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Galileo and the Telescope
Galileo and the Telescope A Discussion of Galileo Galilei and the Beginning of Modern Observational Astronomy ___________________________ Billy Teets, Ph.D. Acting Director and Outreach Astronomer, Vanderbilt University Dyer Observatory Tuesday, October 20, 2020 Image Credit: Giuseppe Bertini General Outline • Telescopes/Galileo’s Telescopes • Observations of the Moon • Observations of Jupiter • Observations of Other Planets • The Milky Way • Sunspots Brief History of the Telescope – Hans Lippershey • Dutch Spectacle Maker • Invention credited to Hans Lippershey (c. 1608 - refracting telescope) • Late 1608 – Dutch gov’t: “ a device by means of which all things at a very great distance can be seen as if they were nearby” • Is said he observed two children playing with lenses • Patent not awarded Image Source: Wikipedia Galileo and the Telescope • Created his own – 3x magnification. • Similar to what was peddled in Europe. • Learned magnification depended on the ratio of lens focal lengths. • Had to learn to grind his own lenses. Image Source: Britannica.com Image Source: Wikipedia Refracting Telescopes Bend Light Refracting Telescopes Chromatic Aberration Chromatic aberration limits ability to distinguish details Dealing with Chromatic Aberration - Stop Down Aperture Galileo used cardboard rings to limit aperture – Results were dimmer views but less chromatic aberration Galileo and the Telescope • Created his own (3x, 8-9x, 20x, etc.) • Noted by many for its military advantages August 1609 Galileo and the Telescope • First observed the -
The Telescope Lenses, Which Turned the Image Upside Down but Improved the Clarity Dramatically
The image produced by the first refracting telescope was Name right side up. However, the clarity of the image was less than ideal. Johannes Kepler worked to improve the image produced by the refracting telescope. He used two convex The Telescope lenses, which turned the image upside down but improved the clarity dramatically. His design soon became popular By Phyllis Naegeli and remains in use today. Do you like to lie on your back and gaze One problem associated with the refracting telescope was at the stars? What constellations can you the rainbow halo it produced around the object in view. Sir name? Have you ever used a telescope to Isaac Newton did not care for the halo produced by the get a closer look at the universe? Do you refracting telescope. He set out to improve the design, know how a telescope works? which led him to work on the reflecting telescope. The design used a curved mirror to collect light from an object. A telescope is used to see distant objects A secondary flat mirror reflected the image to the side of up close. There are two basic types of the tube where it is viewed through an eyepiece. Newton telescopes - the refracting telescope and also used a shorter, fatter tube allowing magnification to be the reflecting telescope. Each will help increased by using larger mirrors. Newton's design you to see the planets, moon, or stars. Both eliminated the rainbow halo produced by the convex lenses use a tube and have an eyepiece to focus the image for you of the refracting telescope. -
Phobos, Deimos: Formation and Evolution Alex Soumbatov-Gur
Phobos, Deimos: Formation and Evolution Alex Soumbatov-Gur To cite this version: Alex Soumbatov-Gur. Phobos, Deimos: Formation and Evolution. [Research Report] Karpov institute of physical chemistry. 2019. hal-02147461 HAL Id: hal-02147461 https://hal.archives-ouvertes.fr/hal-02147461 Submitted on 4 Jun 2019 HAL is a multi-disciplinary open access L’archive ouverte pluridisciplinaire HAL, est archive for the deposit and dissemination of sci- destinée au dépôt et à la diffusion de documents entific research documents, whether they are pub- scientifiques de niveau recherche, publiés ou non, lished or not. The documents may come from émanant des établissements d’enseignement et de teaching and research institutions in France or recherche français ou étrangers, des laboratoires abroad, or from public or private research centers. publics ou privés. Phobos, Deimos: Formation and Evolution Alex Soumbatov-Gur The moons are confirmed to be ejected parts of Mars’ crust. After explosive throwing out as cone-like rocks they plastically evolved with density decays and materials transformations. Their expansion evolutions were accompanied by global ruptures and small scale rock ejections with concurrent crater formations. The scenario reconciles orbital and physical parameters of the moons. It coherently explains dozens of their properties including spectra, appearances, size differences, crater locations, fracture symmetries, orbits, evolution trends, geologic activity, Phobos’ grooves, mechanism of their origin, etc. The ejective approach is also discussed in the context of observational data on near-Earth asteroids, main belt asteroids Steins, Vesta, and Mars. The approach incorporates known fission mechanism of formation of miniature asteroids, logically accounts for its outliers, and naturally explains formations of small celestial bodies of various sizes. -
