PS2.1 | Exploring the Mysteries of Jupiter’s Icy Moons and their Space Environment
Exploring the Mysteries of Jupiter’s Icy Moons and their Space Environment
Convener: Haje Korth | Co-conveners: Emma Bunce, Bonnie Buratti, Umberto De Filippis, Anezina Solomonidou, Claire Vallat
Orals
| Wed, 17 Apr, 14:00–15:45 (CEST)
 
Room L1, Thu, 18 Apr, 10:45–12:25 (CEST)
 
Room L1
Posters on site
| Attendance Thu, 18 Apr, 16:15–18:00 (CEST) | Display Thu, 18 Apr, 14:00–18:00
 
Hall X3
Orals |
Wed, 14:00
Thu, 16:15
The arrival of the Europa Clipper and Jupiter Icy Moons Explorer (JUICE) spacecraft at Jupiter in the early 2030s will represent a watershed moment in the field of planetary science by providing, for the first time, simultaneous long-term observations in the Jovian system by two spacecraft. These missions are poised to provide unprecedented insights into the complex, enigmatic, and potentially habitable icy moons of the Jupiter system. This conference session aims to bring together scientists to discuss the latest advancements in our understanding of the Jupiter system and the implications for habitability, geology, and planetary science. It will feature updates and highlights from the Juice and Europa Clipper missions, including mission objectives, instrumentation, and recent developments. In addition, we will delve into the geology of Jupiter’s icy moons, with a particular focus on Europa and Ganymede; explore the characterization, chemical composition, thermal dynamics, and potential habitability of their subsurface oceans; and investigate the evidence for cryovolcanic activity, its implications for surface processes, and its role in shaping these worlds. We further extend the discussion to the complex interaction of the moons with Jupiter’s magnetic environment and the effects of radiation on their surfaces. The Europa Clipper and Juice missions offer a unique opportunity to unlock the secrets of the Jupiter system and its icy moons through individual and joint science investigations. We invite contributions on these topics from scientists at all career stages and backgrounds with the aim to foster collaboration, share knowledge, and inspire further research in this exciting and rapidly evolving field of planetary science.

Orals: Wed, 17 Apr | Room L1

Chairpersons: Haje Korth, Umberto De Filippis, Anezina Solomonidou
14:00–14:05
14:05–14:15
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EGU24-20679
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On-site presentation
Nicolas Altobelli, Olivier Witasse, Claire Vallat, Ignacio Tanco, Angela Dietz, and Christian Erd and the JUICE TEAMS

The JUICE mission has been launched by an Ariane 5 launcher on April 14, 2023 and is now on its way to reach Jupiter and its icy moons in 2031. The focus of JUICE is to characterise the conditions that may have led to the emergence of habitable environments among the Jovian icy satellites, with special emphasis on the internally active ocean-bearing worlds, Ganymede and Europa. Following a Jupiter Touring phase of 4 years, JUICE will become the first orbiter of a moon that is not our own, entering Ganymede orbit in 2034.

The spacecraft passed its commissioning review successfully on July 19, 2023, following the Near Earth Commissioning Phase (NECP), and, despite a few hickups, the ESA and multi-national instruments teams are now operating our interplanetary ship successfully. The preparation of the first combined flyby of the Earth and the Moon  in the history of space exploration (August 2024) is on-going. The first planning training exercise was completed by the Science Ground Segment, complementing the preparation of the strategic science planning of the Jupiter Tour.

How to cite: Altobelli, N., Witasse, O., Vallat, C., Tanco, I., Dietz, A., and Erd, C. and the JUICE TEAMS: The JUICE mission - an overview, since launch and beyond , EGU General Assembly 2024, Vienna, Austria, 14–19 Apr 2024, EGU24-20679, https://doi.org/10.5194/egusphere-egu24-20679, 2024.

14:15–14:25
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EGU24-14097
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On-site presentation
Kathleen L. Craft, Robert Pappalardo, Bonnie Buratti, Haje Korth, Ingrid Daubar, Cynthia Phillips, Rachel Klima, Sam Howell, Erin Leonard, Alexandra Matiella Novak, Trina Ray, Jennifer Kampmeier, and Brian Paczkowski and the Europa Clipper Science Team

Scheduled to launch in October 2024, NASA’s Europa Clipper will set out on a journey to explore the habitability of Jupiter’s icy ocean world Europa. After a 5.5 yr cruise that includes gravity assists at Mars and Earth, the spacecraft will enter orbit around Jupiter and will perform nearly 50 flybys of Europa over a four-year period. To explore Europa as an integrated system and achieve a complete picture of its habitability, the Europa Clipper mission has three main science objectives to characterize: (1) the ice shell and ocean including their heterogeneity, properties, and surface–ice–ocean exchange; (2) Europa’s composition including any non-ice materials on the surface and in the atmosphere, and any carbon-containing compounds; and (3) Europa’s geology including surface features and localities of high science interest. Additionally, several cross-cutting science topics will be investigated through searching for any current or recent activity in the form of thermal anomalies and plumes, performing geodetic and radiation measurements, and assessing high-resolution, co-located observations at select sites to provide reconnaissance for a potential future landed mission. These science objectives will be accomplished using a highly capable suite of remote-sensing and in-situ instruments. The remote sensing payload consists of the Europa Ultraviolet Spectrograph (Europa-UVS), the Europa Imaging System (EIS) consisting of a wide and a narrow angle camera (WAC, NAC), the Mapping Imaging Spectrometer for Europa (MISE), the Europa Thermal Imaging System (E-THEMIS), and the Radar for Europa Assessment and Sounding: Ocean to Near-surface (REASON). The in-situ instruments are the Europa Clipper Magnetometer (ECM), the Plasma Instrument for Magnetic Sounding (PIMS), the SUrface Dust Analyzer (SUDA), and the MAss Spectrometer for Planetary Exploration (MASPEX). Gravity and radio science will be obtained using the spacecraft's telecommunication system, and valuable scientific data will be acquired by the spacecraft’s radiation monitoring system.

Assembly, test, and launch operations (ATLO) of the Europa Clipper spacecraft are progressing well, and the flight system integration and environmental testing has been completed at the Jet Propulsion Laboratory. Currently, the flight system is undergoing operations testing, and in May 2024, the spacecraft will be shipped to NASA’s Kennedy Space Center at Cape Canaveral, Florida. There, the remaining integration activities will occur for the solar array and REASON antennas followed by final flight system tests. The launch period begins on 10 October 2024. To provide details on the mission’s instruments and planned investigations, the Europa Clipper science team is publishing manuscripts in a special issue of Space Science Reviews, and the team continues to work towards optimizing science return through preparation of the mission’s Strategic Science Planning Guide. As well, collaborative science opportunities with ESA’s JUpiter ICy moons Explorer (JUICE) mission, which will overlap in its tour period at Jupiter and make observations of Europa, are being discussed informally among the science teams. Onward to Europa!

How to cite: Craft, K. L., Pappalardo, R., Buratti, B., Korth, H., Daubar, I., Phillips, C., Klima, R., Howell, S., Leonard, E., Matiella Novak, A., Ray, T., Kampmeier, J., and Paczkowski, B. and the Europa Clipper Science Team: The Europa Clipper Mission and its Final Stretch to Launch, EGU General Assembly 2024, Vienna, Austria, 14–19 Apr 2024, EGU24-14097, https://doi.org/10.5194/egusphere-egu24-14097, 2024.

14:25–14:35
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EGU24-10976
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ECS
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On-site presentation
Mathis Pinceloup, Mathieu Bouffard, Steven Vance, Mohit Melwani Daswani, and Marshall Styczinski

Chemically stratified layers in the deep oceans of icy moons may strongly influence the oceans’ dynamics, thermal and chemical evolution, and therefore their habitability. Such layers can form during the differentiation of the refractory cores as they heat up due to the decay of long-lived radioactive elements. In the case of Ganymede, salts could be transported through the high-pressure ice layer to form a denser salt water layer at the base of the ocean. Such a layer would inhibit ocean convection, limiting chemical and thermal transport. It is therefore crucial to understand how these layers form and what specific signatures they may leave in geophysical observations of future space missions. The present work describes numerical simulations of the formation of stratified layers and the predicted observables that could be detected by instruments on the JUICE spacecraft.

3-D numerical simulations of Ganymede’s rotating ocean are performed with the PARODY code. Rayleigh-Bénard convection is imposed. We investigate the effect of either a constant flux of heavy salts or a fixed composition at the base of the ocean. Two regimes are identified by varying the dimensionless chemical Rayleigh (buoyancy over viscosity) and Schmidt numbers (viscosity over diffusivity). In the first regime, heavy salts are entrained and mixed in the convective region. In the second regime, the entrainment is too weak and a chemically stratified layer develops, eventually filling the entire ocean.

Extrapolation to Ganymede suggests the current existence of a chemically stratified layer at the base of the ocean with a thickness close to 30 km. By considering different stratifications in Ganymede’s ocean in the PlanetProfile and ForcedTides codes, we show that signatures of stratified layers might be detected in the gravity field, induced magnetic field, and tidal deformation responses. The problem of non-uniqueness in the individual observations points to the need to jointly invert these datasets from the JUICE mission to constrain the existence and properties of stratified oceanic layers.

How to cite: Pinceloup, M., Bouffard, M., Vance, S., Melwani Daswani, M., and Styczinski, M.: Formation of chemically stratified layer in Ganymede’s ocean: implications for upcoming JUICE mission, EGU General Assembly 2024, Vienna, Austria, 14–19 Apr 2024, EGU24-10976, https://doi.org/10.5194/egusphere-egu24-10976, 2024.

14:35–14:45
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EGU24-1416
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On-site presentation
Michele Dougherty

One of the most important realizations that planetary scientists have come to in the last 20 years is that in the search for potential habitability in our solar system, the focus need not only be on planetary bodies close to the Sun, where water on the surface is in liquid state. Based on Galileo and Cassini observations in the Jupiter and Saturn systems, there are many potential places in our solar system where sub-surface liquid water oceans may exist.

JUICE magnetometer (J-MAG) measurements (such as those made by the magnetometers on the Galileo and Cassini spacecraft) enable an understanding to be gained of the interior structure of the icy moons of Jupiter, specifically those of Ganymede, Callisto and Europa. Of particular interest are knowledge of the depth at which the liquid oceans reside beneath their icy surfaces, the strength of any internal magnetic fields such as at Ganymede and the strength of any induced magnetic fields arising within these oceans.

The primary science objectives of JUICE which will be constrained by the magnetic field observations and which drove the performance requirements of the J-MAG instrument include:

  • At Ganymede:
  • Characterization of the extent of the ocean and its relation to the deeper interior
  • Characterization of the ice shell
  • Characterization of the local environment and its interactions with the Jovian magnetosphere
  • Description of the deep interior and magnetic field generation
  • At Europa, further constrain the depth of the liquid ocean and its conductivity
  • At Callisto, characterize the outer shells, including the ocean

 

How to cite: Dougherty, M.: Using magnetic field observations from the Galilean moons to diagnose ocean properties, EGU General Assembly 2024, Vienna, Austria, 14–19 Apr 2024, EGU24-1416, https://doi.org/10.5194/egusphere-egu24-1416, 2024.

