A Transitory Overview
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The Tierras Observatory: an Ultra-Precise Photometer to Characterize Nearby Terrestrial Exoplanets
The Tierras Observatory: An ultra-precise photometer to characterize nearby terrestrial exoplanets Juliana Garc´ıa-Mej´ıaa, David Charbonneaua, Daniel Fabricanta, Jonathan M. Irwina, Robert Fataa, Joseph M. Zajaca, and Peter E. Dohertya aCenter for Astrophysics Harvard and Smithsonian, 60 Garden Street, Cambridge MA j ABSTRACT We report on the status of the Tierras Observatory, a refurbished 1.3-m ultra-precise fully-automated photometer located at the F. L. Whipple Observatory atop Mt. Hopkins, Arizona. Tierras is designed to limit systematic errors, notably precipitable water vapor (PWV), to 250 ppm, enabling the characterization of terrestrial planet transits orbiting < 0:3 R stars, as well as the potential discovery of exo-moons and exo-rings. The design choices that will enable our science goals include: a four-lens focal reducer and field-flattener to increase the field-of-view of the telescope from a 11:940 to a 0:48◦ side; a custom narrow bandpass (40:2 nm FWHM) filter centered around 863:5 nm to minimize PWV errors known to limit ground-based photometry of red dwarfs; and a deep-depletion 4K 4K CCD with a 300ke- full well and QE> 85% in our bandpass, operating in frame transfer mode. We are also× pursuing the design of a set of baffles to minimize the significant amount of scattered light reaching the image plane. Tierras will begin science operations in early 2021. Keywords: ultra-precise photometry, terrestrial planet detection, exoplanet instrumentation, transit method 1. INTRODUCTION The construction of observatories tailor-built to routinely achieve precise photometry from the ground is mo- tivated by the multitude of exoplanetary and stellar phenomena whose exploration will be enabled with high- cadence, ultra-precise time series of diverse stellar targets. -
Dust Environment and Dynamical History of a Sample of Short-Period Comets II
A&A 571, A64 (2014) Astronomy DOI: 10.1051/0004-6361/201424331 & c ESO 2014 Astrophysics Dust environment and dynamical history of a sample of short-period comets II. 81P/Wild 2 and 103P/Hartley 2 F. J. Pozuelos1;3, F. Moreno1, F. Aceituno1, V. Casanova1, A. Sota1, J. J. López-Moreno1, J. Castellano2, E. Reina2, A. Climent2, A. Fernández2, A. San Segundo2, B. Häusler2, C. González2, D. Rodriguez2, E. Bryssinck2, E. Cortés2, F. A. Rodriguez2, F. Baldris2, F. García2, F. Gómez2, F. Limón2, F. Tifner2, G. Muler2, I. Almendros2, J. A. de los Reyes2, J. A. Henríquez2, J. A. Moreno2, J. Báez2, J. Bel2, J. Camarasa2, J. Curto2, J. F. Hernández2, J. J. González2, J. J. Martín2, J. L. Salto2, J. Lopesino2, J. M. Bosch2, J. M. Ruiz2, J. R. Vidal2, J. Ruiz2, J. Sánchez2, J. Temprano2, J. M. Aymamí2, L. Lahuerta2, L. Montoro2, M. Campas2, M. A. García2, O. Canales2, R. Benavides2, R. Dymock2, R. García2, R. Ligustri2, R. Naves2, S. Lahuerta2, and S. Pastor2 1 Instituto de Astrofísica de Andalucía (CSIC), Glorieta de la Astronomía s/n, 18008 Granada, Spain e-mail: [email protected] 2 Amateur Association Cometas-Obs, Spain 3 Universidad de Granada-Phd Program in Physics and Mathematics (FisyMat), 18071 Granada, Spain Received 3 June 2014 / Accepted 5 August 2014 ABSTRACT Aims. This paper is a continuation of the first paper in this series, where we presented an extended study of the dust environment of a sample of short-period comets and their dynamical history. On this occasion, we focus on comets 81P/Wild 2 and 103P/Hartley 2, which are of special interest as targets of the spacecraft missions Stardust and EPOXI. -
List of Missions Using SPICE (PDF)
