Surface Water-Ice Deposits in the Northern Shadowed Regions of Ceres
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Modelling and the Transit of Venus
Modelling and the transit of Venus Dave Quinn University of Queensland <[email protected]> Ron Berry University of Queensland <[email protected]> Introduction enior secondary mathematics students could justifiably question the rele- Svance of subject matter they are being required to understand. One response to this is to place the learning experience within a context that clearly demonstrates a non-trivial application of the material, and which thereby provides a definite purpose for the mathematical tools under consid- eration. This neatly complements a requirement of mathematics syllabi (for example, Queensland Board of Senior Secondary School Studies, 2001), which are placing increasing emphasis on the ability of students to apply mathematical thinking to the task of modelling real situations. Success in this endeavour requires that a process for developing a mathematical model be taught explicitly (Galbraith & Clatworthy, 1991), and that sufficient opportu- nities are provided to students to engage them in that process so that when they are confronted by an apparently complex situation they have the think- ing and operational skills, as well as the disposition, to enable them to proceed. The modelling process can be seen as an iterative sequence of stages (not ) necessarily distinctly delineated) that convert a physical situation into a math- 1 ( ematical formulation that allows relationships to be defined, variables to be 0 2 l manipulated, and results to be obtained, which can then be interpreted and a n r verified as to their accuracy (Galbraith & Clatworthy, 1991; Mason & Davis, u o J 1991). The process is iterative because often, at this point, limitations, inac- s c i t curacies and/or invalid assumptions are identified which necessitate a m refinement of the model, or perhaps even a reassessment of the question for e h t which we are seeking an answer. -
New Voyage to Rendezvous with a Small Asteroid Rotating with a Short Period
Hayabusa2 Extended Mission: New Voyage to Rendezvous with a Small Asteroid Rotating with a Short Period M. Hirabayashi1, Y. Mimasu2, N. Sakatani3, S. Watanabe4, Y. Tsuda2, T. Saiki2, S. Kikuchi2, T. Kouyama5, M. Yoshikawa2, S. Tanaka2, S. Nakazawa2, Y. Takei2, F. Terui2, H. Takeuchi2, A. Fujii2, T. Iwata2, K. Tsumura6, S. Matsuura7, Y. Shimaki2, S. Urakawa8, Y. Ishibashi9, S. Hasegawa2, M. Ishiguro10, D. Kuroda11, S. Okumura8, S. Sugita12, T. Okada2, S. Kameda3, S. Kamata13, A. Higuchi14, H. Senshu15, H. Noda16, K. Matsumoto16, R. Suetsugu17, T. Hirai15, K. Kitazato18, D. Farnocchia19, S.P. Naidu19, D.J. Tholen20, C.W. Hergenrother21, R.J. Whiteley22, N. A. Moskovitz23, P.A. Abell24, and the Hayabusa2 extended mission study group. 1Auburn University, Auburn, AL, USA ([email protected]) 2Japan Aerospace Exploration Agency, Kanagawa, Japan 3Rikkyo University, Tokyo, Japan 4Nagoya University, Aichi, Japan 5National Institute of Advanced Industrial Science and Technology, Tokyo, Japan 6Tokyo City University, Tokyo, Japan 7Kwansei Gakuin University, Hyogo, Japan 8Japan Spaceguard Association, Okayama, Japan 9Hosei University, Tokyo, Japan 10Seoul National University, Seoul, South Korea 11Kyoto University, Kyoto, Japan 12University of Tokyo, Tokyo, Japan 13Hokkaido University, Hokkaido, Japan 14University of Occupational and Environmental Health, Fukuoka, Japan 15Chiba Institute of Technology, Chiba, Japan 16National Astronomical Observatory of Japan, Iwate, Japan 17National Institute of Technology, Oshima College, Yamaguchi, Japan 18University of Aizu, Fukushima, Japan 19Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA, USA 20University of Hawai’i, Manoa, HI, USA 21University of Arizona, Tucson, AZ, USA 22Asgard Research, Denver, CO, USA 23Lowell Observatory, Flagstaff, AZ, USA 24NASA Johnson Space Center, Houston, TX, USA 1 Highlights 1. -
EPSC2012-280 2012 European Planetary Science Congress 2012 Eeuropeapn Planetarsy Science Ccongress C Author(S) 2012
