White Paper on the Case for Landed Mercury Exploration Within The
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Matematikken Viser Vej Til Mars
S •Matematikken The viser vej til Mars Kim Plauborg © The Terma Group 2016 THE BEGINNING Terma has been in Space since man walked on the Moon! © The Terma Group 2016 FROM ESRO TO EXOMARS Terma powered the first comet landing ever! BREAKING NEWS The mission ends today when the Rosetta satellite will set down on the surface In 2014 the Rosetta satellite deployed the small lander Philae, which landed on the cometof 67P morethe than 10 comet years after Rosetta was launched. © The Terma Group 2016 FROM ESRO TO EXOMARS Rosetta Mars Express Technology Venus Express evolution and Galileo enhancement Small GEO BepiColombo ExoMars © The Terma Group 2016 Why go Mars? Getting to and landing on Mars is difficult ! © The Terma Group 2016 THE EXOMARS PROGRAMME Two ESA missions to Mars in cooperation with Roscosmos with the main objective to search for evidence of life 2016 Mission Trace Gas Orbiter Schiaparelli 2020 Mission Rover Surface platform © The Terma Group 2016 EXOMARS 2016 14th March 2016 Launched from Baikonur cosmodrome, Kazakhstan © The Terma Group 2016 EXOMARS 2016 16th October 2016 Separation of Schiaparelli from the orbiter © The Terma Group 2016 SCHIAPARELLI Schiaparelli (EDM) - an entry, descent and landing demonstrator module © The Terma Group 2016 EXOMARS 2016 19th October 2016 Landing of Schiaparelli the surface of Mars © The Terma Group 2016 EXOMARS 2016 19th October 2016 Landing of Schiaparelli the surface of Mars © The Terma Group 2016 EXOMARS 2020 © The Terma Group 2016 TERMA AND EXOMARS Terma deliveries to the ExoMars 2016 mission • Remote Terminal Power Unit for Schiaparelli • Mission Control System • Spacecraft Simulator • Support for the Launch and Early Orbit Phase © The Terma Group 2016 ExoMars RTPU The RTPU is a central unit in the Schiaparelli lander. -
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. -
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). -
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. -
DLR Developments and Application Ideas for Interplanetary Cubesats
DLR developments and application ideas for interplanetary cubesats iCubeSat, Milano 2019 Jens Biele1, Michael Maibaum1, Caroline Lange2, Thimo Grundmann2, Stephan Ulamec1, Marcus Thomas Knopp3, Frank-Cyrus Roshani3 1DLR German Aerospace Center, RB-MUSC, Cologne, Germany 2DLR German Aerospace Center, Bremen, Germany 3DLR German Aerospace Center, GSOC, Munich, Germany www.DLR.de • Chart 3 > Lecture > Author • Document > Date SKAD-Study [FRANK, MARCUS] • Orbiter as relais station for Mars-Rover • ………. Designs flown or studied (DLR) Hopper(10-25 kg) MASCOT (30, 70 kg) Philae (100 kg) Leonard MASCOT (10 kg) Folie 4 > Vortrag > Autor Folie 5 > Vortrag > Autor Study Flow of MASCOT („how to shrink a lander..“) • December 2008 – September 2009: feasibility study, with CNES, in context of Marco Polo and Hayabusa-2, with common requirements: • 3 iterations of different mass (95kg, 35kg & 10kg) and P/L • Settled on 10 kg lander package including 3 kg of P/L • Ho, T.-M., et al. (2016). "MASCOT—The Mobile Asteroid Surface Scout Onboard the Hayabusa2 Mission." Space Science Reviews 208(1-4): 339– 374. • ➔ Design of MASCOT 10 kg: a nanosat (30x30*20 cm³) . Could be a 18 U cubesat! Large ~ 95 kg, Philae hertitage Middle ~ 35 kg, Xtra Small ~ 10 kg, No post-landing Up-righting + mobility mobility MASCOT Payload (25% of total mass!) Instrument Science Goals Heritage Institute; PI/IM Mass [kg] MAG magnetization of the NEA MAG of ROMAP on Rosetta TU Braunschweig Lander (Philae), ESA VEX, 0,15 → formation history Themis K.H. Glassmeier / U. Auster mineralogical composition ESA ExoMars, Russia and characterize grains Phobos GRUNT, ESA size and structure of Rosetta, ESA ExoMars IAS Paris µOmega surface soil samples at μ- rover 2018, Rosetta / Philae J.P. -
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. -
Mariner to Mercury, Venus and Mars
