首页 > 最新文献

Icarus最新文献

英文 中文
Masses of binary asteroid systems with strong solar perturbations
IF 2.5 2区 物理与天体物理 Q2 ASTRONOMY & ASTROPHYSICS Pub Date : 2025-03-17 DOI: 10.1016/j.icarus.2025.116546
M.I. Varfolomeev , N.V. Emelyanov
We give refined values for the masses for the following binary asteroid systems with strong solar perturbations: (379) Huenna, (3548) Eurybates-Queta, (3749) Balam, (88611) Teharonhiawako-Sawiskera, (160256) 2002 PD149, (341520) Mors-Somnus, (364171) 2006 JZ81, (524531) 2002 XH91, 1998 WW31, and 2003 QY90. The masses were refined by numeric integration of the equations of motion where perturbations from the Sun’s gravity were taken into account. Assuming the satellite orbits to be close to Keplerian, the initial integration parameters and the masses of the systems can be refined by the least-squares method in which the coefficients of the conditional equations are calculated using the Keplerian motion formulae. For some systems with strong solar perturbations (2001 QW322, 2006 BR284, 2006 CH69, (525462) 2005 EO304, (612147) 2000 CF105, (612687) 2003 UN284) the masses could not be refined since the rms residuals increase when solar perturbations are taken into account, which can be caused by insufficient interval or amount of observations. For most systems, the obtained values for masses are within the error limits of the values obtained using only Keplerian model. However, for a number of satellites, the Keplerian model of motion, which does not take into account solar perturbations, gives significant deviations in the apparent positions exceeding the accuracy of modern observations. These systems are (379) Huenna, (3548) Eurybates-Queta, (3749) Balam, (160256) 2002 PD149, and (364171) 2006 JZ81. For the systems for which it was possible to refine the masses, we give elements of their satellites’ osculating orbits for the epoch close to the date of their first observation.
{"title":"Masses of binary asteroid systems with strong solar perturbations","authors":"M.I. Varfolomeev ,&nbsp;N.V. Emelyanov","doi":"10.1016/j.icarus.2025.116546","DOIUrl":"10.1016/j.icarus.2025.116546","url":null,"abstract":"<div><div>We give refined values for the masses for the following binary asteroid systems with strong solar perturbations: (379) Huenna, (3548) Eurybates-Queta, (3749) Balam, (88611) Teharonhiawako-Sawiskera, (160256) 2002 PD<sub>149</sub>, (341520) Mors-Somnus, (364171) 2006 JZ<sub>81</sub>, (524531) 2002 XH<sub>91</sub>, 1998 WW<sub>31</sub>, and 2003 QY<sub>90</sub>. The masses were refined by numeric integration of the equations of motion where perturbations from the Sun’s gravity were taken into account. Assuming the satellite orbits to be close to Keplerian, the initial integration parameters and the masses of the systems can be refined by the least-squares method in which the coefficients of the conditional equations are calculated using the Keplerian motion formulae. For some systems with strong solar perturbations (2001 QW<sub>322</sub>, 2006 BR<sub>284</sub>, 2006 CH<sub>69</sub>, (525462) 2005 EO<sub>304</sub>, (612147) 2000 CF<sub>105</sub>, (612687) 2003 UN<sub>284</sub>) the masses could not be refined since the rms residuals increase when solar perturbations are taken into account, which can be caused by insufficient interval or amount of observations. For most systems, the obtained values for masses are within the error limits of the values obtained using only Keplerian model. However, for a number of satellites, the Keplerian model of motion, which does not take into account solar perturbations, gives significant deviations in the apparent positions exceeding the accuracy of modern observations. These systems are (379) Huenna, (3548) Eurybates-Queta, (3749) Balam, (160256) 2002 PD<sub>149</sub>, and (364171) 2006 JZ<sub>81</sub>. For the systems for which it was possible to refine the masses, we give elements of their satellites’ osculating orbits for the epoch close to the date of their first observation.</div></div>","PeriodicalId":13199,"journal":{"name":"Icarus","volume":"434 ","pages":"Article 116546"},"PeriodicalIF":2.5,"publicationDate":"2025-03-17","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"143644815","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":2,"RegionCategory":"物理与天体物理","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
The impact of cometary outbursts on the orbits of comets in the Oort cloud
IF 2.5 2区 物理与天体物理 Q2 ASTRONOMY & ASTROPHYSICS Pub Date : 2025-03-11 DOI: 10.1016/j.icarus.2025.116547
A.Y. Merkulova, A.K. Pavlov, D.V. Belousov
The surface layers of cometary nuclei are intensively irradiated by high energy protons, α-particles and heavy ions of galactic cosmic ray (GCR), leading to the formation of ions and radicals in the comet's matter. At low temperatures, high concentrations of radicals accumulated in the ice can be followed by a rapid release of energy during spontaneous or induced recombination. This process can provoke a gas release from the comet's surface layers. The resulting gas flux leads to a change in the velocity of comets, which affects the stability of their orbits. Repeated outbursts can occur over the comet's lifetime in the Oort cloud. This mechanism depends on the comet's size, the initial eccentricity, and the ejected mass during the outburst. We modeled the impact of repeated cometary outbursts on the orbits of comets in the Oort cloud. The results indicate that 49.5 % of comets with radii Rc = 0.4 km and 72.4 % of comets with Rc = 0.3 km and initial eccentricities ec ≥ 0.9 could leave the Oort cloud due to repeated outbursts. This fraction leaving comets for the initial eccentricities ec > 0 is 19.3 % for Rc = 0.4 km and 54.1 % for Rc = 0.3 km, respectively. The mechanism has the most effect on highly elongated orbits of comets.
