Evolution of Titan's Atmosphere During the Late Heavy Bombardment

Total Page:16

File Type:pdf, Size:1020Kb

Evolution of Titan's Atmosphere During the Late Heavy Bombardment Evolution of Titan’s atmosphere during the Late Heavy Bombardment Nadejda Marouninaa, Gabriel Tobiea, Sabrina Carpya, Julien Monteuxa,b, Benjamin Charnayc, Olivier Grasseta aLaboratoire de Plan´etologie et G´eodynamique, Universit´ede Nantes, CNRS, UMR-6112, 2, rue de la Houssini`ere, 44322 Nantes cedex France. bLaboratoire Magmas et Volcans, Universit´eBlaise Pascal – CNRS – IRD, OPGC, 5 rue Kessler, 63038 Clermont-Ferrand, France cVirtual Planetary Laboratory, University of Washington, Seattle, WA 98195, USA Abstract The mass and composition of Titan’s massive atmosphere, which is dominated by N2 and CH4 at present, have probably varied all along its history owing to a combination of exogenous and endogenous processes. In the present study, we investigate its fate during the Late Heavy Bombardment (LHB) by modeling the competitive loss and supply of volatiles by cometary im- pacts and their consequences on the atmospheric balance. For surface albedos ranging between 0.1 and 0.7, we examine the emergence of an atmosphere during the LHB as well as the evolution of a primitive atmosphere with various masses and compositions prior to this event, accounting for impact-induced crustal NH3-N2 conversion and subsequent outgassing as well as impact- induced atmospheric erosion. By considering an impactor population characteristic of the LHB, we show that the generation of a N2-rich atmosphere with a mass equivalent to the present-day one requires ammonia mass fraction of 2 to 5 %, depending on surface albedos, in an icy layer of at least 50 km below the surface, implying an undifferentiated interior at the time of LHB. Except for high surface albedos (AS ≥ 0:7) where most of the released N2 remain frozen at the surface, our calculations indicate that the high-velocity impacts led to a strong atmospheric erosion. For a differentiated Titan with a thin ammonia-enriched crust (≤ 5 km) and AS < 0:6 , any atmosphere preexisting before the LHB should be more than 5 times more massive than at present, in order to sustain an atmosphere equivalent to the present-day one. This implies that either a massive atmosphere was formed on Titan during its accretion or that the nitrogen-rich atmosphere was generated after the LHB. Keywords: Titan, atmosphere; impact processes; atmosphere, evolution 1. Introduction Saturn’s largest satellite Titan is the only satellite in the Solar System possessing a dense atmosphere. Presently, it is composed predominantly of N2(∼98%) and CH4(∼ 2%) (e.g. Griffith et al., 2013). However, this atmospheric composition has probably varied through time since the accretion of the satellite due to various external and internal processes. Owing to continuous photochemical destruction and atmospheric escape, the lifetime of atmospheric methane is cur- rently of the order of ∼20 Ma (e.g. Griffith et al., 2013). Moreover, the isotopic 13C/12C ratio in Preprint submitted to Icarus May 27, 2015 CH4, measured by the mass spectrometer of the Huygens probe (GCMS) (Niemann et al., 2010), indicates that the present-day methane is not fractionated relative to Solar System standards, im- plying that it has been recently injected in the atmosphere (less than 1 Gyr ago (Mandt et al., 2012)). The origin of N2 is probably more ancient. The main constraint on its origin is provided by 36 −7 the Ar/N2 ratio measured by the Huygens GCMS (∼2.7×10 , Niemann et al. (2010)), which 5 36 is ∼3×10 times smaller than the solar value (Owen, 1982). As N2 and Ar should be trapped in similar rates either by direct condensation or clathration in the solar nebula (Owen, 1982; Mousis et al., 2002), this low value indicates that the nitrogen was not originally captured as N2 but as easily condensible nitrogen compounds such as NH3 (Atreya et al., 2009). Moreover, Mandt 14 15 et al. (2014) showed that the N/ N ratio measured in Titan’s N2 (Niemann et al., 2010) is con- sistent with isotopic ratio recently inferred from NH2 radicals produced by the photodissociation of NH3 in comets (Rousselot et al., 2014; Shinnaka et al., 2014), providing additional evidence for ammonia as the main source of nitrogen on Titan. Several mechanisms have been proposed to explain the conversion of NH3 into N2 at Titan’s conditions: photochemical conversion (Atreya et al., 1978), impact-induced conversion in the atmosphere (McKay et al., 1988; Ishimaru et al., 2011) or in a NH3-enriched icy crust (Sekine et al., 2011), as well as endogenic processes (Glein et al., 2009; Tobie et al., 2012). Here we focus on the conversion proposed by Sekine et al. (2011). Delivery of volatiles by impact has likely occurred all along Titan’s history (Griffith and Zahnle, 1995), with more intense flux during the accretion period and the Late Heavy Bombard- ment (LHB). Following the Nice model (Gomes et al., 2005; Morbidelli et al., 2005; Tsiganis et al., 2005), this intense bombardment would have affected