1/7/20 Data Restorations Selected Past Users Current/Pending Users Examples of Possible Future Users Apollo 15, 16 [L] Magellan [L] Cassini Orbiter NASA Discovery Program Mariner 2 [L] Clementine (NRL) Mars Odyssey NASA New Frontiers Program Mariner 9 [L] Mars 96 (RSA) Mars Exploration Rover Lunar IceCube (Moorehead State) Mariner 10 [L] Mars Pathfinder Mars Reconnaissance Orbiter LunaH-Map (Arizona State) Viking Orbiters [L] NEAR Mars Science Laboratory Luna-Glob (RSA) Viking Landers [L] Deep Space 1 Juno Aditya-L1 (ISRO) Pioneer 10/11/12 [L] Galileo MAVEN Examples of Users not Requesting NAIF Help Haley armada [L] Genesis SMAP (Earth Science) GOLD (LASP, UCF) (Earth Science) [L] Phobos 2 [L] (RSA) Deep Impact OSIRIS REx Hera (ESA) Ulysses [L] Huygens Probe (ESA) [L] InSight ExoMars RSP (ESA, RSA) Voyagers [L] Stardust/NExT Mars 2020 Emmirates Mars Mission (UAE via LASP) Lunar Orbiter [L] Mars Global Surveyor Europa Clipper Hayabusa-2 (JAXA) Helios 1,2 [L] Phoenix NISAR (NASA and ISRO) Proba-3 (ESA) EPOXI Psyche Parker Solar Probe GRAIL Lucy EUMETSAT GEO satellites [L] DAWN Lunar Reconnaissance Orbiter MOM (ISRO) Messenger Mars Express (ESA) Chandrayan-2 (ISRO) Phobos Sample Return (RSA) ExoMars 2016 (ESA, RSA) Solar Orbiter (ESA) Venus Express (ESA) Akatsuki (JAXA) STEREO [L] Rosetta (ESA) Korean Pathfinder Lunar Orbiter (KARI) Spitzer Space Telescope [L] [L] = limited use Chandrayaan-1 (ISRO) New Horizons Kepler [L] [S] = special services Hayabusa (JAXA) JUICE (ESA) Hubble Space Telescope [S][L] Kaguya (JAXA) Bepicolombo (ESA, JAXA) James Webb Space Telescope [S][L] LADEE Altius (Belgian earth science satellite) ISO [S] (ESA) Armadillo (CubeSat, by UT at Austin) Last updated: 1/7/20 Smart-1 (ESA) Deep Space Network Spectrum-RG (RSA) NAIF has or had project-supplied funding to support mission operations, consultation for flight team members, and SPICE data archive preparation. -
EPOXI COMET ENCOUNTER FACT SHEET Nov
EPOXI COMET ENCOUNTER FACT SHEET Nov. 2, 2010 Quick Facts Flyby Spacecraft Dimensions: 3.3 meters (10.8 feet) long, 1.7 meters (5.6 feet) wide, and 2.3 meters (7.5 feet) high Weight: 601 kilograms (1,325 pounds) at launch, consisting of 517 kilograms (1,140 pounds) spacecraft and 84 kilograms (185 pounds) fuel. On 10/25/10 there was 4 kilograms (8.8 pounds) of fuel remaining. Power: 2.8-meter-by-2.8-meter (9-foot-by-9 foot) solar panel providing up to 750 watts, depending on distance from sun. Power storage via small, 16-amp- hourrechargeable nickel hydrogen battery Comet Hartley 2 Nucleus shape: Elongated Nucleus size (estimated): About 2.2 kilometers (1.4 miles) long Nucleus mass: Roughly 280 million metric tons Nucleus rotation period: About 18 hours Nucleus composition: Water ice, carbon dioxide ice, silicate dust Mission Launch: Jan. 12, 2005 Launch site: Cape Canaveral Air Force Station, Florida Launch vehicle: Delta II 7925 with Star 48 upper stage Impact with Tempel 1: 10:52 p.m. PDT July 3, 2005 (1:52 a.m. EDT July 4, 2005) Earth-comet distance at time of impact: 133.6 million kilometers (83 million miles) Total distance traveled by spacecraft from Earth to Tempel 1: 431 million kilometers (268 million miles) Flyby of Hartley 2: About 10 a.m. EDT or 7 a.m. PDT Nov. 4, 2010 Additional distance traveled by spacecraft to Hartley 2: About 4.6 billion kilometers (2.9 billion miles) Program Cost of Deep Impact: $267 million total (not including launch vehicle), consisting of $252 million spacecraft development and $15 million mission operations Cost of EPOXI extended mission: $42 million, for operations from 2007 to end of project at the end of fiscal year 2011. -
Planetary Science
Mission Directorate: Science Theme: Planetary Science Theme Overview Planetary Science is a grand human enterprise that seeks to discover the nature and origin of the celestial bodies among which we live, and to explore whether life exists beyond Earth. The scientific imperative for Planetary Science, the quest to understand our origins, is universal. How did we get here? Are we alone? What does the future hold? These overarching questions lead to more focused, fundamental science questions about our solar system: How did the Sun's family of planets, satellites, and minor bodies originate and evolve? What are the characteristics of the solar system that lead to habitable environments? How and where could life begin and evolve in the solar system? What are the characteristics of small bodies and planetary environments and what potential hazards or resources do they hold? To address these science questions, NASA relies on various flight missions, research and analysis (R&A) and technology development. There are seven programs within the Planetary Science Theme: R&A, Lunar Quest, Discovery, New Frontiers, Mars