Exomarsexomars Searchingsearching Forfor Lifelife Onon Thethe Redred Planetplanet Exomars
Total Page:16
File Type:pdf, Size:1020Kb
Load more
Recommended publications
-
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. -
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. -
Huygens Probe Set to Detach from Cassini Orbiter Tonight 24 December 2004
Update: Huygens Probe Set to Detach From Cassini Orbiter Tonight 24 December 2004 mission is approximately $3 billion. Many of these sophisticated instruments are capable of multiple functions, and the data that they gather will be studied by scientists worldwide. Aerosol Collector and Pyrolyser (ACP) will collect aerosols for chemical-composition analysis. After extension of the sampling device, a pump will draw the atmosphere through filters which capture aerosols. Each sampling device can collect about 30 micrograms of material. Descent Imager/Spectral Radiometer (DISR) can take images and make spectral measurements using sensors covering a wide spectral range. A few hundred metres before impact, the instrument will switch on its lamp in order to acquire spectra of the surface material. The highlights of the first year of the Cassini- Doppler Wind Experiment (DWE) uses radio Huygens mission to Saturn can be broken into two signals to deduce atmospheric properties. The chapters: first, the arrival of the Cassini orbiter at probe drift caused by winds in Titan's atmosphere Saturn in June, and second, the release of the will induce a measurable Doppler shift in the carrier Huygens probe on Dec. 24, 2004, on a path signal. The swinging motion of the probe beneath toward Titan. (read PhysOrg story) its parachute and other radio-signal-perturbing effects, such as atmospheric attenuation, may also The Huygens probe, built and managed by the be detectable from the signal. European Space Agency (ESA), is bolted to Cassini and fed electrical power through an Gas Chromatograph and Mass Spectrometer umbilical cable. It has been riding along during the (GCMS) is a versatile gas chemical analyser nearly seven-year journey to Saturn largely in a designed to identify and quantify various "sleep" mode, awakened every six months for atmospheric constituents. -
The Journey to Mars: How Donna Shirley Broke Barriers for Women in Space Engineering
The Journey to Mars: How Donna Shirley Broke Barriers for Women in Space Engineering Laurel Mossman, Kate Schein, and Amelia Peoples Senior Division Group Documentary Word Count: 499 Our group chose the topic, Donna Shirley and her Mars rover, because of our connections and our interest level in not only science but strong, determined women. One of our group member’s mothers worked for a man under Ms. Shirley when she was developing the Mars rover. This provided us with a connection to Ms. Shirley, which then gave us the amazing opportunity to interview her. In addition, our group is interested in the philosophy of equality and we have continuously created documentaries that revolve around this idea. Every member of our group is a female, so we understand the struggles and discrimination that women face in an everyday setting and wanted to share the story of a female that faced these struggles but overcame them. Thus after conducting a great amount of research, we fell in love with Donna Shirley’s story. Lastly, it was an added benefit that Ms. Shirley is from Oklahoma, making her story important to our state. All of these components made this topic extremely appealing to us. We conducted our research using online articles, Donna Shirley’s autobiography, “Managing Martians”, news coverage from the launch day, and our interview with Donna Shirley. We started our research process by reading Shirley’s autobiography. This gave us insight into her college life, her time working at the Jet Propulsion Laboratory, and what it was like being in charge of such a barrier-breaking mission. -
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. -
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. -
Exomars 2016 TGO and Schiaparelli
ESA UNCLASSIFIED – For Official Use estec European Space Research and Technology Centre Keplerlaan 1 2201 AZ Noordwijk The Netherlands T +31 (0)71 565 6565 F +31 (0)71 565 6040 www.esa.int ExoMars 2016 Mission Brief description of TGO and Schiaparelli Prepared by H. Svedhem (SCI-S), K. O’Flaherty (SCI-S) Reference EXM-MS-REP-RSSD-001_TGO-EDM-Description_Iss.1 Issue 1 Revision 0 Date of Issue 28/01/2016 Status 1 Document Type RP Distribution ESA UNCLASSIFIED – For Official Use Reason for change Issue Revision Date Original issue 1 0 4/02/2016 Issue 1 Revision 0 Reason for change Date Pages Paragraph(s) Page 2/20 ExoMars 2016 Mission - Brief description of TGO and Schiaparelli Date: 4/02/2016 Issue 1 Revision 0 ESA UNCLASSIFIED – For Official Use Table of contents: 1 INTRODUCTION ....................................................................................... 