the entire Solar System, due to the destabilization of the planetesimal disk beyond Neptune’s orbit. Because of the gravitational focusing of Saturn (Zahnle et al., 2003), the cumulative mass delivered on Titan during the LHB is estimated to 3×1020 kg (Barr et al., 2010). This intense bombardment, characterized by high impact velocities ( vesc, the escape velocity of the planet or the satellite), may have supplied a huge amount of volatiles (e.g. CH4 and NH3) either by direct contribution from impactor volatil- isation or by impact-induced degassing of Titan’s crust, as suggested by Sekine et al. (2011). High-velocity impactors are also expected to erode the atmosphere during the impact. Studies of impact-induced atmospheric erosion based either on analytic approaches or numerical simu- lations have been mostly focused on Mars and the Earth (Melosh and Vickery, 1989; Svetsov, 2000; Genda and Abe, 2005; Svetsov, 2007; Shuvalov, 2009). Parameterizations of impact- induced erosion were used by Pham et al. (2011) and de Niem et al. (2012) to investigate the atmospheric balance between erosion and volatile supply during the LHB on Mars, Earth and Venus. Here we follow a similar approach for Titan, combining a pressure-induced ammonia conversion from Sekine et al. (2011) and a parameterization of atmospheric erosion by impact from Shuvalov (2010). To investigate the predominant mechanism that governs the fate of Titan’s atmosphere during the LHB, we combine a stochastic approach for the impactor sampling and we monitor the atmo- spheric mass balance between the supply of N2 and CH4 by both impactor and crustal degassing and atmospheric erosion induced by impact. At pressures and temperatures expected on Titan, part of the supplied volatiles may condense at the surface. To estimate the partitioning between the volatiles in the atmosphere and those condensed at the surface, we implemented the atmo- spheric model developed by Lorenz et al. (1999) including radiative and gas-liquid equilibrium. 2 In the particular case of a pure N2 atmosphere, we use the atmospheric equilibrium constrained from 3D GCM simulations. A detailed description of the model is provided in the following section. Simulations of the evolution of Titan’s atmosphere during the LHB, considering a wide range of initial conditions, are presented in section 3. Implications for the origin and evolution of Titan’s atmosphere are discussed in section 4 and our conclusions are summarized in section 5. 2. Model description 2.1. Model of the atmospheric equilibrium The composition of Titan’s atmosphere may have varied throughout Titan’s history. As the mass and composition of Titan’s atmosphere before the LHB is uncertain, we consider various initial conditions prior to the LHB. The presence of methane in Titan’s atmosphere might only be recent and/or episodic (Tobie et al., 2006; Mandt et al., 2012). It is therefore possible that the atmosphere was composed solely of nitrogen at the time of the LHB. Then we consider either pure N2 or N2-CH4 atmospheres up to 10 times Titan’s present-day atmospheric mass. To model the radiative balance as well as the thermodynamic equilibrium between atmospheric and surface volatile reservoirs, we adopt two different modeling approaches for pure N2 and mixed N2-CH4 atmosphere model as detailed hereafter. 2.1.1. Pure N2 atmosphere In the case of a pure N2 atmosphere, the greenhouse effect is limited to collision-induced absorptions of N2 -N2, as N2 has no absorption band in the infrared and visible (Lorenz et al., 1997; Charnay et al., 2014). Equilibrium temperatures and pressures have been evaluated for surface albebos varying between 0.2 and 0.7 (see Table 1), from full 3D GCM simulations, us- ing the Generic LMDZ code employed and described in Charnay et al. (2014), accounting for Rayleigh scattering by N2 and N2 condensation and precipitation at the surface. These simula- tions showed that the greenhouse effect is counterbalanced by the increase of atmospheric albedo due to Rayleigh diffusion, so that the surface temperature is mostly determined by the surface albedo. Moreover, although the condensation of N2 and the atmospheric pressure are mostly controlled by the pole temperature, the GCM simulations showed that the average surface tem- perature remains a good parameter to predict the average atmospheric pressure and hence the average amount of condensed N2 at the surface. For a surface albedo As lower than 0.68, the sur- face temperature is above the freezing point and atmospheric N2 is in equilibrium with liquid N2 at the surface. For As > 0.68, the atmospheric N2 is in equilibrium with solid N2. Atmospheric pressures displayed in Table 1 correspond to saturation pressures of N2. Any excess of N2 is condensed at the surface. Although latitudinal variations of nitrogen condensation are expected based on GCM simulations (Charnay et al., 2014), we assume a uniform distribution of solids or liquids at the surface, and we consider the average temperature and pressure as representative of the surface conditions.
