ORACLE a Mission Concept to Study Mars' Climate, Surface and Interior
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Mars, the Nearest Habitable World – a Comprehensive Program for Future Mars Exploration
Mars, the Nearest Habitable World – A Comprehensive Program for Future Mars Exploration Report by the NASA Mars Architecture Strategy Working Group (MASWG) November 2020 Front Cover: Artist Concepts Top (Artist concepts, left to right): Early Mars1; Molecules in Space2; Astronaut and Rover on Mars1; Exo-Planet System1. Bottom: Pillinger Point, Endeavour Crater, as imaged by the Opportunity rover1. Credits: 1NASA; 2Discovery Magazine Citation: Mars Architecture Strategy Working Group (MASWG), Jakosky, B. M., et al. (2020). Mars, the Nearest Habitable World—A Comprehensive Program for Future Mars Exploration. MASWG Members • Bruce Jakosky, University of Colorado (chair) • Richard Zurek, Mars Program Office, JPL (co-chair) • Shane Byrne, University of Arizona • Wendy Calvin, University of Nevada, Reno • Shannon Curry, University of California, Berkeley • Bethany Ehlmann, California Institute of Technology • Jennifer Eigenbrode, NASA/Goddard Space Flight Center • Tori Hoehler, NASA/Ames Research Center • Briony Horgan, Purdue University • Scott Hubbard, Stanford University • Tom McCollom, University of Colorado • John Mustard, Brown University • Nathaniel Putzig, Planetary Science Institute • Michelle Rucker, NASA/JSC • Michael Wolff, Space Science Institute • Robin Wordsworth, Harvard University Ex Officio • Michael Meyer, NASA Headquarters ii Mars, the Nearest Habitable World October 2020 MASWG Table of Contents Mars, the Nearest Habitable World – A Comprehensive Program for Future Mars Exploration Table of Contents EXECUTIVE SUMMARY .......................................................................................................................... -
Mid-Latitude Ice on Mars: a Science Target for Planetary Climate Histories and an Exploration Target for in Situ Resources
Mid-Latitude Ice on Mars: A Science Target for Planetary Climate Histories and an Exploration Target for In Situ Resources A White Paper submitted to the Planetary Sciences Decadal Survey 2023–2032 Primary Contact: Ali M. Bramson, Purdue University ([email protected]) Authors: Ali M. Bramson1,2 John (Jack) W. Holt2 Eric I. Petersen2,12 Chimira Andres3 Suniti Karunatillake8 Nathaniel E. Putzig6 Jonathan Bapst4 Aditya Khuller9 Hanna G. Sizemore6 Patricio Becerra5 Michael T. Mellon10 Isaac B. Smith6,13 Samuel W. Courville6 Gareth A. Morgan6 David E. Stillman14 Colin M. Dundas7 Rachel W. Obbard11 Paul Wooster15 Shannon M. Hibbard3 Matthew R. Perry6 1Purdue University, 2University of Arizona, 3University of Western Ontario CA, 4Jet Propulsion Laboratory, California Institute of Technology, 5University of Bern CH, 6Planetary Science Institute, 7U.S. Geological Survey, 8Louisiana State University, 9Arizona State University, 10Cornell University, 11SETI Institute, 12University of Alaska Fairbanks, 13York University, 14Southwest Research Institute, 15SpaceX Signatories: Ken Herkenhoff, U.S. Geological Survey Alfred McEwen, U. of Arizona David M. Hollibaugh Baker, NASA GSFC Wendy Calvin, U. of Nevada Reno Stefano Nerozzi, U. of Arizona Nicolas Thomas, U. of Bern, CH Serina Diniega, NASA JPL Paul Hayne, U. of Colorado Boulder Jeffrey Plaut, NASA JPL/Caltech Kim Seelos, JHU/APL Charity Phillips-Lander, SwRI Shane Byrne, U. of Arizona Cynthia Dinwiddie, SwRI Devanshu Jha, MVJ College of Eng., IN Aymeric Spiga, LMD/Sorbonne Université, FR Michael S. Veto, Ball Aerospace Andreas Johnsson, U. of Gothenburg, SE Matthew Chojnacki, PSI Michael Mischna, NASA JPL/Caltech Jacob Widmer, Representing Self Adrian J. Brown, Plancius Research, LLC Carol Stoker, NASA Ames Noora Alsaeed, CU Boulder, LASP Alberto G. -
