzo et al., 2020).

 

How to cite: Nguyen, D. T., Jacquemoud, S., Lucas, A., Douté, S., Ferrari, C., Coustance, S., Marcq, S., and Meygret, A.: Unveiling the characteristics of the lunar surface by massive inversion of the Hapke model, EGU General Assembly 2024, Vienna, Austria, 14–19 Apr 2024, EGU24-17062, https://doi.org/10.5194/egusphere-egu24-17062, 2024.

X3.66
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EGU24-292
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ECS
Iskren Ivanov and Lachezar Filchev

Hyperspectral images, despite their rich spectral information, often suffer from low spatial resolution due to physical constraints in imaging sensors. However, when higher spatial resolution data of the same scene are available, we can perform data fusion to generate hyperspectral images with high spatial resolution. This fused data can be viewed as the output of a synthetic sensor that combines the high spatial and spectral resolution data acquired by different sensors. This fusion allows for new applications with increased accuracy, such as high-resolution mapping of minerals and surface materials. Imaging spectroscopy facilitates the identification and discrimination of materials and their constituents. Data fusion enhances both the spatial and spectral characteristics of the initial data. It is based on the synergistic exploitation of data from different sources, aiming to produce superior results. By integrating data from The Moon Mineralogy Mapper (M3) by NASA and the Imaging Infrared Spectrometer (IIRS) by ISRO, we can improve the spatial and spectral resolutions, enhance measurement accuracy, and reduce uncertainties. This will enable a more precise assessment of the mineral composition of the area of interest. The objective is to fuse high spatial resolution data, which has discontinuities in the spectral domain, with low spatial resolution data that has continuous spectra. The ultimate goal is to estimate an image with high spatial and spectral content, providing a more comprehensive and accurate understanding of the area of interest. We replaced the noisy bands in the M3 and IIRS data and used cubic convolution to resample the M3 bands to the IIRS band’s native spatial resolution. However, the M3 bandwidth is different from the IIRS bandwidths. Nevertheless, this gap-filling procedure will allow us to identify endmembers. As a followup study we are going to employ a spectral unmixing technique to obtain endmembers information and high-resolution abundance matrices from the initial images. Data fusion helps overcome the limitations of individual datasets, exploit the strengths of different sensors, and extract more valuable information.

How to cite: Ivanov, I. and Filchev, L.: Fusion of IIRS and M3 data for the purpouse of finer resolution mineral mapping, EGU General Assembly 2024, Vienna, Austria, 14–19 Apr 2024, EGU24-292, https://doi.org/10.5194/egusphere-egu24-292, 2024.

X3.67
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EGU24-14455
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ECS
Xu Tang, Lixin Gu, Hengci Tian, Qiuli Li, and Jinhua Li

Sulfides are common minerals in lunar rocks and have great implications for lunar magma origin and subsequent evolution. Pentlandite as an important sulfide, usually coexisted with troilite, which could indicate the geological thermal history of lunar rocks. Previous researchers proposed three potential mechanisms to explain the origin of pentlandite in lunar soil: (i) the reaction between mobilized sulfur and metallic FeNi, ilmenite and an Fe-bearing silicate; (ii) it is formed by the reaction between migrating Ni and troilite; (iii) pentlandite may exsolve from the Ni-rich troilite during the cooling of rocks. Here, we used the scanning electron microscopy (SEM), X-Ray electron probe micro-analyzer (EPMA) and transmission electron microscopy (TEM) to decipher the formation mechanisms of pentlandite in Chang’e-5 (CE-5) lunar soils. Our results show that pentlandites occurred as lamella and veinlets in troilites from basalts and breccias, forming a troilite-pentlandite assemblage. Crystallographic data from TEM provide the first robust evidence that pentlandites from both basalts and breccias were exsolved from the host troilite during the magma cooling, rather than formed by the reaction between mobilized sulfur and metallic FeNi, or mobilized Ni with troilite. Furthermore, we found taenite was exsolved from pentlandite in lunar breccia, forming a troilite-pentlandite-taenite assemblage. Given exclusively exsolved taenite and higher Ni content in troilite in breccia than that in basalts, it suggests the origin of pentlandite in breccia may involve a geological process involving the addition of exotic meteorite materials. Finally, we established two atom shuffling models to describe the transformation mechanism from troilite to pentlandite, and pentlandite to taenite. This work provides new insights into the origin and geological evolution of lunar sulfides, and also provides new method for the study of mineral evolution in other extraterrestrial samples.

