The Pulse of the Volcano: Discovery of Episodic Activity at Prometheus on Io
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Io in the Near Infrared: Near-Infrared Mapping Spectrometer (NIMS) Results from the Galileo Tlybys in 1999 and 2000 Rosaly M
JOURNAL OF GEOPHYSICAL RESEARCH, VOL. 106, NO. El2, PAGES 33,053-33,078, DECEMBER 25, 2001 Io in the near infrared: Near-Infrared Mapping Spectrometer (NIMS) results from the Galileo tlybys in 1999 and 2000 Rosaly M. C. Lopes,• L. W. Kamp,• S. Dout6,2 W. D. Smythe,• R. W. Carlson,• A. S. McEwen, 3 P. E. Geissler,3 S. W. Kieffer, 4 F. E. Leader, s A. G. Davies, • E. Barbinis,• R. Mehlman,s M. Segura,• J. Shirley,• and L. A. Soderblom6 Abstract. Galileo'sNear-Infrared Mapping Spectrometer(NIMS) observedIo duringthe spacecraft'sthree flybysin October 1999, November 1999, and February 2000. The observations,which are summarizedhere, were used to map the detailed thermal structure of activevolcanic regions and the surfacedistribution of SO2 and to investigatethe origin of a yet unidentified compoundshowing an absorptionfeature at ---1 •m. We present a summaryof the observationsand results,focusing on the distributionof thermal emission and of SO2 deposits.We find high eruption temperatures,consistent with ultramafic volcanism,at Pele. Such temperaturesmay be present at other hot spots,but the hottest areas may be too small for those temperaturesto be detected at the spatial resolutionof our observations.Loki is the site of frequent eruptions,and the low thermal emissionmay representlavas cooling on the caldera'ssurface or the coolingcrust of a lava lake. High- resolutionspectral observations of Emakong caldera show thermal emissionand SO2 within the same pixels,implying that patchesof SO2 frost and patchesof coolinglavas or sulfur flows are presentwithin a few kilometersfrom one another. Thermal maps of Prometheusand Amirani showthat these two hot spotsare characterizedby long lava flows.The thermal profilesof flows at both locationsare consistentwith insulatedflows, with the Amirani flow field havingmore breakoutsof fresh lava along its length. -
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. -
Appendix 1: Io's Hot Spots Rosaly M
Appendix 1: Io's hot spots Rosaly M. C. Lopes,Jani Radebaugh,Melissa Meiner,Jason Perry,and Franck Marchis Detections of plumes and hot spots by Galileo, Voyager, HST, and ground-based observations. Notes and sources . (N) NICMOS hot spots detected by Goguen etal . (1998). (D) Hot spots detected by C. Dumas etal . in 1997 and/or 1998 (pers. commun.). Keck are hot spots detected by de Pater etal . (2004) and Marchis etal . (2001) from the Keck telescope using Adaptive Optics. (V, G, C) indicate Voyager, Galileo,orCassini detection. Other ground-based hot spots detected by Spencer etal . (1997a). Galileo PPR detections from Spencer etal . (2000) and Rathbun etal . (2004). Galileo SSIdetections of hot spots, plumes, and surface changes from McEwen etal . (1998, 2000), Geissler etal . (1999, 2004), Kezthelyi etal. (2001), and Turtle etal . (2004). Galileo NIMS detections prior to orbit C30 from Lopes-Gautier etal . (1997, 1999, 2000), Lopes etal . (2001, 2004), and Williams etal . (2004). Locations of surface features are approximate center of caldera or feature. References de Pater, I., F. Marchis, B. A. Macintosh, H. G. Rose, D. Le Mignant, J. R. Graham, and A. G. Davies. 2004. Keck AO observations of Io in and out of eclipse. Icarus, 169, 250±263. 308 Appendix 1: Io's hot spots Goguen, J., A. Lubenow, and A. Storrs. 1998. HST NICMOS images of Io in Jupiter's shadow. Bull. Am. Astron. Assoc., 30, 1120. Geissler, P. E., A. S. McEwen, L. Keszthelyi, R. Lopes-Gautier, J. Granahan, and D. P. Simonelli. 1999. Global color variations on Io. Icarus, 140(2), 265±281. -
Volcanism on Io II Eruption Plumes on Io Ionian Plumes: SO2 Source
