Simulating Exomars Rosalind Franklin Rover Operations
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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. -
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. -
Outline of Aurora Funding
Outline of Aurora funding The £3 million from the Aurora Science Programme has gone to the following 17 academics and individual scientists working at UK research organisations: 1. An improved understanding of Mars photochemistry using NOMAD and ACS measurements – Professor Paul Palmer, Edinburgh University - £73,442 The proposal aims to develop the existing photochemistry (the chemistry effects of light) to prepare for measurements collected by the NOMAD and ACS instruments aboard the Trace Gas Orbiter. They will develop the chemical mechanism so it can be used to interpret observed variations of atmospheric gases on Mars. 2. Dust storms and the dust transport cycle: their impact on the Martian climate in a multi annual reanalysis of MCS, THEMIS and TGO/ACS data – Professor Peter Read, Oxford University - £346,592 The proposal aims to improve our understanding of the Martian dust cycle, its impact on climate and the physical features of the Martian surface. Using a new approach towards analysing daily variations in the Martian atmosphere it is proposed to extend this dataset using measurements of the Martian atmosphere from the Mars Reconnaissance Orbiter and Mars Odyssey missions in orbit around Mars, and from the Atmospheric Chemistry Suite (ACS) on ESA's Trace Gas Orbiter mission when they become available. This may be useful for future spacecraft operations at the Martian surface, as well as to improve our understanding of both the present and past states of the Martian climate. 3. ExoMars TGO Guest Investigator Support – Dr Matt Balme, Open University - £56,367 This proposal seeks funding for a Guest Investigator position on ESA's ExoMars Trace Gas Orbiter mission. -
EDL – Lessons Learned and Recommendations
."#!(*"# 0 1(%"##" !)"#!(*"#* 0 1"!#"("#"#(-$" ."!##("""*#!#$*#( "" !#!#0 1%"#"! /!##"*!###"#" #"#!$#!##!("""-"!"##&!%%!%&# $!!# %"##"*!%#'##(#!"##"#!$$# /25-!&""$!)# %"##!""*&""#!$#$! !$# $##"##%#(# ! "#"-! *#"!,021 ""# !"$!+031 !" )!%+041 #!( !"!# #$!"+051 # #$! !%#-" $##"!#""#$#$! %"##"#!#(- IPPW Enabled International Collaborations in EDL – Lessons Learned and Recommendations: Ethiraj Venkatapathy1, Chief Technologist, Entry Systems and Technology Division, NASA ARC, 2 Ali Gülhan , Department Head, Supersonic and Hypersonic Technologies Department, DLR, Cologne, and Michelle Munk3, Principal Technologist, EDL, Space Technology Mission Directorate, NASA. 1 NASA Ames Research Center, Moffett Field, CA [email protected]. 2 Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR), German Aerospace Center, [email protected] 3 NASA Langley Research Center, Hampron, VA. [email protected] Abstract of the Proposed Talk: One of the goals of IPPW has been to bring about international collaboration. Establishing collaboration, especially in the area of EDL, can present numerous frustrating challenges. IPPW presents opportunities to present advances in various technology areas. It allows for opportunity for general discussion. Evaluating collaboration potential requires open dialogue as to the needs of the parties and what critical capabilities each party possesses. Understanding opportunities for collaboration as well as the rules and regulations that govern collaboration are essential. The authors of this proposed talk have explored and established collaboration in multiple areas of interest to IPPW community. The authors will present examples that illustrate the motivations for the partnership, our common goals, and the unique capabilities of each party. The first example involves earth entry of a large asteroid and break-up. NASA Ames is leading an effort for the agency to assess and estimate the threat posed by large asteroids under the Asteroid Threat Assessment Project (ATAP). -
Argops) Solution to the 2017 Astrodynamics Specialist Conference Student Competition