14:45–14:55
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EGU24-6318
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On-site presentation
Tim Van Hoolst, Gabriel Tobie, and Claire Vallat and the JUICE WG1 SSR

On 14 April 2023, the JUpiter ICy moons Explorer (JUICE) of ESA was launched from Europe's Spaceport in French Guiana. It will arrive at Jupiter and its moons in July 2031. Here we describe how JUICE will investigate the interior of the three icy Galilean moons, Ganymede, Callisto and Europa. Best insights into their interior, such as from an induced magnetic field, tides, rotation variations, and radar reflections, will be obtained during close flybys of the moons with altitudes of about 1000 km or less and during the Ganymede orbital phase at an average altitude of about 500 km and less. The 9-month long orbital phase around Ganymede, the first of its kind around another moon than our moon, will allow an unprecedented and detailed insight into the moon’s interior, from the central regions where a magnetic field is generated to the internal ocean and outer ice shell. Multiple flybys of Callisto will constrain the density structure, clarify the differences in evolution compared to Ganymede and will provide key constraints on the origin and early evolution of the Jupiter system. JUICE will visit Europa only during two close flybys and will perform geophysical investigations on selected areas, complementary to those performed by Europa Clipper.

We emphasize the synergistic aspects of the different geophysical investigations, showing how different instruments will work together to probe the hydrosphere, internal differentiation, dynamics, and evolution of these icy moons. In situ measurements and remote sensing observations will support the geophysical instruments to achieve these goals by providing complementary information about tectonics, potential plumes, surface composition, and exchange processes between ocean, ice and surface. Additional insight into the dissipative processes in the Jupiter system will be provided by accurate tracking of the JUICE spacecraft.

 

How to cite: Van Hoolst, T., Tobie, G., and Vallat, C. and the JUICE WG1 SSR: Investigating the interior of Ganymede, Callisto and Europa with JUICE, EGU General Assembly 2024, Vienna, Austria, 14–19 Apr 2024, EGU24-6318, https://doi.org/10.5194/egusphere-egu24-6318, 2024.

14:55–15:05
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EGU24-4522
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On-site presentation
Krishan Khurana, Hao Cao, and Lars Stixrude

Under low pressure and temperature, most rocks have extremely low electrical conductivities (< 10-9 S/m) which rise dramatically at temperatures encountered in deep interiors of solid bodies. The presence of ferric iron (Fe3+), whose abundance is related to the oxygen fugacity of the rock, lowers the activation energy of conduction and enhances rock conductivity further. Most models of the interior of Europa are consistent with the presence of a highly-conducting metallic iron core with a radius between 200 and 700 km (e.g., Kuskov and Kronrod, 2005). Thus, the mantle and the core of Europa are likely highly conducting and are expected to create measurable induction response. Accounting for this deep conductivity would not only improve the modeling of the physical parameters of the ocean but help further constrain the properties of Europa’s deeper interior.

Since the discovery of induction response from Europa’s ocean (Khurana et al., 1998), numerous studies have reexamined the electromagnetic induction signatures obtained by the Galileo spacecraft using increasingly sophisticated techniques to model the induction field and the moon/plasma interaction field (see e.g. Zimmer et al. 2000; Schilling et al. 2007; Vance et al. 2021). However, these studies have ignored the effect of induction from the deeper interior. Also, no studies have been performed for lower conductivities of the ocean and for longer period waves (such as the orbital period of Europa = 85.2 h) which can probe deeper even through a highly conducting ocean.

To address this problem, we have used the recursive method of Srivastava (1966) for a multiple layer model of Europa’s deep interior. The results from this preliminary exploration show that for a range of core radii and mantle conductivities, the deeper interior modifies the signal from the ocean by several nT at the two primary frequencies. The 85.2 h period penetrates through the ocean and elicits increasing response from the deep mantle as its conductivity is increased (from generation of stronger eddy currents). The 11.1 h period on the other hand produces a weaker response  with increasing mantle conductivity because the eddy currents are already at their highest level (100% induction from the ocean) but begin to follow a deeper path through the mantle and thus their magnetic response at the surface appears weaker.

Khurana, K.K., M.G. Kivelson, D. J. Stevenson, and others (1998) Induced magnetic fields as evidence for subsurface oceans in Europa and Callisto, Nature, 395, 777-780.

Kuskov O.L. and V.A. Kronrod (2005) Internal structure of Europa and Callisto, Icarus, 177, 550-569.

Srivastava, S.P. (1966) Theory of the magnetotelluric method for a spherical conductor, Geophys. J. Roy. Astro. Soc. 11, 373-387.

Vance, S. D., Styczinski, M. J., Bills, B. G., Cochrane, C. J., Soderlund, K. M., Gomez-Perez, N., & Paty, C. (2021). Magnetic induction responses of Jupiter's ocean moons including effects from adiabatic convection. J. Geophys. Res. : Planets, 126, e2020JE006418.

Zimmer, C., K.K. Khurana, and M.G. Kivelson (2000) Subsurface oceans on Europa and Callisto:  Constraints from Galileo magnetometer observations, Icarus, 147, 329.

How to cite: Khurana, K., Cao, H., and Stixrude, L.: The Impact of Europa’s Deep Interior on the Electromagnetic Induction Signal from Europa’s Ocean, EGU General Assembly 2024, Vienna, Austria, 14–19 Apr 2024, EGU24-4522, https://doi.org/10.5194/egusphere-egu24-4522, 2024.

15:05–15:15
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EGU24-8353
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On-site presentation
Giuseppe Mitri

Solid-state convection has been proposed to occur within Europa’s ice shell based both on the interpretation of observed geological activity during Galileo spacecraft exploration and theoretical investigations. Laboratory experiments have investigated the effect of grain size insensitive creep and grain size sensitive creep on the ductile behaviour of polycrystalline ice. The ice grain size and the ice impurities content and, consequently, the viscosity of the ice within Europa’s ice shell are poorly constrained, limiting the possibility to understand if solid-state convection can occur under Europa’s ice shell conditions. To investigate how diurnal tidal flexing and the internal dynamics of Europa’s ice shell influence the ice grain crystals’ evolution, we adopted a thermal-mechanical numerical model that uses finite differences and marker-in-cell techniques, implementing the dynamic recrystallization of the ice and the ice grain evolution in a self-consistent way with the numerical model. We found that solid-state convection within Europa’s ice shell can occur if it is diurnally tidally deformed, as the tidal stresses within the ice shell operate to reduce the ice grain sizes and the ice viscosity. We discuss future radio science experiments, in combination with radar sounder investigations, that will be capable of characterizing the possible presence of solid-state convection within Europa’s ice shell.

Acknowledgements: G.M. acknowledges support from the Italian Space Agency (2023-6- HH.0).

How to cite: Mitri, G.: Dynamic recrystallization within Europa’s ice shell: Implications for solid-state convection , EGU General Assembly 2024, Vienna, Austria, 14–19 Apr 2024, EGU24-8353, https://doi.org/10.5194/egusphere-egu24-8353, 2024.

15:15–15:25
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EGU24-9753
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ECS
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On-site presentation
Hamish Hay, Richard Katz, and Ian Hewitt

The rocky Jovian moon, Io, exhibits global volcanism that is driven by heat dissipated by tidal deformation. The large rate of heat exported by this volcanism, in conjunction with evidence in the form of magnetic induction, suggests that the mantle may contain a significant fraction of partial melt. This melt may be present in regions where both solid and liquid coexist at the macroscale. Nevertheless, existing models to investigate the location and magnitude of tidal heating consider an internal structure consisting of layers of pure solid or liquid. Such models are not appropriate for tidal deformation of partially molten materials. Building upon recent advancements in the theory of gravitational poroviscoelastic dynamics, we model tidal heating within Io, taking into account the effect of a two-phase, partially molten asthenosphere. 

The solid regions are modelled as a Maxwell viscoelastic material, and the top and bottom of the asthenosphere are treated as impermeable boundaries. We find that tidal dissipation within the fluid-filled pores depends on the ratio of the asthenosphere’s permeability to the melt’s viscosity. Thus, a low-viscosity melt and highly permeable pore-network favour enhanced tidal dissipation within the fluid. When this ratio, representing the Darcy drag, is large enough, fluid dissipation can exceed that within the solid grains when solid viscosity is high (> 1017 Pa s) or ultra-low (< 1011 Pa s). Tidal dissipation by the pore-hosted melt exhibits its own distinct tidal heating pattern, which always produces enhanced heating towards low latitudes.

How to cite: Hay, H., Katz, R., and Hewitt, I.: Tidal Dissipation in a Partially Molten Asthenosphere on Io, EGU General Assembly 2024, Vienna, Austria, 14–19 Apr 2024, EGU24-9753, https://doi.org/10.5194/egusphere-egu24-9753, 2024.

15:25–15:35
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EGU24-11367
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ECS
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On-site presentation
Ishan Mishra and Bonnie Buratti

Spiked, icy features, akin to the ‘penitentes’ on Earth [1], have been found on other airless bodies in the solar system as well, such as the 'bladed terrains' of Pluto [2] and the 'spires' of Callisto [3]. These features, thought to be formed due to sublimation erosion, are present in young, crater-less regions and hence represent an active response of the surfaces of these bodies to changing seasonal and climatic conditions. Interestingly, penitente formation has also been hypothesized on Europa [4], albeit the feasibility of that process on Europa has been questioned [5]. A fundamental limitation of testing this hypothesis for Europa is the lack of images at the resolution of the proposed penitente features (~ 15 m), unlike the images of the bladed terrains of Pluto from New Horizons and spires of Callisto from Galileo which clearly show these features. 

Photometric roughness models peer below the resolution limit of the camera to offer a glimpse of any surface roughness that is in the geometric optics limit.  Our roughness model [6], which has been successfully fit to a range of planetary bodies [7,8], will enable us to probe the surface roughness of Europa and test the penitente-hypothesis. We are locating Galileo images from the equatorial regions of Europa (within an equatorial zone restricted to ±24° where they are hypothesized to exist) and extracting scans of specific intensity (I/F) with backplanes of geometric coordinates. We will fit these I/F curves with our photometric model to derive roughness values, which will be compared to the proposed roughness of ~ 60° [4]. This predicted roughness is very high, so its effect on the light reflected from the surface should be easily detectable. To get a useful point of comparison for the roughness values we obtain for Europa, we will also perform a roughness analysis of the spires of Callisto, which are in a similar size regime of ~ 100 m. 

[1] Claudin, P. et al. (2015), Phys. Rev. E, 92(3), 033015; [2] Moore, J., et al. 2018, Icarus 300, 129-144, [3] Howard, A. D., & Moore, J. M. (2008). GRL, 35(3), L03203 [4] Hobley, D.E.J. et al. (2018). Nat. Geosci., 11(12), 901-904. [5] Hand, K.P. et al. ( 2020). Nat. Geosci., 13(1), 17-19. [6] Buratti, B. J., & J. Veverka (1985), Icarus 64, 320-328; [7] Buratti, B. J. et al. (2006). Planet. & Space Sci. 54, 1498-1509 [8] Lee, J. et al.  (2010), Icarus 206, 623-630.

How to cite: Mishra, I. and Buratti, B.: Testing the penitente hypothesis on Europa via photometric roughness, EGU General Assembly 2024, Vienna, Austria, 14–19 Apr 2024, EGU24-11367, https://doi.org/10.5194/egusphere-egu24-11367, 2024.