Laser Retroreflectors for Insight and an International Mars Geophysical Network (MGN)
50th Lunar and Planetary Science Conference 2019 (LPI Contrib. No. 2132) 1492.pdf Laser Retroreflectors for InSight and an International Mars Geophysical Network (MGN). S. Dell’Agnello1, G.O. Delle Monache1, L. Porcelli1,2, M. Tibuzzi1, L. Salvatori1, C. Mondaini1, M. Muccino1, L. Ioppi1, O. Luongo1, M. Petrassi1, G. Bianco1,3, R. Vittori1,4, W.B. Banerdt5, J.F. Grinblat5, C. Benedetto3, F. Pasquali3, R. Mugnuolo3, D.C. Gruel5, J.L.Vago6 and P. Baglioni6. 1Istituto Nazionale di Fisica Nucleare–Laboratori Nazionali di Frascati (INFN–LNF), Via E. Fermi 40, 00044, Frascati, Italy ([email protected]); 2Dipartimento di Fisica, Università della Calabria (UniCal), Via P. Bucci, 87036, Arcavacata di Rende, Italy; 3Agenzia Spaziale Italiana– Centro di Geodesia Spaziale “Giuseppe Colombo” (ASI–CGS), Località, Terlecchia 75100, Matera, Italy; 4Italian Air Force, Rome, Italy, ASI and Embassy of Italy in Washington DC; 5NASA–Jet Propulsion Laboratory (JPL), California Institute of Technology, Pasadena, CA 91109, USA; 6ESA–ESTEC, Noordwijk, The Netherlands. Abstract. There are laser retroreflectors on the Moon, of the INFN-ASI Affiliation-Association to NASA- but there were no laser retroreflectors on Mars until the SSERVI sservi.nasa.gov) is shown in the figure below. NASA InSight mission [1][2] landed and started oper- ating successfully on the surface of the red planet on Nov. 26, 2018. The ESA ExoMars Schiaparelli mis- sion, which unfortunately failed Mars landing in 2016, was carrying a laser retroreflector like InSight [3]. These instruments are positioned by measuring the time-of-flight of short laser pulses, the so-called “laser ranging” technique (for details on satellite/lunar laser ranging and altimetry see https://ilrs.gsfc.nasa.gov). -
Church of the Brethren May Meet Hrre In
' ' , s i * Take inventory of your printed” sup One word can tell the Btory of con plies; If you need anything, the - tinued business activity in the com - j ■ ' Times stands ready to give munity—Advertising. vi:;/ you Bervice, • . AND THE SJIOUE TIMES FOUR CENTS /,-;t VOL. LX . No. 33 OCEAN GROVE, NEW JERSEY, FRIDAY, AUGUST 16, 1935 - / ' : $ THOMSON GETS ‘MARTHA" IS BIBLE LESSON HOTEL MEN WANT CHURCH 7,500 HEAR BISHOP MOUZON Mrs. Gertrude Brown To Teach At OF THE BRETHREN RARE SOUVENIRS St; Paul’s MORE PUBLICITY in Au ditoriu m sermons “Martha” is the Bible class les MAY MEET HRRE IN 1936 THREE ANNIVERSARY: MEMOS son for .the coming Sundny. Text, WILL REQUEST LARGER BUD “Jesus loved! Martha and her sister ARE PRESENTED and! Lazarus,” John,: 11:5: Read GET APPROPRIATION. Preacher Sees Chance For Uniting of Three Luke, 10\38-42 and John, VI '.17-28. National Convention Would Bring Eight Thou Sixth Founders’ Day, Stokes Gold Dr, Francis Harvey Green will be Appoint Nominating Committee Branches of Methodist Church—Prays For en Wedding and Dr. Ballard’s the teacher 'at the|. Auditorium For Report at September Meet sand Delegates for Eight Days—Dr. Hen Bible Class,, at" 2.30. .Written Ques Birthday Arc Noted In Special ing of Ocean Grove Hotel As Kingdom of God and Revival of Hope, tions will be answered at the begin son Offers Buildings for Sessions—Ar Announcements. ning of theperiod. sociation. Endorse Play-Ground Faith and Love— Gives His Definition of Three precious documents have The Assembly BiblejClhss, which D rive/ rangements Committee Decides Today. -
