Exploring Mars July 2020
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VI FORSKER PÅ MARS Kort Om Aktiviteten I Mange Tiår Har Mars Vært Et Yndet Objekt for Forskere Verden Over
VI FORSKER PÅ MARS Kort om aktiviteten I mange tiår har Mars vært et yndet objekt for forskere verden over. Men hvorfor det? Hva er det med den røde planeten som er så interessant? Her forsøker vi å gi en oversikt over hvorfor vi er så opptatt av Mars. Hva har vi oppdaget, og hva er det vi tenker å gjøre? Det finnes en planet i solsystemet vårt som bare er bebodd av roboter -MARS- Læringsmål Elevene skal kunne - gi eksempler på dagsaktuell forskning og drøfte hvordan ny kunnskap genereres gjennom samarbeid og kritisk tilnærming til eksisterende kunnskap - utforske, forstå og lage teknologiske systemer som består av en sender og en mottaker - gjøre rede for energibevaring og energikvalitet og utforske ulike måter å omdanne, transportere og lagre energi på VI FORSKER PÅ MARS side 1 Innhold Kort om aktiviteten ................................................................................................................................ 1 Læringsmål ................................................................................................................................................ 1 Mars gjennom historien ...................................................................................................................... 3 Romkappløp mot Mars ................................................................................................................... 3 2000-tallet gir rovere i fleng ....................................................................................................... 4 Hva nå? ...................................................................................................................................................... -
Mars Reconnaissance Orbiter
Chapter 6 Mars Reconnaissance Orbiter Jim Taylor, Dennis K. Lee, and Shervin Shambayati 6.1 Mission Overview The Mars Reconnaissance Orbiter (MRO) [1, 2] has a suite of instruments making observations at Mars, and it provides data-relay services for Mars landers and rovers. MRO was launched on August 12, 2005. The orbiter successfully went into orbit around Mars on March 10, 2006 and began reducing its orbit altitude and circularizing the orbit in preparation for the science mission. The orbit changing was accomplished through a process called aerobraking, in preparation for the “science mission” starting in November 2006, followed by the “relay mission” starting in November 2008. MRO participated in the Mars Science Laboratory touchdown and surface mission that began in August 2012 (Chapter 7). MRO communications has operated in three different frequency bands: 1) Most telecom in both directions has been with the Deep Space Network (DSN) at X-band (~8 GHz), and this band will continue to provide operational commanding, telemetry transmission, and radiometric tracking. 2) During cruise, the functional characteristics of a separate Ka-band (~32 GHz) downlink system were verified in preparation for an operational demonstration during orbit operations. After a Ka-band hardware anomaly in cruise, the project has elected not to initiate the originally planned operational demonstration (with yet-to-be used redundant Ka-band hardware). 201 202 Chapter 6 3) A new-generation ultra-high frequency (UHF) (~400 MHz) system was verified with the Mars Exploration Rovers in preparation for the successful relay communications with the Phoenix lander in 2008 and the later Mars Science Laboratory relay operations. -
Generate Viewsheds of Mastcam Images from the Curiosity Rover, Using Arcgis® and Public Datasets
TECHNICAL Coupling Mars Ground and Orbital Views: Generate REPORTS: METHODS Viewsheds of Mastcam Images From the Curiosity 10.1029/2020EA001247 Rover, Using ArcGIS® and Public Datasets Key Points: 1 2 1 3 4 • Mastcam images from the Curiosity M. Nachon , S. Borges , R. C. Ewing , F. Rivera‐Hernández , N. Stein , and rover are available online but lack a J. K. Van Beek5 public method to be placed back in the Mars orbital context 1Department of Geology and Geophysics, Texas A&M University, College Station, TX, USA, 2Department of Astronomy • This procedure allows users to and Planetary Sciences—College of Engineering, Forestry, and Natural Sciences, Northern Arizona University, Flagstaff, generate