4 2 EXOMARS TRACE GAS ORBITER AND SCHIAPARELLI MISSION (2016) . 5 3 EXOMARS TRACE GAS ORBITER (TGO) .................................................. 9 4 EXOMARS TRACE GAS ORBITER INSTRUMENTS .................................. 10 5 SCHIAPARELLI: THE EXOMARS ENTRY, DESCENT AND LANDING DEMONSTRATOR MODULE ........................................................................ 12 6 SCHIAPARELLI SCIENCE PACKAGE AND SCIENCE INVESTIGATIONS17 Page 3/20 ExoMars 2016 Mission - Brief description of TGO and Schiaparelli Date: 4/02/2016 Issue 1 Revision 0 ESA UNCLASSIFIED – For Official Use 1 INTRODUCTION This document presents a brief summary of the ExoMars 2016 mission and its two major elements, the Trace Gas Orbiter, TGO, and the Entry descent and landing Demonstrator Model, EDM, - Schiaparelli. It also gives an overview of the TGO and Schiaparelli scientific investigations and the corresponding instruments. The text is derived from information available on the ESA Exploration web-site, http://exploration.esa.int/mars/. -
Long-Range Rovers for Mars Exploration and Sample Return
2001-01-2138 Long-Range Rovers for Mars Exploration and Sample Return Joe C. Parrish NASA Headquarters ABSTRACT This paper discusses long-range rovers to be flown as part of NASA’s newly reformulated Mars Exploration Program (MEP). These rovers are currently scheduled for launch first in 2007 as part of a joint science and technology mission, and then again in 2011 as part of a planned Mars Sample Return (MSR) mission. These rovers are characterized by substantially longer range capability than their predecessors in the 1997 Mars Pathfinder and 2003 Mars Exploration Rover (MER) missions. Topics addressed in this paper include the rover mission objectives, key design features, and Figure 1: Rover Size Comparison (Mars Pathfinder, Mars Exploration technologies. Rover, ’07 Smart Lander/Mobile Laboratory) INTRODUCTION NASA is leading a multinational program to explore above, below, and on the surface of Mars. A new The first of these rovers, the Smart Lander/Mobile architecture for the Mars Exploration Program has Laboratory (SLML) is scheduled for launch in 2007. The recently been announced [1], and it incorporates a current program baseline is to use this mission as a joint number of missions through the rest of this decade and science and technology mission that will contribute into the next. Among those missions are ambitious plans directly toward sample return missions planned for the to land rovers on the surface of Mars, with several turn of the decade. These sample return missions may purposes: (1) perform scientific explorations of the involve a rover of almost identical architecture to the surface; (2) demonstrate critical technologies for 2007 rover, except for the need to cache samples and collection, caching, and return of samples to Earth; (3) support their delivery into orbit for subsequent return to evaluate the suitability of the planet for potential manned Earth. -
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]. -
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. -
The Space Race Continues
The Space Race Continues The Evolution of Space Tourism from Novelty to Opportunity Matthew D. Melville, Vice President Shira Amrany, Consulting and Valuation Analyst HVS GLOBAL HOSPITALITY SERVICES 369 Willis Avenue Mineola, NY 11501 USA Tel: +1 516 248-8828 Fax: +1 516 742-3059 June 2009 NORTH AMERICA - Atlanta | Boston | Boulder | Chicago | Dallas | Denver | Mexico City | Miami | New York | Newport, RI | San Francisco | Toronto | Vancouver | Washington, D.C. | EUROPE - Athens | London | Madrid | Moscow | ASIA - 1 Beijing | Hong Kong | Mumbai | New Delhi | Shanghai | Singapore | SOUTH AMERICA - Buenos Aires | São Paulo | MIDDLE EAST - Dubai HVS Global Hospitality Services The Space Race Continues At a space business forum in June 2008, Dr. George C. Nield, Associate Administrator for Commercial Space Transportation at the Federal Aviation Administration (FAA), addressed the future of commercial space travel: “There is tangible work underway by a number of companies aiming for space, partly because of their dreams, but primarily because they are confident it can be done by the private sector and it can be done at a profit.” Indeed, private companies and entrepreneurs are currently aiming to make this dream a reality. While the current economic downturn will likely slow industry progress, space tourism, currently in its infancy, is poised to become a significant part of the hospitality industry. Unlike the space race of the 1950s and 1960s between the United States and the former Soviet Union, the current rivalry is not defined on a national level, but by a collection of first-mover entrepreneurs that are working to define the industry and position it for long- term profitability.