{"title":"The impact of cometary outbursts on the orbits of comets in the Oort cloud","authors":"A.Y. Merkulova,&nbsp;A.K. Pavlov,&nbsp;D.V. Belousov","doi":"10.1016/j.icarus.2025.116547","DOIUrl":"10.1016/j.icarus.2025.116547","url":null,"abstract":"<div><div>The surface layers of cometary nuclei are intensively irradiated by high energy protons, α-particles and heavy ions of galactic cosmic ray (GCR), leading to the formation of ions and radicals in the comet's matter. At low temperatures, high concentrations of radicals accumulated in the ice can be followed by a rapid release of energy during spontaneous or induced recombination. This process can provoke a gas release from the comet's surface layers. The resulting gas flux leads to a change in the velocity of comets, which affects the stability of their orbits. Repeated outbursts can occur over the comet's lifetime in the Oort cloud. This mechanism depends on the comet's size, the initial eccentricity, and the ejected mass during the outburst. We modeled the impact of repeated cometary outbursts on the orbits of comets in the Oort cloud. The results indicate that 49.5 % of comets with radii R<sub>c</sub> = 0.4 km and 72.4 % of comets with R<sub>c</sub> = 0.3 km and initial eccentricities e<sub>c</sub> ≥ 0.9 could leave the Oort cloud due to repeated outbursts. This fraction leaving comets for the initial eccentricities e<sub>c</sub> &gt; 0 is 19.3 % for R<sub>c</sub> = 0.4 km and 54.1 % for R<sub>c</sub> = 0.3 km, respectively. The mechanism has the most effect on highly elongated orbits of comets.</div></div>","PeriodicalId":13199,"journal":{"name":"Icarus","volume":"434 ","pages":"Article 116547"},"PeriodicalIF":2.5,"publicationDate":"2025-03-11","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"143620612","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":2,"RegionCategory":"物理与天体物理","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
Mars ionosphere TEC estimation from MARSIS data: A new approach
IF 2.5 2区 物理与天体物理 Q2 ASTRONOMY & ASTROPHYSICS Pub Date : 2025-03-11 DOI: 10.1016/j.icarus.2025.116545
M. Cartacci , B. Sánchez-Cano , A. Cicchetti , R. Noschese , B. Langlais , R. Orosei
We describe a new implementation of the Contrast Method (CM) algorithm (Picardi and Sorge, 2000; Ilyushin Ya and Kunitsyn, 2004; Cartacci et al., 2013) used to correct the phase distortion of the echoes recorded by the Mars Advanced Radar for Subsurface and Ionosphere Sounding (MARSIS) (Picardi et al., 2005; Jordan et al., 2009) in its subsurface mode.
The New CM is designed following an improved approach which allows not only to perform its original task but also to estimate the Total Electron Content (TEC) of the Mars ionosphere with a better accuracy respect to the past (Cartacci et al., 2013; Cartacci et al., 2017), in the nightside when the transmitted frequency is close to the ionosphere plasma frequency as well as in the dayside, thanks to a lesser use of theoretical approximations in the method development.
Moreover, taking advantage of almost 16 years of MARSIS operations, corresponding to about 8700 orbits, we present an improved global map of the night side TEC variations due to the interaction with the Mars crustal magnetic field (Safaeinili et al., 2007; Cartacci et al., 2013).
{"title":"Mars ionosphere TEC estimation from MARSIS data: A new approach","authors":"M. Cartacci ,&nbsp;B. Sánchez-Cano ,&nbsp;A. Cicchetti ,&nbsp;R. Noschese ,&nbsp;B. Langlais ,&nbsp;R. Orosei","doi":"10.1016/j.icarus.2025.116545","DOIUrl":"10.1016/j.icarus.2025.116545","url":null,"abstract":"<div><div>We describe a new implementation of the Contrast Method (CM) algorithm (<span><span>Picardi and Sorge, 2000</span></span>; <span><span>Ilyushin Ya and Kunitsyn, 2004</span></span>; <span><span>Cartacci et al., 2013</span></span>) used to correct the phase distortion of the echoes recorded by the Mars Advanced Radar for Subsurface and Ionosphere Sounding (MARSIS) (<span><span>Picardi et al., 2005</span></span>; <span><span>Jordan et al., 2009</span></span>) in its subsurface mode.</div><div>The New CM is designed following an improved approach which allows not only to perform its original task but also to estimate the Total Electron Content (TEC) of the Mars ionosphere with a better accuracy respect to the past (<span><span>Cartacci et al., 2013</span></span>; <span><span>Cartacci et al., 2017</span></span>), in the nightside when the transmitted frequency is close to the ionosphere plasma frequency as well as in the dayside, thanks to a lesser use of theoretical approximations in the method development.</div><div>Moreover, taking advantage of almost 16 years of MARSIS operations, corresponding to about 8700 orbits, we present an improved global map of the night side TEC variations due to the interaction with the Mars crustal magnetic field (<span><span>Safaeinili et al., 2007</span></span>; <span><span>Cartacci et al., 2013</span></span>).</div></div>","PeriodicalId":13199,"journal":{"name":"Icarus","volume":"434 ","pages":"Article 116545"},"PeriodicalIF":2.5,"publicationDate":"2025-03-11","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"143636296","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":2,"RegionCategory":"物理与天体物理","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
The effects of measured slope on Martian lava flow modeling
IF 2.5 2区 物理与天体物理 Q2 ASTRONOMY & ASTROPHYSICS Pub Date : 2025-03-07 DOI: 10.1016/j.icarus.2025.116544
Frances P. Russo , Ian T.W. Flynn , Sean I. Peters , Michael S. Ramsey
One of the most frequently used methods for modeling lava flows on Mars is commonly called the “standard rheologic approach” (SRA). This method requires measurements of the flow dimensions (e.g., width, length, thickness) and local topography (e.g., slope), which are used in equations of viscosity and yield strength, for example. Topography is a critical input for most lava flow models, a detailed analysis of how the input slope value affects the results using the SRA is needed. Here we present a topographic sensitivity analysis of SRA modeling, using the minimum, maximum, and one standard deviation of measured slope values. We investigated sixteen lava flows, fourteen south and two north of Arsia Mons, Mars. Depending on the input slope, a 5 % to 60 % change in viscosity, and a 5 % to 70 % change in yield strength was found. This viscosity range produced an inferred composition change from a basalt to an andesite for eight of the sixteen flows. We also tested a single flow using the SRA and derived slopes from MOLA, HRSC, and CTX digital elevation models (DEMs). The same compositional shift from a basalt to an andesite occurred with increasing DEM resolution. These results highlight the importance of testing the full range of possible slopes and using the highest resolution topographic dataset available to avoid inaccurate interpretation of flow composition. If only low to moderate DEM datasets are available, the results should be interpreted with caution.