Mastcam image viewsheds: 3 4 locate in a map view the Mars AZ, USA, Department of Earth Sciences, Dartmouth College, Hanover, NH, USA, Division of Geological and Planetary 5 terrains visible in Mastcam images Sciences, California Institute of Technology, Pasadena, CA, USA, Malin Space Science Systems, San Diego, CA, USA • This procedure uses ArcGIS® and publicly available Mars datasets Abstract The Mastcam (Mast Camera) instrument onboard the NASA Curiosity rover provides an Supporting Information: exclusive view of Mars: High‐resolution color images from Mastcam allow users to study Gale crater's • Dataset S1 geologic terrains along Curiosity's path. These ground observations complement the spatially broader • Dataset S2 • Dataset S3 views of Gale crater provided by spacecrafts from orbit. However, for a given Mastcam image, it can be • Table S1 challenging to locate the corresponding terrains on the orbital view. No method for locating Mastcam images • Table S2 onto orbital images had been made publicly available. -
Gnc 2021 Abstract Book
GNC 2021 ABSTRACT BOOK Contents GNC Posters ................................................................................................................................................... 7 Poster 01: A Software Defined Radio Galileo and GPS SW receiver for real-time on-board Navigation for space missions ................................................................................................................................................. 7 Poster 02: JUICE Navigation camera design .................................................................................................... 9 Poster 03: PRESENTATION AND PERFORMANCES OF MULTI-CONSTELLATION GNSS ORBITAL NAVIGATION LIBRARY BOLERO ........................................................................................................................................... 10 Poster 05: EROSS Project - GNC architecture design for autonomous robotic On-Orbit Servicing .............. 12 Poster 06: Performance assessment of a multispectral sensor for relative navigation ............................... 14 Poster 07: Validation of Astrix 1090A IMU for interplanetary and landing missions ................................... 16 Poster 08: High Performance Control System Architecture with an Output Regulation Theory-based Controller and Two-Stage Optimal Observer for the Fine Pointing of Large Scientific Satellites ................. 18 Poster 09: Development of High-Precision GPSR Applicable to GEO and GTO-to-GEO Transfer ................. 20 Poster 10: P4COM: ESA Pointing Error Engineering -
JUICE Red Book
ESA/SRE(2014)1 September 2014 JUICE JUpiter ICy moons Explorer Exploring the emergence of habitable worlds around gas giants Definition Study Report European Space Agency 1 This page left intentionally blank 2 Mission Description Jupiter Icy Moons Explorer Key science goals The emergence of habitable worlds around gas giants Characterise Ganymede, Europa and Callisto as planetary objects and potential habitats Explore the Jupiter system as an archetype for gas giants Payload Ten instruments Laser Altimeter Radio Science Experiment Ice Penetrating Radar Visible-Infrared Hyperspectral Imaging Spectrometer Ultraviolet Imaging Spectrograph Imaging System Magnetometer Particle Package Submillimetre Wave Instrument Radio and Plasma Wave Instrument Overall mission profile 06/2022 - Launch by Ariane-5 ECA + EVEE Cruise 01/2030 - Jupiter orbit insertion Jupiter tour Transfer to Callisto (11 months) Europa phase: 2 Europa and 3 Callisto flybys (1 month) Jupiter High Latitude Phase: 9 Callisto flybys (9 months) Transfer to Ganymede (11 months) 09/2032 – Ganymede orbit insertion Ganymede tour Elliptical and high altitude circular phases (5 months) Low altitude (500 km) circular orbit (4 months) 06/2033 – End of nominal mission Spacecraft 3-axis stabilised Power: solar panels: ~900 W HGA: ~3 m, body fixed X and Ka bands Downlink ≥ 1.4 Gbit/day High Δv capability (2700 m/s) Radiation tolerance: 50 krad at equipment level Dry mass: ~1800 kg Ground TM stations ESTRAC network Key mission drivers Radiation tolerance and technology Power budget and solar arrays challenges Mass budget Responsibilities ESA: manufacturing, launch, operations of the spacecraft and data archiving PI Teams: science payload provision, operations, and data analysis 3 Foreword The JUICE (JUpiter ICy moon Explorer) mission, selected by ESA in May 2012 to be the first large mission within the Cosmic Vision Program 2015–2025, will provide the most comprehensive exploration to date of the Jovian system in all its complexity, with particular emphasis on Ganymede as a planetary body and potential habitat. -