15:35–15:45
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EGU24-6113
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On-site presentation
Mathilde Kervazo, Gabriel Tobie, Marie Behounkova, Caroline Dumoulin, and Gaël Choblet

Volcanic activity at Europa’s seafloor is one of the key questions regarding the habitability of its subsurface ocean. The suitable conditions for hydrothermalism on Europa’s seafloor are conditioned by the heat released from the underlying silicate mantle, supplied by both radiogenic and tidal heating. The orbital resonance between Io, Europa, and Ganymede forces their orbit and maintains non-zero eccentricities. Tidal heating due to eccentricity tides on Io is so extreme that it  produces intense volcanism.  Even though tidal heating  in Europa’s silicate mantle is expected to be much weaker than on Io due to its greater distance to Jupiter,   Běhounková et al. [1] showed that it may still be sufficient to maintain Europa’s mantle in a partially molten state  for several tens to hundred millions of years, particularly during periods of increased eccentricity. Due to inefficient melt transport through the thick lithosphere of Europa [2], melt produced during periods of enhanced eccentricity may accumulate and in turn affect the tidal heating, as it is the case for Io, implying a possible runaway melt process in the silicate interior of Europa.

 

In this context, the goal of this study is to evaluate the effect of melt accumulation on the tidal heat production of Europa’s silicate mantle. For that purpose, we follow the approach developed to model the solid tides in Io’s partially molten interior [3], taking into account the effect of melt on the viscoelastic properties of the mantle. We adapt it to the context of Europa, corresponding to a deeper and thinner asthenosphere than on Io. We show that, whatever the partially molten layer thickness, melt accumulation increases tidal heat production and tidal dissipation even exceeds radiogenic heating. For equivalent volume of accumulated melt, the thinner the layer, the more pronounced this effect is. Our results show that the accumulation of melt, over timescales consistent with the 3D model prediction of Běhounková et al. [1], may significantly affect the tidal dissipation amplitude and its pattern. The potential presence of such melt accumulations may be tested by future measurements by Europa Clipper and JUICE from the combined analysis of gravimetric, altimetric and magnetic data, which might reveal long-wavelength anomalies which could be confronted to our model prediction.

 

[1] Běhounková et al., GRL, 48(3), e2020GL090077 (2021),  [2] Bland and Elder, GRL, 49(5), e2021GL096939 (2022). [3] Kervazo et al., A&A, 650, A72 (2021)

 

How to cite: Kervazo, M., Tobie, G., Behounkova, M., Dumoulin, C., and Choblet, G.: Impact of melt accumulation on tidal heat production in Europa’s mantle, EGU General Assembly 2024, Vienna, Austria, 14–19 Apr 2024, EGU24-6113, https://doi.org/10.5194/egusphere-egu24-6113, 2024.

Orals: Thu, 18 Apr | Room L1

Chairpersons: Emma Bunce, Umberto De Filippis, Claire Vallat
10:45–10:55
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EGU24-17570
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On-site presentation
Sascha Kempf and the SUDA Science Team

The Surface Dust Analyser (SUDA) is a dust impact mass spectrometer onboard of the Europa Clipper mission for investigating the surface composition of the Galilean moon Europa. The instrument is a Time--Of--Flight (TOF) impact mass spectrometer derived from previously flown dust compositional analyzers on Giotto, Stardust, and Cassini. SUDA uses the technology of the successful Cosmic Dust Analyzer (CDA) operating on Cassini and employs advanced reflectron-type ion optics for increased mass resolution. The instrument will measure the mass, speed, charge, elemental and isotopic composition of impacting grains.

 

Atmosphereless planetary moons such as the Galilean satellites are wrapped into a ballistic dust exosphere populated by tiny samples from the moon's surface produced by impacts of fast micrometeoroids. SUDA will measure the composition of such surface ejecta during close flybys at Europa to obtain key chemical constraints for revealing the satellite's composition, history, and geological evolution. Because of their ballistic orbits, detected ejecta can be traced back to the surface with a spatial resolution roughly equal to the instantaneous altitude of the spacecraft.

SUDA will detect a wide variety of compounds from Europa's surface over a concentration range of percent to ppm and connect them to their origin on the surface. This allows simultaneous compositional mapping of many organic and inorganic components, including both major and trace compounds, with a single instrument. Any recent tectonic activity, cryovolcanism, or resurfacing event is detectable by variations in the surface composition. This can be linked to corresponding geological features, including the analysis of compositional variations across large craters on Europa. SUDA will further the understanding of Europa's surface couples to its interior source regions.

In this presentation, we will discuss SUDA's unique capabilities to collect compositional ground truth from orbit and how SUDA contributes to the Europa Clipper science goals.

How to cite: Kempf, S. and the SUDA Science Team: SUDA: A SUrface Dust Analyser for compositional mapping of the Galilean moon Europa, EGU General Assembly 2024, Vienna, Austria, 14–19 Apr 2024, EGU24-17570, https://doi.org/10.5194/egusphere-egu24-17570, 2024.

10:55–11:05
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EGU24-6579
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On-site presentation
Ujjwal Raut, Silvia Protopapa, Bereket D Mamo, Geronimo Villanueva, Richard J Cartwright, Benjamin D Teolis, Kurt D Retherford, and Diana L Blaney

Recent JWST observations reveal a higher abundance of endogenic CO2 at Tara Regio, a prominent leading hemisphere chaos (Villanueva et al., 2023; Trumbo and Brown, 2023). Prior findings from Keck also show an excess of H2O2 in the same region (Trumbo et al., 2019). Could the emplacement of the ocean-derived CO2 onto Europa’s surface influence radiolytic chemistry to boost peroxide yields in these enigmatic chaos regions? Increased H2O2 at fractured chaos terrains where ocean-surface exchange is more likely is exciting from a habitability stance, as it may facilitate oxidant delivery to the subsurface ocean.

We present laboratory results that show H2O2 synthesis increases by 2-3 folds in the presence of trace amounts of CO2 (< 3 %) when compared to radiolysis of pure water ice. We also discuss correlations between CO2 and H2O2 abundances in the JWST datasets to determine whether Europa’s endogenous CO2 indeed conspires to inflate H2O2 at Tara Regio and possibly other chaos terrains. These JWST observations combined with emerging laboratory measurements set the stage for detailed mapping of CO2 (via its 2.7 and ~4.23-4.29 µm absorptions) and H2O2 (via its 3.5 µm absorption) with MISE (Europa Clipper) and MAJIS (JUICE) at unprecedented spatial resolution.

References:

  • Villanueva, G. L. et al., (2023) Science, 381, 1305–1308 
  • Trumbo, S. K and Brown, M. E. (2023) Science, 381, 1308–1311
  • Trumbo, S. K. et al. (2019) Astronomical Journal, 158, 127

How to cite: Raut, U., Protopapa, S., Mamo, B. D., Villanueva, G., Cartwright, R. J., Teolis, B. D., Retherford, K. D., and Blaney, D. L.: Can endogenic CO2 inflate radiolytic H2O2 in Europa’s Chaos?, EGU General Assembly 2024, Vienna, Austria, 14–19 Apr 2024, EGU24-6579, https://doi.org/10.5194/egusphere-egu24-6579, 2024.

11:05–11:15
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EGU24-13816
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ECS
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Virtual presentation
Elodie Lesage, Samuel M. Howell, Julia W. Miller, Mariam Naseem, Justine Villette, Marc Neveu, Mohit Melwani Daswani, and Steven D. Vance

Introduction. Europa, the most visibly active icy moon of Jupiter, is a prime target for the search for life in the outer solar system. Two spacecraft missions, Europa Clipper from the National Aeronautics and Space Administration (NASA) and the Jupiter Icy Moon Explorer (JUICE) from the European Space Agency (ESA), will conduct extensive observations of its surface, gravity field and environment starting 2030. It has been proposed that liquid briny water reservoirs could be injected and stored in Europa’s ice shell, causing the formation of various geological features. In particular, these reservoirs could occasionally trigger eruptions [1], resulting in flows on the surface and vapor plumes in the atmosphere.

If shallow liquid brine reservoirs are indeed present in Europa's ice shell, they would leave surface evidence that future missions could detect, including local thermal anomalies, ice shell thickness change, and erupted briny solutions with time varying salinity. We present a novel simulation that models thermal, physical, and compositional ice shell and reservoir evolution and eruption, and that predicts the various signatures detectable by future robotic exploration.

Cryomagma chemistry. We conserve enthalpy to solve the coupled chemical evolution and pressurization of freezing brines stored in Europa’s ice shell using current best estimates of the oceanic composition [2] to predict the composition of erupted cryolava. This composition varies with time, as salts concentrate during freezing [3], which could lead to erupted brines of varying composition depending on the reservoir frozen fraction when the eruption is triggered. The equilibrium freezing of oceanic brines is modeled using the software PHREEQC to obtain the liquid and solid fraction of each component of the aqueous solution as a function of the temperature. 

Ice shell and reservoir modelling. We simultaneously model the ice shell and reservoir thermal, physical, and compositional evolution self-consistently building upon the framework of [4]. We solve for the conservation of enthalpy using conservative finite differences in a one-dimensional (1D) spherical shell, propagated explicitly forward in time. The thermophysical properties of the multiphase model are temperature-, pressure-, and composition dependant, thus the composition and physical state are consistently updated at every time step. Finally, modeled eruption frequency and eruptive characteristics are dependent on the properties and their gradients in ice surrounding the reservoir.

Results. Outputs of the model include the temporal evolution of the temperature in the ice shell, reservoir, and at the surface, and the time of eruptions and erupted cryomagma composition (Fig. 1).

Figure 1: Temporal evolution of signatures of a 1 km thick cryomagma reservoir located 1 km bellow the surface.

Acknowledgements. Portions of this research were carried out at the Jet  Propulsion Laboratory, California Institute of Technology, under contract with the National Aeronautics and Space Administration (NASA). This work was supported by NASA’s Solar System Workings program (grants #80NM0018F0612 and #80NSSC20K0139)

References. [1] Lesage et al. (2022) PSJ 3(7), 170, [2] Melwani Daswani et al. (2021) GRL 48(18), [3] Naseem et al. (2023) PSJ 4(9), 181, [4] Howell, S. M. (2021) PSJ 2(4), 129.

How to cite: Lesage, E., Howell, S. M., Miller, J. W., Naseem, M., Villette, J., Neveu, M., Melwani Daswani, M., and Vance, S. D.: Cryovolcanism inside out: Signatures of past and present cryovolcanism on Europa, EGU General Assembly 2024, Vienna, Austria, 14–19 Apr 2024, EGU24-13816, https://doi.org/10.5194/egusphere-egu24-13816, 2024.

11:15–11:25
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EGU24-13075
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ECS
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On-site presentation
Paul S. Szabo, Andrew R. Poppe, Andreas Mutzke, Lucas Liuzzo, and Shane R. Carberry Mogan

Ion precipitation onto Ganymede, shaped by interaction between the Jovian plasma and Ganymede’s magnetosphere, has been connected to brightness patterns and radiolysis products on its surface [1,2]. JUICE will measure ion fluxes in-situ at around 500 km altitude, leaving uncertainties for the precipitation patterns on the surface [3]. At Earth’s Moon, backscattered Energetic Neutral Atoms (ENAs) have been shown to be suitable for studying the ion-surface interaction from an orbiting spacecraft [4]. We now present the first modeling of ENAs created by backscattered H, O and S ions at Ganymede, which will enable JUICE to remotely observe the ion impacts. Using the SDTrimSP code [5], which has been verified for backscattered ENAs at the Moon [6, 7], we account for inputs of magnetospheric plasma precipitation from hybrid simulations [8] and Ganymede’s surface composition from telescopic observations [9].

