Phoenix Mars Mission
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Wind Measurements of Martian Dust Devils from Hirise
EPSC Abstracts Vol. 6, EPSC-DPS2011-570, 2011 EPSC-DPS Joint Meeting 2011 c Author(s) 2011 Wind Measurements of Martian Dust Devils from HiRISE D. S. Choi (1) and C. M. Dundas (2) (1) Department of Planetary Sciences, University of Arizona, Tucson, AZ, USA ([email protected]) (2) United States Geological Survey, Flagstaff, AZ, USA Abstract servation crosses an active feature such as a dust devil, changes in the active feature are apparent from the We report direct measurements of the winds within three separate views. Treating the dust clouds as pas- Martian dust devils from HiRISE imagery. The cen- sive tracers of motion then allows for the direct mea- tral color swath of the HiRISE instrument observes surement of wind velocities. the surface by using separate CCDs and color filters in We utilize measurements from manual (hand-eye) rapid cadence. Active features, such as a dust devil, tracking of the clouds through image blinking, as appear in motion when serendipitously captured by well as automated correlation methods [9]. Typically, this region of the instrument. Our measurements re- manual measurements are more successful than au- veal clear circulation within the vortices, and that the tomated measurements. The relatively diffuse dust majority of overall wind magnitude within a dust devil clouds, combined with the static background terrain, 1 is between 10 and 30 m s− . cause the automated software to incorrectly report the movement as stationary. Successful automated results were obtained from images with more substantial dust 1. Introduction clouds and relatively featureless background terrain. Direct measurements of the winds within a Martian dust devil [1] are challenging to obtain. -
Selection of the Insight Landing Site M. Golombek1, D. Kipp1, N
Manuscript Click here to download Manuscript InSight Landing Site Paper v9 Rev.docx Click here to view linked References Selection of the InSight Landing Site M. Golombek1, D. Kipp1, N. Warner1,2, I. J. Daubar1, R. Fergason3, R. Kirk3, R. Beyer4, A. Huertas1, S. Piqueux1, N. E. Putzig5, B. A. Campbell6, G. A. Morgan6, C. Charalambous7, W. T. Pike7, K. Gwinner8, F. Calef1, D. Kass1, M. Mischna1, J. Ashley1, C. Bloom1,9, N. Wigton1,10, T. Hare3, C. Schwartz1, H. Gengl1, L. Redmond1,11, M. Trautman1,12, J. Sweeney2, C. Grima11, I. B. Smith5, E. Sklyanskiy1, M. Lisano1, J. Benardino1, S. Smrekar1, P. Lognonné13, W. B. Banerdt1 1Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91109 2State University of New York at Geneseo, Department of Geological Sciences, 1 College Circle, Geneseo, NY 14454 3Astrogeology Science Center, U.S. Geological Survey, 2255 N. Gemini Dr., Flagstaff, AZ 86001 4Sagan Center at the SETI Institute and NASA Ames Research Center, Moffett Field, CA 94035 5Southwest Research Institute, Boulder, CO 80302; Now at Planetary Science Institute, Lakewood, CO 80401 6Smithsonian Institution, NASM CEPS, 6th at Independence SW, Washington, DC, 20560 7Department of Electrical and Electronic Engineering, Imperial College, South Kensington Campus, London 8German Aerospace Center (DLR), Institute of Planetary Research, 12489 Berlin, Germany 9Occidental College, Los Angeles, CA; Now at Central Washington University, Ellensburg, WA 98926 10Department of Earth and Planetary Sciences, University of Tennessee, Knoxville, TN 37996 11Institute for Geophysics, University of Texas, Austin, TX 78712 12MS GIS Program, University of Redlands, 1200 E. Colton Ave., Redlands, CA 92373-0999 13Institut Physique du Globe de Paris, Paris Cité, Université Paris Sorbonne, France Diderot Submitted to Space Science Reviews, Special InSight Issue v. -
DISR) on the Huygens Probe