Rapid Development of Navigation Payloads for Galileo Full Operational Capability
Changing the economics of space RAPID DEVELOPMENT OF NAVIGATION PAYLOADS FOR GALILEO FULL OPERATIONAL CAPABILITY Alex da Silva Curiel Dubai, January 2011 SSTL - the company UK-based satellite manufacturing company owned by EADS Astrium NV (99%) and the University of Surrey (1%) • Formed in 1985, the Company now employs >320 staff and occupies dedicated facilities in Surrey, Kent & Colorado 2 A history of success 34 Satellites completed – c.200 satellite years on-orbit experience 10 Further satellites (35-43) - currently being prepared for launch 18 payloads in progress (4 optical, 14 navigation) HERITAGE: Flight proven - low risk RESULTS: All projects fixed price, delivered on-time and on-budget SUCCESS: Very high mission success – 100% mission success in last 10 years – proven equipment and full redundancy CUSTOMERS: Variety of customers including many “blue chip” operators as well as 15 successful training programmes 3 What is Galileo? Galileo is a joint initiative of the European Commission (EC) and the European Space Agency (ESA). Galileo will be Europe’s own global navigation satellite system, providing a highly accurate, guaranteed global positioning service under civilian control. It will be inter-operable with GPS and GLONASS, the two other global satellite navigation systems 4 Galileo Services • Galileo offers 5 services: – Open signal, dual frequency, mass market use – Commercial signal, better accuracy, service guarantee – authenticated data – Safety-of-Life signal, high integrity service certified for use in safety related -
Seasonal and Interannual Variability of Solar Radiation at Spirit, Opportunity and Curiosity Landing Sites
Seasonal and interannual variability of solar radiation at Spirit, Opportunity and Curiosity landing sites Álvaro VICENTE-RETORTILLO1, Mark T. LEMMON2, Germán M. MARTÍNEZ3, Francisco VALERO4, Luis VÁZQUEZ5, Mª Luisa MARTÍN6 1Departamento de Física de la Tierra, Astronomía y Astrofísica II, Universidad Complutense de Madrid, Madrid, Spain, [email protected]. 2Department of Atmospheric Sciences, Texas A&M University, College Station, TX, USA, [email protected]. 3Department of Climate and Space Sciences and Engineering, University of Michigan, Ann Arbor, MI, USA, [email protected]. 4Departamento de Física de la Tierra, Astronomía y Astrofísica II, Universidad Complutense de Madrid, Madrid, Spain, [email protected]. 5Departamento de Matemática Aplicada, Universidad Complutense de Madrid, Madrid, Spain, [email protected]. 6Departamento de Matemática Aplicada, Universidad de Valladolid, Segovia, Spain, [email protected]. Received: 14/04/2016 Accepted: 22/09/2016 Abstract In this article we characterize the radiative environment at the landing sites of NASA's Mars Exploration Rover (MER) and Mars Science Laboratory (MSL) missions. We use opacity values obtained at the surface from direct imaging of the Sun and our radiative transfer model COMIMART to analyze the seasonal and interannual variability of the daily irradiation at the MER and MSL landing sites. In addition, we analyze the behavior