Recommended publications
  • Application Note 160
    APPLICATION NOTE 160 Degas Options for Sample Preparation Introduction A degas study was conducted to determine the effectiveness 1. Inert environment – shift from of flow versus vacuum degas. An amorphous silica- adsorbed phase to inert. alumina and a microporous zeolite were prepared by both techniques and then nitrogen isotherms were collected 2. Heat – increase the rate. for both materials. The resulting isotherms established equivalence between vacuum versus flow degas. Vacuum versus Flowing Degas Methods In the present study we accept that temperature may be controlled by various methods and that commercial temperature controllers provide repeatable performance. Rather than studying temperature control, this document will evaluate the topic of vacuum versus flowing degas. 1. Vacuum degas utilizes mass action as the only method for shifting the chemical equilibrium. An adsorbed molecule has a concentration on the surface, C and a negligible pressure, P=0 in the vapor phase. The pressure is maintained near zero since the sample is in a vacuum. Heating the sample increases the rate of transfer from the adsorbed molecules to the inert environment. 2. Flowing degas also utilizes mass action Theory by constant inert purge. The desorbed molecules are swept from the system Typical degas options include vacuum or flowing degas. The via the continuous inert gas flow and the basic concept of degas is quite simple. The sample material partial pressure of the desorbed molecules is placed in an inert environment. This inert environment in an inert stream approaches zero in a exploits chemical potential and creates a favorable state for manner similar to the vacuum technique.
    [Show full text]
  • Titan and the Moons of Saturn Telesto Titan
    The Icy Moons and the Extended Habitable Zone Europa Interior Models Other Types of Habitable Zones Water requires heat and pressure to remain stable as a liquid Extended Habitable Zones • You do not need sunlight. • You do need liquid water • You do need an energy source. Saturn and its Satellites • Saturn is nearly twice as far from the Sun as Jupiter • Saturn gets ~30% of Jupiter’s sunlight: It is commensurately colder Prometheus • Saturn has 82 known satellites (plus the rings) • 7 major • 27 regular • 4 Trojan • 55 irregular • Others in rings Titan • Titan is nearly as large as Ganymede Titan and the Moons of Saturn Telesto Titan Prometheus Dione Titan Janus Pandora Enceladus Mimas Rhea Pan • . • . Titan The second-largest moon in the Solar System The only moon with a substantial atmosphere 90% N2 + CH4, Ar, C2H6, C3H8, C2H2, HCN, CO2 Equilibrium Temperatures 2 1/4 Recall that TEQ ~ (L*/d ) Planet Distance (au) TEQ (K) Mercury 0.38 400 Venus 0.72 291 Earth 1.00 247 Mars 1.52 200 Jupiter 5.20 108 Saturn 9.53 80 Uranus 19.2 56 Neptune 30.1 45 The Atmosphere of Titan Pressure: 1.5 bars Temperature: 95 K Condensation sequence: • Jovian Moons: H2O ice • Saturnian Moons: NH3, CH4 2NH3 + sunlight è N2 + 3H2 CH4 + sunlight è CH, CH2 Implications of Methane Free CH4 requires replenishment • Liquid methane on the surface? Hazy atmosphere/clouds may suggest methane/ ethane precipitation. The freezing points of CH4 and C2H6 are 91 and 92K, respectively. (Titan has a mean temperature of 95K) (Liquid natural gas anyone?) This atmosphere may resemble the primordial terrestrial atmosphere.