Data Archive Users’ Guide for the Descent Imager and Spectral Radiometer (DISR) on the Huygens Probe By: The DISR Team 29 January 2013 Version 2.0 International Traffic in Arms Regulations (ITAR) disclosure... Evaluation by the Export Officer of the University of Arizona's Office for the Responsible Conduct of Research (ORCR) has deemed that this document is not subject to International Traffic in Arms Regulations (ITAR) control, and is not restricted by the Arms Export Control Act. It is suitable for public release, and its distribution is unlimited. DISR - C. See 29 January 2013 Index 1.0 Introduction & Science Objectives .................................................................................. 3 2.0 Instrument Description.................................................................................................... 4 3.0 Titan Descent Sequence & Divergences ...................................................................... 11 4.0 Archive Description....................................................................................................... 15 5.0 Data Calibration............................................................................................................ 19 5.1 General Information.................................................................................................. 19 5.2 Descent Cycles......................................................................................................... 20 5.3 Lamp Datasets ........................................................................................................ -
Oxygen Exosphere of Mars: Evidence from Pickup Ions Measured By
Oxygen Exosphere of Mars: Evidence from Pickup Ions Measured by MAVEN By Ali Rahmati Submitted to the graduate degree program in the Department of Physics and Astronomy, and the Graduate Faculty of the University of Kansas in partial fulfillment of the requirements for the degree of Doctor of Philosophy. ________________________________ Professor Thomas E. Cravens, Chair ________________________________ Professor Philip S. Baringer ________________________________ Professor David Braaten ________________________________ Professor Mikhail V. Medvedev ________________________________ Professor Stephen J. Sanders Date Defended: 22 January 2016 The Dissertation Committee for Ali Rahmati certifies that this is the approved version of the following dissertation: Oxygen Exosphere of Mars: Evidence from Pickup Ions Measured by MAVEN ________________________________ Professor Thomas E. Cravens, Chair Date approved: 22 January 2016 ii Abstract Mars possesses a hot oxygen exosphere that extends out to several Martian radii. The main source for populating this extended exosphere is the dissociative recombination of molecular oxygen ions with electrons in the Mars ionosphere. The dissociative recombination reaction creates two hot oxygen atoms that can gain energies above the escape energy at Mars and escape from the planet. Oxygen loss through this photochemical reaction is thought to be one of the main mechanisms of atmosphere escape at Mars, leading to the disappearance of water on the surface. In this work the hot oxygen exosphere of Mars is modeled using a two-stream/Liouville approach as well as a Monte-Carlo simulation. The modeled exosphere is used in a pickup ion simulation to predict the flux of energetic oxygen pickup ions at Mars. The pickup ions are created via ionization of neutral exospheric oxygen atoms through photo-ionization, charge exchange with solar wind protons, and electron impact ionization. -
Tianwen-1: China's Mars Mission
Tianwen-1: China's Mars Mission drishtiias.com/printpdf/tianwen-1-china-s-mars-mission Why In News China will launch its first Mars Mission - Tianwen-1- in July, 2020. China's previous ‘Yinghuo-1’ Mars mission, which was supported by a Russian spacecraft, had failed after it did not leave the earth's orbit and disintegrated over the Pacific Ocean in 2012. The National Aeronautics and Space Administration (NASA) is also going to launch its own Mars mission in July, the Perseverance which aims to collect Martian samples. Key Points The Tianwen-1 Mission: It will lift off on a Long March 5 rocket, from the Wenchang launch centre. It will carry 13 payloads (seven orbiters and six rovers) that will explore the planet. It is an all-in-one orbiter, lander and rover system. Orbiter: It is a spacecraft designed to orbit a celestial body (astronomical body) without landing on its surface. Lander: It is a strong, lightweight spacecraft structure, consisting of a base and three sides "petals" in the shape of a tetrahedron (pyramid- shaped). It is a protective "shell" that houses the rover and protects it, along with the airbags, from the forces of impact. Rover: It is a planetary surface exploration device designed to move across the solid surface on a planet or other planetary mass celestial bodies. 1/3 Objectives: The mission will be the first to place a ground-penetrating radar on the Martian surface, which will be able to study local geology, as well as rock, ice, and dirt distribution. It will search the martian surface for water, investigate soil characteristics, and study the atmosphere. -