Volcanism on Io II GLY 424/524 April 22, 2002 Eruption Plumes on Io Ionian Plumes: SO2 Source • Low gravity, atmospheric pressure • Liquid SO2 “pockets” beneath the surface • Plumes on Io ~60 - 450 km – Superheated upon contact with magma – Old Faithful would be 35 km tall on Io – Boil, erupt • Powered by SO and SO2 • Vertical crustal recycling of SO2 “snow” – Tvashtar plume detected August 2001 and “frost” deposits – 500 km tall • Most plumes from lava flow front rather – Particles determined to be SO2 “snowflakes” than vent – Interaction of hot lava with old SO2 “snow” Sulfur gas (S2 or SO2) lands on the cold surface. Atoms rearrange into (S3, S4), which give the surface a red color. Eventually, S8 forms ordinary pale yellow sulfur. 1 Io Volcanic Styles Io Volcanic Styles Continued • Promethean • Pillanian – Prometheus = type locale – Pillan = type locale • Also Amirani • Also Tvashtar • Zamama • I-31A hot-spot • Culann – Short-lived, high-effusion-rate eruptions – Long-lived, steady eruptions • Large pyroclastic deposits • Produces compound flow field • Open-channel or open-sheet flows • Takes years to decades • Associated with “wandering” plumes • Lava lakes – Extensive plume deposits – Loki = type locale – Extensive, rapidly emplace flows • Also Emakong, Pele, Tupan – High temperatures Prometheus Prometheus Prometheus Prometheus • Io’s “Old Faithful” – Active since 1979 – Observed by Voyager 1 • Eruption Plume – 80 km tall – Plume source migrated 85 km to the west since 1979 • Lava flow – ~100 km long – Apparently originates in caldera 2 Prometheus Caldera & flow-front plume Prometheus Pillan Pele & Pillan April, 1997 September, 1997 July, 1999 12 km/px 5 km/px 12 km/px Pillan ~400 km diameter Pillan eruption • http://www.digitalradiance.com/sng/Io_volc ano.htm 3 Pillan Lava flows High-res images near Pillan Patera 7.2 km long ~9 m/pixel Pillan lava flows; 19 m/px Tvashtar Bright regions are saturated pixels, indicating HOT fire- fountaining on Io Temps >1600K F.o.v. -
Page 1 57° 50° 40° 30° 20° 10° 0° -10° -20° -30° -40° -50° -57° 57° 50
180° 0° DODONA PLANUM 210° 330° 150° 30° 60° -60° . Bochica . Hatchawa Patera Patera . Nusku Patera . Hiruko Heno . Inti . Patera Patera Patera 70° -70° 240° 300° 60° 120° Tvashtar . Taranis Patera Iynx TARSUS Aramazd Mensa . Patera Tvashtar Paterae Haemus REGIO Montes Mensae LERNA REGIO 80° Echo -80°Mensa . Chors Nile Montes N Patera E M . Viracocha E Patera A 90° CHALYBES 270° 90° P 270° L A . Mithra N Patera U REGIO M . Vivasvant Patera . Crimea Mons 80° -80° Pyerun . Patera Dazhbog 120° 60° Patera . 300° 240° 70° -70° ILLYRIKON REGIO 60° -60° 30° 150° 330° 210° 0° 180° NORTH POLAR REGION SOUTH POLAR REGION 180° 170° 160° 150° 140° 130° 120° 110° 100° 90° 80° 70° 60° 50° 40° 30° 20° 10° 0° 350° 340° 330° 320° 310° 300° 290° 280° 270° 260° 250° 240° 230° 220° 210° 200° 190° 180° 57° 57° Nile Montes Dazhbog Patera CHALYBES REGIO 50° 50° . Kinich Ahau . Savitr Patera Patera Surt Zal Montes Lei-Kung Zal Fluctus . Fo Patera 40° 40° Patera Thor . Amaterasu . Dusura Patera Patera BULICAME . Manua Patera Shango REGIO Arinna . _ Patera Ukko . Atar Fluctus . Patera Patera Heiseb Isum 30° . 30° Fuchi Patera Patera Reshef Euxine . Patera Mons Patera Volund . Thomagata Amirani Patera . Shakuru Skythia Mons Girru . Mongibello . Tiermes Patera . Susanoo Donar Surya Estan Patera Patera . Patera Mons Patera Fluctus Patera Monan Daedalus 20° . Patera Loki . 20° Zamama Maui . Gish Bar Patera Mons Mulungu Steropes Maui . Patera . Patera Ruaumoko . Camaxtli Patera Gish Bar Sobo Patera . Patera Patera Fluctus Monan Loki Chaac . Ababinili Tien Mu Mons Llew . Balder Patera . Fjorgynn Patera . -
IO CONTROL POINTS and the ELEVATION of GEOLOGICAL FEATURES. P. Schuster1, J. Oberst1, A. Hoffmeister1,, G. Neukum1 and the Galil