    [Show full text]
  • Degas Backfill Gas Selection for Micromeritics Gas Adsorption Instruments
    Application Note 73 Degas Backfill Gas Selection for Micromeritics Gas Adsorption Instruments Introduction adsorbed gas is one type of contaminant that you Specific surface areas and pore volume distribu- wish to remove during degassing, using nitrogen tions are often determined using gas adsorption as the backfill gas partially defeats the purpose of techniques. Prior to analysis, any adsorbed gas or degassing. Obviously, nitrogen is not a true inert vapor phase (such as water or other volatiles) gas when it comes to microporous materials. should be removed from the sample. This process is often referred to as degassing the sample. Therefore, for materials which tend to adsorb nitrogen, helium is a better choice as the backfill Degassing usually involves either heating the gas. Helium adsorption at room temperature is sample or flowing an inert gas across the sample negligible, even in the high energy pores of most during evacuation. In either case, molecules being microporous samples. desorbed from the surface of the sample are removed from the sample tube. After degassing, There are some highly microporous materials in the sample tube can be sealed and removed in one which helium (if used as the backfill gas) is ex- of the following conditions: tremely difficult to remove due to diffusion. Complete removal requires great care as well as • Under vacuum using the TranSealTM, an appa- time-consuming tasks. Otherwise its presence can ratus which is inserted into the sample tube. It severely distort an adsorption isotherm. is designed to close when removed from the degassing port and open automatically when For samples where neither nitrogen nor helium are installed on the sample port, maintaining a ideal, a vacuum-sealed transfer is the most vacuum-tight seal.
    [Show full text]
  • Computer Simulation Applied to Studying Continuous Spirit Distillation and Product Quality Control
    View metadata, citation and similar papers at core.ac.uk brought to you by CORE provided by Elsevier - Publisher Connector Food Control 22 (2011) 1592e1603 Contents lists available at ScienceDirect Food Control journal homepage: www.elsevier.com/locate/foodcont Computer simulation applied to studying continuous spirit distillation and product quality control Fabio R.M. Batista, Antonio J.A. Meirelles* Laboratory EXTRAE, Department of Food Engineering, Faculty of Food Engineering, University of Campinas e UNICAMP, Campinas, Brazil article info abstract Article history: This work aims to study continuous spirit distillation by computational simulation, presenting some Received 7 June 2010 strategies of process control to regulate the volatile content. The commercial simulator Aspen (Plus and Received in revised form dynamics) was selected. A standard solution containing ethanol, water and 10 minor components rep- 2 March 2011 resented the wine to be distilled. A careful investigation of the vaporeliquid equilibrium was performed Accepted 8 March 2011 for the simulation of two different industrial plants. The simulation procedure was validated against experimental results collected from an industrial plant for bioethanol distillation. The simulations were Keywords: conducted with and without the presence of a degassing system, in order to evaluate the efficiency of Spirits fi Distillation this system in the control of the volatile content. To improve the ef ciency of the degassing system, fl Simulation a control loop based on a feedback controller was developed. The results showed that re ux ratio and Aspen Plus product flow rate have an important influence on the spirit composition. High reflux ratios and spirit Degassing flow rates allow for better control of spirit contamination.
    [Show full text]
  • Liquid Degassing and Gasification Solutions
    CARBONATION NITROGENATION LIQUID DEGASSING AND DECARBONATION GASIFICATION SOLUTIONS Providing sanitary processing equipment and customized services Since 1885 CO2 Control of Beer Adjust the carbonation level in beer. Sometimes natural fermentation does not create enough CO2 for the end product which impacts taste and the head of a beer. On the same note, removal of excess CO2 in over-carbonated beer is also an easy process. Nitrogenation of Beer There is a niche market for stout beer where nitrogen is added to beer to improve the foam head on top of the beer. Liqui-Cel® Membranes Liqui-Cel membrane contactors are leading gas transfer devices, commonly used in carbon dioxide removal, deoxygenation, nitrogenation and carbonation. Capable of achieving <1 ppm CO2 and <1 ppb O2, they provide precision in gas control. Because of their cleanliness and predictability, Liqui-Cel membranes are the standard degassing technology in ultrapure water applications. Due to the small footprint, lower installation costs and modular nature of the system, they provide flexibility and can be readily expanded to meet growing capacity. Membranes come in multiple sizes so that you can maximize efficiency and performance while taking into account the desired flow rate and footprint requirements. Need more info? Contact your local sales representative or visit our website at www.mgnewell.com. CREATE A SMOOTH BEER—A “KEG” BEER HOW IT WORKS Liqui-Cel membranes use a microporous hollow fiber membrane to add and/or remove gases from liquids. The hollow fiber is knitted into an array and wrapped around a center tube inside of the membrane housing.