How a Cartoon Series Helped the Public Care About Rosetta and Philae 13 How a Cartoon Series Helped the Public Care About Rosetta and Philae
How a Cartoon Series Helped the Public Care about Best Practice Rosetta and Philae Claudia Mignone Anne-Mareike Homfeld Sebastian Marcu Vitrociset Belgium for European Space ATG Europe for European Space Design & Data GmbH Agency (ESA) Agency (ESA) [email protected] [email protected] [email protected] Carlo Palazzari Emily Baldwin Markus Bauer Design & Data GmbH EJR-Quartz for European Space Agency (ESA) European Space Agency (ESA) [email protected] [email protected] [email protected] Keywords Karen S. O’Flaherty Mark McCaughrean Outreach, space science, public engagement, EJR-Quartz for European Space Agency (ESA) European Space Agency (ESA) visual storytelling, fairy-tale, cartoon, animation, [email protected] [email protected] anthropomorphising Once upon a time... is a series of short cartoons1 that have been developed as part of the European Space Agency’s communication campaign to raise awareness about the Rosetta mission. The series features two anthropomorphic characters depicting the Rosetta orbiter and Philae lander, introducing the mission story, goals and milestones with a fairy- tale flair. This article explores the development of the cartoon series and the level of engagement it generated, as well as presenting various issues that were encountered using this approach. We also examine how different audiences responded to our decision to anthropomorphise the spacecraft. Introduction internet before the spacecraft came out of exciting highlights to come, using the fairy- hibernation (Bauer et al., 2016). The four tale narrative as a base. The hope was that In late 2013, the European Space Agency’s short videos were commissioned from the video would help to build a degree of (ESA) team of science communicators the cross-media company Design & Data human empathy between the public and devised a number of outreach activ- GmbH (D&D). -
The Reference Mission of the NASA Mars Exploration Study Team
NASA Special Publication 6107 Human Exploration of Mars: The Reference Mission of the NASA Mars Exploration Study Team Stephen J. Hoffman, Editor David I. Kaplan, Editor Lyndon B. Johnson Space Center Houston, Texas July 1997 NASA Special Publication 6107 Human Exploration of Mars: The Reference Mission of the NASA Mars Exploration Study Team Stephen J. Hoffman, Editor Science Applications International Corporation Houston, Texas David I. Kaplan, Editor Lyndon B. Johnson Space Center Houston, Texas July 1997 This publication is available from the NASA Center for AeroSpace Information, 800 Elkridge Landing Road, Linthicum Heights, MD 21090-2934 (301) 621-0390. Foreword Mars has long beckoned to humankind interest in this fellow traveler of the solar from its travels high in the night sky. The system, adding impetus for exploration. ancients assumed this rust-red wanderer was Over the past several years studies the god of war and christened it with the have been conducted on various approaches name we still use today. to exploring Earth’s sister planet Mars. Much Early explorers armed with newly has been learned, and each study brings us invented telescopes discovered that this closer to realizing the goal of sending humans planet exhibited seasonal changes in color, to conduct science on the Red Planet and was subjected to dust storms that encircled explore its mysteries. The approach described the globe, and may have even had channels in this publication represents a culmination of that crisscrossed its surface. these efforts but should not be considered the final solution. It is our intent that this Recent explorers, using robotic document serve as a reference from which we surrogates to extend their reach, have can continuously compare and contrast other discovered that Mars is even more complex new innovative approaches to achieve our and fascinating—a planet peppered with long-term goal. -