Our simulation results support that backscattering is an important formation process mainly for atomic H and O populations, whose properties are directly related to the precipitation conditions. Especially backscattered H ENAs dominate over any sputtered ENAs [10] above at least around 1 keV, making them ideal candidates for observing the plasma-surface interaction at Ganymede. Compared to lunar ENAs, backscattering probabilities are lower, but extended high-energy tails occur due to energetic ion populations in the Jovian plasma. The backscattering process thus creates neutral atom contributions that are candidates for observation with both JUICE’s JNA and JENI instruments.

 

[1]          S. Fatemi, et al., Geophys. Res. Lett. 43 (2016), 4745.

[2]          S.K. Trumbo, et al., Sci. Adv. 9 (2023), eadg3724.

[3]          C. Plainaki , et al., Astrophys. J. 940 (2022), 186.

[4]          Y. Futaana, et al., Gephys. Res. Lett. 40 (2013), 262.

[5]          A. Mutzke, et al., IPP Report 2019-02 (2019).

[6]          P.S. Szabo, et al., Geophys. Res. Lett. 49 (2022), e2022GL101232.

[7]          P.S. Szabo, et al., J. Geophys. Res.: Planets 128 (2023), e2023JE007911.

[8]          A.R. Poppe, et al., J. Geophys. Space Phys. 123 (2018), 4614.

[9]          N. Ligier, et al., Icarus 333 (2019), 496.

[10]       A. Pontoni, et al., J. Geophys. Space Phys. 127 (2022), e2021JA029439.

 

 

How to cite: Szabo, P. S., Poppe, A. R., Mutzke, A., Liuzzo, L., and Carberry Mogan, S. R.: Constraining Ion Precipitation onto Ganymede’s Surface with Backscattered Energetic Neutral Atoms, EGU General Assembly 2024, Vienna, Austria, 14–19 Apr 2024, EGU24-13075, https://doi.org/10.5194/egusphere-egu24-13075, 2024.

11:25–11:35
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EGU24-6809
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On-site presentation
J. Hunter Waite, James L. Burch, Tim Brockwell, David T. Young, Kelly Miller, Christopher R Glein, Danielle Y. Wyrick, Benjamin D. Teolis, Scott J. Bolton, Mathieu Choukroun, Melissa A. McGrath, William B. McKinnon, Olivier Mousis, Mark A. Sephton, Everett Shock, Mikhail Yu Zolotov, Steven C. Persyn, John M Stone, Rebecca Perryman, and Christine Ray and the MASPEX Science and Instrument Teams

The MAss Spectrometer for Planetary EXploration (MASPEX) is a multi-bounce time-of-flight neutral gas mass spectrometer with unprecedented spaceborne mass resolution and sensitivity. It is capable of measuring and identifying minor and trace gases requiring mass resolution of m/Δm ~ 25,000 at abundances of parts-per-million in Europa’s exosphere. Exospheric sources of gases include exsolved, sublimed, sputtered, and radiolytically produced volatiles from Europa’s surface and interior. These gases can be used to characterize surface composition and identify volatiles outgassed from Europa’s interior. Of particular relevance in characterizing Europa’s habitability are the ratios of organic compounds such as alkanes, alkenes, alkynes, alcohols, ethers, aldehydes, amides, amines, and nitriles that undergo chemical transformations, which can be used to determine oxidation states, pH, temperature, and free energy availability of an interior ocean, perched lake, or a gas source region in the ice shell (e.g., a diapir).

 

This paper presents: 1) the principles and ground-calibrated performance of the MASPEX instrument that is now integrated onto the Europa Clipper spacecraft and planned to be launched in October of 2024, 2) the planned scientific investigation and its critical role in the study of Europa’s habitability, 3) the operational plans, and 4) the anticipated data products from the MASPEX investigation. The paper will also discuss the complexity of the investigation and its requisite need for the acquisition of supporting geochemical, impact fragmentation, and sputtering/radiolytic data sets that help to characterize the geochemical reaction framework and the anticipated modification of chemical species due to impacts with the instrument’s thermalizing chamber, and from radiolysis and sputtering. In the latter context we present the science team’s efforts to generate the necessary data sets, and we encourage interested scientists to contribute to this important endeavor, which is essential for the maximum success of the MASPEX investigation.

How to cite: Waite, J. H., Burch, J. L., Brockwell, T., Young, D. T., Miller, K., Glein, C. R., Wyrick, D. Y., Teolis, B. D., Bolton, S. J., Choukroun, M., McGrath, M. A., McKinnon, W. B., Mousis, O., Sephton, M. A., Shock, E., Zolotov, M. Y., Persyn, S. C., Stone, J. M., Perryman, R., and Ray, C. and the MASPEX Science and Instrument Teams: The Europa Clipper MASPEX Investigation, EGU General Assembly 2024, Vienna, Austria, 14–19 Apr 2024, EGU24-6809, https://doi.org/10.5194/egusphere-egu24-6809, 2024.

11:35–11:45
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EGU24-352
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ECS
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On-site presentation
Leander Schlarmann, Audrey Vorburger, Shane R. Carberry Mogan, and Peter Wurz

In this study, we use the Direct Simulation Monte Carlo (DSMC) method [1] to investigate the collisional fraction of the atmospheres of Europa, Ganymede, and Callisto. The extent of the collisional atmosphere of the icy moons is still subject to ongoing debate. While Europa’s atmosphere is tenuous and effectively collisionless, the exobase for Ganymede and Callisto is expected to be located above a thin collision-dominated atmospheric layer [2].

In the 2030s, both ESA's Jupiter Icy Moons Explorer (JUICE) and NASA's Europa Clipper mission are set to explore Jupiter's icy moons from up close, using high-resolution mass spectrometers to sample their atmospheres. The Neutral gas and Ion Mass spectrometer (NIM) of the Particle Environment Package (PEP) onboard JUICE [3] and the MAss Spectrometer for Planetary EXploration (MASPEX) onboard Europa Clipper [4] will determine the atmospheric composition of the moons and potentially sample plume material on Europa. The collisional fraction of their atmospheres affects the abundances of the various species that will be measured, and hence also the deduction of the underlying surface composition. Therefore, obtaining a comprehensive understanding of atmospheric structures, including the collisional fraction, is imperative for both missions. This knowledge is essential to ensure the correct interpretation of the measured data once it becomes available.

The DSMC method is a computation technique, where rarefied gas flows are simulated by tracking the motion of individual particles, including their collisions and interactions, to provide insight into the macroscopic gas dynamics. Therefore, this method is ideal for studying thin atmospheres that transition from being collisional near the surface to ballistic at higher altitudes, such as the atmospheres of the icy Galilean moons. The model [5, 6] used herein includes different physical and chemical processes that create the atmospheres of the icy moons, such as sputtering due to interactions with Jupiter's magnetosphere, the sublimation of surface ice, and photochemical reactions.

[1] Bird, G. A. (1994). Molecular gas dynamics and the direct simulation of gas flows.
[2] Schlarmann, L., et al. (2024), in preparation.
[3] Grasset, O., et al. (2013). Planetary and Space Science, 78, 1-21.
[4] Phillips, C. B., and Pappalardo, R. T. (2014). Eos, Transactions AGU, 95(20), 165-167.
[5] Carberry Mogan, S. R., et al. (2021). Icarus, 368, 114597.
[6] Carberry Mogan, S. R., et al. (2022). Journal of Geophysical Research: Planets, 127(11).

How to cite: Schlarmann, L., Vorburger, A., Carberry Mogan, S. R., and Wurz, P.: Exploring the Collisionality of the Icy Galilean Moon Atmospheres., EGU General Assembly 2024, Vienna, Austria, 14–19 Apr 2024, EGU24-352, https://doi.org/10.5194/egusphere-egu24-352, 2024.

11:45–11:55
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EGU24-7724
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On-site presentation
Norbert Krupp, Elias Roussos, Markus Fränz, Peter Kollmann, George Clark, Chris Paranicas, Krishan Khurana, Stas Barabash, and Andre Galli

 

The Galileo spacecraft performed close flybys of the moon Ganymede between 1996 and 2001. We reanalysed data of the energetic particles detector EPD onboard Galileo and derived the particle fluxes, energy spectra, and pitch angle distributions in the energy range of several keV to MeV during Ganymede flybys G2, G7, G8, G28, and G29. We find sharp dropouts in ion and electron fluxes as signatures of the loss cones inside the Ganymede magnetosphere as well as trapped electron distribution. Additionally, bi-directional field-aligned and butterfly distributions were found as well. We discuss these findings compared with simulation results in charactering Ganymede’s magnetosphere and in the context of future measurements with the Particle Environment Package PEP onboard the Juice mission which will be in orbit around Ganymede in 2032.

How to cite: Krupp, N., Roussos, E., Fränz, M., Kollmann, P., Clark, G., Paranicas, C., Khurana, K., Barabash, S., and Galli, A.: Energetic particle measurements near Ganymede: Galileo EPD data revisited and perspectives for Juice PEP, EGU General Assembly 2024, Vienna, Austria, 14–19 Apr 2024, EGU24-7724, https://doi.org/10.5194/egusphere-egu24-7724, 2024.

11:55–12:05
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EGU24-11772
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On-site presentation
Arnaud Beth, Marina Galand, Ronan Modolo, François Leblanc, Xianzhe Jia, Hans Huybrighs, and Gianluca Carnielli
The Galileo spacecraft flew by Ganymede, down to 0.1 RG from the surface for the closest, six times giving us insight into its plasma environment. Its ionosphere, made of ions born from the ionisation of neutrals present in Ganymede’s exosphere, represents the bulk of the plasma near the moon around closest approach. As it has been revealed by Galileo and Juno, near closest approach the ion population is dominated by low-energy ions from the water ion group (O+, HO+, H2O+) and O2+. However, little is known about their density, spatial distribution, and effect on the surface weathering of the moon itself. Galileo G2 flyby has been extensively studied. Based on a comparison between observations and 3D test-particle simulations, Carnielli et al. (2020a and 2020b) confirmed the ion composition (debated at the time), highlighted the inconsistency between the assumed exospheric densities and the observed ionospheric densities, and derived the contribution of ionospheric ions as an exospheric source. However, other flybys of Ganymede are also available (e.g. G1, G7, G8, G28, and G29) providing in-situ measurements at different phases of Ganymede around Jupiter or jovian magnetospheric conditions at the moon. We extend the original study by Carnielli et al. to other flybys, and compare our modelled ion moments (ion number density, velocity, and energy distribution) with Galileo in-situ data. We discuss our results and contrast them with those obtained for the G2 flyby.
 
 

How to cite: Beth, A., Galand, M., Modolo, R., Leblanc, F., Jia, X., Huybrighs, H., and Carnielli, G.: Ionospheric environment of Ganymede during the Galileo flybys, EGU General Assembly 2024, Vienna, Austria, 14–19 Apr 2024, EGU24-11772, https://doi.org/10.5194/egusphere-egu24-11772, 2024.