    [Show full text]
  • Dupont™ Ligasep™ Degasification Technology Brochure
    Water Solutions DuPont™ Ligasep™ Degasification technology Reliably and Sustainably producing industrial water Introduction Cutting-edge in design, but simple in operation When industrial equipment is in contact with water used Ligasep modules feature a radial flow design that more effectively in a process or as an ingredient, oxygen and carbon dioxide removes gases and have our advanced skinned membranes in that water cause corrosion. at the core. This next-generation approach prevents seepage Degassing this water is essential, and our Ligasep system does of water vapor across the membrane, removing the necessity so precisely and highly autonomously. for a more expensive water-sealed vacuum pump and reducing the risk of failure. As it generates a deeper vacuum, no additional Compared to large and high-maintenance conventional systems, nitrogen is required to further dissolve the oxygen, saving on Ligasep uses advanced membrane technology to take out all the production of N2 and other scavengers. question marks – consuming less energy and chemicals to give industrial producers a precisely engineered, smaller and cost-effective Ligasep is highly flexible, low on OPEX and capable of fast solution that extends their equipment service life and increases start-ups and seamless adaptation to fluctuating flows. process uptime. Easy to maintain, the system is highly automated so you will not need on-site expertise to supervise it. Should the need arise, our technicians are soon on-site to give it a service. Gas Removal Sealing resin Gas Removal Water Outlet N2 Inlet Degassed Water Water Hollow fiber O2 Sealing resin * Water circulate Gas Hollow fiber alongside the Removal exterior of hollow fibers Water Inlet Ligasep uses an intelligent design with two types of membrane for effective O2 & CO2 removal.
    [Show full text]
  • The Lakes and Seas of Titan • Explore Related Articles • Search Keywords Alexander G
    EA44CH04-Hayes ARI 17 May 2016 14:59 ANNUAL REVIEWS Further Click here to view this article's online features: • Download figures as PPT slides • Navigate linked references • Download citations The Lakes and Seas of Titan • Explore related articles • Search keywords Alexander G. Hayes Department of Astronomy and Cornell Center for Astrophysics and Planetary Science, Cornell University, Ithaca, New York 14853; email: [email protected] Annu. Rev. Earth Planet. Sci. 2016. 44:57–83 Keywords First published online as a Review in Advance on Cassini, Saturn, icy satellites, hydrology, hydrocarbons, climate April 27, 2016 The Annual Review of Earth and Planetary Sciences is Abstract online at earth.annualreviews.org Analogous to Earth’s water cycle, Titan’s methane-based hydrologic cycle This article’s doi: supports standing bodies of liquid and drives processes that result in common 10.1146/annurev-earth-060115-012247 Annu. Rev. Earth Planet. Sci. 2016.44:57-83. Downloaded from annualreviews.org morphologic features including dunes, channels, lakes, and seas. Like lakes Access provided by University of Chicago Libraries on 03/07/17. For personal use only. Copyright c 2016 by Annual Reviews. on Earth and early Mars, Titan’s lakes and seas preserve a record of its All rights reserved climate and surface evolution. Unlike on Earth, the volume of liquid exposed on Titan’s surface is only a small fraction of the atmospheric reservoir. The volume and bulk composition of the seas can constrain the age and nature of atmospheric methane, as well as its interaction with surface reservoirs. Similarly, the morphology of lacustrine basins chronicles the history of the polar landscape over multiple temporal and spatial scales.