Lunar and Planetary Science XXXI 2043.pdf IO CONTROL POINTS AND THE ELEVATION OF GEOLOGICAL FEATURES. P. Schuster1, J. Oberst1, A. Hoffmeister1,, G. Neukum1 and the Galileo SSI Team, 1DLR, Institute of Space Sensors and Planetary Exploration, 12484 Berlin, Germany, e-mail: [email protected]. Introduction There are several ways to study the topography on Io. Shadow measurements [1], photoclinometric techniques [2], and stereophotogrammetry [3,4,5] are typically used for geological studies of the surface. In contrast, control net calculations [6,7] or limb measurements [8] are traditionally more often used to study the global shape and geodesy of this Galilean satellite. In this study, we focus on the control point network method. With images from the GEM, the quality of the Io control point network has greatly improved. We attempted to generate control points in the areas of known geological features, e.g. mountains and active plume centers, to demonstrate that control point heights can be used to study the morphology of geological features. Images and Control Points Images obtained during the GEM, allowed us to recently update our control net, spanning over 360 degrees of Fig.1: Boösaule Mons, control points longitude and ranging from +60 to -60 degrees latitude. ———————————————————————— The polar latitudes were not accessible for this study, Point 1 2 3 4 5 6 because Galileos orbit was essentially equatorial and ———————————————————————— measurements to closer than 30 degrees to the limb proved Elevation [km] 8.8 14.6 15.8 2.1 -2.0 1.6 to be inaccurate. Error [km] 2.9 2.9 2.9 2.9 2.9 2.9 We selected 26 images (out of a total of several hundred) ———————————————————————— with resolutions ranging from 2.4 to 15.3 from orbits 1-22. -
Numerical Modeling of Ionian Volcanic Plumes with Entrained Particulates
Icarus 172 (2004) 479–502 www.elsevier.com/locate/icarus Numerical modeling of ionian volcanic plumes with entrained particulates J. Zhang ∗, D.B. Goldstein, P.L. Varghese, L. Trafton, C. Moore, K. Miki Department of Aerospace Engineering, The University of Texas at Austin, 1 University Station, C0600, Austin, TX 78712-0235, USA Received 18 November 2003; revised 27 May 2004 Available online 12 September 2004 Abstract Volcanic plumes on Jupiter’s moon Io are modeled using the direct simulation Monte Carlo (DSMC) method. The modeled volcanic vent is interpreted as a “virtual” vent. A parametric study of the “virtual” vent gas temperature and velocity is performed to constrain the gas properties at the vent by observables, particularly the plume height and the surrounding condensate deposition ring radius. Also, the flow of refractory nano-size particulates entrained in the gas is modeled with “overlay” techniques which assume that the background gas flow is not altered by the particulates. The column density along the tangential line-of-sight and the shadow cast by the plume are calculated and compared with Voyager and Galileo images. The parametric study indicates that it is possible to obtain a unique solution for the vent temperature and velocity for a large plume like Pele. However, for a small Prometheus-type plume, several different possible combinations of vent temperature and velocity result in both the same shock height and peak deposition ring radius. Pele and Prometheus plume particulates are examined in detail. Encouraging matches with observations are obtained for each plume by varying both the gas and particle parameters. -
Active Volcanism on Io: Global Distribution and Variations in Activity
Icarus 140, 243–264 (1999) Article ID icar.1999.6129, available online at http://www.idealibrary.com on Active Volcanism on Io: Global Distribution and Variations in Activity Rosaly Lopes-Gautier Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California 91109 E-mail: [email protected] Alfred S. McEwen Department of Planetary Sciences, Lunar and Planetary Laboratory, University of Arizona, P. O. Box 210092, Tucson, Arizona 85721-0092 William B. Smythe Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California 91109 P. E. Geissler Department of Planetary Sciences, Lunar and Planetary Laboratory, University of