Looking for Life on Mars Professor Andrew Coates 23 September 2020
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A Stringent Upper Limit of 20 Pptv for Methane on Mars and Constraints on Its Dispersion Outside Gale Crater F
A&A 650, A140 (2021) Astronomy https://doi.org/10.1051/0004-6361/202140389 & © F. Montmessin et al. 2021 Astrophysics A stringent upper limit of 20 pptv for methane on Mars and constraints on its dispersion outside Gale crater F. Montmessin1 , O. I. Korablev2 , A. Trokhimovskiy2 , F. Lefèvre3 , A. A. Fedorova2 , L. Baggio1 , A. Irbah1 , G. Lacombe1, K. S. Olsen4 , A. S. Braude1 , D. A. Belyaev2 , J. Alday4 , F. Forget5 , F. Daerden6, J. Pla-Garcia7,8 , S. Rafkin8 , C. F. Wilson4, A. Patrakeev2, A. Shakun2, and J. L. Bertaux1 1 LATMOS/IPSL, UVSQ Université Paris-Saclay, Sorbonne Université, CNRS, Guyancourt, France e-mail: [email protected] 2 Space Research Institute (IKI) RAS, Moscow, Russia 3 LATMOS/IPSL, Sorbonne Université, UVSQ Université Paris-Saclay, CNRS, Paris, France 4 AOPP, Oxford University, Oxford, UK 5 Laboratoire de Météorologie Dynamique, Sorbonne Université, Paris, France 6 BIRA-IASB, Bruxelles, Belgium 7 Centro de Astrobiología (CSIC?INTA), Torrejón de Ardoz, Spain 8 Southwest Research Institute, Boulder, CO, USA Received 20 January 2021 / Accepted 23 April 2021 ABSTRACT Context. Reports on the detection of methane in the Martian atmosphere have motivated numerous studies aiming to confirm or explain its presence on a planet where it might imply a biogenic or more likely a geophysical origin. Aims. Our intent is to complement and improve on the previously reported detection attempts by the Atmospheric Chemistry Suite (ACS) on board the ExoMars Trace Gas Orbiter (TGO). This latter study reported the results of a campaign that was a few months in length, and was significantly hindered by a dusty period that impaired detection performances. -
Lara (Lander Radioscience) on the Exomars 2020 Surface Platform
EPSC Abstracts Vol. 13, EPSC-DPS2019-891-1, 2019 EPSC-DPS Joint Meeting 2019 c Author(s) 2019. CC Attribution 4.0 license. LaRa (Lander Radioscience) on the ExoMars 2020 Surface Platform. Véronique Dehant1,2, Sébastien Le Maistre1, Rose-Marie Baland1, Özgür Karatekin1, Marie-Julie Péters1, Attilio Rivoldini1, Tim Van Hoolst1, Bart Van Hove1, Marie Yseboodt1, and Alexander Kosov3 (1) Royal Observatory of Belgium (ROB), Brussels, Belgium, (2) Université catholique de Louvain, Louvain-la-Neuve, Belgium, (3) Space Research Institute Russian Academy of Sciences (IKI), Moscow, Russia Abstract The surface platform Kazachok will house the radio science experiment LaRa (Lander Radioscience) to support specific scientific objectives of the ExoMars 2020 mission. The LaRa experiment is described and the scientific objectives and strategies are detailed in this presentation. Figure 1. LaRa principle. 1. Introduction 2. The LaRa instrument In the last decade, several missions and observations As LaRa performs a coherent retransmission of the have brought new data on the planet Mars, obtained uplink carrier to the downlink carrier, the downlink by either spacecraft orbiting around Mars or landers frequency is scaled by a constant multiplier, the and rovers on the surface. Among other things, the transponder ratio (880/749). By emitting the uplink information acquired will improve our understanding signal from Earth, the masers in the ground stations of Mars’ interior, evolution and habitability. Data ensure frequency stability of LaRa’s radiosignal. obtained by new space missions are driving further The LaRa instrument is built in collaboration with progress in this field. In 2020, the European Space other Belgian actors under the lead of ESA PRODEX, Agency ESA and the Russian space agency and ROB providing the instrument specifications. -
Mars Reconnaissance Orbiter Navigation Strategy for the Exomars Schiaparelli EDM Lander Mission
Jet Propulsion Laboratory California Institute of Technology Mars Reconnaissance Orbiter Navigation Strategy for the ExoMars Schiaparelli EDM Lander Mission Premkumar R. Menon Sean V. Wagner, David C. Jefferson, Eric J. Graat, Kyong J. Lee, and William B. Schulze AAS/AIAA Astrodynamics Specialist Conference San Antonio, Texas February 5–9, 2017 AAS Paper 17-337 © 2017 California Institute of Technology. Government Sponsorship Acknowledged. Mars Reconnaissance Orbiter Project Mars Reconnaissance Orbiter (Mission, Spacecraft and PSO) The Mars Reconnaissance Orbiter mission launched in August 2005 from the Cape Canaveral Air Force Station arriving at Mars in March 2006 started science operations in