    [Show full text]
  • Lateral Degassing Method for Disposable Film-Chip Microfluidic
    membranes Article Lateral Degassing Method for Disposable Film-Chip Microfluidic Devices Suhee Park, Hyungseok Cho, Junhyeong Kim and Ki-Ho Han * Center for Nano Manufacturing, Department of Nanoscience and Engineering, Inje University, Gimhae 50834, Gyongnam, Korea; [email protected] (S.P.); [email protected] (H.C.); [email protected] (J.K.) * Correspondence: [email protected] Abstract: It is critical to develop a fast and simple method to remove air bubbles inside microchan- nels for automated, reliable, and reproducible microfluidic devices. As an active degassing method, this study introduces a lateral degassing method that can be easily implemented in disposable film-chip microfluidic devices. This method uses a disposable film-chip microchannel superstrate and a reusable substrate, which can be assembled and disassembled simply by vacuum pressure. The disposable microchannel superstrate is readily fabricated by bonding a microstructured poly- dimethylsiloxane replica and a silicone-coated release polymeric thin film. The reusable substrate can be a plate that has no function or is equipped with the ability to actively manipulate and sense substances in the microchannel by an elaborately patterned energy field. The degassing rate of the lateral degassing method and the maximum available pressure in the microchannel equipped with lateral degassing were evaluated. The usefulness of this method was demonstrated using complex structured microfluidic devices, such as a meandering microchannel, a microvortex, a gradient micromixer, and a herringbone micromixer, which often suffer from bubble formation. In conclusion, as an easy-to-implement and easy-to-use technique, the lateral degassing method will be a key Citation: Park, S.; Cho, H.; Kim, J.; technique to address the bubble formation problem of microfluidic devices.
    [Show full text]
  • Liquid Sulfur Degassing: Fundamentals and New Technology Development
    LIQUID SULPHUR DEGASSING: FUNDAMENTALS AND NEW TECHNOLOGY DEVELOPMENT IN SULPHUR RECOVERY P.D. Clark, Department of Chemistry, University of Calgary and Alberta Sulphur Research Ltd., M.A. Shields, M. Huang and N.I. Dowling, Alberta Sulphur Research Ltd. and D. Cicerone, Cicerone & Associates LLC. Contact: [email protected] Abstract Liquid sulphur degassing remains an important component of a Claus sulphur recovery system as a result of the need to produce high purity liquid and solid sulphur (< 10 ppmw residual H2S). Importantly, this process must be accomplished without increasing plant emissions. At present, several effective technologies exist for sulphur degassing, mostly based on air sparge of the liquid in a variety of contraptions. These processes produce large volumes of air contaminated with sulphur vapour, H2O, H2S and SO2 which, if compressed back into the air supply systems, cause plugging and corrosion problems. Formerly, the contaminated air was flowed to the incinerator but this practice is calculated to lower total sulphur recovery by as much as 0.1 %. One objective of this paper is to review the fundamentals of sulphur degassing with air explaining how H2Sx is decomposed and why SO2 is always produced when air is used. Secondly, new data on liquid sulphur degassing with solid catalysts will be discussed, and it will be explained how this information could be applied to liquid sulphur degassing both upstream and downstream of the sulphur locks. These adaptations will avoid use of air and should improve overall sulphur recovery as well as achieve sulphur degassing. Lastly, it will be shown that modifications to sulphur condensers throughout the plant may allow simultaneous degassing and, possibly, an increase in overall sulphur recovery.
    [Show full text]
  • The Origin of Titan's Atmosphere: Some Recent Advances
    The origin of Titan’s atmosphere: some recent advances By Tobias Owen1 & H. B. Niemann2 1University of Hawaii, Institute for Astronomy, 2680 Woodlawn Drive, Honolulu, HI 96822, USA 2Laboratory for Atmospheres, Goddard Space Fight Center, Greenbelt, MD 20771, USA It is possible to make a consistent story for the origin of Titan’s atmosphere starting with the birth of Titan in the Saturn subnebula. If we use comet nuclei as a model, Titan’s nitrogen and methane could easily have been delivered by the ice that makes up ∼50% of its mass. If Titan’s atmospheric hydrogen is derived from that ice, it is possible that Titan and comet nuclei are in fact made of the same protosolar ice. The noble gas abundances are consistent with relative abundances found in the atmospheres of Mars and Earth, the sun, and the meteorites. Keywords: Origin, atmosphere, composition, noble gases, deuterium 1. Introduction In this note, we will assume that Titan originated in Saturn’s subnebula as a result of the accretion of icy planetesimals: particles and larger lumps made of ice and rock. Alibert & Mousis (2007) reached this same point of view using an evolutionary, turbulent model of Saturn’s subnebula. They found that planetesimals made in the solar nebula according to their model led to a huge overabundance of CO on Titan. We obviously have no direct measurements of the composition of these planetes- imals. We can use comets as a guide, always remembering that comets formed in the solar nebula where conditions must have been different from those in Saturn’s subnebula, e.g., much colder.