AAS 17-621 THE ASTRODYNAMICS RESEARCH GROUP OF PENN STATE (ARGOPS) SOLUTION TO THE 2017 ASTRODYNAMICS SPECIALIST CONFERENCE STUDENT COMPETITION Jason A. Reiter,* Davide Conte,1 Andrew M. Goodyear,* Ghanghoon Paik,* Guanwei. He,* Peter C. Scarcella,* Mollik Nayyar,* Matthew J. Shaw* We present the methods and results of the Astrodynamics Research Group of Penn State (ARGoPS) team in the 2017 Astrodynamics Specialist Conference Student Competition. A mission (named Minerva) was designed to investigate Asteroid (469219) 2016 HO3 in order to determine its mass and volume and to map and characterize its surface. This data would prove useful in determining the necessity and usefulness of future missions to the asteroid. The mission was designed such that a balance between cost and maximizing objectives was found. INTRODUCTION Asteroid (469219) 2016 HO3 was discovered recently and has yet to be explored. It lies in a quasi-orbit about the Earth such that it will follow the Earth around the Sun for at least the next several hundred years providing many opportunities for relatively low-cost missions to the body. Not much is known about 2016 HO3 except a general size range, but its close proximity to Earth makes a scientific mission more feasible than other near-Earth objects. A Request For Proposal (RFP) was provided to university teams searching for cost-efficient mission design solutions to assist in the characterization of the asteroid and the assessment of its potential for future, more in-depth missions and possible resource utilization. The RFP provides constraints on launch mass, bus size as well as other mission architecture decisions, and sets goals for scientific mapping and characterization. -
Change in the Wind and Climate at the Exomars 2022 Landing Site in Oxia Planum (Mars)
52nd Lunar and Planetary Science Conference 2021 (LPI Contrib. No. 2548) 1442.pdf CHANGE IN THE WIND AND CLIMATE AT THE EXOMARS 2022 LANDING SITE IN OXIA PLANUM (MARS). S. Silvestro1,2, D. Tirsch3, A. Pacifici4, F. Salese5,4, D.A. Vaz6, A. Neesemann7, C.I. Popa1, M. Pajola8, G. Franzese1, G. Mongelluzzo1,9, A.C. Ruggeri1, F. Cozzolino1, C. Porto1, F. Esposito1. 1INAF, Osservatorio Astronomico di Capodimonte, Napoli, Italy ([email protected]). 2SETI Institute, Carl Sagan Center, Mountain View, CA, USA. 3Institute of Planetary Research, DLR, Berlin, Germany. 4IRSPS, Università G. D’Annunzio, Pescara, Italy. 5Centro de Astrobiología, CSIC- INTA, Madrid. 6CESR University of Coimbra, Portugal. 7Freie Universitat, Berlin, Germany. 8INAF, Osservatorio Astronomico di Padova, Padova, Italy. 9Department of Industrial Engineering, Università Federico II, Napoli, Italy. Introduction: The ESA/ROSCOSMOS ExoMars Ridges are even visible in association with impact crater 2022 (a rover named “Rosalind Franklin” and a surface ejecta and are superimposed by 10-25 m craters and platform named “Kazachok”) [1] will land in Oxia boulders, so they pre-date these impact events (Fig. 1c). Planum (18.2° N; 24.3° W) to search for signs of past or When associated with crater ejecta, ridges locally show present life on Mars and to perform long-term two different crests (Fig. 2b). Both crests are truncated atmospheric investigations [2,3]. Oxia Planum shows by craters, which suggest that the double crest large outcrops of clay-rich Noachian-aged arrangement was emplaced before the impacts (Fig. 2c). phyllosilicates [4,5]. The clay bearing unit is To better understand the relative age of the ridges, we unconformably overlain by an Amazonian dark resistant mapped their occurrence on 316 craters in the study area unit (Adru), which was interpreted to be remnants of an that we qualitatively classified as relatively Early Amazonian (2.6 Ga) volcanic material [4]. -
Exploration of Mars by the European Space Agency 1
Exploration of Mars by the European Space Agency Alejandro Cardesín ESA Science Operations Mars Express, ExoMars 2016 IAC Winter School, November 20161 Credit: MEX/HRSC History of Missions to Mars Mars Exploration nowadays… 2000‐2010 2011 2013/14 2016 2018 2020 future … Mars Express MAVEN (ESA) TGO Future ESA (ESA- Studies… RUSSIA) Odyssey MRO Mars Phobos- Sample Grunt Return? (RUSSIA) MOM Schiaparelli ExoMars 2020 Phoenix (ESA-RUSSIA) Opportunity MSL Curiosity Mars Insight 2020 Spirit The data/information contained herein has been reviewed and approved for release by JPL Export Administration on the basis that this document contains no export‐controlled information. Mars Express 2003-2016 … First European Mission to orbit another Planet! First mission of the “Rosetta family” Up and running since 2003 Credit: MEX/HRSC First European Mission to orbit another Planet First European attempt to land on another Planet Original mission concept Credit: MEX/HRSC December 2003: Mars Express Lander Release and Orbit Insertion Collission trajectory Bye bye Beagle 2! Last picture Lander after release, release taken by VMC camera Insertion 19/12/2003 8:33 trajectory Credit: MEX/HRSC Beagle 2 was found in January 2015 ! Only 6km away from landing site OK Open petals indicate soft landing OK Antenna remained covered Lessons learned: comms at all time! Credit: MEX/HRSC Mars Express: so many missions at once Mars Mission Phobos Mission Relay Mission Credit: MEX/HRSC Mars Express science investigations Martian Moons: Phobos & Deimos: Ionosphere, surface, -