12:05–12:15
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EGU24-8573
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ECS
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Virtual presentation
Antoine Schneeberger, Olivier Mousis, and Jonathan Lunine

At the very end of its growth, Jupiter became surrounded by a disk composed of gas and dust, where the Galilean moon presumably formed. It is supposed that satellitesimals formed by streaming instability and grew by pebble accretion. Once the satellitesimals reacedh a significant size, they undergone an inward type I migration by gravitational interaction with the disk. In the early stages of the circumplanetary disk, the migration of satellitesimals occurred over so short timescales that most bodies fell onto Jupiter, suggesting that the Galilean moons formed later during the disk’s evolution.  Other studies suggest that the moons sequentially formed and migrated inward. This suggests that the moons were trapped in mean motion resonances, halting their migration.  In the coming years, the ESA mission JUICE and NASA mission Europa-Clipper will study the Galilean moons composition and provide hints on their formation conditions.

In this context, we aim to model the evolution of a 2-dimensional circumplanetary disk around Jupiter. To do this, we have constructed a quasi-stationary circumplanetary disk model that considers viscous heating, accretion heating, and heating of the upper layers of the circumplanetary disk by Jupiter. The thermal structure is determined by a grey atmosphere radiative transfer model. We show that the heating by Jupiter of the upper layers of the disk induces flaring and disk self-shadowing effects, which locally increase and decrease the disk temperature, respectively. The resulting temperature variations can be up to 50 K relative to the surrounding disk temperature. Consequently, the circumplanetary disk can produce transient hotter and colder regions that can last up to 10 kyr. The alternance of hot and cold regions in the Jovian circumplanetary disk has then profound implications for the formation conditions of the Galilean moons.

How to cite: Schneeberger, A., Mousis, O., and Lunine, J.: Impact of Jupiter's heating and self-shadowing on the structure of its circumplanetary disk , EGU General Assembly 2024, Vienna, Austria, 14–19 Apr 2024, EGU24-8573, https://doi.org/10.5194/egusphere-egu24-8573, 2024.

12:15–12:25
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EGU24-12178
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On-site presentation
Pontus Brandt, George Clark, Peter Kollmann, Donald G. Mitchell, Malamati Gkioulidou, Dennis Haggerty, Stanislav Barabash, Peter Wurz, Norbert Krupp, Elias Roussos, Carol Paty, Xianzhe Jia, Krishan Khurana, Frederic Allegrini, Angele Pontoni, and H. Todd Smith

The Jovian Energetic Neutrals and Ions (JENI) Camera and the Jovian Energetic Electrons (JoEE) belong to the six-sensor suite Particle Environment Package (PEP) on board the JUICE mission. JENI is a combined ion and ENA camera with 90˚x120˚ Field-of-View and an energy range from a few keV to 110 keV for ENAs and 5 MeV for ions. Only one mission, Cassini, has captured ENA images of the Jovian system before during its distant flyby. Those images revealed emissions coming from the Europa neutral gas torus, but were too distant to resolve details on its spatial distribution and variability. The Juno mission has detected ENA emissions originating from both the Europa and also the Io torus, that indicate azimuthally asymmetric distributions. In ENA mode, JENI will image the Europa and Io tori, to investigate their spatial distribution and long-term variability providing global constraints to physical models of their sources. Although a predominant fraction of the ENAs from the tori originate from charge exchange between magnetospheric energetic ions and the neutral gas, a significant fraction may originate from charge exchange between the energetic ions and the ambient plasma in the tori. This opens up the intriguing possibility to also diagnose the plasma dynamics and distribution of the tori. JENI also targets the explosive recurrences of vast regions of heated plasma in the Jovian magnetotail (“injections”) that may be the engine behind the periodic radio emissions from rotating, magnetized planets, such as Saturn, Jupiter and perhaps even brown dwarfs. In ion mode, JENI will provide the detailed in-situ measurements of the energetic ion environment necessary to understand the physical heating and transport processes underlying the global context provided by the ENA images. JoEE is an electron spectrometer that near-simultaneously provide the energetic electron spectrum in multiple look directions over the energy range from 28 keV up to 2 MeV. JoEE’s prime objectives are to investigate the acceleration mechanisms of Jovian radiation belt electrons and their interaction with the Jovian moons. The Juno mission has recently made important electron measurements that provides useful guidance for deepening the JoEE objectives.

In this presentation an overview is given of JENI and JoEE, with emphasis on the ENA observations and their expected science return. This includes imaging of the Europa and Io tori distribution and variability, quasi-periodic magnetospheric injections, and their relation to rotationally periodic radio emissions from planets and brown dwarfs.

How to cite: Brandt, P., Clark, G., Kollmann, P., Mitchell, D. G., Gkioulidou, M., Haggerty, D., Barabash, S., Wurz, P., Krupp, N., Roussos, E., Paty, C., Jia, X., Khurana, K., Allegrini, F., Pontoni, A., and Smith, H. T.: Energetic Neutral Atom (ENA) Imaging and In-Situ Energetic Particle Exploration of the Jovian Magnetosphere and Moon Environment from JUICE/PEP, EGU General Assembly 2024, Vienna, Austria, 14–19 Apr 2024, EGU24-12178, https://doi.org/10.5194/egusphere-egu24-12178, 2024.

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

Display time: Thu, 18 Apr, 14:00–Thu, 18 Apr, 18:00
Chairpersons: Haje Korth, Claire Vallat, Anezina Solomonidou
X3.49
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EGU24-6577
Haje Korth, Robert Pappalardo, and Bonnie Buratti and the Europa Clipper Flight System Engineering Team

At the beginning of the next decade, the Europa Clipper Flight System will enter orbit around Jupiter and, over a four-year period, will fly by Europa nearly 50 times to explore the habitability of this planet’s moon Europa. The Flight System comprises (1) the Propulsion Module, which provides the thermally-controlled spacecraft structure, propulsion subsystem, and solar array; (2) the Avionics Module, which enables spacecraft guidance, navigation, and control operations, provides power conditioning and computer resources which stores and prioritizes science data for downlink; (3) the Radio-Frequency Module, which provides telemetry uplink and science data downlink capabilities; and (4) a highly capable suite of remote-sensing and in-situ instruments to achieve the science objectives of the mission. The remote sensing payload consists of the Europa Ultraviolet Spectrograph (Europa-UVS), the Europa Imaging System (EIS), the Mapping Imaging Spectrometer for Europa (MISE), the Europa Thermal Imaging System (E-THEMIS), and the Radar for Europa Assessment and Sounding: Ocean to Near-surface (REASON). The in-situ instruments comprise the Europa Clipper Magnetometer (ECM), the Plasma Instrument for Magnetic Sounding (PIMS), the SUrface Dust Analyzer (SUDA), and the MAss Spectrometer for Planetary Exploration (MASPEX). Gravity and radio science will be achieved using the spacecraft's telecommunication system, and valuable scientific data will be acquired by the spacecraft’s radiation monitoring system. The mission is presently in the assembly, testing, and launch operations (ATLO) phase. The Propulsion and RF Modules have been delivered from the Johns Hopkins Applied Physics Laboratory (APL) to the Jet Propulsion Laboratory (JPL). The flight system integration and environmental testing has been completed at the Jet Propulsion Laboratory. The flight system is presently undergoing a series of operations tests. In May 2024, it will be shipped to Kennedy Space Center, where it will be integrated with the solar array, which was delivered to the location earlier this year. The launch period begins on 10 October 2024, and once lifted off, the Europa Clipper will be cruising to the Jupiter System with gravity assists by Mars followed by Earth on the way. Go Europa Clipper!

How to cite: Korth, H., Pappalardo, R., and Buratti, B. and the Europa Clipper Flight System Engineering Team: The Europa Clipper Flight System on its Path to Launch , EGU General Assembly 2024, Vienna, Austria, 14–19 Apr 2024, EGU24-6577, https://doi.org/10.5194/egusphere-egu24-6577, 2024.

X3.50
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EGU24-17407
Umberto De Filippis, Paolo Cappuccio, Mauro Di benedetto, and Luciano Iess

The JUpiter ICy moons Explorer (JUICE) mission is a cornerstone of the European Space Agency (ESA). The mission was launched in April 2023 from Kourou with an Ariane V launcher and is expected to arrive at Jupiter in 2031. JUICE will investigate the gas giant planet Jupiter, its atmosphere, magnetosphere, and its icy moons, Ganymede, Europa and Callisto. The mission will focus on Ganymede, during the low altitude circular and polar orbital phase.

The spacecraft will carry a suite of scientific instruments, including a camera, a spectrometer, a radar system, a laser altimeter, and a suite of instrumentation dedicated to radio science experiments: the Ka-band Transponder (KaT), the Ultra Stable Oscillator (USO) and the High Accuracy Accelerometer (HAA).

The Gravity & Geophysics of Jupiter and Galilean Moons experiment (3GM) instrumentation will be used to study the gravity field up to degree and order 40 of Ganymede and the extent of internal oceans on the icy moons. Furthermore, during radio occultations, the 3GM experiment will investigate the structure of the neutral atmospheres and ionospheres of Jupiter and its moons.

The HAA accelerometer will play a fundamental role during the 3GM experiment even if it will not directly measure any of the physical quantities connected with the experiment scientific goals. It aims to measure the perturbations of non-gravitational forces that the JUICE spacecraft will undergo during 3GM measurements with an accuracy of  in the frequency band of  Hz. Such perturbations are mainly induced by the propellant sloshing within the tanks, especially during the moon flybys. These perturbing accelerations are included in the orbital determination algorithm. In this work we show the first inflight data collected by the HAA instrument during the cruise. We present the data collected after launch (April-June 2023) during the deployment of the spacecraft moving appendages such as the RIME antenna, the Langmuir probes and the magnetometer boom. The analysis of these data aims to preliminary characterize the instrument behaviour and the spacecraft dynamic environment. Additionally, we show the analysis of the HAA data collected during the first payload checkout (January 2024), with a focus on the preliminary assessment on the instrument in-flight scientific performances.  

How to cite: De Filippis, U., Cappuccio, P., Di benedetto, M., and Iess, L.: Analysis of the first data collected by the High Accuracy Accelerometer (HAA) onboard the JUICE spacecraft, EGU General Assembly 2024, Vienna, Austria, 14–19 Apr 2024, EGU24-17407, https://doi.org/10.5194/egusphere-egu24-17407, 2024.

X3.51
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EGU24-20774
Stas Barabash, Pontus Brandt, Peter Wurz, George Clark, Norbert Krupp, Elias Roussos, Gabriella Stenberg Wieser, Philipp Wittmann, Markus Fränz, Manabu Shimoyama, Martin Wieser, Peter Kollmann, and Donald Mitchell

The Jupiter bound JUICE mission (JUpiter ICy moons Explorer) was successfully launched on April 14, 2023 and is currently executing its 8-year interplanetary cruise phase. JUICE carries three comprehensive instrument suites to fully characterize particles, fields, and waves. The JUICE space plasma instrumentation constitutes the most comprehensive and capable heliophysics payload ever flown, or planned, in the important but not-well explored the solar system region between 1 and 5 au.