    [Show full text]
  • Hydrocarbon Lakes on Titan
    Icarus 186 (2007) 385–394 www.elsevier.com/locate/icarus Hydrocarbon lakes on Titan Giuseppe Mitri a,∗,AdamP.Showmana, Jonathan I. Lunine a,b, Ralph D. Lorenz a,c a Department of Planetary Sciences and Lunar and Planetary Laboratory, University of Arizona, 1629 E. University Blvd., Tucson, AZ 85721-0092, USA b Istituto di Fisica dello Spazio Interplanetario INAF-IFSI, Via del Fosso del Cavaliere, 00133 Rome, Italy c Now at Space Department, Johns Hopkins University Applied Physics Laboratory, 11100 Johns Hopkins Road, Laurel, MD 20723-6099, USA Received 9 March 2006; revised 6 September 2006 Available online 7 November 2006 Abstract The Huygens Probe detected dendritic drainage-like features, methane clouds and a high surface relative humidity (∼50%) on Titan in the vicinity of its landing site [Tomasko, M.G., and 39 colleagues, 2005. Nature 438, 765–778; Niemann, H.B., and 17 colleagues, 2005. Nature 438, 779–784], suggesting sources of methane that replenish this gas against photo- and charged-particle chemical loss on short (10–100) million year timescales [Atreya, S.K., Adams, E.Y., Niemann, H.B., Demick-Montelara, J.E., Owen, T.C., Fulchignoni, M., Ferri, F., Wilson, E.H., 2006. Planet. Space Sci. In press]. On the other hand, Cassini Orbiter remote sensing shows dry and even desert-like landscapes with dunes [Lorenz, R.D., and 39 colleagues, 2006a. Science 312, 724–727], some areas worked by fluvial erosion, but no large-scale bodies of liquid [Elachi, C., and 34 colleagues, 2005. Science 308, 970–974]. Either the atmospheric methane relative humidity is declining in a steady fashion over time, or the sources that maintain the relative humidity are geographically restricted, small, or hidden within the crust itself.
    [Show full text]
  • The Exploration of Titan with an Orbiter and a Lake Probe
    Planetary and Space Science ∎ (∎∎∎∎) ∎∎∎–∎∎∎ Contents lists available at ScienceDirect Planetary and Space Science journal homepage: www.elsevier.com/locate/pss The exploration of Titan with an orbiter and a lake probe Giuseppe Mitri a,n, Athena Coustenis b, Gilbert Fanchini c, Alex G. Hayes d, Luciano Iess e, Krishan Khurana f, Jean-Pierre Lebreton g, Rosaly M. Lopes h, Ralph D. Lorenz i, Rachele Meriggiola e, Maria Luisa Moriconi j, Roberto Orosei k, Christophe Sotin h, Ellen Stofan l, Gabriel Tobie a,m, Tetsuya Tokano n, Federico Tosi o a Université de Nantes, LPGNantes, UMR 6112, 2 rue de la Houssinière, F-44322 Nantes, France b Laboratoire d’Etudes Spatiales et d’Instrumentation en Astrophysique (LESIA), Observatoire de Paris, CNRS, UPMC University Paris 06, University Paris-Diderot, Meudon, France c Smart Structures Solutions S.r.l., Rome, Italy d Center for Radiophysics and Space Research, Cornell University, Ithaca, NY 14853, United States e Dipartimento di Ingegneria Meccanica e Aerospaziale, Università La Sapienza, 00184 Rome, Italy f Institute of Geophysics and Planetary Physics, Department of Earth and Space Sciences, Los Angeles, CA, United States g LPC2E-CNRS & LESIA-Obs., Paris, France h Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA, United States i Johns Hopkins University, Applied Physics Laboratory, Laurel, MD, United States j Istituto di Scienze dell‘Atmosfera e del Clima (ISAC), Consiglio Nazionale delle Ricerche (CNR), Rome, Italy k Istituto di Radioastronomia (IRA), Istituto Nazionale
    [Show full text]