ESA JAXA Bepicolombo Mercury Mission
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Michael Garcia Hubble Space Telescope Users Committee (STUC)
Hubble Space Telescope Users Committee (STUC) April 16, 2015 Michael Garcia HST Program Scientist [email protected] 1 Hubble Sees Supernova Split into Four Images by Cosmic Lens 2 NASA’s Hubble Observations suggest Underground Ocean on Jupiter’s Largest Moon Ganymede file:///Users/ file:///Users/ mrgarci2/Desktop/mrgarci2/Desktop/ hs-2015-09-a-hs-2015-09-a- web.jpg web.jpg 3 NASA’s Hubble detects Distortion of Circumstellar Disk by a Planet 4 The Exoplanet Travel Bureau 5 TESS Transiting Exoplanet Survey Satellite CURRENT STATUS: • Downselected April 2013. • Major partners: - PI and science lead: MIT - Project management: NASA GSFC - Instrument: Lincoln Laboratory - Spacecraft: Orbital Science Corp • Agency launch readiness date NLT June 2018 (working launch date August 2017). • High-Earth elliptical orbit (17 x 58.7 Earth radii). Standard Explorer (EX) Mission PI: G. Ricker (MIT) • Development progressing on plan. Mission: All-Sky photometric exoplanet - Systems Requirement Review (SRR) mapping mission. successfully completed on February Science goal: Search for transiting 12-13, 2014. exoplanets around the nearby, bright stars. Instruments: Four wide field of view (24x24 - Preliminary Design Review (PDR) degrees) CCD cameras with overlapping successfully completed Sept 9-12, 2014. field of view operating in the Visible-IR - Confirmation Review, for approval to enter spectrum (0.6-1 micron). implementation phase, successfully Operations: 3-year science mission after completed October 31, 2014. launch. - Mission CDR on track for August 2015 6 JWST Hardware Progress JWST remains on track for an October 2018 launch within its replan budget guidelines 7 WFIRST / AFTA Widefield Infrared Survey Telescope with Astrophysics Focused Telescope Assets Coronagraph Technology Milestones Widefield Detector Technology Milestones 1 Shaped Pupil mask fabricated with reflectivity of 7/21/14 1 Produce, test, and analyze 2 candidate 7/31/14 -4 10 and 20 µm pixel size. -
Mission to Jupiter
This book attempts to convey the creativity, Project A History of the Galileo Jupiter: To Mission The Galileo mission to Jupiter explored leadership, and vision that were necessary for the an exciting new frontier, had a major impact mission’s success. It is a book about dedicated people on planetary science, and provided invaluable and their scientific and engineering achievements. lessons for the design of spacecraft. This The Galileo mission faced many significant problems. mission amassed so many scientific firsts and Some of the most brilliant accomplishments and key discoveries that it can truly be called one of “work-arounds” of the Galileo staff occurred the most impressive feats of exploration of the precisely when these challenges arose. Throughout 20th century. In the words of John Casani, the the mission, engineers and scientists found ways to original project manager of the mission, “Galileo keep the spacecraft operational from a distance of was a way of demonstrating . just what U.S. nearly half a billion miles, enabling one of the most technology was capable of doing.” An engineer impressive voyages of scientific discovery. on the Galileo team expressed more personal * * * * * sentiments when she said, “I had never been a Michael Meltzer is an environmental part of something with such great scope . To scientist who has been writing about science know that the whole world was watching and and technology for nearly 30 years. His books hoping with us that this would work. We were and articles have investigated topics that include doing something for all mankind.” designing solar houses, preventing pollution in When Galileo lifted off from Kennedy electroplating shops, catching salmon with sonar and Space Center on 18 October 1989, it began an radar, and developing a sensor for examining Space interplanetary voyage that took it to Venus, to Michael Meltzer Michael Shuttle engines. -
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. -
Cosmic Vision 2015-2025