EPSC Abstracts Vol. 7 EPSC2012-280 2012 European Planetary Science Congress 2012 EEuropeaPn PlanetarSy Science CCongress c Author(s) 2012 A Simulation of exosphere of Ceres Ruby Lin Tu (1), Wing-Huen Ip(1,2,3) and Yung-Ching Wang (3) (1) Institute of Space Science, National Central University, Taiwan, (2) Institute of Astronomy, National Central University, Taiwan, (3) Space Science Institute, Macau University Science and Technology, Macau Abstract For the purpose of tracing the ballistic trajectories of water molecules on Ceres’ surface, we have to After Vesta, the NASA Dawn spacecraft will visit the produce a surface temperature map by omitting the largest asteroid Ceres, to carry out in-depth topographic variations and the presence of impact observations of its surface morphology and craters. Our model solves the heat conduction mineralogical composition. We examine different equation by taking account of the energy balance source mechanisms of a possible surface-bounded condition at the surface boundary and the lower exosphere composed of water molecules and other boundary condition (with dT/dz=0) into account. In species. Our preliminary assessment is that solar between the heat diffusion equation is solved by wind interaction and meteoroid impact are not using the Crank-Nicolson finite difference routine adequate because of the large injection speed of the gas at production relative to the surface escape velocity of Ceres. One potential source is a low-level (1) outgassing effect from its subsurface due to thermal sublimation. In this work, the scenario of building up a tenuous exosphere by ballistic transport and the eventual recycling of the water molecules to the polar cold trap is described. -
Icarus 316 (2018) 63–83
Icarus 316 (2018) 63–83 Contents lists available at ScienceDirect Icarus journal homepage: www.elsevier.com/locate/icarus The Ac-5 (Fejokoo) quadrangle of Ceres: Geologic map and geomorphological evidence for ground ice me diate d surface processes ∗ Kynan H.G. Hughson a, , C.T. Russell a, D.A. Williams b, D.L. Buczkowski c, S.C. Mest d, J.H. Pasckert e, J.E.C. Scully f, J.-P. Combe g, T. Platz d,h, O. Ruesch i, F. Preusker j, R. Jaumann j, A. Nass j, T. Roatsch j, A. Nathues h, M. Schaefer h, B.E. Schmidt k, H.T. Chilton k, A. Ermakov f, S. Singh g, L.A. McFadden i, C.A. Raymond f a Department of Earth, Planetary, and Space Sciences, University of California Los Angeles, 595 Charles E. Young Drive East, Los Angeles, CA 90095, USA b School of Earth and Space Exploration, Arizona State University, PO Box 871404, Tempe, AZ 85287-1404, USA c Johns Hopkins University Applied Physics Laboratory, 11100 Johns Hopkins Rd, Laurel, MD 20723, USA d Planetary Science Institute, 1700 E Fort Lowell Rd # 106, Tucson, AZ 85719, USA e University of Münster, Schlossplatz 2, 48149 Münster, Germany f Jet Propulsion Laboratory, 4800 Oak Grove Dr, Pasadena, CA 91109, USA g Bear Fight Institute, 22 Fiddler’s Rd, Winthrop, WA 98862, USA h Max Planck Institute for Solar System Research, Justus-von-Liebig-Weg 3, 37077 Göttingen, Germany i NASA Goddard Space Flight Center, 8800 Greenbelt Rd, Greenbelt, MD 20771, USA j German Aerospace Center (DLR), Friedrichstraße 171, 10117 Berlin, Germany k School of Earth ans Atmospheric Sciences, Georgia Institute of Technology, 311 Ferst Dr, Atlanta, GA 30318, USA a r t i c l e i n f o a b s t r a c t Article history: NASA’s Dawn spacecraft arrived at Ceres on March 6, 2015, and has been studying the dwarf planet Received 10 August 2016 through a series of successively lower orbits. -
Predictable Patterns in Planetary Transit Timing Variations and Transit Duration Variations Due to Exomoons
Astronomy & Astrophysics manuscript no. ms c ESO 2016 June 21, 2016 Predictable patterns in planetary transit timing variations and transit duration variations due to exomoons René Heller1, Michael Hippke2, Ben Placek3, Daniel Angerhausen4, 5, and Eric Agol6, 7 1 Max Planck Institute for Solar System Research, Justus-von-Liebig-Weg 3, 37077 Göttingen, Germany; [email protected] 2 Luiter Straße 21b, 47506 Neukirchen-Vluyn, Germany; [email protected] 3 Center for Science and Technology, Schenectady County Community College, Schenectady, NY 12305, USA; [email protected] 4 NASA Goddard Space Flight Center, Greenbelt, MD 20771, USA; [email protected] 5 USRA NASA Postdoctoral Program Fellow, NASA Goddard Space Flight Center, 8800 Greenbelt Road, Greenbelt, MD 