Exploration, Outer Planets, and Technology. R&A supports two operating missions with international partners (Rosetta and Hayabusa), as well as sample curation, data archiving, dissemination and analysis, and Near Earth Object Observations. The Lunar Quest Program consists of small robotic spacecraft missions, Missions of Opportunity, Lunar Science Institute, and R&A. Discovery has two spacecraft in prime mission operations (MESSENGER and Dawn), an instrument operating on an ESA Mars Express mission (ASPERA-3), a mission in its development phase (GRAIL), three Missions of Opportunities (M3, Strofio, and LaRa), and three investigations using re-purposed spacecraft: EPOCh and DIXI hosted on the Deep Impact spacecraft and NExT hosted on the Stardust spacecraft. -
Planetary Science Update & Perspectives on Venus Exploration
Planetary Science Update & Perspectives on Venus Exploration Presentation at VEXAG James L. Green Director, Planetary Science Division May 6, 2008 1 Outline • FY09 Presidents Budget • Venus exploration opportunities: – Plans for next New Frontiers – Plans for next Discovery – Plans for SALMON – R&A opportunities 2 BUDGET BY SCIENCE THEME 3 Planetary Division 4 Planetary Division 5 What Changed, What’s the Same What Changed: • Initiated an Outer Planets Flagship (OPF) study activity joint with ESA/JAXA. • Lunar Science Research augmented to include a series of small lunar spacecraft. • Augments and enhances R&A to return more results from Planetary missions. • Discovery Program: Includes the recently selected MoOs (EPOXI and Stardust-NExT), adds Aspera-3 2nd extension (ESA/Mars Express), and selected GRAIL. • Preserves critical ISP work FY08 thru FY10, but deletes outyear activities in favor of more critical R&A and RPS enhancements. • Completes the Advanced Stirling RPS development and prepares for flight demonstration. • Mars Scout 2011 delayed to 2013 due to conflict of interest discovered during proposal evaluation. • Direction to the Mars Program to study Mars Sample Return (MSR) as a next decade goal • Expands US participation on the ESA/ExoMars mission by funding the potential selection of BOTH candidate U.S. instruments and EDL support. What’s the Same: • Discovery Program: MESSENGER, Dawn, Mars Express/Aspera-3, Chandraayn/MMM • New Frontiers Program: Juno and New Horizons • Mars Program: Odyssey, MER, MRO, Phoenix, MSL • Research -
OLLI Talk on Exoplanets
OLLI SC211 SPACE EXPLORATION: THE SEARCH FOR LIFE BEYOND EARTH April 13, 2017 Michal Peri NASA Solar System Ambassador Exoplanet2 Detection • Methods • Missions • Discoveries • Resources Image: C. Pulliam & D. Aguilar/CfA A long history … in our imaginations 3 https://en.wikipedia.org/wiki/Giordano_Bruno#/media/File:Relief_Bruno_Campo_dei_Fiori_n1.jpg Giordano Bruno in his De l'infinito universo et mondi (1584) suggested that "stars are other suns with their own planets” that “have no less virtue nor a nature different to that of our earth" and, like Earth, "contain animals and inhabitants.” For this heresy, he was burned by the inquisition. 3 https://www.loc.gov/today/cyberlc/feature_wdesc.php?rec=7148 5 Detection Methods Radial Velocity 619 planets Gravitational Microlensing 44 planets Direct Imaging 44 planets Transit 2771 planets Velocity generates Doppler 7 Shift Sound star receding star approaching Light wave “stretched” → red shift wave “squashed” → blue shift Orbiting planet causes Doppler shift in starlight 8 https://exoplanets.nasa.gov/interactable/11/ Radial Velocity Method 9 • The most successful method of detecting exoplanets pre-2010 • Doppler shifts in the stellar spectrum reveal presence of planetary companion(s) • Measure lower limit of the planetary mass and orbital parameters Doppler Shift Time Nikole K. Lewis, STScI Radial Velocity Detections Radial Velocity 1992 Planetary Mass 10 Detection Methods Radial Velocity 619 planets Gravitational Microlensing 44 planets Direct Imaging 44 planets Transit 2771 planets • Microlens -
Simulation of Attitude and Orbital Disturbances Acting on ASPECT Satellite in the Vicinity of the Binary Asteroid Didymos