Solar System Solar System
Delta Science Reader SolarSolar SystemSystem Delta Science Readers are nonfiction student books that provide science background and support the experiences of hands-on activities. Every Delta Science Reader has three main sections: Think About . , People in Science, and Did You Know? Be sure to preview the reader Overview Chart on page 4, the reader itself, and the teaching suggestions on the following pages. This information will help you determine how to plan your schedule for reader selections and activity sessions. Reading for information is a key literacy skill. Use the following ideas as appropriate for your teaching style and the needs of your students. The After Reading section includes an assessment and writing links. OVERVIEW Students will: discover facts about the Solar System In the Delta Science Reader Solar System, students take a tour of the Sun and the explore the planets and other objects in the planets. Other space objects such as dwarf Solar System planets, comets, asteroids, and meteoroids discuss the function of a table of contents, are explored. Students read about the headings, and a glossary rotation and revolution of the planets and interpret photographs and graphics to the causes of night and day, seasonal answer questions changes, and the phases of the Moon. The book describes the work of a planetary complete a KWL chart geologist. In addition, students discover organize information in a variety of ways how telescopes work. delta science modules Solar System 119 © Delta Education LLC. All rights reserved. -
Lecture 12 the Rings and Moons of the Outer Planets October 15, 2018
Lecture 12 The Rings and Moons of the Outer Planets October 15, 2018 1 2 Rings of Outer Planets • Rings are not solid but are fragments of material – Saturn: Ice and ice-coated rock (bright) – Others: Dusty ice, rocky material (dark) • Very thin – Saturn rings ~0.05 km thick! • Rings can have many gaps due to small satellites – Saturn and Uranus 3 Rings of Jupiter •Very thin and made of small, dark particles. 4 Rings of Saturn Flash movie 5 Saturn’s Rings Ring structure in natural color, photographed by Cassini probe July 23, 2004. Click on image for Astronomy Picture of the Day site, or here for JPL information 6 Saturn’s Rings (false color) Photo taken by Voyager 2 on August 17, 1981. Click on image for more information 7 Saturn’s Ring System (Cassini) Mars Mimas Janus Venus Prometheus A B C D F G E Pandora Enceladus Epimetheus Earth Tethys Moon Wikipedia image with annotations On July 19, 2013, in an event celebrated the world over, NASA's Cassini spacecraft slipped into Saturn's shadow and turned to image the planet, seven of its moons, its inner rings -- and, in the background, our home planet, Earth. 8 Newly Discovered Saturnian Ring • Nearly invisible ring in the plane of the moon Pheobe’s orbit, tilted 27° from Saturn’s equatorial plane • Discovered by the infrared Spitzer Space Telescope and announced 6 October 2009 • Extends from 128 to 207 Saturnian radii and is about 40 radii thick • Contributes to the two-tone coloring of the moon Iapetus • Click here for more info about the artist’s rendering 9 Rings of Uranus • Uranus -- rings discovered through stellar occultation – Rings block light from star as Uranus moves by. -
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. -
Solar Orbiter Assessment Study and Model Payload
Solar Orbiter assessment study and model payload N.Rando(1), L.Gerlach(2), G.Janin(4), B.Johlander(1), A.Jeanes(1), A.Lyngvi(1), R.Marsden(3), A.Owens(1), U.Telljohann(1), D.Lumb(1) and T.Peacock(1). (1) Science Payload & Advanced Concepts Office, (2) Electrical Engineering Department, (3) Research and Scientific Support Department, European Space Agency, ESTEC, Postbus 299, NL-2200AG, Noordwijk, The Netherlands (4) Mission Analysis Office, European Space Agency, ESOC, Darmstadt, Germany ABSTRACT The Solar Orbiter mission is presently in assessment phase by the Science Payload and Advanced Concepts Office of the European Space Agency. The mission is confirmed in the Cosmic Vision programme, with the objective of a launch in October 2013 and no later than May 2015. The Solar Orbiter mission incorporates both a near-Sun (~0.22 AU) and a high-latitude (~ 35 deg) phase, posing new challenges in terms of protection from the intense solar radiation and related spacecraft thermal control, to