20771, USA 6 Astronomy Department, University of Washington, Seattle, WA 98195, USA; [email protected] 7 NASA Astrobiology Institute’s Virtual Planetary Laboratory, Seattle, WA 98195, USA Received 22 March 2016; Accepted 12 April 2016 ABSTRACT We present new ways to identify single and multiple moons around extrasolar planets using planetary transit timing variations (TTVs) and transit duration variations (TDVs). For planets with one moon, measurements from successive transits exhibit a hitherto unde- scribed pattern in the TTV-TDV diagram, originating from the stroboscopic sampling of the planet’s orbit around the planet–moon barycenter. This pattern is fully determined and analytically predictable after three consecutive transits. The more measurements become available, the more the TTV-TDV diagram approaches an ellipse. For planets with multi-moons in orbital mean motion reso- nance (MMR), like the Galilean moon system, the pattern is much more complex and addressed numerically in this report. -
Lunar & Planetary Surface Power Management & Distribution
NASA SBIR 2020 Phase I Solicitation Z1.05 Lunar & Planetary Surface Power Management & Distribution Lead Center: GRC Participating Center(s): GSFC, JSC Technology Area: TA3 Space Power and Energy Storage Scope Title Innovative ways to transmit high power for lunar & Mars surface missions Scope Description The Global Exploration Roadmap (January 2018) and the Space Policy Directive (December 2017) detail NASA’s plans for future human-rated space missions. A major factor in this involves establishing bases on the lunar surface and eventually Mars. Surface power for bases is envisioned to be located remotely from the habitat modules and must be efficiently transferred over significant distances. The International Space Station (ISS) has the highest power (100kW), and largest space power distribution system with eight interleaved micro-grids providing power functions similar to a terrestrial power utility. Planetary bases will be similar to the ISS with expectations of multiple power sources, storage, science, and habitation modules, but at higher power levels and with longer distribution networks providing interconnection. In order to enable high power (>100kW) and longer distribution systems on the surface of the moon or Mars, NASA is in need of innovative technologies in the areas of lower mass/higher efficiency power electronic regulators, switchgear, cabling, connectors, wireless sensors, power beaming, power scavenging, and power management control. The technologies of interest would need to operate in extreme temperature environments, including lunar night, and could experience temperature changes from -153C to 123C for lunar applications, and -125C to 80C for Mars bases. In addition to temperature extremes, technologies would need to withstand (have minimal degradation from) lunar dust/regolith, Mars dust storms, and space radiation levels. -
Ceres Survey Atlas Derived from Dawn Framing Camera Images
Planetary and Space Science ∎ (∎∎∎∎) ∎∎∎–∎∎∎ Contents lists available at ScienceDirect Planetary and Space Science journal homepage: www.elsevier.com/locate/pss Ceres Survey Atlas derived from Dawn Framing Camera images Th. Roatsch a,n, E. Kersten a, K.-D. Matz a, F. Preusker a, F. Scholten a, R. Jaumann a, C.A. Raymond b, C.T. Russell c a Institute of Planetary Research, German Aerospace Center (DLR), Berlin, Germany b Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA, USA c Institute of Geophysics, UCLA, Los Angeles, CA, USA article info abstract Article history: The Dawn Framing Camera (FC) acquired almost 900 clear filter images of Ceres with a resolution of Received 10 November 2015 about 400 m/pixels during the seven cycles in the Survey orbit in June 2015. We ortho-rectified 42 Received in revised form images from the third cycle and produced a global, high-resolution, controlled mosaic of Ceres. This 26 November 2015 global mosaic is the basis for a high-resolution Ceres atlas that consists of 3 tiles mapped at a scale of Accepted 16 December 2015 1:2,000,000. The nomenclature used in this atlas was proposed by the Dawn team and was approved by the International Astronomical Union (IAU). The whole atlas is available to the public through the Dawn Keywords: GIS web page [http://dawn_gis.dlr.de/atlas]. Dawn & 2015 Elsevier Ltd. All rights reserved. Ceres Dwarf planets Planetary mapping 1. Introduction followed by the radiometric calibration of the images (Schröder et al., 2013,2014). The Dawn mission has mapped Ceres during the Survey orbit The next step towards the cartographic products is to ortho- phase from an altitude of 4424 km (Russell and Raymond, 2011)in rectify the images to the proper scale and map projection type. -