{"title":"The effects of measured slope on Martian lava flow modeling","authors":"Frances P. Russo ,&nbsp;Ian T.W. Flynn ,&nbsp;Sean I. Peters ,&nbsp;Michael S. Ramsey","doi":"10.1016/j.icarus.2025.116544","DOIUrl":"10.1016/j.icarus.2025.116544","url":null,"abstract":"<div><div>One of the most frequently used methods for modeling lava flows on Mars is commonly called the “standard rheologic approach” (SRA). This method requires measurements of the flow dimensions (e.g., width, length, thickness) and local topography (e.g., slope), which are used in equations of viscosity and yield strength, for example. Topography is a critical input for most lava flow models, a detailed analysis of how the input slope value affects the results using the SRA is needed. Here we present a topographic sensitivity analysis of SRA modeling, using the minimum, maximum, and one standard deviation of measured slope values. We investigated sixteen lava flows, fourteen south and two north of Arsia Mons, Mars. Depending on the input slope, a 5 % to 60 % change in viscosity, and a 5 % to 70 % change in yield strength was found. This viscosity range produced an inferred composition change from a basalt to an andesite for eight of the sixteen flows. We also tested a single flow using the SRA and derived slopes from MOLA, HRSC, and CTX digital elevation models (DEMs). The same compositional shift from a basalt to an andesite occurred with increasing DEM resolution. These results highlight the importance of testing the full range of possible slopes and using the highest resolution topographic dataset available to avoid inaccurate interpretation of flow composition. If only low to moderate DEM datasets are available, the results should be interpreted with caution.</div></div>","PeriodicalId":13199,"journal":{"name":"Icarus","volume":"434 ","pages":"Article 116544"},"PeriodicalIF":2.5,"publicationDate":"2025-03-07","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"143644946","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":2,"RegionCategory":"物理与天体物理","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"OA","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
The mineralogical composition of Jezero Crater Western Fan: Multigaussian modeling of Perseverance/SuperCam near-infrared observations and overview of major units
IF 2.5 2区 物理与天体物理 Q2 ASTRONOMY & ASTROPHYSICS Pub Date : 2025-03-07 DOI: 10.1016/j.icarus.2025.116538
C. Royer , F. Poulet , R.C. Wiens , F. Montmessin , P. Beck , O. Beyssac , É. Clavé , E. Dehouck , T. Fouchet , J.R. Johnson , L. Mandon , S. Bernard , G. Caravaca , S. le Mouélic , C. Pilorget , C. Quantin-Nataf , S. Maurice , A. Cousin
The analysis of the mineralogical composition of rocks within the Jezero crater, Mars, enables the reconstruction of the aqueous activity history of the site, formed during the planet’s early epochs. Numerous secondary minerals resulting from aqueous alteration, as well as some primary minerals, are observable through near-infrared reflectance spectroscopy, as performed by the IRS/SuperCam instrument onboard the Perseverance rover. The characterization of these minerals, their distribution within geological units, as well as the composition of their assemblages, is crucial for deciphering the chemical, climatic, and geological history of the Jezero crater. In order to systematically study the growing number of IR spectra collected by the instrument, we have developed an automated method for extracting the characteristics of absorption bands, based on their modeling using a combination of Gaussian curves (MultiGM). The application of this method to the entire IRS dataset reveals a significant diversity of minerals distributed throughout the rover traverse, with a near-systematic presence of phyllosilicates in bedrocks, as well as increasingly frequent occurrences of carbonates on the delta, particularly within the Margin unit. These carbonates exhibit variable 2.5 μm band positions attributed to different Fe and Mg compositions. The delta front presents the sole unit generally enriched in Fe/Mg sulfates (Yori Pass/Hogwallow Flats) accompanied by occurrences of bassanite (hydrated CaSO4), whereas the presence of sulfates in other delta units and the crater floor is more sporadic and corresponds to fracture/vesicle fills. Finally, almost all the rocks analyzed with IRS/SuperCam are notably dominated by phyllosilicates signatures (Fe/Mg-smectites, serpentine), excepted for a few outcrops caping the Delta. This phyllosilicate presence witnesses the extended surficial (smectites) and hydrothermal (serpentine) aqueous alteration of Jezero’s rocks, either in situ or carried from the watershed.