The Analysis of Life Struggle in Andy Weir's
THE ANALYSIS OF LIFE STRUGGLE IN ANDY WEIR‘S NOVEL THE MARTIAN A THESIS BY ALEMINA BR KABAN REG. NO. 140721012 DEPARTMENT OF ENGLISH FACULTY OF CULTURAL STUDIES UNIVERSITY OF SUMATERA UTARA MEDAN 2018 UNIVERSITAS SUMATERA UTARA THE ANALYSIS OF LIFE STRUGGLE IN ANDY WEIR‘S NOVEL THE MARTIAN A THESIS BY ALEMINA BR KABAN REG. NO. 140721012 SUPERVISOR CO-SUPERVISOR Drs. Parlindungan Purba,M.Hum. Riko Andika Pohan, S.S., M.Hum. NIP.1963021619 89031003001 NIP. 1984060920150410010016026 Submitted to Faculty of Cultural Studies University of Sumatera Utara Medan in partial fulfilment of the requirements for the degree of Sarjana Sastra from Department of English DEPARTMENT OF ENGLISH FACULTY OF CULTURAL STUDIES UNIVERSITY OF SUMATERA UTARA MEDAN 2018 UNIVERSITAS SUMATERA UTARA Approved by the Department of English, Faculty of Cultural Studies University of Sumatera Utara (USU) Medan as thesis for The Sarjana Sastra Examination. Head, Secretary, Prof. T.Silvana Sinar,Dipl.TEFL,MA.,Ph.D Rahmadsyah Rangkuti, M.A. Ph.D. NIP. 19571117 198303 2 002 NIP. 19750209 200812 1 002 UNIVERSITAS SUMATERA UTARA Accepted by the Board of Examiners in partial fulfillment of requirements for the degree of Sarjana Sastra from the Department of English, Faculty of Cultural Studies University of Sumatera Utara, Medan. The examination is held in Department of English Faculty of Cultural Studies University of Sumatera Utara on July 6th, 2018 Dean of Faculty of Cultural Studies University of Sumatera Utara Dr. Budi Agustono, M.S. NIP.19600805 198703 1 001 Board of Examiners Rahmadsyah Rangkuti, M.A., Ph.D __________________ Drs. Parlindungan Purba, M.Hum. -
Balloon Powered Phoenix Mars Lander Model (Simplified Version)
balloon powered Phoenix Mars Lander Model (simplified version) by Steve Widmark Mountain View High School, Mountain View, CA What is Phoenix? Phoenix is NASA’s latest mission to Mars. Launched on a Delta II rocket on August 4 th , 2007, the Phoenix lander will touch down in the northern region of Mars on May 25, 2008. Once there, it will dig into the Martian permafrost using a robotic arm and analyze the composition of the soil and ice it removes with a sophisticated automated laboratory. In a nutshell, the goal of the mission is to determine if the Martian surface is (or was) capable of supporting life. Unlike the previous rover missions to Mars that made bounce landings using air bags, Phoenix will make a powered landing employing twelve thrusters positioned around the spacecraft. The model demonstrates this method of landing with a single balloon “thruster.” For more information about the Phoenix mission go to http://phoenix.lpl.arizona.edu Materials and tools: 1 parts sheet color printed on 110 lb (#110) card stock 1 balloon (lander flies best with a 5” balloon) 1 small paper clip clear tape glue sick or white glue scissors pencil Directions: Note: If the directions tell you to bend a tab down, this means to bend the tab down with the printed portion of the part facing up. If the directions tell you to bend a tab up, this means to bend the tab up with the printed portion of the part facing up. The front side of a part is the side with the printing. -
An Economic Analysis of Mars Exploration and Colonization Clayton Knappenberger Depauw University
DePauw University Scholarly and Creative Work from DePauw University Student research Student Work 2015 An Economic Analysis of Mars Exploration and Colonization Clayton Knappenberger DePauw University Follow this and additional works at: http://scholarship.depauw.edu/studentresearch Part of the Economics Commons, and the The unS and the Solar System Commons Recommended Citation Knappenberger, Clayton, "An Economic Analysis of Mars Exploration and Colonization" (2015). Student research. Paper 28. This Thesis is brought to you for free and open access by the Student Work at Scholarly and Creative Work from DePauw University. It has been accepted for inclusion in Student research by an authorized administrator of Scholarly and Creative Work from DePauw University. For more information, please contact [email protected]. An Economic Analysis of Mars Exploration and Colonization Clayton Knappenberger 2015 Sponsored by: Dr. Villinski Committee: Dr. Barreto and Dr. Brown Contents I. Why colonize Mars? ............................................................................................................................ 