(Unin)Habitable? Runaway Greenhouse
GEOS 22060/ GEOS 32060 / ASTR 45900 What makes a planet (unin)habitable? Runaway greenhouse Lecture 8 Tuesday 30 April 2019 Logiscs • Homework 1 and Homework 2 are graded • Homework 3 will be issued on Wed or Thu and due on Fri 10 • Total number of homeworks will be 6 (hopefully 7) • Midterm feedback form results: Course outline Founda6ons (1-2 weeks) • Earth history • HZ concept, atmospheric science essenEals • Post-Hadean Earth system Principles – how are habitable planets ini6ated and sustained? (4-5 weeks) • Volale supply, volale escape TODAY • Runaway greenhouse, moist greenhouse • Long-term climate evoluEon • Specifics (2.5 weeks) • Hyperthermals on Earth Earth science • Early Mars • Oceans within ice-covered moons • Exoplanetary systems e.g. TRAPPIST-1 system planetary science Lecture 7 wrap-up • Energy-limit: XUV driven escape more-likely- than-not sculpts the exoplanet radius-period distribuEon (‘photo-evaporaon valley’) • Diffusion limit: what regulates H loss from Venus, Earth and Mars today • Impact erosion – giant impacts and planetesimal impacts Wrap-up: impact erosion Nuclear tests Hydrocode Terrestrial impact craters Two-stage gas gun Formaon of Earth-sized planets involves giant (oligarchic) impacts. Masses of resulEng planets (Earths) * = giant impacts The output underlying this plot was generated by C. Cossou. The Moon-forming Simula8on intended to impact was not reproduce “typical” the last big impact Kepler system of short-period, on Earth, but it was 8ghtly-packed inner planets the last Eme that Earth hit another planet. The atmosphere-loss escape efficiency of giant impacts is set by the ground-moEon speed Schlichng & Mukhopadhay 2018 Ocean removal by giant impacts? (Ocean vaporizaon != ocean removal) Simulaons suggest that the Moon- forming impact was marginally able to remove any pre-exisEng Earth ocean 2 Qs ~ ve for oligarchic impact Stewart et al. -
Water Loss from Terrestrial Planets with CO2-Rich Atmospheres
Water loss from terrestrial planets with CO2-rich atmospheres R. D. Wordsworth Department of the Geophysical Sciences, University of Chicago, 60637 IL, USA [email protected] and R. T. Pierrehumbert Department of the Geophysical Sciences, University of Chicago, 60637 IL, USA ABSTRACT Water photolysis and hydrogen loss from the upper atmospheres of terrestrial planets is of fundamental importance to climate evolution but remains poorly understood in general. Here we present a range of calculations we performed to study the dependence of water loss rates from terrestrial planets on a range of atmospheric and external parameters. We show that CO2 can only cause sig- nificant water loss by increasing surface temperatures over a narrow range of conditions, with cooling of the middle and upper atmosphere acting as a bottle- neck on escape in other circumstances. Around G-stars, efficient loss only occurs on planets with intermediate CO2 atmospheric partial pressures (0.1 to 1 bar) that receive a net flux close to the critical runaway greenhouse limit. Because G-star total luminosity increases with time but XUV/UV luminosity decreases, this places strong limits on water loss for planets like Earth. In contrast, for a CO2-rich early Venus, diffusion limits on water loss are only important if clouds caused strong cooling, implying that scenarios where the planet never had surface liquid water are indeed plausible. Around M-stars, water loss is primarily a func- arXiv:1306.3266v2 [astro-ph.EP] 12 Oct 2013 tion of orbital distance, with planets that absorb less flux than ∼ 270 W m−2 (global mean) unlikely to lose more than one Earth ocean of H2O over their lifetimes unless they lose all their atmospheric N2/CO2 early on. -
A Disintegrating Minor Planet Transiting a White Dwarf!