{"title":"The mineralogical composition of Jezero Crater Western Fan: Multigaussian modeling of Perseverance/SuperCam near-infrared observations and overview of major units","authors":"C. Royer ,&nbsp;F. Poulet ,&nbsp;R.C. Wiens ,&nbsp;F. Montmessin ,&nbsp;P. Beck ,&nbsp;O. Beyssac ,&nbsp;É. Clavé ,&nbsp;E. Dehouck ,&nbsp;T. Fouchet ,&nbsp;J.R. Johnson ,&nbsp;L. Mandon ,&nbsp;S. Bernard ,&nbsp;G. Caravaca ,&nbsp;S. le Mouélic ,&nbsp;C. Pilorget ,&nbsp;C. Quantin-Nataf ,&nbsp;S. Maurice ,&nbsp;A. Cousin","doi":"10.1016/j.icarus.2025.116538","DOIUrl":"10.1016/j.icarus.2025.116538","url":null,"abstract":"<div><div>The analysis of the mineralogical composition of rocks within the Jezero crater, Mars, enables the reconstruction of the aqueous activity history of the site, formed during the planet’s early epochs. Numerous secondary minerals resulting from aqueous alteration, as well as some primary minerals, are observable through near-infrared reflectance spectroscopy, as performed by the IRS/SuperCam instrument onboard the <em>Perseverance</em> rover. The characterization of these minerals, their distribution within geological units, as well as the composition of their assemblages, is crucial for deciphering the chemical, climatic, and geological history of the Jezero crater. In order to systematically study the growing number of IR spectra collected by the instrument, we have developed an automated method for extracting the characteristics of absorption bands, based on their modeling using a combination of Gaussian curves (MultiGM). The application of this method to the entire IRS dataset reveals a significant diversity of minerals distributed throughout the rover traverse, with a near-systematic presence of phyllosilicates in bedrocks, as well as increasingly frequent occurrences of carbonates on the delta, particularly within the Margin unit. These carbonates exhibit variable 2.5 <span><math><mi>μ</mi></math></span>m band positions attributed to different Fe and Mg compositions. The delta front presents the sole unit generally enriched in Fe/Mg sulfates (Yori Pass/Hogwallow Flats) accompanied by occurrences of bassanite (hydrated CaSO<sub>4</sub>), whereas the presence of sulfates in other delta units and the crater floor is more sporadic and corresponds to fracture/vesicle fills. Finally, almost all the rocks analyzed with IRS/SuperCam are notably dominated by phyllosilicates signatures (Fe/Mg-smectites, serpentine), excepted for a few outcrops caping the Delta. This phyllosilicate presence witnesses the extended surficial (smectites) and hydrothermal (serpentine) aqueous alteration of Jezero’s rocks, either <em>in situ</em> or carried from the watershed.</div></div>","PeriodicalId":13199,"journal":{"name":"Icarus","volume":"434 ","pages":"Article 116538"},"PeriodicalIF":2.5,"publicationDate":"2025-03-07","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"143601006","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":2,"RegionCategory":"物理与天体物理","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
Stress analysis of asteroids during atmospheric entry and implications for the breakup criterion
IF 2.5 2区 物理与天体物理 Q2 ASTRONOMY & ASTROPHYSICS Pub Date : 2025-03-07 DOI: 10.1016/j.icarus.2025.116526
Théo A. Rulko , Aaditya Rau , Grégoire Chomette , Lorien Wheeler , Donovan Mathias , Jessie Dotson , Raúl Radovitzky
Observations of asteroid fragmentation upon atmospheric entry have been used as a basis to estimate asteroid mechanical strength by the simplifying assumption that strength corresponds to ram pressure at burst. However, it is unclear whether ram pressure is a good scalar measure of the stresses that induce fracture. In this work, we study the stress fields prior to break-up in idealized as well as representative irregular asteroids as they enter the atmosphere. We develop a model for elastic, homogeneous, monolithic asteroids subject to aerodynamic, inertial, and centrifugal loads applied via the Meteor Equations and modified Newtonian aerodynamic theory. We obtain an analytical solution to the elasticity boundary value problem for an idealized circular asteroid. Alongside it, detailed finite element solutions are used to both verify the analytical model and to quantify the effects of asteroid shape irregularity on the state of stress. We find that the stresses that drive brittle fracture in asteroids may be an order of magnitude lower than the ram pressure, which could have significant implications for strengths inferred from breakup observations. We also quantify the effect of the spin of the asteroid as it tumbles through the atmosphere and the regimes in which spin-induced stresses dominate. Finally, we find that asteroids with small shape variations are well-approximated as spheres, but that large shape irregularities, like at the necks of elongated or contact binary asteroids, may lead to the appearance of regions of tensile bending stress. Conclusions are drawn about the usefulness of the ram pressure alone as a measure of stress in asteroids.
