Tuesday, March 2, 2010 POSTER SESSION I: MISSION PLANS and CONCEPTS 7:00 P.M
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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. -
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. -
Global Exploration Roadmap
The Global Exploration Roadmap January 2018 What is New in The Global Exploration Roadmap? This new edition of the Global Exploration robotic space exploration. Refinements in important role in sustainable human space Roadmap reaffirms the interest of 14 space this edition include: exploration. Initially, it supports human and agencies to expand human presence into the robotic lunar exploration in a manner which Solar System, with the surface of Mars as • A summary of the benefits stemming from creates opportunities for multiple sectors to a common driving goal. It reflects a coordi- space exploration. Numerous benefits will advance key goals. nated international effort to prepare for space come from this exciting endeavour. It is • The recognition of the growing private exploration missions beginning with the Inter- important that mission objectives reflect this sector interest in space exploration. national Space Station (ISS) and continuing priority when planning exploration missions. Interest from the private sector is already to the lunar vicinity, the lunar surface, then • The important role of science and knowl- transforming the future of low Earth orbit, on to Mars. The expanded group of agencies edge gain. Open interaction with the creating new opportunities as space agen- demonstrates the growing interest in space international science community helped cies look to expand human presence into exploration and the importance of coopera- identify specific scientific opportunities the Solar System. Growing capability and tion to realise individual and common goals created by the presence of humans and interest from the private sector indicate and objectives. their infrastructure as they explore the Solar a future for collaboration not only among System. -
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, -
JAXA's Space Exploration Activities
JAXA’s Space Exploration Activities Jun Gomi, Deputy Director General, JAXA Hayabusa 2 ✓ Asteroid Explorer of the C-type asteroid ✓ Launched in December, 2014 ✓ Reached target asteroid “Ryugu” in 2018 ✓ First successful touchdown to Ryugu on February 22, 2019 ✓ Return to Earth in 2020 (162173) Ryugu 2 Hayabusa 2 (c) JAXA, University of Tokyo, Kochi University, Rikkyo University, (c) JAXA, University of Tokyo, Kochi University, Rikkyo University, Nagoya University, Chiba Institute of Technology, Meiji University, Nagoya University, Chiba Institute of Technology, Meiji University, University of Aizu and AIST. University of Aizu, AIST Asteroid Ryugu photographed from a Asteroid Ryugu from an altitude of 6km. distance of about 20 km. The image Image was captured with the Optical was taken on June 30, 2018. Navigation Camera on July 20, 2018. Hayabusa 2 4 JAXA’s Plan for Space Exploration International • Utilization of ISS/Kibo • Cis-Lunar Platform (Gateway) Cooperation • Lunar exploration and beyond Industry & • JAXA Space Exploration Innovation Academia Hub Partnerships • Science Community discussions JAXA’s Overall Scenario for International Space Exploration Mars, others ★ Initial Exploration ★ Full Fledge Exploration MMX: JFY2024 • Science and search for life • Utilization feasibility exam. Kaguya Moon ©JAXA ©JAXA ©JAXA ©JAXA ©JAXA Full-fledged Exploration & SLIM Traversing exploration(2023- ) Sample Return(2026- ) Utilization (JFY2021) • Science exploration • S/R from far side • Cooperative science/resource • Water prospecting • Technology demo for human mission exploration by robotic and human HTV-X der.(2026- ) • Small probe deploy, data relay etc. Gateway Phase 1 Gateway (2022-) Phase 2 • Support for Lunar science Earth • Science using deep space Promote Commercialization International Space Station 6 SLIM (Smart Lander for Investigating Moon) ✓ Demonstrate pin-point landing on the moon. -
Initial Analysis Team Introduction