Space Science Cosmic Vision 2015-2025 Eight new mission proposals selected for ESA’s future scientific programme that proposed the mission. The space research com- The Science Mission Team defines a model payload munity’s long-term goals and ESA engineering teams for their research pro- undertake the technical grammes are to maintain assessment. The aim of the Assessment Phase is the present level of re- to define the mission to a search satellites in orbit sufficient level to show the around 2018 – 20 as scientific value and technical feasibility. well as working with and The main objectives evaluating possible new of the Definition Phase are missions. to establish the cost and implementation schedule In October, after a Space Science for the project. At the end Advisory Committee meeting (SSAC), of the definition phase, the candidate missions were selected for the Prime Contractor for further assessment and consideration for the Implementation Phase launch in 2017/2018. is selected. Competition That is the result of the Cosmic between potential Prime Contractors is necessary. It Vision 2015-2025’s Call for Proposals LISA (Laser Interferometer Space is also essential that the design and costing announced earlier this year. The response Antenna) moved from Cosmic Vision 2005- is based on the actual mission, i.e. with the was enormous and many interesting fields 2015. were represented in the proposals that selected PI (Principal Investigator) funded were presented. Fifty new proposals were instruments and selected new technologies, presented, twice the amount of proposals so that the competing contractors have compared to the previous ESA calls in a firm basis on which to make their Read more about the selected 1999. -
Presentation of Cosmic Vision 2015-2025 to Community
Cosmic Vision 2015 – 2025 ESA’s new long term plan for space science Missions in preparation Bepi-Colombo 2012 Lisa 2014 Corot Herschel-Planck (CNES-ESA) 2007 . 2006 JWST (NASA-ESA) Astro-F 2011 (Japan-ESA) 2006 Lisa- Venus Express Pathfinder 2009 Gaia Solar . 2005 Microscope 2011-12 Orbiter (CNES-ESA) 2015 2008 2005 2006 2007 2008 2009 2010 2011 2012 2013 2014 2015 Cosmic Vision process • Cosmic Vision 2015 –2025 process launched on 2 April 04 with call for Science themes • 1June 04: deadline for proposal submission • July 04: Analysis of responses by the ESA Science advisory bodies (AWG, SSWG, FPAG, SSAC) • 15-16 September 04: Workshop in Paris (~400 participants) • Nov 04: progress report to SPC • Spring 05: presentation of Cosmic Vision 2015-2025 to community • May 05: Endorsement of Cosmic Vision by SPC Grand themes 1. What are the conditions for life and planetary formation? 2. How does the Solar System work. 3. What are the fundamental laws of the Universe? 4. How did the Universe originate and what is it made of? 1. What are the conditions for life and planetary formation? 1.1 From gas and dust to stars and planets. 1.2 From exo-planets to bio-markers. 1.3 Life and habitability in the Solar System 2. How does the Solar System work ? 2.1 From the Sun to the edge of the Solar System 2.2 The building blocks of the Solar System, gaseous giants and their moons Solar System Roadmap (1) 2015-2025 Look at Small Scales! Understand Space plasmas EARTH MAGNETOSPHERIC SWARM, SOLAR POLAR ORBITER, HELIOPAUSE PROBE 2020 Go Outward! Explore the outer Solar System JUPITER & EUROPA PROBE Solar System Roadmap (2) 2015-2020 Look for Life! Everywhere in Solar System Mars rovers and sample return, Europa Probe 2020-2025 Seek Ground Truth! Land on NEOs, Moons, Planets,look below surface, return samples Jupiter and Europa Probe, NEO Sample Return 3. -
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. -
Ices on Mercury: Chemistry of Volatiles in Permanently Cold Areas of Mercury’S North Polar Region
Icarus 281 (2017) 19–31 Contents lists available at ScienceDirect Icarus journal homepage: www.elsevier.com/locate/icarus Ices on Mercury: Chemistry of volatiles in permanently cold areas of Mercury’s north polar region ∗ M.L. Delitsky a, , D.A. Paige b, M.A. Siegler c, E.R. Harju b,f, D. Schriver b, R.E. Johnson d, P. Travnicek e a California Specialty Engineering, Pasadena, CA b Dept of Earth, Planetary and Space Sciences, University of California, Los Angeles, CA c Planetary Science Institute, Tucson, AZ d Dept of Engineering Physics, University of Virginia, Charlottesville, VA e Space Sciences Laboratory, University of California, Berkeley, CA f Pasadena City College, Pasadena, CA a r t i c l e i n f o a b s t r a c t Article history: Observations by the MESSENGER spacecraft during its flyby and orbital observations of Mercury in 2008– Received 3 January 2016 2015 indicated the presence of cold icy