{"title":"Stress analysis of asteroids during atmospheric entry and implications for the breakup criterion","authors":"Théo A. Rulko ,&nbsp;Aaditya Rau ,&nbsp;Grégoire Chomette ,&nbsp;Lorien Wheeler ,&nbsp;Donovan Mathias ,&nbsp;Jessie Dotson ,&nbsp;Raúl Radovitzky","doi":"10.1016/j.icarus.2025.116526","DOIUrl":"10.1016/j.icarus.2025.116526","url":null,"abstract":"<div><div>Observations of asteroid fragmentation upon atmospheric entry have been used as a basis to estimate asteroid mechanical strength by the simplifying assumption that strength corresponds to ram pressure at burst. However, it is unclear whether ram pressure is a good scalar measure of the stresses that induce fracture. In this work, we study the stress fields prior to break-up in idealized as well as representative irregular asteroids as they enter the atmosphere. We develop a model for elastic, homogeneous, monolithic asteroids subject to aerodynamic, inertial, and centrifugal loads applied via the Meteor Equations and modified Newtonian aerodynamic theory. We obtain an analytical solution to the elasticity boundary value problem for an idealized circular asteroid. Alongside it, detailed finite element solutions are used to both verify the analytical model and to quantify the effects of asteroid shape irregularity on the state of stress. We find that the stresses that drive brittle fracture in asteroids may be an order of magnitude lower than the ram pressure, which could have significant implications for strengths inferred from breakup observations. We also quantify the effect of the spin of the asteroid as it tumbles through the atmosphere and the regimes in which spin-induced stresses dominate. Finally, we find that asteroids with small shape variations are well-approximated as spheres, but that large shape irregularities, like at the necks of elongated or contact binary asteroids, may lead to the appearance of regions of tensile bending stress. Conclusions are drawn about the usefulness of the ram pressure alone as a measure of stress in asteroids.</div></div>","PeriodicalId":13199,"journal":{"name":"Icarus","volume":"434 ","pages":"Article 116526"},"PeriodicalIF":2.5,"publicationDate":"2025-03-07","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"143593525","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":2,"RegionCategory":"物理与天体物理","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
Measurement of the three-dimensional shape and size distribution of 17 lunar regolith simulants: Simulant shape and size inter-comparison and simulant shape comparison with Apollo 11 and Apollo 14 lunar regolith
IF 2.5 2区 物理与天体物理 Q2 ASTRONOMY & ASTROPHYSICS Pub Date : 2025-03-05 DOI: 10.1016/j.icarus.2025.116542
O.L. Kafka , N.H. Moser , A.N. Chiaramonti , E.J. Garboczi , R.P. Wilkerson , D.L. Rickman
Lunar regolith simulants are manufactured in order to provide a higher volume, much less expensive and more available source of material, compared to real lunar regolith material, with which to test various instruments and machines designed to operate on the lunar surface. The particle size distribution and mineralogy of these materials is engineered but not the particle shape, although particle shape does play an important role in many engineering applications. Thus, the three-dimensional (3D) shape of these materials has rarely been characterized and never compared to each other and to real lunar regolith material. The focus of this paper is to provide 3D shape and size distribution of 17 different simulants, use this data to compare these materials against each other and provide these data in a NIST database. Over 1.1 M particles are in this database, with their 3D shape stored as STL files. The particle size range considered is roughly 7 μm to 1 mm. With the recent publication of 3D characterizations of lunar regolith material from the Apollo 11 and Apollo 14 missions, these characterizations are also compared to equivalent data for the real lunar regolith material. Both mare and highland simulants are studied using graphical comparisons as well as size and shape figure of merit analysis. This kind of 3D characterization provides the information that new engineering manufacturing techniques will need to enable the engineering of particle shape for new lunar regolith simulants, since the ability to make particle shape measurements relevant to manufacturing and use is a prerequisite for any such engineering. This database can also serve as a source of “digital twins” or “virtual simulants” for modeling studies both of individual particle properties and of packed particle geometry and properties.
{"title":"Measurement of the three-dimensional shape and size distribution of 17 lunar regolith simulants: Simulant shape and size inter-comparison and simulant shape comparison with Apollo 11 and Apollo 14 lunar regolith","authors":"O.L. Kafka ,&nbsp;N.H. Moser ,&nbsp;A.N. Chiaramonti ,&nbsp;E.J. Garboczi ,&nbsp;R.P. Wilkerson ,&nbsp;D.L. Rickman","doi":"10.1016/j.icarus.2025.116542","DOIUrl":"10.1016/j.icarus.2025.116542","url":null,"abstract":"<div><div>Lunar regolith simulants are manufactured in order to provide a higher volume, much less expensive and more available source of material, compared to real lunar regolith material, with which to test various instruments and machines designed to operate on the lunar surface. The particle size distribution and mineralogy of these materials is engineered but not the particle shape, although particle shape does play an important role in many engineering applications. Thus, the three-dimensional (3D) shape of these materials has rarely been characterized and never compared to each other and to real lunar regolith material. The focus of this paper is to provide 3D shape and size distribution of 17 different simulants, use this data to compare these materials against each other and provide these data in a NIST database. Over 1.1 M particles are in this database, with their 3D shape stored as STL files. The particle size range considered is roughly 7 μm to 1 mm. With the recent publication of 3D characterizations of lunar regolith material from the Apollo 11 and Apollo 14 missions, these characterizations are also compared to equivalent data for the real lunar regolith material. Both mare and highland simulants are studied using graphical comparisons as well as size and shape figure of merit analysis. This kind of 3D characterization provides the information that new engineering manufacturing techniques will need to enable the engineering of particle shape for new lunar regolith simulants, since the ability to make particle shape measurements relevant to manufacturing and use is a prerequisite for any such engineering. This database can also serve as a source of “digital twins” or “virtual simulants” for modeling studies both of individual particle properties and of packed particle geometry and properties.</div></div>","PeriodicalId":13199,"journal":{"name":"Icarus","volume":"434 ","pages":"Article 116542"},"PeriodicalIF":2.5,"publicationDate":"2025-03-05","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"143629610","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":2,"RegionCategory":"物理与天体物理","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
Degasing of Phobos in a giant impact scenario: Implications for the MMX sample return mission
IF 2.5 2区 物理与天体物理 Q2 ASTRONOMY & ASTROPHYSICS Pub Date : 2025-03-05 DOI: 10.1016/j.icarus.2025.116462
Sébastien Charnoz, Angela Limare, Eva De Araujo Pereira, Razvan Caracas, Frédéric Moynier
The MMX mission, led by JAXA, is a sample return mission whose primary goal is to test whether the Martian moons, Phobos and Deimos, were formed during a giant impact or were captured. One of the main observations to test these scenarios will be whether Phobos and Deimos have lost volatile elements. If Phobos formed in a giant impact, simulations show that the impact was much less energetic than the Moon-forming impact, with peak temperatures as low as 2000 K. We present here a quantification of the volatile loss in anticipation of the MMX mission, assuming that Phobos’ building blocks were made of bulk silicate Mars material. We investigate the cooling of Phobos in two end-member scenarios : a convective case (relevant for an initially fully molten proto-Phobos) and a conductive case (relevant for an assemblage of 10 m building blocks). A homogeneous evaporation model is used for the convective case, and a diffusion-limited evaporation model is used for the conductive case. In both cases, we find that the cooling time is about 1–10 years in the absence of external heating sources (but the Sun). This leaves little time for evaporation: the most volatile elements, Na and K, may be depleted by 10% for the case of a fully molten and convective proto-Phobos. If Phobos is rather an assemblage of 10 m building blocks that cool conductively, the loss of Na and K would be limited to the first 10 cm below the blocks’ surface (by about 4%) representing about 0.1% loss in averaged bulk composition.