Range Resolution Enhancement of WISDOM/Exomars
Range resolution enhancement of WISDOM/ExoMars radar soundings by the Bandwidth Extrapolation technique: Validation and application to field campaign measurements Nicolas Oudart, Valérie Ciarletti, Alice Le Gall, Marco Mastrogiuseppe, Yann Herve, Wolf-Stefan Benedix, Dirk Plettemeier, Vivien Tranier, Rafik Hassen-Khodja, Christoph Statz, et al. To cite this version: Nicolas Oudart, Valérie Ciarletti, Alice Le Gall, Marco Mastrogiuseppe, Yann Herve, et al.. Range resolution enhancement of WISDOM/ExoMars radar soundings by the Bandwidth Extrapolation tech- nique: Validation and application to field campaign measurements. Planetary and Space Science, Elsevier, 2021, 197 (March), pp.105173. 10.1016/j.pss.2021.105173. insu-03114236v2 HAL Id: insu-03114236 https://hal-insu.archives-ouvertes.fr/insu-03114236v2 Submitted on 28 Jan 2021 HAL is a multi-disciplinary open access L’archive ouverte pluridisciplinaire HAL, est archive for the deposit and dissemination of sci- destinée au dépôt et à la diffusion de documents entific research documents, whether they are pub- scientifiques de niveau recherche, publiés ou non, lished or not. The documents may come from émanant des établissements d’enseignement et de teaching and research institutions in France or recherche français ou étrangers, des laboratoires abroad, or from public or private research centers. publics ou privés. Distributed under a Creative Commons Attribution| 4.0 International License Planetary and Space Science 197 (2021) 105173 Contents lists available at ScienceDirect Planetary -
Page 1 E X O M a R S E X O M a R S
NOTE ADDED BY JPL WEBMASTER: This document was prepared by the European Space Agency. The content has not been approved or adopted by, NASA, JPL, or the California Institute of Technology. This document is being made available for information purposes only, and any views and opinions expressed herein do not necessarily state or reflect those of NASA, JPL, or the California Institute of Technology. EE XX OO MM AA RR SS ExoMars Status th J. L. Vago and the ExoMars Project Team 20 MEPAG Meeting 3–4 March 2009, Arlington, VA (USA) ExoMars Original Objectives Technology Demonstration Objectives : Entry, Descent, and Landing (EDL) of a large payload on the surface of Mars; Surface mobility with a rover having several kilometres range; Access to the subsurface with a drill to acquire samples down to 2 metres; Automatic sample preparation and distribution for analysis with scientific instruments. Scientific Objectives (in order of priority): To search for signs of past and present life on Mars; To characterise the water/geochemical environment as a function of depth in the shallow subsurface; To study the surface environment and identify hazards to future human missions; To investigate the planet’s subsurface and deep interior to better understand its evolution and habitability. What is ExoMars Now? KEY REQUIREMENTS FOR EXOMARS : (but also for all future ESA Mars exploration missions) Clear synergy of technology and science goals: ExoMars has to land; ExoMars has to rove; ExoMars has to drill; ExoMars has to perform novel organics -
The Pancam Instrument for the Exomars Rover
ASTROBIOLOGY ExoMars Rover Mission Volume 17, Numbers 6 and 7, 2017 Mary Ann Liebert, Inc. DOI: 10.1089/ast.2016.1548 The PanCam Instrument for the ExoMars Rover A.J. Coates,1,2 R. Jaumann,3 A.D. Griffiths,1,2 C.E. Leff,1,2 N. Schmitz,3 J.