remain compatible with the programmatic constraints of a medium class mission. This paper provides an overview of the assessment study activities, with specific emphasis on the definition of the model payload and its accommodation in the spacecraft. The main results of the industrial activities conducted with Alcatel Space and EADS-Astrium are summarized. Keywords: Solar physics, space weather, instrumentation, mission assessment, Solar Orbiter 1. INTRODUCTION The Solar Orbiter mission was first discussed at the Tenerife “Crossroads” workshop in 1998, in the framework of the ESA Solar Physics Planning Group. The mission was submitted to ESA in 2000 and then selected by ESA’s Science Programme Committee in October 2000 to be implemented as a flexi-mission, with a launch envisaged in the 2008- 2013 timeframe (after the BepiColombo mission to Mercury) [1]. -
A Free Spacecraft Simulation Tool
Orbiter: AFreeSpacecraftSimulationTool MartinSchweiger DepartmentofComputerScience UniversityCollegeLondon www.orbitersim.com 2nd ESAWorkshoponAstrodynamics ToolsandTechniques ESTEC,Noordwijk 13-15September2004 Contents • Overview • Scope • Limitations • SomeOrbiterfeatures: • Timepropagation • Gravitycalculation • Rigid-bodymodelandsuperstructures • OrbiterApplicationProgrammingInterface: • Concept • Orbiterinstrumentation • TheVESSELinterfaceclass • Newfeatures: • Air-breatingengines:scramjetdesign • Virtualcockpits • Newvisualeffects • Orbiterasateachingtool • Summaryandfutureplans • Demonstration Overview · Orbiterisareal-timespaceflightsimulationforWindowsPC platforms. · Modellingofatmosphericflight(launchandreentry), suborbital,orbitalandinterplanetarymissions(rendezvous, docking,transfer,swing-byetc.) · Newtonianmechanics,rigidbodymodelofrotation,basic atmosphericflightmodel. · Planetpositionsfrompublicperturbationsolutions.Time integrationofstatevectorsorosculatingelements. · Developedsince2000asaneducationalandrecreational applicationfororbitalmechanicssimulation. · WritteninC++,usingDirectXfor3-Drendering.Public programminginterfacefordevelopmentofexternalmodule plugins. · WithanincreasinglyversatileAPI,developmentfocusis beginningtoshiftfromtheOrbitercoreto3rd partyaddons. Scope · Launchsequencefromsurfacetoorbitalinsertion(including atmosphericeffects:drag,pressure-dependentengineISP...) · Orbitalmanoeuvres(alignmentoforbitalplane,orbit-to-orbit transfers,rendezvous) · Vessel-to-vesselapproachanddocking.Buildingof superstructuresfromvesselmodules(includingsimplerules -
March 21–25, 2016
FORTY-SEVENTH LUNAR AND PLANETARY SCIENCE CONFERENCE PROGRAM OF TECHNICAL SESSIONS MARCH 21–25, 2016 The Woodlands Waterway Marriott Hotel and Convention Center The Woodlands, Texas INSTITUTIONAL SUPPORT Universities Space Research Association Lunar and Planetary Institute National Aeronautics and Space Administration CONFERENCE CO-CHAIRS Stephen Mackwell, Lunar and Planetary Institute Eileen Stansbery, NASA Johnson Space Center PROGRAM COMMITTEE CHAIRS David Draper, NASA Johnson Space Center Walter Kiefer, Lunar and Planetary Institute PROGRAM COMMITTEE P. Doug Archer, NASA Johnson Space Center Nicolas LeCorvec, Lunar and Planetary Institute Katherine Bermingham, University of Maryland Yo Matsubara, Smithsonian Institute Janice Bishop, SETI and NASA Ames Research Center Francis McCubbin, NASA Johnson Space Center Jeremy Boyce, University of California, Los Angeles Andrew Needham, Carnegie Institution of Washington Lisa Danielson, NASA Johnson Space Center Lan-Anh Nguyen, NASA Johnson Space Center Deepak Dhingra, University of Idaho Paul Niles, NASA Johnson Space Center Stephen Elardo, Carnegie Institution of Washington Dorothy Oehler, NASA Johnson Space Center Marc Fries, NASA Johnson Space Center D. Alex Patthoff, Jet Propulsion Laboratory Cyrena Goodrich, Lunar and Planetary Institute Elizabeth Rampe, Aerodyne Industries, Jacobs JETS at John Gruener, NASA Johnson Space Center NASA Johnson Space Center Justin Hagerty, U.S. Geological Survey Carol Raymond, Jet Propulsion Laboratory Lindsay Hays, Jet Propulsion Laboratory Paul Schenk, -
Abstracts of the 50Th DDA Meeting (Boulder, CO)