Science objectives that can be addressed by the JUICE payload include solar wind evolution, collisionless shock interactions and propagation, and particle acceleration, solar energetic particles, pick-up ion (PUI) origin and evolution, turbulent interactions, energetic neutral atom (ENA) imaging, and interplanetary hydrogen observations.

JUICE enables an expansion of inner heliospheric science, connecting to observations in the outer heliosphere and Very Local Interstellar Medium (VLISM) by NASA’s New Horizons, Voyager, and Interstellar Mapping and Acceleration Probe (IMAP) (to launch Feb 2025). New science opportunities are also enabled by the simultaneous observations from Europa Clipper in the same region. JUICE will spend the next six years between 0.7 au and 2.5 au, and in 2029-2031 it will explore the region out to Jupiter. JUICE has no thermal constraints past 1.34 au and the data volume from relevant sensors live well within the available data downlink through its weekly passes using the European Space Tracking (ESTRACK).

In this presentation, we discuss the unique heliophysics observations the six-sensor suite Particle Environment Package (PEP) on board can do in conjunction with other space physics measurements on board JUICE and Europa Clipper. The PEP-suite measures species-resolved energy and angular distributions of electrons (~ 1 eV to ~1.5 MeV), ions (~1 eV to > 10 MeV; energy rage is species dependent); and ENA (~ 5eV to 300 keV). In addition to the PEP instrument suite, JUICE also carries a radiation monitor (RADEM) that can provide complimentary energy and species resolved measurements of very energetic electrons and ions in the solar wind.

How to cite: Barabash, S., Brandt, P., Wurz, P., Clark, G., Krupp, N., Roussos, E., Stenberg Wieser, G., Wittmann, P., Fränz, M., Shimoyama, M., Wieser, M., Kollmann, P., and Mitchell, D.: Unique Heliospheric Measurement Opportunities with the ESA JUICE mission: Science Case for Particle Environment Package (PEP), EGU General Assembly 2024, Vienna, Austria, 14–19 Apr 2024, EGU24-20774, https://doi.org/10.5194/egusphere-egu24-20774, 2024.

X3.52
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EGU24-12317
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ECS
Paolo Haffoud, Yves Langevin, François Poulet, Mathieu Vincendon, Gianrico Filacchione, Giuseppe Piccioni, John Carter, Pierre Guiot, Benoit Lecomte, Cydalise Dumesnil, Alessandra Barbis, Leonardo Tommasi, Sébastien Rodriguez, Stefani Stefania, Federico Tosi, Cédric Pilorget, and Simone De Angelis

 

ESA’s Jupiter Icy Moons Explorer (JUICE) mission scientific payload includes a 2-channels (visible to near-infrared (VISNIR) and infrared (IR)) cryogenic imaging spectrometer instrument called the Moons And Jupiter Imaging Spectrometer (MAJIS). During its ground calibration campaign, this instrument was tested at different operative temperatures, and calibration measurements were acquired to derive the spatial, spectral, and radiometric performances. Following the launch of the JUICE mission to the Jovian System, the first in-flight measurements were acquired during the near-Earth commissioning phase (NECP). In flight, the internal calibration unit (ICU) was used to monitor the instrument’s response.  In particular, the ICU signal provides full illumination of the instrument's field of view. It exhibits several absorption bands thanks to a didymium and a polystyrene filter placed in front of the VISNIR and IR sources, respectively.

The performances of the instrument are evaluated through several metrics, including the absolute spectral calibration, the full width at half maximum of the response (spatial and spectral), the distortions (keystone and smile), and the impact of the optical head temperature.

The flight acquisitions will be presented and compared to the ground calibration analyses, and the current performances of the instrument will be discussed in the context of MAJIS main scientific goals.

How to cite: Haffoud, P., Langevin, Y., Poulet, F., Vincendon, M., Filacchione, G., Piccioni, G., Carter, J., Guiot, P., Lecomte, B., Dumesnil, C., Barbis, A., Tommasi, L., Rodriguez, S., Stefania, S., Tosi, F., Pilorget, C., and De Angelis, S.: Monitoring the performances of MAJIS from ground to flight calibration measurements, EGU General Assembly 2024, Vienna, Austria, 14–19 Apr 2024, EGU24-12317, https://doi.org/10.5194/egusphere-egu24-12317, 2024.

X3.53
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EGU24-1266
Adrienn Luspay-Kuti and the The PIMS Science and Engineering team

Characterizing Europa’s subsurface ocean is critical to assessing Europa’s habitability. Measurements of the magnetic field induced in the conducting Europan ocean in response to Jupiter’s magnetosphere is a proven technique that has successfully demonstrated the existence of subsurface oceans at Io (magma), Europa, and Callisto. In the case of Europa, the dynamic, magnetized plasma flow in the Jovian magnetosphere causes strong magnetic perturbations comparable to those of the induced field strength. Thus, accurate characterization of the ocean by magnetic sounding requires an accurate characterization of the plasma properties. The Plasma Instrument for Magnetic Sounding (PIMS) will launch on the Europa Clipper mission in October 2024 onboard a Falcon Heavy rocket and will measure the plasma properties in Jupiter’s magnetosphere and in Europa’s tenuous atmosphere. PIMS measurements will advance our understanding of the Jovian environment near Europa’s orbit and the interaction of Europa’s atmosphere and surface with Jupiter’s plasma and magnetic field. These scientific advances will, in turn, improve modeling efforts that will ultimately enable a highly accurate separation of the magnetic field due to induction in Europa’s interior from the highly variable magnetic perturbations due to the plasma interactions exterior to Europa. Thus, PIMS will enable the full potential of the induction technique in probing Europa’s interior to be realized, and will help constrain the average thickness of the ice shell and average thickness and salinity of the ocean, as well as characterize the composition and sources of the plasma and volatiles. In this presentation we will overview the PIMS instrument and its final calibration before it was integrated onto the spacecraft.

How to cite: Luspay-Kuti, A. and the The PIMS Science and Engineering team: The Plasma Instrument for Magnetic Sounding (PIMS): Measuring the Plasma Influence on Magnetic Induction on the Europa Clipper mission  , EGU General Assembly 2024, Vienna, Austria, 14–19 Apr 2024, EGU24-1266, https://doi.org/10.5194/egusphere-egu24-1266, 2024.

X3.54
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EGU24-1750
Patrick Brown and the The J-MAG Instrument Team

JUICE is an ESA L-Class interplanetary mission to the Jupiter system that was launched on the 14th April 2023 from Kourou, French Guiana. It will make in-situ and remote sensing measurements of Jupiter and the Galilean moons during a three-year science operation phase starting in July 2031. The tour will include a high-latitude phase, fly-bys of Callisto and Europa culminating in elliptical and circular orbits of Ganymede down to an altitude of 200 km. Detection and characterization of potential sub-surface oceans on Europa and Ganymede are a key science goal of the mission as is the interaction between Ganymede’s internal magnetic field with the Jovian field.  Constraining the depth and conductivity of any subsurface ocean on Ganymede will be achieved through measurement of response to two magnetic inducing signals, one at Ganymede’s orbital period (171.7 hrs) and the other at Jupiter’s synodic period (10.5 hrs) which together drive a requirement for in-flight accuracy of 0.2nT. The combination of such low frequency and low amplitude scientific signals places a unique set of EMC cleanliness requirements on the spacecraft system and on the performance of the instrument configuration.

J-MAG is the DC magnetometer instrument on JUICE measuring the low frequency magnetic field vector in the range [0-64 Hz]. It is composed of a conventional dual fluxgate design together with a Coupled Dark State Magnetometer (CDSM) absolute scalar sensor and an electronics box accommodated within a vault on the main platform. All three sensors are mounted on the outer segment of a 10.6 m boom. The scalar sensor is included to enable calibration of the fluxgate sensors during the Ganymede phase where the magnetic field is highly variable and traditional techniques for fluxgate offset calibration (such as spacecraft rolls or analysis of incompressible waves in the solar wind) are not viable.  

We report on the instrument design and challenges presented by the mission environment and trajectory. We will present the performance of the magnetometer on ground and a summary of the initial results from the near-Earth commissioning phase that took place during May 2023.

 

How to cite: Brown, P. and the The J-MAG Instrument Team: The J-MAG Magnetometer: Instrument design, performance, and initial in-flight results., EGU General Assembly 2024, Vienna, Austria, 14–19 Apr 2024, EGU24-1750, https://doi.org/10.5194/egusphere-egu24-1750, 2024.

X3.55
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EGU24-10327
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ECS
Christoph Amtmann, Andreas Pollinger, Michaela Ellmeier, Michele Dougherty, Patrick Brown, Roland Lammegger, Alexander Betzler, Martín Agú, Christian Hagen, Irmgard Jernej, Josef Wilfinger, Richard Baughen, Alex Strickland, and Werner Magnes

The presentation discusses the accuracy of the scalar Coupled Dark State Magnetometer on board the Jupiter Icy Moon Explorer (JUICE) mission of the European Space Agency. The scalar magnetometer MAGSCA is part of the J-MAG instrument.

MAGSCA is an optical, omni-directional scalar magnetometer based on coherent population trapping, a quantum interference effect, within the hyperfine manifold of the 87Rb D1 line. The measurement principle is only based on natural constants and therefore, it is in principle drift free and no calibration is required. However, the technical realisation can influence the measurement accuracy.
The most dominating effects are heading characteristics, which are deviations of the magnetic field strength measurements from the ambient magnetic field strength.

The verification of the accuracy and precision of the instrument is required to ensure its compliance with the performance requirement of the mission: 0.2 nT (1-σ).
The verification is carried out with four dedicated sensor orientations in a Merritt coil system, which is located in the geomagnetic Conrad observatory. The coil system is used to compensate the Earth’s magnetic field and to apply appropriate test fields to the sensor. 

A novel method is presented which separates the heading characteristics of the instrument from residual (offset) fields within the coil system by fitting a mathematical model to the measured data. It allows verifying that the MAGSCA sensor unit does not have a measurable remanent magnetisation as well as that the desired accuracy of 0.2 nT (1-σ) is achieved by the MAGSCA flight hardware for the JUICE Mission.

How to cite: Amtmann, C., Pollinger, A., Ellmeier, M., Dougherty, M., Brown, P., Lammegger, R., Betzler, A., Agú, M., Hagen, C., Jernej, I., Wilfinger, J., Baughen, R., Strickland, A., and Magnes, W.: Accuracy of the Scalar Magnetometer aboard ESA's JUICE Mission, EGU General Assembly 2024, Vienna, Austria, 14–19 Apr 2024, EGU24-10327, https://doi.org/10.5194/egusphere-egu24-10327, 2024.

X3.56
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EGU24-20110
Emma Bunce, Louise Prockter, and Mathieu Choukroun and the JUICE Clipper Science Committee

ESA’s JUpiter ICy moons Explorer (JUICE) launched on April 14, 2023, beginning an eight-year journey to the Jupiter system. Arriving in 2031, JUICE will make 35 total flybys of Ganymede, Europa, and Callisto before going into orbit about Ganymede. NASA’s Europa Clipper is scheduled to launch in October 2024, arriving in the Jupiter system in 2030, a year ahead of JUICE. Clipper will spend a year in the system before undertaking 49 flybys of Europa during a nominal three-year primary mission phase, while also making multiple serendipitous flybys of Ganymede and Callisto. Having two highly instrumented spacecraft in close proximity in time and space affords unprecedented opportunities for synergistic observations during the missions’ main orbital phases, and unique heliospheric and magnetosphere science during cruise and Jupiter approach.