November 2006. MRO has completed 10 years since launch (50,000 orbits by Mar 2017) and to date has returned nearly 300 Terabytes of data. MRO Primary Science Orbit (PSO): • Sun-synchronous orbit ascending node at 3:00 PM ± 15 minutes Local Mean Solar Time (LMST) (daylight equatorial crossing) • Periapsis is frozen about the Mars South Pole • Near-repeat ground track walk (GTW) every 17-day, 211 orbit (short-term repeat) MRO targeting cycle, exact repeat after 4602 orbits. The nominal GTW is 32.45811 km West each 211 orbit cycle (maintained with periodic maneuvers). MRO Spacecraft: • Spacecraft Bus: 3-axis stabilized ACS system; 3-meter diameter High Gain Antenna; hydrazine propulsion system • Instrument Suite: HiRISE Camera, CRISM Imaging spectrometer, Mars Climate Sounder, Mars Color Imager, Context Camera, Shallow Subsurface Radar, Electra engineering payload (among other instrument payloads) 2/07/17 MRO support of ExoMars Schiaparelli Lander Overflight Relay PRM-3 4. MRO shall have good overflight pass geometry within the first 2 Sols after landing. -
Exomars Schiaparelli Direct-To-Earth Observation Using GMRT
TECHNICAL ExoMars Schiaparelli Direct-to-Earth Observation REPORTS: METHODS 10.1029/2018RS006707 using GMRT S. Esterhuizen1, S. W. Asmar1 ,K.De2, Y. Gupta3, S. N. Katore3, and B. Ajithkumar3 Key Point: • During ExoMars Landing, GMRT 1Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA, USA, 2Cahill Center for Astrophysics, observed UHF transmissions and California Institute of Technology, Pasadena, CA, USA, 3National Centre for Radio Astrophysics, Pune, India Doppler shift used to identify key events as only real-time aliveness indicator Abstract During the ExoMars Schiaparelli separation event on 16 October 2016 and Entry, Descent, and Landing (EDL) events 3 days later, the Giant Metrewave Radio Telescope (GMRT) near Pune, India, Correspondence to: S. W. Asmar, was used to directly observe UHF transmissions from the Schiaparelli lander as they arrive at Earth. The [email protected] Doppler shift of the carrier frequency was measured and used as a diagnostic to identify key events during EDL. This signal detection at GMRT was the only real-time aliveness indicator to European Space Agency Citation: mission operations during the critical EDL stage of the mission. Esterhuizen, S., Asmar, S. W., De, K., Gupta, Y., Katore, S. N., & Plain Language Summary When planetary missions, such as landers on the surface of Mars, Ajithkumar, B. (2019). ExoMars undergo critical and risky events, communications to ground controllers is very important as close to real Schiaparelli Direct-to-Earth observation using GMRT. time as possible. The Schiaparelli spacecraft attempted landing in 2016 was supported in an innovative way. Radio Science, 54, 314–325. A large radio telescope on Earth was able to eavesdrop on information being sent from the lander to other https://doi.org/10.1029/2018RS006707 spacecraft in orbit around Mars. -
Aerothermodynamic Analysis of a Mars Sample Return Earth-Entry Vehicle" (2018)
Old Dominion University ODU Digital Commons Mechanical & Aerospace Engineering Theses & Dissertations Mechanical & Aerospace Engineering Summer 2018 Aerothermodynamic Analysis of a Mars Sample Return Earth- Entry Vehicle Daniel A. Boyd Old Dominion University, [email protected] Follow this and additional works at: https://digitalcommons.odu.edu/mae_etds Part of the Aerodynamics and Fluid Mechanics Commons, Space Vehicles Commons, and the Thermodynamics Commons Recommended Citation Boyd, Daniel A.. "Aerothermodynamic Analysis of a Mars Sample Return Earth-Entry Vehicle" (2018). Master of Science (MS), Thesis, Mechanical & Aerospace Engineering, Old Dominion University, DOI: 10.25777/xhmz-ax21 https://digitalcommons.odu.edu/mae_etds/43 This Thesis is brought to you for free and open access by the Mechanical & Aerospace Engineering at ODU Digital Commons. It has been accepted for inclusion in Mechanical & Aerospace Engineering Theses & Dissertations by an authorized administrator of ODU Digital Commons. For more information, please contact [email protected]. AEROTHERMODYNAMIC ANALYSIS OF A MARS SAMPLE RETURN EARTH-ENTRY VEHICLE by Daniel A. Boyd B.S. May 2008, Virginia Military Institute M.A. August 2015, Webster University A Thesis Submitted to the Faculty of Old Dominion University in Partial Fulfillment of the Requirements for the Degree of MASTER OF SCIENCE AEROSPACE ENGINEERING OLD DOMINION UNIVERSITY August 2018 Approved by: __________________________ Robert L. Ash (Director) __________________________ Oktay Baysal (Member) __________________________ Jamshid A. Samareh (Member) __________________________ Shizhi Qian (Member) ABSTRACT AEROTHERMODYNAMIC ANALYSIS OF A MARS SAMPLE RETURN EARTH-ENTRY VEHICLE Daniel A. Boyd Old Dominion University, 2018 Director: Dr. Robert L. Ash Because of the severe quarantine constraints that must be imposed on any returned extraterrestrial samples, the Mars sample return Earth-entry vehicle must remain intact through sample recovery. -