Abstracts of the 50th DDA Meeting (Boulder, CO) American Astronomical Society June, 2019 100 — Dynamics on Asteroids break-up event around a Lagrange point. 100.01 — Simulations of a Synthetic Eurybates 100.02 — High-Fidelity Testing of Binary Asteroid Collisional Family Formation with Applications to 1999 KW4 Timothy Holt1; David Nesvorny2; Jonathan Horner1; Alex B. Davis1; Daniel Scheeres1 Rachel King1; Brad Carter1; Leigh Brookshaw1 1 Aerospace Engineering Sciences, University of Colorado Boulder 1 Centre for Astrophysics, University of Southern Queensland (Boulder, Colorado, United States) (Longmont, Colorado, United States) 2 Southwest Research Institute (Boulder, Connecticut, United The commonly accepted formation process for asym- States) metric binary asteroids is the spin up and eventual fission of rubble pile asteroids as proposed by Walsh, Of the six recognized collisional families in the Jo- Richardson and Michel (Walsh et al., Nature 2008) vian Trojan swarms, the Eurybates family is the and Scheeres (Scheeres, Icarus 2007). In this theory largest, with over 200 recognized members. Located a rubble pile asteroid is spun up by YORP until it around the Jovian L4 Lagrange point, librations of reaches a critical spin rate and experiences a mass the members make this family an interesting study shedding event forming a close, low-eccentricity in orbital dynamics. The Jovian Trojans are thought satellite. Further work by Jacobson and Scheeres to have been captured during an early period of in- used a planar, two-ellipsoid model to analyze the stability in the Solar system. The parent body of the evolutionary pathways of such a formation event family, 3548 Eurybates is one of the targets for the from the moment the bodies initially fission (Jacob- LUCY spacecraft, and our work will provide a dy- son and Scheeres, Icarus 2011). -
Building and Maintaining the International Space Station (ISS)
/ Building and maintaining the International Space Station (ISS) is a very complex task. An international fleet of space vehicles launches ISS components; rotates crews; provides logistical support; and replenishes propellant, items for science experi- ments, and other necessary supplies and equipment. The Space Shuttle must be used to deliver most ISS modules and major components. All of these important deliveries sustain a constant supply line that is crucial to the development and maintenance of the International Space Station. The fleet is also responsible for returning experiment results to Earth and for removing trash and waste from the ISS. Currently, transport vehicles are launched from two sites on transportation logistics Earth. In the future, the number of launch sites will increase to four or more. Future plans also include new commercial trans- ports that will take over the role of U.S. ISS logistical support. INTERNATIONAL SPACE STATION GUIDE TRANSPORTATION/LOGISTICS 39 LAUNCH VEHICLES Soyuz Proton H-II Ariane Shuttle Roscosmos JAXA ESA NASA Russia Japan Europe United States Russia Japan EuRopE u.s. soyuz sL-4 proton sL-12 H-ii ariane 5 space shuttle First launch 1957 1965 1996 1996 1981 1963 (Soyuz variant) Launch site(s) Baikonur Baikonur Tanegashima Guiana Kennedy Space Center Cosmodrome Cosmodrome Space Center Space Center Launch performance 7,150 kg 20,000 kg 16,500 kg 18,000 kg 18,600 kg payload capacity (15,750 lb) (44,000 lb) (36,400 lb) (39,700 lb) (41,000 lb) 105,000 kg (230,000 lb), orbiter only Return performance -
NASA Advisory Council Planetary Protection Subcommittee, May 20‐21, 2014
NASA Advisory Council Planetary Protection Subcommittee, May 20‐21, 2014 NASA ADVISORY COUNCIL Planetary Protection Subcommittee May 20-21, 2014 NASA Headquarters Washington, D.C. MEETING MINUTES _____________________________________________________________ Eugene Levy, Chair ____________________________________________________________ Gale Allen, Executive Secretary Report prepared by Joan M. Zimmermann Zantech IT, Inc. 1 NASA Advisory Council Planetary Protection Subcommittee, May 20-2t 2014 Table of Contents Introduction 3 PPO Update and Review 3 MSL Lessons Learned 5 InSight Status 8 Planetary Science and Mars Program Update 10 Contamination Limits for Planetary Life Detection 12 Mars Landing Site Selection Process 14 ESA 2018 Landing Site Selection 15 Mars 2020 Project Status 15 Public Comment 16 Discussion 16 Ethics Briefing 17 Discussion 17 Science Mission Directorate and Planetary Protection 17 Update on Special Regions Parameters 19 Status of Phobos /Demos Materials 21 Outer Solar System Special Regions: Enceladus and Beyond 22 JAXA Sample Return Working Group 23 Public Comment 24 Discussion 25 Appendix A- Attendees Appendix 8- Membership roster Appendix C- Presentations Appendix D- Agenda 2 NASA Advisory Council Planetary Protection Subcommittee, May 20-2t 2014 May 20.2014 Introduction The Executive Secretary of the Planetary Protection Subcommittee (PPS), Dr. Gale Allen, made preparatory announcements. Dr. Eugene Levy, PPS Chair, opened the meeting and noted there would be a heavy focus on Mars exploration, as it has become a timely and important issue. Introductions were made around the meeting room. Planetary Protection Office Update and Review Dr. Catharine Conley, Planetary Protection Officer (PPO) for NASA, briefly described the broad base of experience in the PPS, and reviewed the purpose of Planetary Protection (PP) and the policy, as it applies to all missions.