While there are currently no firm commitments from NASA or ESA to accomplish science beyond that of each mission’s primary science objectives, discussions are ongoing and the task of the appointed JUICE-Clipper Steering Committee (JCSC) is to provide recommendation of compelling joint science opportunities between the two missions.

This paper will focus on the cruise and Jupiter approach phases. We have identified a number of potential opportunities for investigating the evolution of the solar wind plasma and interplanetary magnetic field and related structures such as monitoring Coronal Mass Ejections (CMEs) or Corotating Interaction Regions (CIRs) during times when the two spacecraft are radially aligned (i.e. at similar heliocentric longitudes) or at similar heliocentric distances, as well as radio science observations of the solar wind and/or Solar Energetic Particle (SEP) events that could be observed throughout interplanetary transfer. There is also potential for investigating the evolution of solar wind structures and disturbances when both spacecraft are “connected” through Parker Spiral field lines. The cruise science return from JUICE and Clipper could be further enhanced by data from other operational spacecraft (e.g., BepiColombo, Solar Orbiter, Parker Solar Probe, MAVEN, IMAP, Psyche), thus expanding the catalogue of opportunities for these identified configurations, as well as simultaneous observations by ground and space-based observatories (e.g., JWST, Keck, etc.). The >1 year Jupiter approach phase of the JUICE spacecraft while Clipper orbits within the jovian magnetosphere provides an unrivalled opportunity to study the complexity of the solar wind-magnetosphere interaction and aurora at Jupiter, a topic where there remain many open questions. This phase would provide a unique opportunity for preparatory joint observations to understand if and how the solar wind influences the moon’s local space environment, and the related interaction with Jupiter’s rapidly rotating magnetosphere.

How to cite: Bunce, E., Prockter, L., and Choukroun, M. and the JUICE Clipper Science Committee: ESA JUICE and NASA Europa Clipper: Joint Science Opportunities during Cruise and Jupiter Approach, EGU General Assembly 2024, Vienna, Austria, 14–19 Apr 2024, EGU24-20110, https://doi.org/10.5194/egusphere-egu24-20110, 2024.

X3.57
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EGU24-6262
Louise Prockter, Emma Bunce, and Mathieu Choukroun and the JUICE-Clipper Steering Committee

Launched in April, 2023, ESA’s JUpiter ICy moons Explorer (JUICE) is en route to the Jupiter system. Upon arrival in 2031, the spacecraft will orbit Jupiter for 3.5 years, making 35 total encounters with Ganymede, Europa, and Callisto, before going into orbit about Ganymede for 1 year.  NASA’s Europa Clipper is scheduled to launch in October 2024, and arrives in the Jupiter system in 2030, a year before JUICE. Orbiting Jupiter, the Clipper spacecraft will spend a year in the system before focusing on ~52 flybys of Europa during a nominal four-year primary mission phase, while also making multiple serendipitous flybys of Ganymede and Callisto. Having two highly instrumented spacecraft in close proximity in time and space affords unprecedented opportunities for synergistic observations of Europa, Ganymede, Callisto, Io, Jupiter’s atmosphere, magnetosphere and environment, and Jupiter’s small satellites and rings, as well as opportunities for unique heliospheric and magnetosphere science during the JUICE and Clipper missions’ cruise and Jupiter-approach phases.

Analysis of potential joint science opportunities is underway by a small team of scientists from the JUICE and Clipper mission teams. Ideas have been collated from JCSC members as well as from three joint Clipper-JUICE workshops (2018, 2019, 2022), and the Science Traceability Matrix from a prior joint ESA-NASA study, the Europa Jupiter System Mission (EJSM). We recently produced a report on science that can be accomplished during the two spacecrafts’ cruise and Jupiter approach phases (Bunce et al., this meeting), and are now investigating potential opportunities once JUICE and Clipper are in orbit around Jupiter. Multiple opportunities exist for joint science at several different targets within the Jovian system, including two opportunities near Europa where the spacecraft are within 0.5Rj of each other and only a few hours apart. Scientific objectives may fall into one or more categories: (1) time dependent, in which both spacecraft must acquire data at same time, or one spacecraft’s observations inform the other’s observations; (2) space dependent, in which each spacecraft acquires data from specific parts of the Jovian system, or both observe the same target with similar, or different viewing geometries; and (3) an increase in science data (e.g. temporal or spatial coverage) made possible due to the availability of additional instrument types or data collection opportunities.

There are currently no firm commitments from NASA or ESA to accomplish science beyond that of each mission’s primary science objectives. However, discussions are ongoing and we are optimistic that our recommendations for the unprecedented opportunities afforded by the two missions’ alignment will enable funding support to be found. In this paper, we discuss some of the potential combined science from JUICE and Clipper that could further enhance understanding of the of the Jupiter system and the origin and habitability of the Galilean moons.

How to cite: Prockter, L., Bunce, E., and Choukroun, M. and the JUICE-Clipper Steering Committee: Exploring the Jupiter System through unique joint JUICE and Europa Clipper observations, EGU General Assembly 2024, Vienna, Austria, 14–19 Apr 2024, EGU24-6262, https://doi.org/10.5194/egusphere-egu24-6262, 2024.

X3.58
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EGU24-11664
Claire Vallat, Rosario Lorente, and Nicolas Altobelli and the The Juice Science Team

Juice is the first large mission chosen in the framework of ESA’s Cosmic Vision 2015-2025 program.

The focus of Juice is to characterize the conditions that might have led to the emergence of habitable environments among the Jovian icy satellites, in particular Ganymede, Europa and Callisto. Juice will also perform a multidisciplinary investigation of the Jupiter system as an archetype for gas giants.

The spacecraft payload consists of 10 state-of-the-art instruments (and one experiment that use the spacecraft telecommunication system with ground-based instruments) that will perform remote and in-situ measurements of Jupiter, its moons and their environment.

 

From a trajectory’s point of view, the mission calls for a three-year orbital survey of the Jupiter system followed by an additional 9 months in orbit around Ganymede for an in-depth characterization of Ganymede as a planetary object and possible habitat. During the Jupiter orbital phase, Juice will perform a sequence of 67 orbits of different periods and inclinations around the planet including several flybys of the Galilean moons, 2 of which as close as 400km altitude from Europa in July 2032.

The Juice top level Europa science goals are the determination of the composition of the non-ice materials and understanding their origin (deep interior vs exogenic), the search for liquid water under active sites and the study of the activity processes at play on the moon.

A representative detailed science operations plan has been developed by the science team covering a 24 hour-period around the first flyby of Europa in July 2032. The plan considers the latest knowledge on instrument and spacecraft resources and performances available at the time of the study.

This work presents the geometry and mission constraints associated to the flyby as well as the observation strategy chosen by the different payload; the remote sensing package’s strategy includes exosphere characterization (including potential plume detection) through limb observations and surface characterization at different scales and wavelengths, both on the inbound (dayside) and outbound (nightside) part of the flyby. At low altitude and centered around closest approach, the geophysics package will perform topography and surface roughness measurement using the laser altimeter as well as surface sounding down to a depth of up to ~ 9 km with the ice penetrating radar. Radio science range rate measurement will support the estimate of the main quadrupole coefficients and the testing of the hydrostatic hypothesis. The in-situ package will operate continuously to monitor the Europa plasma, neutral and electromagnetic wave environment. The resulting harmonized operations timeline, together with resources limitations and the assessment on the expected science return is discussed.

How to cite: Vallat, C., Lorente, R., and Altobelli, N. and the The Juice Science Team: A detailed science and operations analysis of the first flyby of Europa by the Juice spacecraft, EGU General Assembly 2024, Vienna, Austria, 14–19 Apr 2024, EGU24-11664, https://doi.org/10.5194/egusphere-egu24-11664, 2024.

X3.59
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EGU24-19302
Thomas Cornet, Guillaume Cruz-Mermy, Ines Belgacem, Francois Andrieu, and Frederic Schmidt

The NASA Galileo spacecraft explored the Jupiter system between 1995 and 2003. The spacecraft was equipped with the Near-Infrared Mapping Spectrometer instrument (NIMS), able to probe Jupiter’s atmosphere and the icy moons’ surface composition in the near-infrared with its 17 detectors operating between 0.7 to 5.2 microns [1]. The Galileo NIMS dataset was collected during flybys, which resulted in a series of very diverse data cubes, viewing geometries and spatial resolutions. In addition, depending on the instrument mode used to collect the data, and on the instrument’s own health status, the NIMS infrared spectra were collected with a varying spectral sampling (between 15 and 408 wavelengths), and an evolving absolute wavelength calibration over the course of the mission. Despite its heterogeneity and complexity of use, the Galileo/NIMS dataset is one of the most valuable resource to model and map the surface properties (composition, grain size, roughness, phase function) of Jupiter’s moons, which are the prime targets of the Europa Clipper [2] and ESA JUICE [3] missions in this decade.

We converted the Galileo/NIMS calibrated dataset publicly available on the PDS Imaging Node (as g-cubes) into a MySQL relational database, which allows to quickly select and extract radiance factors (I/F), geometry data, and metadata from the entire NIMS data set. The smallest element in the database is a spectrum (i.e. one pixel). Using SQL queries relying on the pixel viewing geometry (incidence, emission, phase, and azimuth) and the geographic pixel location (latitudes and longitudes on a target), phase curves and/or collections of spectra can be easily retrieved. Individual g-cubes data can also be accessed upon request. We used this database framework, together with Bayesian inversion methods and the Hapke model [4,5], to perform detailed compositional studies on Europa’s dark lineaments [6,7], and spectro-photometric modeling of broader regions of interest located in different hemispheres [8].

 

References

[1] Carlson et al., Space Science Reviews, 60, 457-502, 1992.

[2] Howell and Pappalardo, Nat Commun 11, 1311, 2020.

[3] Grasset et al., Plan Spac Sci 78, 1-21, 2013.

[4] Hapke, Icarus 221, 1079-1083, 2012.

[5] Hapke, Cambridge University Press, 1993.

[6] Cruz Mermy et al., Icarus 394, 115379, 2023.

[7] Andrieu et al., EPSC 2022.

[8] Belgacem et al., EPSC, 2022.

How to cite: Cornet, T., Cruz-Mermy, G., Belgacem, I., Andrieu, F., and Schmidt, F.: Studying the icy moons of Jupiter using a database framework, EGU General Assembly 2024, Vienna, Austria, 14–19 Apr 2024, EGU24-19302, https://doi.org/10.5194/egusphere-egu24-19302, 2024.

X3.60
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EGU24-9464
Markus Fränz, Patrick Bambach, Henning Fischer, Philipp Heumüller, Norbert Krupp, Wolfgang Kühne, Elias Roussos, Robert Labudda, and Stas Barabash

The magnetosphere of Jupiter is apart from the Sun the strongest source of charged particles in the Solar system. The interaction of these particles with the exospheres of the Jovian moons forms one of the most complex plasma laboratories encountered by human space flight. For this reason the plasma analyzer package forms a crucial experiment of the Jupiter Icy Moon Explorer (JUICE). As part of the Plasma Environment Package (PEP) we describe a combined electron and ion spectrometer which is able to measure the electron and ion distribution functions in the energy range 1 to 50000 eV with high sensitivity and time resolution. This instrument is called the Jovian Electron and Ion Analyzer, JEI. We report on the general performance of the instrument and on first observations of the solar wind during commissioning of the instrument in space.