Arizona, P. O. Box 210092, Tucson, Arizona 85721-0092 L. Kamp and A. G. Davies Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California 91109 J. R. Spencer Lowell Observatory, Flagstaff, Arizona 86001 L. Keszthelyi Department of Planetary Sciences, Lunar and Planetary Laboratory, University of Arizona, P. O. Box 210092, Tucson, Arizona 85721-0092 R. Carlson Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California 91109 F. E. Leader and R. Mehlman Institute of Geophysics and Planetary Physics, University of California—Los Angeles, Los Angeles, California 90095 L. Soderblom Branch of Astrogeologic Studies, U.S. Geological Survey, Flagstaff, Arizona 86001 and The Galileo NIMS and SSI Teams Received June 23, 1998; revised February 10, 1999 in 1979. A total of 61 active volcanic centers have been identified Io’s volcanic activity has been monitored by instruments aboard from Voyager, groundbased, and Galileo observations. Of these, 41 the Galileo spacecraft since June 28, 1996. We present results from are hot spots detected by NIMS and/or SSI. -
Nuclear Power to Advance Space Exploration Gary L
Poster Paper P. 7.7 First Flights: Nuclear Power to Advance Space Exploration Gary L. Bennett E. W. Johnson Metaspace Enterprises EWJ Enterprises Emmett, Idaho Centerville, Ohio International Air & Space Symposium and Exposition Dayton Convention Center 14-17 July 2003 Dayton, Ohio USA r ... penni.. l .. 10 p~bli . h ..... ..,."b ll .~, ... ~ t .d til. <Op)'rigbt 0 ........ aomod oa tho fin' po_" ...... A1M.IIdd ..., yri ,hl, ... rit< .. AIM hrmi.. lou Dop a_I, 18(11 AI . ..od ... B<l1 Ori .... S.11e SIlO , R.stu. VA. 20191""-i44 FIRST FLIGHTS: NUCLEAR POWER TO ADVANCE SPACE EXPLORATION Gary L. Bennett E. W. Johnson Metaspace Enterprises EWJ Enterprises 5000 Butte Road 1017 Glen Arbor Court Emmett, Idaho 83617-9500 Centerville, Ohio 45459-5421 Tel/Fax: 1+208.365.1210 Telephone: 1+937.435.2971 E-mail: [email protected] E-mail: [email protected] Abstract One of the 20th century's breakthroughs that enabled and/or enhanced challenging space flights was the development of nuclear power sources for space applications. Nuclear power sources have allowed spacecraft to fly into regions where sunlight is dim or virtually nonexistent. Nuclear power sources have enabled spacecraft to perform extended missions that would have been impossible with more conventional power sources (e.g., photovoltaics and batteries). It is fitting in the year of the 100th anniversary of the first powered flight to consider the advancements made in space nuclear power as a natural extension of those first flights at Kitty Hawk to extending human presence into the Solar System and beyond. Programs were initiated in the mid 1950s to develop both radioisotope and nuclear reactor power sources for space applications. -
Voyage to Jupiter. INSTITUTION National Aeronautics and Space Administration, Washington, DC
DOCUMENT RESUME ED 312 131 SE 050 900 AUTHOR Morrison, David; Samz, Jane TITLE Voyage to Jupiter. INSTITUTION National Aeronautics and Space Administration, Washington, DC. Scientific and Technical Information Branch. REPORT NO NASA-SP-439 PUB DATE 80 NOTE 208p.; Colored photographs and drawings may not reproduce well. AVAILABLE FROMSuperintendent of Documents, U.S. Government Printing Office, Washington, DC 20402 ($9.00). PUB TYPE Reports - Descriptive (141) EDRS PRICE MF01/PC09 Plus Postage. DESCRIPTORS Aerospace Technology; *Astronomy; Satellites (Aerospace); Science Materials; *Science Programs; *Scientific Research; Scientists; *Space Exploration; *Space Sciences IDENTIFIERS *Jupiter; National Aeronautics and Space Administration; *Voyager Mission ABSTRACT This publication illustrates the features of Jupiter and its family of satellites pictured by the Pioneer and the Voyager missions. Chapters included are:(1) "The Jovian System" (describing the history of astronomy);(2) "Pioneers to Jupiter" (outlining the Pioneer Mission); (3) "The Voyager Mission"; (4) "Science and Scientsts" (listing 11 science investigations and the scientists in the Voyager Mission);.