If external sources of heating were present (such as a hot radiating Mars or a hot surrounding disk), and the body was kept at T > 1400K (our assumed rheological transition temperature) for more than 10 years, a larger loss of Na and K is found. If degassing lasted more than 100 years with exterior temperature > 1400K, then all Na and K may have been lost for the convective case, and more than 50% for the conductive case. Furthermore, a significant fraction of the refractory elements may also have been lost in both cases. K abundance will be measured from space by the MEGANE instrument onboard the MMX mission. If low K content is measured by the MEGANE instrument, this would favor the giant impact formation scenario and would imply either a long cooling time of the proto-Phobos (100 years), or degassing prior to the assembling of the proto-Phobos. If MEGANE does not measure K depletion, this could mean either that Phobos was not formed in a giant impact, or that it formed in a giant impact but experienced a short cooling time (<10 years). In that case, laboratory analysis of the returned sample will be crucial in deciphering the origin of Phobos by focusing on various volatile elements and constraining their isotopic ratios.
{"title":"Degasing of Phobos in a giant impact scenario: Implications for the MMX sample return mission","authors":"Sébastien Charnoz,&nbsp;Angela Limare,&nbsp;Eva De Araujo Pereira,&nbsp;Razvan Caracas,&nbsp;Frédéric Moynier","doi":"10.1016/j.icarus.2025.116462","DOIUrl":"10.1016/j.icarus.2025.116462","url":null,"abstract":"<div><div>The MMX mission, led by JAXA, is a sample return mission whose primary goal is to test whether the Martian moons, Phobos and Deimos, were formed during a giant impact or were captured. One of the main observations to test these scenarios will be whether Phobos and Deimos have lost volatile elements. If Phobos formed in a giant impact, simulations show that the impact was much less energetic than the Moon-forming impact, with peak temperatures as low as 2000 K. We present here a quantification of the volatile loss in anticipation of the MMX mission, assuming that Phobos’ building blocks were made of bulk silicate Mars material. We investigate the cooling of Phobos in two end-member scenarios : a convective case (relevant for an initially fully molten proto-Phobos) and a conductive case (relevant for an assemblage of 10 m building blocks). A homogeneous evaporation model is used for the convective case, and a diffusion-limited evaporation model is used for the conductive case. In both cases, we find that the cooling time is about 1–10 years in the absence of external heating sources (but the Sun). This leaves little time for evaporation: the most volatile elements, Na and K, may be depleted by 10% for the case of a fully molten and convective proto-Phobos. If Phobos is rather an assemblage of 10 m building blocks that cool conductively, the loss of Na and K would be limited to the first 10 cm below the blocks’ surface (by about 4%) representing about 0.1% loss in averaged bulk composition.</div><div>If external sources of heating were present (such as a hot radiating Mars or a hot surrounding disk), and the body was kept at T <span><math><mo>&gt;</mo></math></span> 1400K (our assumed rheological transition temperature) for more than 10 years, a larger loss of Na and K is found. If degassing lasted more than 100 years with exterior temperature <span><math><mo>&gt;</mo></math></span> 1400K, then all Na and K may have been lost for the convective case, and more than 50% for the conductive case. Furthermore, a significant fraction of the refractory elements may also have been lost in both cases. K abundance will be measured from space by the MEGANE instrument onboard the MMX mission. If low K content is measured by the MEGANE instrument, this would favor the giant impact formation scenario and would imply either a long cooling time of the proto-Phobos (<span><math><mo>≥</mo></math></span>100 years), or degassing prior to the assembling of the proto-Phobos. If MEGANE does not measure K depletion, this could mean either that Phobos was not formed in a giant impact, or that it formed in a giant impact but experienced a short cooling time (<span><math><mo>&lt;</mo></math></span>10 years). In that case, laboratory analysis of the returned sample will be crucial in deciphering the origin of Phobos by focusing on various volatile elements and constraining their isotopic ratios.</div></div>","PeriodicalId":13199,"journal":{"name":"Icarus","volume":"434 ","pages":"Article 116462"},"PeriodicalIF":2.5,"publicationDate":"2025-03-05","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"143601005","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":2,"RegionCategory":"物理与天体物理","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
A 3D thermophysical model for binary asteroid systems: Application to the BYORP effect on (175706) 1996 FG3
IF 2.5 2区 物理与天体物理 Q2 ASTRONOMY & ASTROPHYSICS Pub Date : 2025-03-01 DOI: 10.1016/j.icarus.2025.116527
Kya C. Sorli , Paul O. Hayne , Rachel H. Cueva , Chloe J. Long , Jay W. McMahon , Daniel J. Scheeres
Binary asteroids originate from a wide range of evolutionary pathways, and are the targets of several previous and upcoming spacecraft missions. Differential heating and radiation on asymmetric asteroids can cause measurable changes in their rotation rates and spin axes, collectively known as the Yarkovsky–O’Keefe–Radzievskii–Paddack (YORP) effect. In binary systems, such radiation-driven torques can cause changes to the mutual asteroid orbits, termed the binary YORP or BYORP effect. To study how binary asteroid shapes and thermophysical properties affect surface temperatures and BYORP, we developed a new 3D thermophysical model. This model can be applied to binary asteroid systems, solitary asteroids, and other airless bodies with complex topography. The model balances direct insolation, 1D conduction, visible light reflection, and mutual heating through scattered infrared radiation. Using 3D ray tracing, we include eclipses, shadowing from horizons and topography, as well as the mutual radiation exchange between the primary and secondary asteroids. Using this model, we perform