Summary and contents of the press conference Overview • Since the return of the sample in December of last year, curation activities have been conducted for the initial analysis of the sample. • Curation activities are aimed at cataloguing the sample without compromising the scientific value in order to provide information that contributes to further detailed scientific analysis. • Today’s report is that part of the catalogued sample is ready for delivery. Contents 1. Report from the curation team (T. Usui, E. Nakamura, M. Ito) 2. Report from the initial analysis teamS. TachibanaH. YurimotoT. Nakamura T. NoguchiR. OkazakiH. YabutaH. Naraoka 2021/6/17 Hayabusa2 reporter briefing 2 Report from the curation team Tomohiro USUIJAXA Eizo NAKAMURAOkayama University Motoo ITOJAMSTEC Ryugu sample curation work The initial description of the Ryugu sample was performed without removing the sample from the clean chamber, in order to avoid contamination from the global environment CC3-1 Opening the sample container under vacuum environment CC3-2 Sample collection under vacuum CC3-3 Transition from vacuum to nitrogen environment CC4-1 Handling of submillimeter-sized particles CC4-2 Handling / observation / sorting of relatively large particles (> mm) 2021/6/17 Hayabusa2 reporter briefing 4 Achievement of the world’s first sample collection and storage of asteroid samples under vacuum conditions Samples collected under vacuum on December 15, 2020 will not be distributed at this time, but continued to be stored under vacuum (CC3-2) for future -
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. -
Exomars Rover Battery Modeling & Life Tests
ExoMars Rover Battery Modeling & Life Tests Geoff Dudley NASA Aerospace Battery Workshop Huntsville USA November 16-18 2010 ExoMars Rover Battery • Mass is critical ! Nominal mission duration: 180 sols • Battery ExoMars Rover Battery | G. Dudley | Nov 16-18 2010 | NASA Aerospace Battery Workshop | Page 2 Background to tests - 1 • Low ambient temperature means either battery has to operate cold or extra is energy needed from somewhere to maintain higher battery temperature • Li-Ion cell manufacturers data sheets show discharge capability down to below -20 deg. C but rarely indicate low temperature charge capability • Required charge rates are quite low for rover application so low-temperature charging was investigated • ABSL recommended 4 cell candidates for low temperature tests at ESTEC (based on specific energy at low temperatures) • 2 of these down-selected for life tests as 6s1p strings: • ABSL 18650 LV (2.2 Ah nameplate capacity) • ABSL 18650 NL (2.4 Ah nameplate capacity) ExoMars Rover Battery | G. Dudley | Nov 16-18 2010 | NASA Aerospace Battery Workshop | Page 3 Background to tests - 2 • ESTEC tests carried out under contract to ABSL in the frame of ExoMars phase B1 “Rover Vehicle Battery Breadboard” activity. – By 180 cycles of life testing both cell types showed large dispersion in voltage, capacity and resistance – Evidence for lithium plating • Characterisation tests performed in parallel with life tests – NL cell model (derived from these) subsequently confirmed that Li plating was inevitable at the charge rates previously used. – Model used to help select a more suitable charge management • New life tests on new 6s1p modules of NL and LV cell types with new charge management – After 120 sols discontinued worst-performing cell module (LV) and replaced by second NL module using more aggressive charge management ExoMars Rover Battery | G. -
The Pipeline for the Exomars DREAMS Scientific Data Archiving
The pipeline for the ExoMars DREAMS scientific data archiving P. Schipani,1 L. Marty,1 M. Mannetta,1 F. Esposito,1 C. Molfese,1 A. Aboudan, 2 V. Apestigue-Palacio,3 I. Arruego-Rodriguez,3 C. Bettanini,2 G. Colombatti,2 S. Debei,2 M. Genzer,4 A-M. Harri,4 E. Marchetti,5 F. Montmessin,6 R. 5 5 7 Mugnuolo, S. Pirrotta, C. Wilson, 1INAF - Capodimonte Astronomical Observatory, I-80131 Naples, Italy; pietro.schipani@ oacn.inaf.it 2CISAS, Via Venezia 15, I-35131 Padua, Italy 3Instituto Nacional de Tecnica Aeroespacial (INTA), Madrid, Spain 4Finnish Meteorological Institute (FMI), Erik Palmenin aukio 1, FI-00560 Helsinki, Finland 5Agenzia Spaziale Italiana (ASI), Via del Politecnico, I-00133 Roma, Italy 6LATMOS - CNRS, Quartier des Garennes, 11 bd d’Alembert, F-78280 Guyancourt, France 7Oxford University, Parks Road, Oxford, United Kingdom Abstract. DREAMS (Dust Characterisation, Risk