of the direct and diffuse components of the solar radiation at these landing sites. Key words: Solar radiation; Mars Exploration Rovers; Mars Science Laboratory; opacity, dust; radiative transfer model; Mars exploration. Variabilidad estacional e interanual de la radiación solar en las coordenadas de aterrizaje de Spirit, Opportunity y Curiosity Resumen El presente artículo está dedicado a la caracterización del entorno radiativo en los lugares de aterrizaje de las misiones de la NASA de Mars Exploration Rover (MER) y de Mars Science Laboratory (MSL). -
NASA Satellite Laser Ranging Program
NASA Satellite Laser Ranging Program NASA Goddard Space Flight Center Ron Sebeny MOBLAS 4 Station Manager December 9, 2011 What is Satellite Laser Ranging? Map of International Laser Ranging Service (ILRS) Network Metsahovi PotsdamRiga Mendeleevo Borowiec Komsomolsk Herstmonceux Wettzell Zimmerwald Graz Simiez Changchun Grasse (2) Maidanak Cagliari KtiKatzive lly Beijing Greenbelt San Fernando Matera Keystone (4) Monument Peak Riyadh Wuhan Simosato McDonald Helwan Shanghai Kunming Santiago de Cuba Haleakala Arequipa South Africa Tahiti Yarragadee CiConcepcion Mt. Stromlo Legend: NASA NASA Partner International Cooperating Project: Satellite Laser Ranging (SLR) NASA SLR Network: • Eight Ground Stations • Part of International Laser Ranging Service (ILRS) • Data operations – Data reception, processing, and analysis – Orbit determination – Acquisition generation – Data Archive Laser Ranging Satellite Missions (past/present) : • Geodetic: – Larets, Starlette, Stella, Ajisai, LAGEOS-1, LAGEOS-2, Etalon-1, Etalon-2, BLITS • Earth Sensing/Technology Demonstration: – CHAMP, GRACE-A, GRACE-B, ICESat, Jason-1, Jason-2, Envisat, ERS-2, ETS-8, Beacon-C, TerraSAR-X, SOHLA-1, GOCE, CryoSat-2 • NitiNavigation: – GLONASS-102, GLONASS-115, GLONASS-120, GPS-35, GPS-36, GIOVE-A, GIOVE-B, Compass-M1 4 MOBLAS 4 Monument Peak MOBLAS 4 Monument Peak What is LRO? • Lunar Reconnaissance Orbiter – NASA’s Mission to map the moons surface with highest accuracy to date (highly successful thus far) • Laser ranggging to LRO will imp rove the scientific value of the -
First Galileo Satellites Galileo In-Orbit Validation Element
BR-251cover 7/8/06 13:28 Page 1 BR-251 Galileo Joint Undertaking Rue du Luxembourg 3 B-1000 Brussels, Belgium Tel: +32 2 507 80 00 The First Fax: +32 2 507 80 01 Email: [email protected] http://www.galileoju.com European Space Agency Directorate of European Union and Industrial Programmes Galileo Satellites 8-10 rue Mario Nikis F-75738 Paris Cedex 15, France Tel: +33 1 53 69 77 26 Fax: +33 1 53 69 72 86 Email: [email protected] http://www.esa.int/navigation/ European Commission Galileo In-Orbit Validation Element Directorate General for Energy and Transport Unit E.4 Satellite Navigation System (Galileo), Intelligent Transport, DM28 1/64 B-1049 Brussels, Belgium GIOVE Tel: +32 2 29 56040 Fax: +32 2 296 5372 Email: [email protected] http://europa.eu.int/comm/dgs/energy_transport/galileo/ BR-251cover 7/8/06 13:28 Page 2 BR-251 (2nd imprint, August 2006) Published by: ESA Publications Division ESTEC, PO Box 299 2200 AG Noordwijk The Netherlands Editor: Andrew Wilson Design/Layout: Eva Ekstrand Text coordination: Dominique Detain Copyright: ©2006 European Space Agency ISSN: 0250-1589 ISBN: 92-9092-497-7 Photo/image credits: Royal Astronomical Society Library (p.18), C. Beetles/Bridgeman-Giraudon (p.18), Galileo Price: 10 Euros Industries (pp. 7, 11); ESA: P.Carril (front cover, pp. 4, 5, 6, 7), S. Corvaja (front cover, pp. 6, 12), D. Detain (p. 13), J. Huart (pp. 3, 8, 9), A. Le Floch (pp. 4, 10, 16), E. Pedoussaut (p. 13), P.Sebirot (front cover),Trimaran (p. -