A Disintegrating Minor Planet Transiting a White Dwarf! Andrew Vanderburg1, John Asher Johnson1, Saul Rappaport2, Allyson Bieryla1, Jonathan Irwin1, John Arban Lewis1, David Kipping1,3, Warren R. Brown1, Patrick Dufour4, David R. Ciardi5, Ruth Angus1,6, Laura Schaefer1, David W. Latham1, David Charbonneau1, Charles Beichman5, Jason Eastman1, Nate McCrady7, Robert A. Wittenmyer8, & Jason T. Wright9,10. ! White dwarfs are the end state of most stars, including We initiated follow-up ground-based photometry to the Sun, after they exhaust their nuclear fuel. Between better time-resolve the transits seen in the K2 data (Figure 1/4 and 1/2 of white dwarfs have elements heavier than S1). We observed WD 1145+017 frequently over the course helium in their atmospheres1,2, even though these of about a month with the 1.2-meter telescope at the Fred L. elements should rapidly settle into the stellar interiors Whipple Observatory (FLWO) on Mt. Hopkins, Arizona; unless they are occasionally replenished3–5. The one of the 0.7-meter MINERVA telescopes, also at FLWO; abundance ratios of heavy elements in white dwarf and four of the eight 0.4-meter telescopes that compose the atmospheres are similar to rocky bodies in the Solar MEarth-South Array at Cerro Tololo Inter-American system6,7. This and the existence of warm dusty debris Observatory in Chile. Most of these data showed no disks8–13 around about 4% of white dwarfs14–16 suggest interesting or significant signals, but on two nights we that rocky debris from white dwarf progenitors’ observed deep (up to 40%), short-duration (5 minutes), planetary systems occasionally pollute the stars’ asymmetric transits separated by the dominant 4.5 hour atmospheres17. -
Icebreaker: a Lunar South Pole Exploring Robot Cmu-Ri-Tr-97-22
ICEBREAKER: A LUNAR SOUTH POLE EXPLORING ROBOT CMU-RI-TR-97-22 Matthew C. Deans Alex D. Foessel Gregory A. Fries Diana LaBelle N. Keith Lay Stewart Moorehead Ben Shamah Kimberly J. Shillcutt Professor: Dr. William Whittaker The Robotics Institute Carnegie Mellon University Pittsburgh PA 15213 Spring 1996-97 Executive Summary Icebreaker: A Lunar South Pole Exploring Robot Due to the low angles of sunlight at the lunar poles, craters and other depressions in the polar regions can contain areas which are in permanent darkness and are at cryogenic temperatures. Many scientists have theorized that these cold traps could contain large quantities of frozen volatiles such as water and carbon dioxide which have been deposited over billions of years by comets, meteors and solar wind. Recent bistatic radar data from the Clementine mission has yielded results consistent with water ice at the South Pole of the Moon however Earth based observations from the Arecibo Radar Observatory indicate that ice may not exist. Due to the controversy surrounding orbital and Earth based observations, the only way to definitively answer the question of whether ice exists on the Lunar South Pole is in situ analysis. The discovery of water ice and other volatiles on the Moon has many important benefits. First, this would provide a source of rocket fuel which could be used to power rockets to Earth, Mars or beyond, avoiding the high cost of Earth based launches. Secondly, water and carbon dioxide along with nitrogen from ammonia form the essential elements for life and could be used to help support human colonies on the Moon. -
Contents JUPITER Transits
1 Contents JUPITER Transits..........................................................................................................5 JUPITER Conjunct Sun..............................................................................................6 JUPITER Opposite Sun............................................................................................10 JUPITER Sextile Sun...............................................................................................14 JUPITER Square Sun...............................................................................................17 JUPITER Trine Sun..................................................................................................20 JUPITER Conjunct Moon.........................................................................................23 JUPITER Opposite Moon.........................................................................................28 JUPITER Sextile Moon.............................................................................................32 JUPITER Square Moon............................................................................................36 JUPITER Trine Moon................................................................................................40 JUPITER Conjunct Mercury.....................................................................................45 JUPITER Opposite Mercury.....................................................................................48 JUPITER Sextile Mercury........................................................................................51