global temperature modeling of the binary asteroid (175706) 1996 FG3, a target of the Janus mission. At perihelion, we find that the 1996 FG3 system experiences temperatures between 100 and 475 K. We also find that eclipses and thermal inertia can alter surface temperatures on the secondary by up to 14%, with a mean difference due to radiation from the primary of just over 1%. These radiative effects decrease with higher thermal inertia. We also present a model for calculating the BYORP effect using the results of the binary thermophysical model. This model compares well to analytical approximations of the BYORP coefficient B, and suggests that thermal effects such as eclipses and thermal inertia can reduce torque in the 1996 FG3 system and alter the BYORP coefficient B by up to several percent. Though small, these second-order effects may produce significant dynamical changes. For 1996 FG3, eclipses alter B by approximately 7%, resulting in a lower torque on the secondary. In the absence of tidal effects, this change would reduce the contraction of the semimajor axis by about 20 meters over 10,000 years. Mutual radiation from the primary also causes a small nonzero change to B, although of an order of magnitude smaller. Our findings suggest that thermal effects can alter temperatures and BYORP calculations sufficiently that they should be included when modeling binaries, and the relative importance of each effect is predicted to vary with the properties of the system being studied.
{"title":"A 3D thermophysical model for binary asteroid systems: Application to the BYORP effect on (175706) 1996 FG3","authors":"Kya C. Sorli ,&nbsp;Paul O. Hayne ,&nbsp;Rachel H. Cueva ,&nbsp;Chloe J. Long ,&nbsp;Jay W. McMahon ,&nbsp;Daniel J. Scheeres","doi":"10.1016/j.icarus.2025.116527","DOIUrl":"10.1016/j.icarus.2025.116527","url":null,"abstract":"<div><div>Binary asteroids originate from a wide range of evolutionary pathways, and are the targets of several previous and upcoming spacecraft missions. Differential heating and radiation on asymmetric asteroids can cause measurable changes in their rotation rates and spin axes, collectively known as the Yarkovsky–O’Keefe–Radzievskii–Paddack (YORP) effect. In binary systems, such radiation-driven torques can cause changes to the mutual asteroid orbits, termed the binary YORP or BYORP effect. To study how binary asteroid shapes and thermophysical properties affect surface temperatures and BYORP, we developed a new 3D thermophysical model. This model can be applied to binary asteroid systems, solitary asteroids, and other airless bodies with complex topography. The model balances direct insolation, 1D conduction, visible light reflection, and mutual heating through scattered infrared radiation. Using 3D ray tracing, we include eclipses, shadowing from horizons and topography, as well as the mutual radiation exchange between the primary and secondary asteroids. Using this model, we perform global temperature modeling of the binary asteroid (175706) 1996 FG3, a target of the Janus mission. At perihelion, we find that the 1996 FG3 system experiences temperatures between <span><math><mo>∼</mo></math></span>100 and 475 K. We also find that eclipses and thermal inertia can alter surface temperatures on the secondary by up to 14%, with a mean difference due to radiation from the primary of just over 1%. These radiative effects decrease with higher thermal inertia. We also present a model for calculating the BYORP effect using the results of the binary thermophysical model. This model compares well to analytical approximations of the BYORP coefficient <span><math><mi>B</mi></math></span>, and suggests that thermal effects such as eclipses and thermal inertia can reduce torque in the 1996 FG3 system and alter the BYORP coefficient <span><math><mi>B</mi></math></span> by up to several percent. Though small, these second-order effects may produce significant dynamical changes. For 1996 FG3, eclipses alter <span><math><mi>B</mi></math></span> by approximately 7%, resulting in a lower torque on the secondary. In the absence of tidal effects, this change would reduce the contraction of the semimajor axis by about 20 meters over 10,000 years. Mutual radiation from the primary also causes a small nonzero change to <span><math><mi>B</mi></math></span>, although of an order of magnitude smaller. Our findings suggest that thermal effects can alter temperatures and BYORP calculations sufficiently that they should be included when modeling binaries, and the relative importance of each effect is predicted to vary with the properties of the system being studied.</div></div>","PeriodicalId":13199,"journal":{"name":"Icarus","volume":"434 ","pages":"Article 116527"},"PeriodicalIF":2.5,"publicationDate":"2025-03-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"143578091","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":2,"RegionCategory":"物理与天体物理","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"OA","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
Disintegration and separation of the bilobate-shaped meteoric fragment during hypersonic atmospheric entry
IF 2.5 2区 物理与天体物理 Q2 ASTRONOMY & ASTROPHYSICS Pub Date : 2025-02-27 DOI: 10.1016/j.icarus.2025.116537
Ziwen Li , Yong Yu , Xiangyuan Zeng , Haoyu Li , Tongge Wen , Xiaoran Yan
A novel method for simulating the disintegration of bilobate-shaped meteoric fragments is presented, which integrates aerodynamic interactions, rotational dynamics, structural strength, and ablation into the analysis. A disintegration criterion is proposed in this method, based on a comparison between the mechanism strength of the sintered bond and the required contact force to maintain the integrity of the bilobate shape. The disintegration of fragment 109 from the Morávka meteoroid, which deviates from the Weibull-like scaling law, is explained physically by applying this approach. Predictive numerical simulations are conducted by varying the initial attitudes, geometries, strengths, and angular velocities of the bilobate-shaped fragments. During atmospheric entry, variations in attitude, landing positions, and residual masses are analyzed as indicators of characteristics in the dynamical evolution.