materials hiding in permanently-shadowed craters in Mercury’s Revised 29 July 2016 north polar region. These icy condensed volatiles are thought to be composed of water ice and frozen Accepted 2 August 2016 organics that can persist over long geologic timescales and evolve under the influence of the Mercury Available online 4 August 2016 space environment. Polar ices never see solar photons because at such high latitudes, sunlight cannot Keywords: reach over the crater rims. The craters maintain a permanently cold environment for the ices to persist. Mercury surface ices magnetospheres However, the magnetosphere will supply a beam of ions and electrons that can reach the frozen volatiles radiolysis and induce ice chemistry. -
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. -
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. -
Bepicolombo - a Mission to Mercury
BEPICOLOMBO - A MISSION TO MERCURY ∗ R. Jehn , J. Schoenmaekers, D. Garc´ıa and P. Ferri European Space Operations Centre, ESA/ESOC, Darmstadt, Germany ABSTRACT BepiColombo is a cornerstone mission of the ESA Science Programme, to be launched towards Mercury in July 2014. After a journey of nearly 6 years two probes, the Magneto- spheric Orbiter (JAXA) and the Planetary Orbiter (ESA) will be separated and injected into their target orbits. The interplanetary trajectory includes flybys at the Earth, Venus (twice) and Mercury (four times), as well as several thrust arcs provided by the solar electric propulsion module. At the end of the transfer a gravitational capture at the weak stability boundary is performed exploiting the Sun gravity. In case of a failure of the orbit insertion burn, the spacecraft will stay for a few revolutions in the weakly captured orbit. The arrival conditions are chosen such that backup orbit insertion manoeuvres can be performed one, four or five orbits later with trajectory correction manoeuvres of less than 15 m/s to compensate the Sun perturbations. Only in case that no manoeuvre can be performed within 64 days (5 orbits) after the nominal orbit insertion the spacecraft will leave Mercury and the mission will be lost. The baseline trajectory has been designed taking into account all operational constraints: 90-day commissioning phase without any thrust; 30-day coast arcs before each flyby (to allow for precise navigation); 7-day coast arcs after each flyby; 60-day coast arc before orbit insertion; Solar aspect angle constraints and minimum flyby altitudes (300 km at Earth and Venus, 200 km at Mercury). -
The Search for Another Earth – Part II
GENERAL ARTICLE The Search for Another Earth – Part II Sujan Sengupta In the first part, we discussed the various methods for the detection of planets outside the solar system known as the exoplanets. In this part, we will describe various kinds of exoplanets. The habitable planets discovered so far and the present status of our search for a habitable planet similar to the Earth will also be discussed. Sujan Sengupta is an 1. Introduction astrophysicist at Indian Institute of Astrophysics, Bengaluru. He works on the The first confirmed exoplanet around a solar type of star, 51 Pe- detection, characterisation 1 gasi b was discovered in 1995 using the radial velocity method. and habitability of extra-solar Subsequently, a large number of exoplanets were discovered by planets and extra-solar this method, and a few were discovered using transit and gravi- moons. tational lensing methods. Ground-based telescopes were used for these discoveries and the search region was confined to about 300 light-years from the Earth. On December 27, 2006, the European Space Agency launched 1The movement of the star a space telescope called CoRoT (Convection, Rotation and plan- towards the observer due to etary Transits) and on March 6, 2009, NASA launched another the gravitational effect of the space telescope called Kepler2 to hunt for exoplanets. Conse- planet. See Sujan Sengupta, The Search for Another Earth, quently, the search extended to about 3000 light-years. Both Resonance, Vol.21, No.7, these telescopes used the transit method in order to detect exo- pp.641–652, 2016. planets. Although Kepler’s field of view was only 105 square de- grees along the Cygnus arm of the Milky Way Galaxy, it detected a whooping 2326 exoplanets out of a total 3493 discovered till 2Kepler Telescope has a pri- date. -
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/.