MSS/1: Single‐Station and Single‐Event Marsquake Inversion
RESEARCH ARTICLE MSS/1: Single‐Station and Single‐Event 10.1029/2020EA001118 Marsquake Inversion Special Section: Mélanie Drilleau1,2 , Éric Beucler3 , Philippe Lognonné1 , Mark P. Panning4 , InSight at Mars 5 4 6,7 8 Brigitte Knapmeyer‐Endrun , W. Bruce Banerdt , Caroline Beghein , Savas Ceylan , Martin van Driel8 , Rakshit Joshi9 , Taichi Kawamura1, Amir Khan8,10 , Key Points: Sabrina Menina1 , Attilio Rivoldini11 , Henri Samuel1 , Simon Stähler8 , Haotian Xu6 , • In the framework on the InSight 3 8 8 1 12 mission, a synthetic seismogram Mickaël Bonnin , John Clinton , Domenico Giardini , Balthasar Kenda , Vedran Lekic , 3 2 13 4 using a 3‐D crust and a 1‐D velocity Antoine Mocquet , Naomi Murdoch , Martin Schimmel , Suzanne E. Smrekar , model below is proposed Éléonore Stutzmann1 , Benoit Tauzin14,15 , and Saikiran Tharimena4 • This signal is used to present inversion methods, relying on 1Institut de Physique du Globe de Paris, Sorbonne Paris Cité, CNRS F‐7500511, Université Paris Diderot, Paris, France, different parameterizations, to 2ISAE‐SUPAERO, Toulouse University, Toulouse, France, 3Laboratoire de Planétologie et de Géodynamique, Université constrain the 1‐D structure of Mars 4 • The results demonstrate the de Nantes, Université d'Angers, Nantes, France, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, feasibility of the strategy to retrieve CA, USA, 5Bensberg Observatory, University of Cologne, Cologne, Germany, 6Department of Earth, Planetary, and Space 7 8 VS in the crust, and a fairly good Sciences, -
Why Do We Explore?
Why Do We Explore? Lesson Six Why Do We Explore? About This Lesson Students will work in small teams, each of which will be given a different reason why humans explore. Each team will become the expert on their one reason and will add a letter and summary sentence to an EXPLORE poster using their reason for exploration. With all the reasons on the poster, the word EXPLORE will be complete. Students will be using the skills of working in cooperative learning teams, reading, summarizing, paraphrasing, and creating a sentence that will best represent their reason for exploration. Students will also be illustrating and copying other teams sentences so that each student will have a small copy of the large class- room poster for reference or extension purposes. The teacher will lead a discussion that relates the reasons humans explore to the planned and possible future missions to Mars. Objectives Students will: v review the seven traditional reasons why people explore v write a summary of their reason why humans explore v illustrate their exploration summaries v relate the reasons for exploration to the missions to Mars Background Students do not always realize that the steps in future exploration are built on a tradition of Why Do We Explore? exploration that is as old as humans. This lesson is intended to introduce the concept of exploration through the seven traditional reasons that express why humans have always been explorers. Social scientists know that everyone, no matter how young or old, is constantly exploring the world and how it works. Space exploration, including the possible missions to Mars, has opened up a whole new world for us to explore. -
Mars Subsurface Water Ice Mapping (Swim): Radar Subsurface Reflectors
50th Lunar and Planetary Science Conference 2019 (LPI Contrib. No. 2132) 2069.pdf MARS SUBSURFACE WATER ICE MAPPING (SWIM): RADAR SUBSURFACE REFLECTORS. A. M. Bramson1, E. I. Petersen1, Z. M. Bain2, N. E. Putzig2, G. A. Morgan2, M. Mastrogiuseppe3, M. R. Perry2, I. B. Smith2, H. G. Sizemore2, D. M. H. Baker4, R. H. Hoover5, B. A. Campbell6. 