FROM WET PLANET to RED PLANET Current and Future Exploration Is Shaping Our Understanding of How the Climate of Mars Changed
FROM WET PLANET TO RED PLANET Current and future exploration is shaping our understanding of how the climate of Mars changed. Joel Davis deciphers the planet’s ancient, drying climate 14 DECEMBER 2020 | WWW.GEOLSOC.ORG.UK/GEOSCIENTIST WWW.GEOLSOC.ORG.UK/GEOSCIENTIST | DECEMBER 2020 | 15 FEATURE GEOSCIENTIST t has been an exciting year for Mars exploration. 2020 saw three spacecraft launches to the Red Planet, each by diff erent space agencies—NASA, the Chinese INational Space Administration, and the United Arab Emirates (UAE) Space Agency. NASA’s latest rover, Perseverance, is the fi rst step in a decade-long campaign for the eventual return of samples from Mars, which has the potential to truly transform our understanding of the still scientifi cally elusive Red Planet. On this side of the Atlantic, UK, European and Russian scientists are also getting ready for the launch of the European Space Agency (ESA) and Roscosmos Rosalind Franklin rover mission in 2022. The last 20 years have been a golden era for Mars exploration, with ever increasing amounts of data being returned from a variety of landed and orbital spacecraft. Such data help planetary geologists like me to unravel the complicated yet fascinating history of our celestial neighbour. As planetary geologists, we can apply our understanding of Earth to decipher the geological history of Mars, which is key to guiding future exploration. But why is planetary exploration so focused on Mars in particular? Until recently, the mantra of Mars exploration has been to follow the water, which has played an important role in shaping the surface of Mars. -
Meyer, Michael Mars Exploration and Mars Sample Return
Michael Meyer Lead Scientist Planetary Science Decadal Survey Mars Exploration & Mars Sample Return Panel on Mars, Nov 2, 2020 1 Why Mars? Mars is a habitable planet and has the potential to answer fundamental questions about our Solar System • The potential for life • A geological record of the first billion years of planetary evolution • A drastically changing climate through time • A compelling target for Human Exploration Mars Exploration Program Analysis Group Goals Human Life Climate Geology Exploration I. Determine if Mars ever supported life III. Understand II. Understand the origin and I. Determine if IV. Prepare for the processes evolution of Mars ever human and history of Mars as a supported, or exploration climate on Mars geological still supports life system Life I. Determine if Mars A. Search for evidence of life in environments that have a high potential for habitability and preservation of biosignatures. ever supported, or B. Assess the extent of abiotic organic chemical evolution. still supports, life. Climate II. Understand the A. Characterize the state and controlling processes of the present-day climate of Mars under the current orbital configuration. processes and B. Characterize the history and controlling processes of Mars’ climate in the recent past, history of climate under different orbital configurations. on Mars. C. Characterize Mars’ ancient climate and underlying processes. Geology III. Understand the A. Document the geologic record preserved in the crust and investigate the processes that have created and modified that record. origin and evolution B. Determine the structure, composition, and dynamics of the interior and how it has of Mars as a evolved. -