The Mystery of Methane on Mars and Titan
The Mystery of Methane on Mars & Titan By Sushil K. Atreya MARS has long been thought of as a possible abode of life. The discovery of methane in its atmosphere has rekindled those visions. The visible face of Mars looks nearly static, apart from a few wispy clouds (white). But the methane hints at a beehive of biological or geochemical activity underground. Of all the planets in the solar system other than Earth, own way, revealing either that we are not alone in the universe Mars has arguably the greatest potential for life, either extinct or that both Mars and Titan harbor large underground bodies or extant. It resembles Earth in so many ways: its formation of water together with unexpected levels of geochemical activ- process, its early climate history, its reservoirs of water, its vol- ity. Understanding the origin and fate of methane on these bod- canoes and other geologic processes. Microorganisms would fit ies will provide crucial clues to the processes that shape the right in. Another planetary body, Saturn’s largest moon Titan, formation, evolution and habitability of terrestrial worlds in also routinely comes up in discussions of extraterrestrial biology. this solar system and possibly in others. In its primordial past, Titan possessed conditions conducive to Methane (CH4) is abundant on the giant planets—Jupiter, the formation of molecular precursors of life, and some scientists Saturn, Uranus and Neptune—where it was the product of chem- believe it may have been alive then and might even be alive now. ical processing of primordial solar nebula material. On Earth, To add intrigue to these possibilities, astronomers studying though, methane is special. -
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). -
Exomars Trace Gas Orbiter Operations ESOC
Training Opportunity for Swiss Trainees Reference Title Duty Station CH-2019-OPS-OPE Exomars Trace Gas Orbiter operations ESOC Overview of the unit’s mission: OPS-OP is responsible for mission preparation and flight operations for the ESA fleet of solar and interplanetary spacecraft. The division currently operates four missions (Cluster, Mars Express, ExoMars TGO, Bepi Colombo) and prepares for the launch of three others (Solar Orbiter, ExoMars Rover and Surface Platform, JUICE). Within OPS-OP, the ExoMars TGO unit (OPS-OPE) is responsible for the operations of the Trace Gas Orbiter (TGO) in-orbit around Mars. This includes monitoring, control and mission planning of the satellite as well as the mission responsibility for the required data systems and related interfaces. Overview of the field of activity proposed: The ExoMars TGO is the first in a series of Mars missions undertaken jointly by ESA and Roscosmos. From its 400-km- altitude science orbit TGO shall gain a better understanding of methane and other atmospheric gases present in small concentrations (less than 1% of the atmosphere) which could be evidence for possible biological or geological activity. The Orbiter is also an invaluable Mars telecommunications asset, currently providing communication services to NASA rovers (or landers) on the Mars Surface: it acts as a data relay hub for sending commands to the rovers and downloading rover data to Earth using ESA, NASA and Russian space communication networks. This relay function will serve the ExoMars 2020 mission, combining a European Rover and a Russian science Surface Platform, planned to land on Mars in March 2021. -
Pancam: a Multispectral Imaging Investigation on the NASA 2003 Mars Exploration Rover Mission