How to cite: Tang, X., Gu, L., Tian, H., Li, Q., and Li, J.: Origin of pentlandite in Chang’e-5 lunar soils revealed by transmission electron microscopy, EGU General Assembly 2024, Vienna, Austria, 14–19 Apr 2024, EGU24-14455, https://doi.org/10.5194/egusphere-egu24-14455, 2024.

X3.68
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EGU24-8305
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ECS
Anastasia Consorzi, Daniele Melini, Juan Luis Gonzáles-Santander, and Giorgio Spada

The Andrade rheological law ε(t)=ε0+βtα has been introduced by Andrade in 1910 for the description of elongation in metal wires. Since then, this model has gained increasing popularity in geophysics and planetary sciences, being extremely effective in the description of numerous materials, including polycrystalline ices, amorphous solids and silicate rocks. Recently, many works in the field of planetology have adopted this model for the description of the response of solar system or extra-solar planets to tidal perturbations, especially for bodies whose properties are still poorly constrained. This is because the Andrade rheology can describe transient deformation using a low number of parameters, a highly valued characteristic for the study of planetary bodies for which few observational constraints are available, such as exoplanets. For the Moon, the Andrade rheology provides an accurate description of the viscoelastic tidal deformation, satisfying the observed frequency dependence of the quality factor.

While for uniform bodies described by a steady-state Maxwell rheology the analytical form of the time-dependent Love numbers (LNs) was established long ago, in the case of the transient Andrade model no closed-form solutions have been determined so far. This is mainly due to the fact that the planetary response is normally studied in the Fourier-transformed frequency domain or by numerical methods in the time domain. Closed-form expressions could be important since they have the potential of providing insight into the dependence of LNs upon the model parameters and the viscoelastic relaxation time-scales of the planet.

In this work, we focus on the Andrade rheological law in 1-D and we obtain a previously unknown explicit expression, in the time domain, for the relaxation modulus in terms of the Mittag-Leffler function Eα,β(z), a higher transcendental function that generalises the exponential function. Second, we consider the general response of a uniform, incompressible planetary model - the “Kelvin sphere” - studying the Laplace-transformed, the frequency domain and the time-domain LNs by analytical methods. By exploiting the results obtained in the 1-D case, we establish closed-form expressions of the time domain LNs and we discuss the frequency-domain response of the Kelvin sphere with Andrade rheology analytically.

Our findings exhibit a complex relation between the planet parameters and the resulting deformation. From the analysis of the frequency-dependent LNs we show that dissipation in Earth-like planets is strongly dependent upon the choice of the planet density, rigidity and viscosity, while the variation of the Andrade creep parameter α has an effect that is limited to short-period tidal forcing. Concurrently, the study of the time dependent LNs shows that α regulates the duration of the transient phase, while the remaining parameters set the value of elastic limit, and the rate at which  the fluid limit is reached. Finally, some examples concerning the tidal deformations of the Moon are presented to point out the relevance that the Andrade rheology assumes in this particular case.

How to cite: Consorzi, A., Melini, D., Gonzáles-Santander, J. L., and Spada, G.: Love numbers for an Andrade planet, EGU General Assembly 2024, Vienna, Austria, 14–19 Apr 2024, EGU24-8305, https://doi.org/10.5194/egusphere-egu24-8305, 2024.

X3.69
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EGU24-1023
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ECS
Autonomous Navigation for a Lunar Satellite
(withdrawn)
Sui Chen and Francesco Topputo

Posters virtual: Mon, 15 Apr, 14:00–15:45 | vHall X3

Display time: Mon, 15 Apr, 08:30–Mon, 15 Apr, 18:00
vX3.5
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EGU24-142
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Jean Schneider

I look at what astronomy from the Moon might be like in the visible over the next few decades.
The Moon offers the possibility of installing large telescopes or interferometers with instruments larger than those on orbiting telescopes. I first present examples of ambitious science cases, in particular ideas that cannot be implemented from Earth. I discuss also the issues which I telescope will encounter underlunar conditions. After a general review of observational approaches, from photometry to high contrast and high angular resolution imaging, I propose as a first step a 1-metre-class precursor and explore what science can be done with it.

How to cite: Schneider, J.: Astronomy from the Moon: From Exoplanets to Cosmology in Visible Light, EGU General Assembly 2024, Vienna, Austria, 14–19 Apr 2024, EGU24-142, https://doi.org/10.5194/egusphere-egu24-142, 2024.