(5) "The Voyage to Jupiter--Cetting There" (describing the launch and encounter phase);(6) 'The First Encounter" (showing pictures of Io and Callisto); (7) "The Second Encounter: More Surprises from the 'Land' of the Giant" (including pictures of Ganymede and Europa); (8) "Jupiter--King of the Planets" (describing the weather, magnetosphere, and rings of Jupiter); (9) "Four New Worlds" (discussing the nature of the four satellites); and (10) "Return to Jupiter" (providing future plans for Jupiter exploration). Pictorial maps of the Galilean satellites, a list of Voyager science teams, and a list of the Voyager management team are appended. Eight technical and 12 non-technical references are provided as additional readings. -
O Lunar and Planetary Institute Provided by the NASA Astrophysics Data System LPSC XXI 1183
1182 LPSC SSI DISK-RESOLVED GROUND BASED INFRARED IMAGING OF 10; J.R. Spencer, M.A. Shure, M.E. Ressler, D. Toomey, A. DeNault, W.M. Sinton, U. Hawaii, J.D. Goguen, J.P.L. Using the new InSb 1-5 pm camera "ProtoCAM" developed by the NASA Infrared Telescope Fzcility, we have obtained the first disk-resolved infrared images of 10. The observations were made at the 3.0-m IRTF on Mauna Kea on the nights of 22-24 December UT, during an engineering run. ProtoCAM was operated with a plate scale of 0.136 arcsec/pixel, stellar images indicate a consistent image FWHM of 0.4 arcsec or better on all three nights. This is close to the IRTF diffraction limit and diffraction rings are visible in some images (e.g., Fig. 3, top). Sunlit images of 10 beyond 3 pm (Fig. 1) clearly show the major volcano Loki as a point source against the visible disk (angular diameter 1.2 arcsec), changing position as 10 rotates. We obtained broadband images centered on 2.2 pm, 3.4 pm, and 3.8 pm, and narrowband CVF images at 3.40 pm, 3.90 pm, 4.08 pm, in the strong SOz absorption band, and at 4.80 pm The brightness of Loki relative to 10's disk increases with increasing wavelength but the disk is still discernable at 4.80 microns. The location of Loki on the disk is consistent with the hotspot location determined by Voyager and subsequent ground-based observations [speckle, (I), Callisto occultations (2), and polarimetry (3)]. -
Multi-Body Mission Design in the Saturnian System with Emphasis on Enceladus Accessibility
MULTI-BODY MISSION DESIGN IN THE SATURNIAN SYSTEM WITH EMPHASIS ON ENCELADUS ACCESSIBILITY A Thesis Submitted to the Faculty of Purdue University by Todd S. Brown In Partial Fulfillment of the Requirements for the Degree of Master of Science December 2008 Purdue University West Lafayette, Indiana ii “My Guide and I crossed over and began to mount that little known and lightless road to ascend into the shining world again. He first, I second, without thought of rest we climbed the dark until we reached the point where a round opening brought in sight the blest and beauteous shining of the Heavenly cars. And we walked out once more beneath the Stars.” -Dante Alighieri (The Inferno) Like Dante, I could not have followed the path to this point in my life without the tireless aid of a guiding hand. I owe all my thanks to the boundless support I have received from my parents. They have never sacrificed an opportunity to help me to grow into a better person, and all that I know of success, I learned from them. I’m eternally grateful that their love and nurturing, and I’m also grateful that they instilled a passion for learning in me, that I carry to this day. I also thank my sister, Alayne, who has always been the role-model that I strove to emulate. iii ACKNOWLEDGMENTS I would like to acknowledge and extend my thanks my academic advisor, Professor Kathleen Howell, for both pointing me in the right direction and giving me the freedom to approach my research at my own pace.