Sixth International Conference on Mars (2003) 3029.pdf Pancam: A Multispectral Imaging Investigation on the NASA 2003 Mars Exploration Rover Mission. J.F. Bell III1, S.W. Squyres1, K.E. Herkenhoff2, J. Maki3, M. Schwochert3, A. Dingizian3, D. Brown3, R.V. Morris4, H.M. Arneson1, M.J. Johnson1, J. Joseph1, J.N. Sohl-Dickstein1, and the Athena Science Team. 1Cornell University, Dept. of Astronomy, Ithaca NY 14853-6801; [email protected] , 2USGS Branch of Astrogeology, Flagstaff AZ 86001, 3JPL/Caltech, Pasadena CA 91109, 4NASA/JSC, Code SR, Houston TX 77058. Introduction: One of the six science payload ele- both cameras consist of identical 3-element symmetri- ments carried on each of the NASA Mars Exploration cal lenses with an effective focal length of 42 mm and Rovers (MER; Figure 1) is the Panoramic Camera a focal ratio of f/20, yielding an IFOV of 0.28 System, or Pancam. Pancam consists of three major mrad/pixel or a rectangular Field of View (FOV) of components: a pair of digital CCD cameras, the Pan- 16°× 16° per eye (Figures 3,4). The two eyes are sepa- cam Mast Assembly (PMA), and a radiometric cali- rated by 30 cm horizontally and have a 1° toe-in to bration target [1]. The PMA provides the azimuth and provide adequate parallax for stereo imaging (Figure elevation actuation for the cameras as well as a 1.5 5). The camera FOVs have been determined relative to meter high vantage point from which to image. The the adjacent wide-field stereo Navigation Cameras, and calibration target provides a set of reference color and the Mini-TES FOV. -
Mars 2020 Radiological Contingency Planning
National Aeronautics and Space Administration Mars 2020 Radiological Contingency Planning NASA plans to launch the Mars 2020 rover, produce the rover’s onboard power and to Perseverance, in summer 2020 on a mission warm its internal systems during the frigid to seek signs of habitable conditions in Mars’ Martian night. ancient past and search for signs of past microbial life. The mission will lift off from Cape NASA prepares contingency response plans Canaveral Air Force Station in Florida aboard a for every launch that it conducts. Ensuring the United Launch Alliance Atlas V launch vehicle safety of launch-site workers and the public in between mid-July and August 2020. the communities surrounding the launch area is the primary consideration in this planning. The Mars 2020 rover design is based on NASA’s Curiosity rover, which landed on Mars in 2012 This contingency planning task takes on an and greatly increased our knowledge of the added dimension when the payload being Red Planet. The Mars 2020 rover is equipped launched into space contains nuclear material. to study its landing site in detail and collect and The primary goal of radiological contingency store the most promising samples of rock and planning is to enable an efficient response in soil on the surface of Mars. the event of an accident. This planning is based on the fundamental principles of advance The system that provides electrical power for preparation (including rehearsals of simulated Mars 2020 and its scientific equipment is the launch accident responses), the timely availability same as for the Curiosity rover: a Multi- of technically accurate and reliable information, Mission Radioisotope Thermoelectric Generator and prompt external communication with the (MMRTG). -
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 Impacting Descent Probe for Europa and the Other Galilean Moons of Jupiter
An Impacting Descent Probe for Europa and the other Galilean Moons of Jupiter P. Wurz1,*, D. Lasi1, N. Thomas1, D. Piazza1, A. Galli1, M. Jutzi1, S. Barabash2, M. Wieser2, W. Magnes3, H. Lammer3, U. Auster4, L.I. Gurvits5,6, and W. Hajdas7 1) Physikalisches Institut, University of Bern, Bern, Switzerland, 2) Swedish Institute of Space Physics, Kiruna, Sweden, 3) Space Research Institute, Austrian Academy of Sciences, Graz, Austria, 4) Institut f. Geophysik u. Extraterrestrische Physik, Technische Universität, Braunschweig, Germany, 5) Joint Institute for VLBI ERIC, Dwingelo, The Netherlands, 6) Department of Astrodynamics and Space Missions, Delft University of Technology, The Netherlands 7) Paul Scherrer Institute, Villigen, Switzerland. *) Corresponding author, [email protected], Tel.: +41 31 631 44 26, FAX: +41 31 631 44 05 1 Abstract We present a study of an impacting descent probe that increases the science return of spacecraft orbiting or passing an atmosphere-less planetary bodies of the solar system, such as the Galilean moons of Jupiter. The descent probe is a carry-on small spacecraft (< 100 kg), to be deployed by the mother spacecraft, that brings itself onto a collisional trajectory with the targeted planetary body in a simple manner. A possible science payload includes instruments for surface imaging, characterisation of the neutral exosphere, and magnetic field and plasma measurement near the target body down to very low-altitudes (~1 km), during the probe’s fast (~km/s) descent to the surface until impact. The science goals and the concept of operation are discussed with particular reference to Europa, including options for flying through water plumes and after-impact retrieval of very-low altitude science data.