How to cite: Fränz, M., Bambach, P., Fischer, H., Heumüller, P., Krupp, N., Kühne, W., Roussos, E., Labudda, R., and Barabash, S.: The Jovian Electron and Ion Spectrometer (PEP-JEI) for the JUICE mission, EGU General Assembly 2024, Vienna, Austria, 14–19 Apr 2024, EGU24-9464, https://doi.org/10.5194/egusphere-egu24-9464, 2024.

X3.61
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EGU24-11349
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ECS
Caroline Haslebacher, Louise M. Prockter, Erin J. Leonard, Paul M. Schenk, and Nicolas Thomas

Double ridges are a common linear feature on Europa’s surface. They can be identified by a central trough accompanied by two ridge crests. Usually, the elevation of double ridge crests is not higher than 300 meters (e.g. [1]). Some double ridges run almost perfectly straight for hundreds of kilometers, while others are curved, for example into a cycloidal shape. Several double ridge formation hypotheses exist, which can be separated into cryo-volcanism/-sedimentation and brittle deformation (an overview can be found in [2]). Each proposed formation mechanism results in a unique topographic profile, which allows these hypotheses to be tested. 

We extract topographic profiles of more than 1000 mapped double ridges (perpendicular to their orientation) from a shape-from-shading topographic map. The shape-from-shading topographical map and the double ridge map are based on regional mosaics of Europa (data by [3]), two north-south covering swaths of the trailing and leading hemispheres at the regional scale (~230 m/px). The two regional mosaics were obtained under consistent illumination angles by the solid-state imager (SSI) on the Galileo spacecraft. We map double ridges in the regional mosaics with the help of the deep-learning tool LineaMapper [4]. We manually inspect, adjust, and verify LineaMapper’s predictions while respecting disruptions caused by other cross-cutting surface features.  

With this methodology, we analyze topographic profiles of double ridges in the regional mosaics and match them with unique profiles predicted by cryo-volcanism/-sedimentation and brittle deformation hypotheses. By assuming that, for any lineament, the number of disruptions per kilometer length is a proxy for relative age, we can assess the evolution of double ridge profiles over time, with potential implications for the upcoming space missions Europa Clipper and JUICE. 

[1] F. Nimmo, R. T. Pappalardo, B. Giese. (2003). On the origins of band topography, Europa. Icarus, 166(1), 21-32. 
[2] A.C. Dameron & D. M. Burr. (2018). Europan double ridge morphometry as a test of formation models. Icarus, 305(1), 225-249. 
[3] M. T. Bland, L. A. Weller, B. A. Archinal, E. Smith, B. H. Wheeler, (2021). Improving the Usability of Galileo and Voyager Images of Jupiter's Moon Europa. Earth and Space Science, 8(12). 
[4] C. Haslebacher, N. Thomas, V. T. Bickel, (2024). LineaMapper: A deep learning-powered tool for mapping linear surface features on Europa. Icarus, 410(1).

How to cite: Haslebacher, C., Prockter, L. M., Leonard, E. J., Schenk, P. M., and Thomas, N.: Extraction of topographic profiles of double ridges on Europa , EGU General Assembly 2024, Vienna, Austria, 14–19 Apr 2024, EGU24-11349, https://doi.org/10.5194/egusphere-egu24-11349, 2024.

X3.62
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EGU24-15429
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ECS
Alexis Coyette, Rose-Marie Baland, and Tim Van Hoolst

It is generally assumed that the large icy satellites of Jupiter and of Saturn are, like our Moon, in an equilibrium rotation state called a Cassini State. In this state, the rotation of the satellite is synchronous with the orbital motion and the precession rate of the rotation axis is equal to that of the normal to the orbit. Moreover, the spin axis of the satellite, the normal to its orbit and the normal to the inertial plane remain coplanar and the obliquity (the angle between the normal to the orbit and the spin axis) is constant over time. For satellites with a slow orbital precession rate like the large icy satellites, up to four Cassini states are possible, characterized by a (theoretically) constant obliquity close to 0 (CSI), ± π/2 (CSII and IV) and π (CSIII). From these four states, only two are stable: CSI and CSIII.

We here model these two stable Cassini States of triaxial satellites using an angular momentum approach. In our model, the motion of the spin motion in space is coupled with the polar motion of the satellite and, contrary to what is usually done in the classical Cassini States studies, we do not average the external gravitational torque over short period terms. We can therefore compute the mean obliquity value of the different satellites but also the nutations (small periodic variations) both in obliquity and in longitude, which are due to the periodic variations of the gravitational torque acting on the satellites. We identify and study two causes for the polar motion and their effects on the obliquity: the semi-diurnal polar motion due to the inclination and node precession and the long period polar motion due to the eccentricity and pericenter precession.

How to cite: Coyette, A., Baland, R.-M., and Van Hoolst, T.: Modeling the Cassini States of large icy satellites with an angular momentum approach, EGU General Assembly 2024, Vienna, Austria, 14–19 Apr 2024, EGU24-15429, https://doi.org/10.5194/egusphere-egu24-15429, 2024.

X3.63
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EGU24-6850
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ECS
Rikuto Yasuda, Tomoki Kimura, Baptiste Cecconi, Hiroaki Misawa, Fuminori Tsuchiya, Yasumasa Kasaba, Shinnosuke Satoh, Shotaro Sakai, and Corentin Louis

The ionospheres of Jupiter’s icy moons have been observed by in situ plasma measurements and radio occultation. However, their spatial structures have not yet been fully characterized. To address this issue, we developed a new ray tracing method for modeling the radio occultation of the ionospheres using Jovian auroral radio sources. Applying our method to radio observations with the Galileo spacecraft, we derived the electron density of the ionosphere of Ganymede and Callisto. For Ganymede’s ionosphere, we found that the maximum electron density on the surface was 150 cm-3 in the open magnetic field line regions and 12.5 cm-3 in the closed magnetic field line region during the Galileo Ganymede 01 flyby. The difference in the electron density distribution was correlated with the accessibility of Jovian magnetospheric plasma to the atmosphere and surface of the moons. These results indicated that electron impact ionization of the Ganymede exosphere and sputtering of the surface water ice were effective for the producing Ganymede’s ionosphere. For Callisto’s ionosphere, we found that the densities were 350 cm-3 and 12.5 cm-3 on the night-side hemisphere during Callisto 09 and 30 flybys, respectively. These results combined with previous observations indicated that atmospheric production through sublimation controlled the ionospheric density of Callisto. This method is also applicable to upcoming Jovian radio observation data from the Jupiter Icy Moon Explorer, JUICE. 

How to cite: Yasuda, R., Kimura, T., Cecconi, B., Misawa, H., Tsuchiya, F., Kasaba, Y., Satoh, S., Sakai, S., and Louis, C.: Ray tracing for Jupiter’s icy moon ionospheric occultation of Jovian auroral radio sources, EGU General Assembly 2024, Vienna, Austria, 14–19 Apr 2024, EGU24-6850, https://doi.org/10.5194/egusphere-egu24-6850, 2024.

X3.64
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EGU24-4968
Wei-Ling Tseng, Ian-Lin Lai, Wing-Huen Ip, Hsiang-Wen Hsu, and Yi-Shiang Tzeng

With its subsurface ocean, Europa raises intriguing possibilities about the potential for extraterrestrial life beneath its icy crust. Its unique surface features present a dynamic and complex geophysical landscape that offers valuable insights into its evolution. This study explores the plume dynamics and deposition of icy dust particles on Europa. Utilizing a Direct Simulation Monte Carlo (DSMC) modeling of Europa's gaseous plumes, we use a hybrid model to understand dust dynamics entrained in the plumes. This approach allows us to consider various parameters such as production rate, initial velocity of gas and dust, and size distribution of dust particles, providing a comprehensive view of plume dynamics and highlighting their impact on Europa's surface characteristics. The results showing distinct plume morphologies and dust deposition patterns offer clues to our understanding of Europa's ongoing geological activity and subsurface ocean.

How to cite: Tseng, W.-L., Lai, I.-L., Ip, W.-H., Hsu, H.-W., and Tzeng, Y.-S.: Surface Deposition of Icy Dust Entrained in Europa’s Plumes, EGU General Assembly 2024, Vienna, Austria, 14–19 Apr 2024, EGU24-4968, https://doi.org/10.5194/egusphere-egu24-4968, 2024.

X3.65
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EGU24-2170
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ECS
Shivangi Sharan, Emma Bunce, Michele Dougherty, Xianzhe Jia, and Margaret Kivelson

The interiors of the icy moons of Jupiter hold a key to understanding habitability in the Solar System and beyond. They could serve as prototypes to comprehend similar bodies that might have the potential to sustain life. The magnetic field observations from the Galileo mission between 1996 and 2003 suggest large oceans below the icy crusts of Europa and Callisto and a probable subsurface ocean at Ganymede. It also discovered that Ganymede has an intrinsic magnetic field and a dynamic magnetosphere.

NASA’s Europa Clipper and ESA’s Jupiter ICy moons Explorer (JUICE) missions have been designed to better understand and characterise these icy moons. They aim to confirm the existence of a subsurface ocean at the three moons, in particular, Ganymede and Europa, and constrain their internal structure. The missions would also explore the magnetosphere of Jupiter and its interactions within the Jovian system. Ganymede is the largest moon of our Solar System, capable of producing its own dynamo field and possibly possessing an ocean beneath its surface. However, separating the intrinsic field from the induced field is a difficult problem. Galileo measurements provided two models for Ganymede’s overall internal field- a dipole and quadrupole model or a dipole and induction model. Both the quadrupole and induction signals are quite small and well represent the observations together with the dipole field.

Latest trajectory information for Europa Clipper assuming an October 2024 launch, and the predicted JUICE trajectory following the successful launch in April 2023 show initial close Ganymede flybys. In this study, we use them to understand their trajectories and highlight their importance in confirming the induced signal and thereby the ocean as well as for modelling the dynamo field. The first 2 Clipper and the first 3 JUICE flybys occur within an altitude of 500 km from Ganymede’s surface and are hence useful for overall internal field modelling. We predict the measurements that would be observed from the two internal sources as well as the external magnetospheric source to better understand the signals and decipher their differences. For the intrinsic and external fields, we use dynamo and magnetohydrodynamic models respectively while for the induced field, we use Jupiter’s background field along with the induction equation at the spacecraft locations.

The 5 flybys independently as well as together with the data from the Galileo flybys would enhance our understanding of the different magnetic sources at Ganymede and the fields they produce. These joint early flyby observations will enable us to be better equipped to model the magnetic field components near Ganymede in the orbital phase of the JUICE mission.

How to cite: Sharan, S., Bunce, E., Dougherty, M., Jia, X., and Kivelson, M.: Understanding the interior magnetic fields of Ganymede using flybys of the Europa Clipper and JUICE missions, EGU General Assembly 2024, Vienna, Austria, 14–19 Apr 2024, EGU24-2170, https://doi.org/10.5194/egusphere-egu24-2170, 2024.