{"title":"Disintegration and separation of the bilobate-shaped meteoric fragment during hypersonic atmospheric entry","authors":"Ziwen Li ,&nbsp;Yong Yu ,&nbsp;Xiangyuan Zeng ,&nbsp;Haoyu Li ,&nbsp;Tongge Wen ,&nbsp;Xiaoran Yan","doi":"10.1016/j.icarus.2025.116537","DOIUrl":"10.1016/j.icarus.2025.116537","url":null,"abstract":"<div><div>A novel method for simulating the disintegration of bilobate-shaped meteoric fragments is presented, which integrates aerodynamic interactions, rotational dynamics, structural strength, and ablation into the analysis. A disintegration criterion is proposed in this method, based on a comparison between the mechanism strength of the sintered bond and the required contact force to maintain the integrity of the bilobate shape. The disintegration of fragment 109 from the Morávka meteoroid, which deviates from the Weibull-like scaling law, is explained physically by applying this approach. Predictive numerical simulations are conducted by varying the initial attitudes, geometries, strengths, and angular velocities of the bilobate-shaped fragments. During atmospheric entry, variations in attitude, landing positions, and residual masses are analyzed as indicators of characteristics in the dynamical evolution.</div></div>","PeriodicalId":13199,"journal":{"name":"Icarus","volume":"433 ","pages":"Article 116537"},"PeriodicalIF":2.5,"publicationDate":"2025-02-27","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"143578558","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":2,"RegionCategory":"物理与天体物理","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
期刊
Icarus
全部 Acc. Chem. Res. ACS Applied Bio Materials ACS Appl. Electron. Mater. ACS Appl. Energy Mater. ACS Appl. Mater. Interfaces ACS Appl. Nano Mater. ACS Appl. Polym. Mater. ACS BIOMATER-SCI ENG ACS Catal. ACS Cent. Sci. ACS Chem. Biol. ACS Chemical Health & Safety ACS Chem. Neurosci. ACS Comb. Sci. ACS Earth Space Chem. ACS Energy Lett. ACS Infect. Dis. ACS Macro Lett. ACS Mater. Lett. ACS Med. Chem. Lett. ACS Nano ACS Omega ACS Photonics ACS Sens. ACS Sustainable Chem. Eng. ACS Synth. Biol. Anal. Chem. BIOCHEMISTRY-US Bioconjugate Chem. BIOMACROMOLECULES Chem. Res. Toxicol. Chem. Rev. Chem. Mater. CRYST GROWTH DES ENERG FUEL Environ. Sci. Technol. Environ. Sci. Technol. Lett. Eur. J. Inorg. Chem. IND ENG CHEM RES Inorg. Chem. J. Agric. Food. Chem. J. Chem. Eng. Data J. Chem. Educ. J. Chem. Inf. Model. J. Chem. Theory Comput. J. Med. Chem. J. Nat. Prod. J PROTEOME RES J. Am. Chem. Soc. LANGMUIR MACROMOLECULES Mol. Pharmaceutics Nano Lett. Org. Lett. ORG PROCESS RES DEV ORGANOMETALLICS J. Org. Chem. J. Phys. Chem. J. Phys. Chem. A J. Phys. Chem. B J. Phys. Chem. C J. Phys. Chem. Lett. Analyst Anal. Methods Biomater. Sci. Catal. Sci. Technol. Chem. Commun. Chem. Soc. Rev. CHEM EDUC RES PRACT CRYSTENGCOMM Dalton Trans. Energy Environ. Sci. ENVIRON SCI-NANO ENVIRON SCI-PROC IMP ENVIRON SCI-WAT RES Faraday Discuss. Food Funct. Green Chem. Inorg. Chem. Front. Integr. Biol. J. Anal. At. Spectrom. J. Mater. Chem. A J. Mater. Chem. B J. Mater. Chem. C Lab Chip Mater. Chem. Front. Mater. Horiz. MEDCHEMCOMM Metallomics Mol. Biosyst. Mol. Syst. Des. Eng. Nanoscale Nanoscale Horiz. Nat. Prod. Rep. New J. Chem. Org. Biomol. Chem. Org. Chem. Front. PHOTOCH PHOTOBIO SCI PCCP Polym. Chem.
×
引用
GB/T 7714-2015
复制
MLA
复制
APA
复制
导出至
BibTeX EndNote RefMan NoteFirst NoteExpress
×
0
微信
客服QQ
Book学术公众号 扫码关注我们
反馈
×
意见反馈
请填写您的意见或建议
请填写您的手机或邮箱
×
提示
您的信息不完整,为了账户安全,请先补充。
现在去补充
×
提示
您因"违规操作"
具体请查看互助需知
我知道了
×
提示
现在去查看 取消
×
提示
确定
Book学术官方微信
Book学术文献互助
Book学术文献互助群
群 号:481959085
Book学术
文献互助 智能选刊 最新文献 互助须知 联系我们:info@booksci.cn
Book学术提供免费学术资源搜索服务,方便国内外学者检索中英文文献。致力于提供最便捷和优质的服务体验。
Copyright © 2023 Book学术 All rights reserved.
ghs 京公网安备 11010802042870号 京ICP备2023020795号-1