The GIOVE-A Small Navigation Mission …The First Galileo Satellite in Space Philip E Davies
The GIOVE-A small navigation mission …the first Galileo satellite in space Philip E Davies Surrey Satellite Technology Ltd Logan, Utah, August 2006 ©SSTL GIOVE-A: Programme Overview GIOVE-A GIOVE-A Precursor to European Galileo programme Contracts signed for two test-bed satellites (SSTL & GaIn) for launch before end of 2005 Objectives Secure frequency filings Demonstrate key payload technologies Measure MEO environment Provide Signal-in-Space for experimentation Requirements Two-year mission lifetime Lost-cost, rapid schedule. €28M, 30 months Ideally suited to an SSTL solution ©SSTL 2 GIOVE-A: platform development GIOVE-A The GIOVE-A launch is the first launch of SSTL’s new “Geostationary Minisatellite Platform” (GMP) Propulsion Bay Avionics Plate Payload Frame ©SSTL 3 GIOVE-A: platform architecture GIOVE-A ©SSTL 4 GIOVE-A Design: Platform GIOVE-A Dimensions: 1.3m x 1.3m x 1.8m (stowed) Wet mass: 600kg Power: Sun tracking arrays ~900W Sensors: EHS, ASS, Gyro Actuators: Wheels, Magnetorquers, Cold gas thrusters Pointing: ±0.55° pitch/roll required (3σ), ±0.1° achieved; ±2.1° yaw required, ±1.0° achieved Orbit: NORAD, Laser ranging, GPS, reverse GNSS Propulsion: 90 ms-1 Δv butane cold gas TT&C: S-Band Avionics: SSTL Enhanced Microsat ©SSTL 5 GIOVE-A: Manufacture GIOVE-A Platform manufacture at SSTL ©SSTL 6 7 GIOVE-A TWTA TWTA CAMP CAMP 1 2 Block Diagram GIOVE-A Payload: ©SSTL GIOVE-A: Final Integration GIOVE-A Antenna Payload Bay Avionics Propulsion Bay Integration activities undertaken at SSTL ©SSTL 8 GIOVE-A: Environmental -
Elektronen Mikroskop Electron Microscope Cebrauchsanleitung
Transmissions Elektronen Mikroskop Transmission Electron Microscope 900 Cebrauchsanleitung Operating instructions Operating Instructions Eiectron Microscope EM 900 Chapter I.0 Specifications 2.0 Installation, supply, accessories 3.0 Brief operating instructions 4.0 Description of instrument 5.0 Operation 6.0 Alignment 7.0 Microprocessor-controlled vacuum system 8.0 Maintenance and service 9.0 Interface description 10.0 Sheet film camera (G 34-602) or TFP camera (G 34-607) II.0 Specimen stage and camera controls (G 34-611) 12.0 Miscellaneous: Goniometer (G 34-606), TV camera (G 34-608), Desiccator (G 34-609), 35mm camera (G 34-205), Closed-loop cooling system (G 34-213) Carl Zeiss Postfach 13 69/80 D-7082 Oberkochen West Germany G 34-616-e 1.1 EM 900 Transmission Electron Microscope Specifications of base instrument Chapter 1: Column Factory-aligned Vibration-resistant mounting Chapter 2: Resolution fSOkVI Guaranteed lattice resolution: 0,344nm Guaranteed point resolution: O.Snm Chapter 3: Accelerating voltage 50kV,80kV Stability at 80kV: 8x10"® Chapter 4: Magnification HC mode: Steps 1-5, Low Mag 165, 275, 440, 770, 1,21 Ox Steps 6-15, 1,200, 1,760, 2,800, 4,800, 8,000, 12,000, 20,000, 34,000, 56,000, lOO.OOOx. Focus maintained in the range from 100,000x to 1,200x during change of magnification. HR mode: Steps 1-5, Low Mag 150, 250, 400, 700,1,1 OOx Steps 6-15, 3,000, 4,400, 7,000,12,000, 20,000, 30,000, 50,000, 85,000, 140,000, 250,000x. Focus maintained in the range from 250,000x to 3,000x during change of magnification.