NASA Facts National Aeronautics and Space Administration Jet Propulsion Laboratory California Institute of Technology Pasadena, CA 91109 Mariner to Mercury, Venus and Mars Between 1962 and late 1973, NASA’s Jet carry a host of scientific instruments. Some of the Propulsion Laboratory designed and built 10 space- instruments, such as cameras, would need to be point- craft named Mariner to explore the inner solar system ed at the target body it was studying. Other instru- -- visiting the planets Venus, Mars and Mercury for ments were non-directional and studied phenomena the first time, and returning to Venus and Mars for such as magnetic fields and charged particles. JPL additional close observations. The final mission in the engineers proposed to make the Mariners “three-axis- series, Mariner 10, flew past Venus before going on to stabilized,” meaning that unlike other space probes encounter Mercury, after which it returned to Mercury they would not spin. for a total of three flybys. The next-to-last, Mariner Each of the Mariner projects was designed to have 9, became the first ever to orbit another planet when two spacecraft launched on separate rockets, in case it rached Mars for about a year of mapping and mea- of difficulties with the nearly untried launch vehicles. surement. Mariner 1, Mariner 3, and Mariner 8 were in fact lost The Mariners were all relatively small robotic during launch, but their backups were successful. No explorers, each launched on an Atlas rocket with Mariners were lost in later flight to their destination either an Agena or Centaur upper-stage booster, and planets or before completing their scientific missions. -
ESA & ESOC Overview
NASA PM Challenge 2010 Developing the International Program/Project Management Community 9/10 February 2010 Dr. Bettina Böhm Program & Project Manager Career at ESA | Bettina Böhm | ESA/HQ | 23/11/09 | Page 1 Used with Permission PURPOSE OF ESA / ACTIVITIES “To provide for and promote, for exclusively Space science peaceful purposes, cooperation among Human spaceflight European states in space research and Exploration technology and their space applications.” Earth observation Launchers [Article 2 of ESA Convention] Navigation ESA is one of the few space agencies Telecommunications in the world to combine responsibility Technology in all areas of space activity. Operations Program & Project Manager Career at ESA | Bettina Böhm | ESA/HQ | 23/11/09 | Page 2 ESA FACTS AND FIGURES Over 30 years of experience 18 Member States 2080 staff, thereof 880 in Program Directorates, 790 in Operations and Technical Support and 410 in other Support Directorates 3 500 million Euros budget Over 60 satellites designed and tested Over 60 satellites operated in-flight and 8 missions rescued 16 scientific satellites in operation Five types of launcher developed More than 180 launches made Program & Project Manager Career at ESA | Bettina Böhm | ESA/HQ | 23/11/09 | Page 3 ESA Locations EAC (Cologne) Salmijaervi ESTEC Astronaut training (Noordwijk) Satellite technology development and testing Harwell ESOC ESA HQ (Darmstadt) (Paris) Brussels Satellite operations and ground system technology development ESAC (Villanueva de la Cañada Oberpfaffenhofen -
Imaging the Surface of Mercury Using Ground-Based Telescopes
Planetary and Space Science 49 (2001) 1501–1505 www.elsevier.com/locate/planspasci Imaging the surface of Mercury using ground-based telescopes Michael Mendilloa; ∗, Johan Warellb, Sanjay S. Limayec, Je+rey Baumgardnera, Ann Spragued, Jody K. Wilsona aCenter for Space Physics, Boston University, 725 Commonwealth Avenue Boston, MA 02215, USA bAstronomiska Observatoriet, Uppsala Universitet, SE-751 20 Uppsala, Sweden cSpace Science and Engineering Center, University of Wisconsin, Madison, WI 53706, USA dLunar and Planetary Laboratory, University of Arizona, Tucson, AZ 85721, USA Received 26 October 2000; received in revised form 12 March2001; accepted 4 May 2001 Abstract We describe and compare two methods of short-exposure, high-deÿnition ground-based imaging of the planet Mercury. Two teams have recorded images of Mercury on di+erent dates, from di+erent locations, and withdi+erent observational and data reduction techniques. Both groups have achieved spatial