2 II. Can We Colonize Mars? .................................................................................................................... 11 III. What would it look like? ............................................................................................................... 16 A. National Program ......................................................................................................................... -
Companion Q&A Fact Sheet: What Mars Reveals About Life in Our
What Mars Reveals about Life in Our Universe Companion Q&A Fact Sheet Educators from the Smithsonian’s Air and Space and Natural History Museums assembled this collection of commonly asked questions about Mars to complement the Smithsonian Science How webinar broadcast on March 3, 2021, “What Mars Reveals about Life in our Universe.” Continue to explore Mars and your own curiosities with these facts and additional resources: • NASA: Mars Overview • NASA: Mars Robotic Missions • National Air and Space Museum on the Smithsonian Learning Lab: “Wondering About Astronomy Together” Guide • National Museum of Natural History: A collection of resources for teaching about Antarctic Meteorites and Mars 1 • Smithsonian Science How: “What Mars Reveals about Life in our Universe” with experts Cari Corrigan, L. Miché Aaron, and Mariah Baker (aired March 3, 2021) Mars Overview How long is Mars’ day? Mars takes 24 hours and 38 minutes to spin around once, so its day is very similar to Earth’s. How long is Mars’ year? Mars takes 687 days, almost two Earth years, to complete one orbit around the Sun. How far is Mars from Earth? The distance between Earth and Mars changes as both planets move around the Sun in their orbits. At its closest, Mars is just 34 million miles from the Earth; that’s about one third of Earth’s distance from the Sun. On the day of this program, March 3, 2021, Mars was about 135 million miles away, or four times its closest distance. How far is Mars from the Sun? Mars orbits an average of 141 million miles from the Sun, which is about one-and-a-half times as far as the Earth is from the Sun. -
Navigation Challenges During Exomars Trace Gas Orbiter Aerobraking Campaign
NON-PEER REVIEW Please select category below: Normal Paper Student Paper Young Engineer Paper Navigation Challenges during ExoMars Trace Gas Orbiter Aerobraking Campaign Gabriele Bellei 1, Francesco Castellini 2, Frank Budnik 3 and Robert Guilanyà Jané 4 1 DEIMOS Space located at ESA/ESOC, Robert-Bosch-Str. 5, Darmstadt, 64293, Germany 2 Telespazio VEGA located at ESA/ESOC, Robert-Bosch-Str. 5, Darmstadt, 64293, Germany 3 ESA/ESOC, Robert-Bosch-Str. 5, Darmstadt, 64293, Germany 4 GMV INSYEN located at ESA/ESOC, Robert-Bosch-Str. 5, Darmstadt, 64293, Germany Abstract The ExoMars Trace Gas Orbiter satellite spent one year in aerobraking operations at Mars, lowering its orbit period from one sol to about two hours. This delicate phase challenged the operations team and in particular the navigation system due to the highly unpredictable Mars atmosphere, which imposed almost continuous monitoring, navigation and re-planning activities. An aerobraking navigation concept was, for the first time at ESA, designed, implemented and validated on-ground and in-flight, based on radiometric tracking data and complemented by information extracted from spacecraft telemetry. The aerobraking operations were successfully completed, on time and without major difficulties, thanks to the simplicity and robustness of the selected approach. This paper describes the navigation concept, presents a recollection of the main in-flight results and gives a retrospective of the main lessons learnt during this activity. Keywords: ExoMars, Trace Gas Orbiter, aerobraking, navigation, orbit determination, Mars atmosphere, accelerometer Introduction The ExoMars program is a cooperation between the European Space Agency (ESA) and Roscosmos for the robotic exploration of the red planet.