Assessment, and Environment Analyser on the Martian Surface) is a payload accommodated on the Schiaparelli Entry and Descent Module (EDM) of ExoMars 2016, the ESA and Roscosmos mission to Mars (Esposito (2015), Bettanini et al. (2014)). It is a meteorological station with the additional capability to perform measure- ments of the atmospheric electric fields close to the surface of Mars. The instrument package will make the first measurements of electric fields on Mars, providing data that will be of value in planning the second ExoMars mission in 2020, as well as possible future human missions to the red planet. This paper describes the pipeline to convert the raw telemetries to the final data products for the archive, with associated metadata. -
Human Exploration of Mars Design Reference Architecture 5.0
July 2009 “We are all . children of this universe. Not just Earth, or Mars, or this System, but the whole grand fireworks. And if we are interested in Mars at all, it is only because we wonder over our past and worry terribly about our possible future.” — Ray Bradbury, 'Mars and the Mind of Man,' 1973 Cover Art: An artist’s concept depicting one of many potential Mars exploration strategies. In this approach, the strengths of combining a central habitat with small pressurized rovers that could extend the exploration range of the crew from the outpost are assessed. Rawlings 2007. NASA/SP–2009–566 Human Exploration of Mars Design Reference Architecture 5.0 Mars Architecture Steering Group NASA Headquarters Bret G. Drake, editor NASA Johnson Space Center, Houston, Texas July 2009 ACKNOWLEDGEMENTS The individuals listed in the appendix assisted in the generation of the concepts as well as the descriptions, images, and data described in this report. Specific contributions to this document were provided by Dave Beaty, Stan Borowski, Bob Cataldo, John Charles, Cassie Conley, Doug Craig, Bret Drake, John Elliot, Chad Edwards, Walt Engelund, Dean Eppler, Stewart Feldman, Jim Garvin, Steve Hoffman, Jeff Jones, Frank Jordan, Sheri Klug, Joel Levine, Jack Mulqueen, Gary Noreen, Hoppy Price, Shawn Quinn, Jerry Sanders, Jim Schier, Lisa Simonsen, George Tahu, and Abhi Tripathi. Available from: NASA Center for AeroSpace Information National Technical Information Service 7115 Standard Drive 5285 Port Royal Road Hanover, MD 21076-1320 Springfield, VA 22161 Phone: 301-621-0390 or 703-605-6000 Fax: 301-621-0134 This report is also available in electronic form at http://ston.jsc.nasa.gov/collections/TRS/ CONTENTS 1 Introduction ...................................................................................................................... -
Securing Japan an Assessment of Japan´S Strategy for Space
Full Report Securing Japan An assessment of Japan´s strategy for space Report: Title: “ESPI Report 74 - Securing Japan - Full Report” Published: July 2020 ISSN: 2218-0931 (print) • 2076-6688 (online) Editor and publisher: European Space Policy Institute (ESPI) Schwarzenbergplatz 6 • 1030 Vienna • Austria Phone: +43 1 718 11 18 -0 E-Mail: [email protected] Website: www.espi.or.at Rights reserved - No part of this report may be reproduced or transmitted in any form or for any purpose without permission from ESPI. Citations and extracts to be published by other means are subject to mentioning “ESPI Report 74 - Securing Japan - Full Report, July 2020. All rights reserved” and sample transmission to ESPI before publishing. ESPI is not responsible for any losses, injury or damage caused to any person or property (including under contract, by negligence, product liability or otherwise) whether they may be direct or indirect, special, incidental or consequential, resulting from the information contained in this publication. Design: copylot.at Cover page picture credit: European Space Agency (ESA) TABLE OF CONTENT 1 INTRODUCTION ............................................................................................................................. 1 1.1 Background and rationales ............................................................................................................. 1 1.2 Objectives of the Study ................................................................................................................... 2 1.3 Methodology