resolutions of ¡ 250 km, and the same albedo features and contrast levels appear where the two datasets overlap (longitudes 270–360◦). Dark albedo regions appear as mare and correlate well withsmoothterrain radar signatures. Bright albedo features agree optically, but less well withradar data. Suchconÿrmations of state-of-the-artoptical techniquesintroduce a new era of ground-based exploration of Mercury’s surface and its atmosphere. They o+er opportunities for synergistic, cooperative observations before and during the upcoming Messenger and BepiColombo missions to Mercury. c 2001 Elsevier Science Ltd. All rights reserved. 1. Introduction maximum separation (elongation) to the west and east of the rising or setting Sun, respectively. Under suchconditions, In this paper, we compare the ÿrst results from two new Mercury can be separated from the Sun by up to 28◦. -
First Look at Mercury
PLANETARY SCIENCE Mariner 10 was launched to Mercury by way of Venus on November 3, 1973. It was not the first probe to visit Venus. Both the United States and the Soviet Union previously have sent probes to that mysterious, cloud-shrouded planet. However, Mariner 10 was the first to photographically explore the close-up appearance of the planet, and did so both in visibIe and in ultraviolet light. And Mariner 10 was the first probe of any kind to penetrate interplanetary space beyond the orbit of Venus and to achieve a close look at the planet Mercury. First Look Why go to Mercury? Who needs it? There basically are two kinds of reasons. The first is simple and profound and at Mercury difficult to quantify: The very act of exploration is a positive, cultural activity. No one knows what is going to be found. Finding out what Mercury, what Mars, or BRUCE C. MURRAY what the moon is really like, enlarges the consciousness of all the people who partake of that new reality. TV pictures are of special importance because they provide a way both for the scientist to discover features and concepts he could not have imagined and for the public to directly appreciate and participate in the exploration of a new world. Why go to Mercury? Who needs it? But there are more specific scientific objectives as well. For Mercury, the basic-and anomalous-scientific fact is A planetary scientist that it is a very dense planet: It contains a great amount of tells what the voyage mass for its size. -
Mercury Exploration: Looking to the Future
50th Lunar and Planetary Science Conference 2019 (LPI Contrib. No. 2132) 1105.pdf MERCURY EXPLORATION: LOOKING TO THE FUTURE. K. E. Vander Kaaden1, D. T. Blewett2, P. K. Byrne3, N. L. Chabot2, C. M. Ernst2, S. A. Hauck, II4, F. M. McCubbin5, E. Mazarico6. 1Jacobs, NASA Johnson Space Center, Mail Code XI3, Houston, TX 77058, 2The Johns Hopkins University Applied Physics Laboratory, Laurel, Maryland, 3Planetary Research Group, Department of Marine, Earth, and Atmospheric Sciences, North Carolina State University, Raleigh, NC, 4Department of Earth, Environmental, and Planetary Sciences, Case Western Reserve University, Cleveland, OH, 5ARES NASA Johnson Space Center, 2101 NASA Parkway, Houston, TX 77058, 6NASA Goddard Space Flight Center, Greenbelt, MD. Corresponding Author E-mail: [email protected]. Past Exploration of Mercury: Prior to the return of Future Exploration of Mercury: Despite the data from the NASA MErcury Surface, Space influx of data from the Mariner 10 and MESSENGER ENvironment, GEochemistry, and Ranging spacecraft and the much-anticipated data that will be (MESSENGER) spacecraft [1], information relating to collected by BepiColombo, there is a limit to their Mercury was limited. From the NASA Mariner 10 scientific return. While orbiters could still provide finer flybys, in 1974 and 1975, ~45% of the planet was valuable context, they cannot directly sample surface imaged, its magnetic field was detected, H, He, and O materials, nor probe the interior as a landed mission can. in the exosphere were measured, and other physical Furthermore, an orbiter cannot retrieve a sample to be characteristics of the planet were determined [e.g., 2]. sent to Earth for laboratory-based analyses.