Simulation of attitude and orbital disturbances acting on ASPECT satellite in the vicinity of the binary asteroid Didymos Erick Flores García Space Engineering, masters level (120 credits) 2017 Luleå University of Technology Department of Computer Science, Electrical and Space Engineering Simulation of attitude and orbital disturbances acting on ASPECT satellite in the vicinity of the binary asteroid Didymos Erick Flores Garcia School of Electrical Engineering Thesis submitted for examination for the degree of Master of Science in Technology. Espoo December 6, 2016 Thesis supervisors: Prof. Jaan Praks Dr. Leonard Felicetti Aalto University Luleå University of Technology School of Electrical Engineering Thesis advisors: M.Sc. Tuomas Tikka M.Sc. Nemanja Jovanović aalto university abstract of the school of electrical engineering master’s thesis Author: Erick Flores Garcia Title: Simulation of attitude and orbital disturbances acting on ASPECT satellite in the vicinity of the binary asteroid Didymos Date: December 6, 2016 Language: English Number of pages: 9+84 Department of Radio Science and Engineering Professorship: Automation Technology Supervisor: Prof. Jaan Praks Advisors: M.Sc. Tuomas Tikka, M.Sc. Nemanja JovanoviÊ Asteroid missions are gaining interest from the scientific community and many new missions are planned. The Didymos binary asteroid is a Near-Earth Object and the target of the Asteroid Impact and Deflection Assessment (AIDA). This joint mission, developed by NASA and ESA, brings the possibility to build one of the first CubeSats for deep space missions: the ASPECT satellite. Navigation systems of a deep space satellite differ greatly from the common planetary missions. Orbital environment close to an asteroid requires a case-by-case analysis. -
Thermal Infrared Imaging Experiments of C-Type Asteroid 162173 Ryugu on Hayabusa2
Space Sci Rev DOI 10.1007/s11214-016-0286-8 Thermal Infrared Imaging Experiments of C-Type Asteroid 162173 Ryugu on Hayabusa2 Tatsuaki Okada 1,2 · Tetsuya Fukuhara3 · Satoshi Tanaka1 · Makoto Taguchi3 · Takeshi Imamura4 · Takehiko Arai 1 · Hiroki Senshu5 · Yoshiko Ogawa6 · Hirohide Demura6 · Kohei Kitazato6 · Ryosuke Nakamura7 · Toru Kouyama7 · Tomohiko Sekiguchi8 · Sunao Hasegawa1 · Tsuneo Matsunaga9 · Takehiko Wada1 · Jun Takita2 · Naoya Sakatani1 · Yamato Horikawa10 · Ken Endo6 · Jörn Helbert11 · Thomas G. Müller12 · Axel Hagermann13 Received: 24 September 2015 / Accepted: 31 August 2016 © The Author(s) 2016. This article is published with open access at Springerlink.com Abstract The thermal infrared imager TIR onboard Hayabusa2 has been developed to in- vestigate thermo-physical properties of C-type, near-Earth asteroid 162173 Ryugu. TIR is one of the remote science instruments on Hayabusa2 designed to understand the nature of a volatile-rich solar system small body, but it also has significant mission objectives to pro- vide information on surface physical properties and conditions for sampling site selection B T. Okada [email protected] 1 Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, Sagamihara, Japan 2 Graduate School of Science, The University of Tokyo, Bunkyo Tokyo, Japan 3 Rikkyo University, Tokyo, Japan 4 Graduate School of Frontiers Sciences, The University of Tokyo Kashiwa, Japan 5 Planetary Exploration Research Center, Chiba Institute of Technology, Narashino, Japan 6 Center -
THE ARECIBO OBSERVATORY PLANETARY RADAR SYSTEM. P. A. Taylor 1, M. C. Nolan2, E. G. Rivera-Valentın1, J. E. Richardson1, L. A
47th Lunar and Planetary Science Conference (2016) 2534.pdf THE ARECIBO OBSERVATORY PLANETARY RADAR SYSTEM. P. A. Taylor1, M. C. Nolan2, E. G. Rivera-Valent´ın1, J. E. Richardson1, L. A. Rodriguez-Ford1, L. F. Zambrano-Marin1, E. S. Howell2, and J. T. Schmelz1; 1Arecibo Observatory, Universities Space Research Association, HC 3 Box 53995, Arecibo, PR 00612 ([email protected]); 2Lunar and Planetary Laboratory, University of Arizona, 1629 E. University Blvd., Tucson, AZ 85721. Introduction: The William E. Gordon telescope at of Solar System objects at radio wavelengths. The Arecibo Observatory in Puerto Rico is the largest and unmatched sensitivity of Arecibo allows for detection most sensitive single-dish radio telescope and the most of any potentially hazardous asteroid (PHA; absolute active and powerful planetary radar facility in the world. magnitude H < 22) that comes within ∼0.05 AU of Since opening in 1963, Arecibo has made significant Earth (∼20 lunar distances) and most any asteroid scientific contributions in the fields of planetary science, larger than ∼10 meters (H < 27) within ∼0.015 AU radio astronomy, and space and atmospheric sciences. (∼6 lunar distances) in the Arecibo declination window Arecibo is a facility of the National Science Founda- (0◦ to +38◦), as well as objects as far away as Saturn. tion (NSF) operated under cooperative agreement with In terms of near-Earth objects, Arecibo observations SRI International along with Universities Space Re- are critical for identifying those objects that may be on search Association and Universidad Metropolitana, part a collision course with Earth in addition to providing of the Ana G. -
FY13 High-Level Deliverables
National Optical Astronomy Observatory Fiscal Year Annual Report for FY 2013 (1 October 2012 – 30 September 2013) Submitted to the National Science Foundation Pursuant to Cooperative Support Agreement No. AST-0950945 13 December 2013 Revised 18 September 2014 Contents NOAO MISSION PROFILE .................................................................................................... 1 1 EXECUTIVE SUMMARY ................................................................................................ 2 2 NOAO ACCOMPLISHMENTS ....................................................................................... 4 2.1 Achievements ..................................................................................................... 4 2.2 Status of Vision and Goals ................................................................................. 5 2.2.1 Status of FY13 High-Level Deliverables ............................................ 5 2.2.2 FY13 Planned vs. Actual Spending and Revenues .............................. 8 2.3 Challenges and Their Impacts ............................................................................ 9 3 SCIENTIFIC ACTIVITIES AND FINDINGS .............................................................. 11 3.1 Cerro Tololo Inter-American Observatory ....................................................... 11 3.2 Kitt Peak National Observatory ....................................................................... 14 3.3 Gemini Observatory ........................................................................................ -
Blue Dots Team Transits Working Group Review
**FULL TITLE** ASP Conference Series, Vol. **VOLUME**, **YEAR OF PUBLICATION** **NAMES OF EDITORS** Blue Dots Team Transits Working Group Review A. Sozzetti1, C. Afonso2, R. Alonso3, D. L. Blank4, C. Catala5, H. Deeg6, J. L. Grenfell7, C. Hellier8, D. W. Latham9, D. Minniti10, F. Pont11, and H. Rauer12 Abstract. Transiting planet systems offer an unique opportunity to obser- vationally constrain proposed models of the interiors (radius, composition) and atmospheres (chemistry, dynamics) of extrasolar planets. The spectacular suc- cesses of ground-based transit surveys (more than 60 transiting systems known to-date) and the host of multi-wavelength, spectro-photometric follow-up stud- ies, carried out in particular by HST and Spitzer, have paved the way to the next generation of transit search projects, which are currently ongoing (CoRoT, Kepler), or planned. The possibility of detecting and characterizing transiting Earth-sized planets in the habitable zone of their parent stars appears tanta- lizingly close. In this contribution we briefly review the power of the transit technique for characterization of extrasolar planets, summarize the state of the art of both ground-based and space-borne transit search programs, and illustrate how the science of planetary transits fits within the Blue Dots perspective. 1. Introduction Within the framework of the Blue-Dots Team (BDT) initiative (http://www.blue-dots.net/), the primary goal of the Transits Working Group (TWG) is to gauge the potential and limitations of transit photometry (and follow-up measurements) as a tool 1INAF - Osservatorio Astronomico di Torino, Strada Osservatorio 20, I-10025 Pino Torinese, Italy 2Max Planck Institute for Astronomy, K¨onigstuhl 17, 69117 Heidelberg, Germany 3Observatoire de Gen´eve, Universit´ede Gen`eve, 51 Ch.