-L. Josset,4 G. Paar,5 M. Gunn,6 E. Hauber,3 C.R. Cousins,7 R.E. Cross,6 P. Grindrod,2,8 J.C. Bridges,9 M. Balme,10 S. Gupta,11 I.A. Crawford,2,8 P. Irwin,12 R. Stabbins,1,2 D. Tirsch,3 J.L. Vago,13 T. Theodorou,1,2 M. Caballo-Perucha,5 G.R. Osinski,14 and the PanCam Team Abstract The scientific objectives of the ExoMars rover are designed to answer several key questions in the search for life on Mars. In particular, the unique subsurface drill will address some of these, such as the possible existence and stability of subsurface organics. PanCam will establish the surface geological and morphological context for the mission, working in collaboration with other context instruments. Here, we describe the PanCam scientific objectives in geology, atmospheric science, and 3-D vision. We discuss the design of PanCam, which includes a stereo pair of Wide Angle Cameras (WACs), each of which has an 11-position filter wheel and a High Resolution Camera (HRC) for high-resolution investigations of rock texture at a distance. The cameras and electronics are housed in an optical bench that provides the mechanical interface to the rover mast and a planetary protection barrier. -
MULTI-SCALE ANALYSIS of ALLUVIAL SEDIMENTARY OUTCROPS in UTAH USING EXOMARS 2020 PANCAM, ISEM, and CLUPI EMULATORS
49th Lunar and Planetary Science Conference 2018 (LPI Contrib. No. 2083) 1911.pdf MULTI-SCALE ANALYSIS OF ALLUVIAL SEDIMENTARY OUTCROPS IN UTAH USING EXOMARS 2020 PANCAM, ISEM, and CLUPI EMULATORS. E. J. Allender1, C. R. Cousins1, M. D. Gunn2, R. Barnes3 1School of Earth and Environmental Sciences, University of St Andrews, Irvine Building, North St, St Andrews, UK ([email protected]), 2Department of Physics, Penglais Campus, Aberystwyth University, Aberystwyth, UK, 3Imperial College London, Kensington, London, UK. Introduction: As the launch date for the Instrument emulators were deployed at each site to ESA/Roscosmos ExoMars 2020 rover draws near, the simulate the PanCam, ISEM, and CLUPI instruments need for analysis tools to exploit the wealth of data to onboard ExoMars 2020. These were: the Aberstwyth be returned by its Panoramic Camera (PanCam) [1], University PanCam Emulator (AUPE) [8] (spanning Infrared Spectrometer for Mars (ISEM) [2], and 440-1000 nm), a Spectral Evolution spectrometer CLose-UP Imager (CLUPI) [3] instruments becomes (ISEM-E) spanning 440-2500 nm with hyperspectral increasingly important; the exploitation of integrated reolution, and CLUPI-E - a Sigma DSLR camera con- data from these instruments will be invaluable in de- figured to CLUPI specifications [3]. AUPE and tecting evidence of past habitability on Mars and iden- CLUPI-E mosaics were collected at each site, and tifying drilling locations. ISEM-E data points were collected either as vertical Together, PanCam, ISEM, and CLUPI offer multi- logs, or spanning each distinct unit. Soil and rock sam- scale analysis capabilities in both spatial (~140-1310 ples were also collected for each imaged unit at the µm/pixel at 2 m working distance), and spectral (350- study sites to provide spectral and mineralogical 3300 nm) dimensions. -
Investigating Mars' Atmosphere Using the NOMAD Instrument on The
Investigating Mars’ atmosphere using the NOMAD instrument on the ExoMars Trace Gas Orbiter Supervision team: Dr Manish Patel, Dr Stephen Lewis, Dr Jonathon Mason External supervisor: N/A Lead contact: [email protected] Description: This project provides the opportunity to be directly involved in an active space mission and play a key role in the preparation and exploitation of results from a spaceflight instrument on the ESA ExoMars Trace Gas Orbiter mission, which is currently in orbit around Mars. The project will involve supporting work on: - Continued development of a radiative transfer model of the martian atmosphere in preparation for ExoMars - Characterisation of Flight Spare instrumentation and data interpretation from mid-cruise checkouts - Preparation of new techniques for retrieval of atmospheric species - Exploitation of data returned from the NOMAD-UVIS instrument This mission is aimed at furthering our understanding of the composition and dynamics of the martian environment, through the measurement of trace gases such as ozone and methane in the martian atmosphere from orbit. The project relates to the UVIS channel of the NOMAD instrument; UVIS is an optical spectrometer led by the Open University to measure solar radiation travelling through the martian atmosphere at UV and visible wavelengths, in order to detect and map the presence of ozone, dust and ice clouds in the atmosphere of Mars in unprecedented detail. This project will involve scope for a wide range of potential research from instrument testing through to exploitation of real spaceflight instrument data. The focus of the project is on the retrieval of ozone and aerosol abundance and properties from spectra that will be returned from the UVIS instrument.