1Lunar and Planetary Laboratory, University of Arizona ([email protected]), 2Planetary Science Institute, 3California Institute of Technology, 4NASA Goddard Space Flight Center, 5Southwest Research Institute, 6Smithsonian Institution Introduction: The Subsurface Water Ice Mapping Consistency Mapping: To enable a quantitative as- (SWIM) in the Northern Hemisphere of Mars, supports sessment of how consistent (or inconsistent) the various an effort by NASA’s Mars Exploration Program to de- remote sensing datasets are with the presence of shallow termine in situ resource availability. We are performing (<5 m) and deep (>5 m) ice across these regions, we in- global reconnaissance mapping as well as focused troduce the SWIM Equation. Outlined in detail by Perry multi-dataset mapping from 0º to 60ºN in four longitude et al. [this LPSC], the SWIM Equation yields con- bands: “Arcadia” (150–225ºE, which also contains our sistency values ranging between +1 and -1, where +1 pilot study region), “Acidalia” (290–360ºE), “Onilus” means that the data are consistent with the presence of (0–70ºE, which covers Deuteronilus and Protonilus ice, 0 means that the data give no indications of the pres- Mensae), and “Utopia” (70–150ºE). Our maps are being ence or absence of ice, and -1 means that the data are made available to the community on the SWIM Project inconsistent with the presence of ice. -
Mars Exploration: an Overview of Indian and International Mars Missions Nayamavalsa Scariah1, Dr
Taurian Innovative Journal/Volume 1/ Issue 1 Mars exploration: An overview of Indian and International Mars Missions NayamaValsa Scariah1, Dr. Mili Ghosh2, Dr.A.P.Krishna3 Birla Institute of Technology, Mesra, Ranchi Abstract- Mars is the fourth planet from the sun. It is 1. Introduction also known as red planet because of its iron oxide content. There are lots of missions have been launched to Mars is also known as red planet, because of the mars for better understanding of our neighboring planet. reddish iron oxide prevalent on its surface gives it a There are lots of unmanned spacecraft including reddish appearance. It is the fourth planet from sun. orbiters, landers and rovers have been launched into mars since early 1960. Sputnik was the first satellite The term sol is used to define duration of solar day on launched in 1957 by Soviet Union. After seven failure Mars. A mean Martian solar day or sol is 24 hours 39 missions to Mars, Mariner 4 was the first satellite which minutes and 34.244 seconds. Many space missions to reached the Martian orbiter successfully. The Viking 1 Mars have been planned and launched for Mars was the first lander reached on Mars on 1975. India exploration (Table:1) but most of them failed without successfully launched a spacecraft, Mangalyan (Mars completing the task specially in early attempts th Orbiter Mission) on 5 November, 2013, with five whereas some NASA missions were very payloads to Mars. India was the first nation to successful(such as the twin Mars Exploration Rovers, successfully reach Mars on its first attempt. -
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. -
Appendix 1: Venus Missions
Appendix 1: Venus Missions Sputnik 7 (USSR) Launch 02/04/1961 First attempted Venus atmosphere craft; upper stage failed to leave Earth orbit Venera 1 (USSR) Launch 02/12/1961 First attempted flyby; contact lost en route Mariner 1 (US) Launch 07/22/1961 Attempted flyby; launch failure Sputnik 19 (USSR) Launch 08/25/1962 Attempted flyby, stranded in Earth orbit Mariner 2 (US) Launch 08/27/1962 First successful Venus flyby Sputnik 20 (USSR) Launch 09/01/1962 Attempted flyby, upper stage failure Sputnik 21 (USSR) Launch 09/12/1962 Attempted flyby, upper stage failure Cosmos 21 (USSR) Launch 11/11/1963 Possible Venera engineering test flight or attempted flyby Venera 1964A (USSR) Launch 02/19/1964 Attempted flyby, launch failure Venera 1964B (USSR) Launch 03/01/1964 Attempted flyby, launch failure Cosmos 27 (USSR) Launch 03/27/1964 Attempted flyby, upper stage failure Zond 1 (USSR) Launch 04/02/1964 Venus flyby, contact lost May 14; flyby July 14 Venera 2 (USSR) Launch 11/12/1965 Venus flyby, contact lost en route Venera 3 (USSR) Launch 11/16/1965 Venus lander, contact lost en route, first Venus impact March 1, 1966 Cosmos 96 (USSR) Launch 11/23/1965 Possible attempted landing, craft fragmented in Earth orbit Venera 1965A (USSR) Launch 11/23/1965 Flyby attempt (launch failure) Venera 4 (USSR) Launch 06/12/1967 Successful atmospheric probe, arrived at Venus 10/18/1967 Mariner 5 (US) Launch 06/14/1967 Successful flyby 10/19/1967 Cosmos 167 (USSR) Launch 06/17/1967 Attempted atmospheric probe, stranded in Earth orbit Venera 5 (USSR) Launch 01/05/1969 Returned atmospheric data for 53 min on 05/16/1969 M.