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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. -
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). -
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. -
The Orbital Evolution of Asteroid 367943 Duende (2012 Da14) Under Yarkovsky Effect Influence and Its Implications for Collision with the Earth
Journal of Engineering Science and Technology Special Issue on AASEC’2016, October (2017) 42 - 52 © School of Engineering, Taylor’s University THE ORBITAL EVOLUTION OF ASTEROID 367943 DUENDE (2012 DA14) UNDER YARKOVSKY EFFECT INFLUENCE AND ITS IMPLICATIONS FOR COLLISION WITH THE EARTH JUDHISTIRA ARIA UTAMA1,2,*, TAUFIQ HIDAYAT3, UMAR FAUZI4 1Astronomy Post Graduate Study Program, Institut Teknologi Bandung, Jl. Ganesha 10, Bandung 40132, Indonesia 2Physics Education Department, Universitas Pendidikan Indonesia, Jl. Dr. Setiabudhi 229, Bandung, 40154, Indonesia 3Astronomy Research Division, Institut Teknologi Bandung, Jl. Ganesha 10, Bandung 40132, Indonesia 4Geophysics & Complex System Research Division, Institut Teknologi Bandung, Jl. Ganesha 10, Bandung 40132, Indonesia *Corresponding Author: [email protected] Abstract Asteroid 367943 Duende (2012 DA14) holds the record as the one of Aten subpopulation with H 24 that had experienced deep close encounter event to the Earth (0.09x Earth-Moon distance) as informed in NASA website. In this work, we studied the orbital evolution of 120 asteroid clones and the nominal up to 5 Megayears (Myr) in the future using Swift integrator package with and without the Yarkovsky effect inclusion. At the end of orbital integration with both integrators, we found as many as 17 asteroid clones end their lives as Earth impactor. The prediction of maximum semimajor axis drift for this subkilometer-sized asteroid from diurnal and seasonal variants of Yarkovsky effect was 9.0×10-3 AU/Myr and 2.6×10-4 AU/Myr, respectively. By using the MOID (Minimum Orbital Intersection Distance) data set calculated from our integrators of entire clones and nominal asteroids, we obtained the value of impact rate with the Earth of 2.35×10-7 per year (with Yarkovsky effect) and 2.37×10-7 per year (without Yarkovsky effect), which corresponds to a mean lifetime of 4.25 Myr and 4.22 Myr, respectively. -
Regn Lst 1948 to 2020.Xls
AMERICAN FUCHSIA SOCIETY REGISTERED FUCHSIAS, 1948 - 2020 CULTIVAR REG NO HYBRIDIZER YEAR FORM GROWTH Jardins de France 4439 Massé 2000 sgl up All Square 2335 Adams 1988 sgl up Beatrice Ellen 2336 Adams 1988 sgl up Cardiff Rose 2337 Adams 1988 sgl up/tr Glas Lyn 2338 Adams 1988 sgl up Purple Laddie 2339 Adams 1988 dbl up Velma 1522 Adams 1979 sgl up Windmill 4556 Adams 2001 dbl up Bo Bo 1587 Adkins 1980 dbl up Bonnie Sue 1550 Adkins 1980 dbl tr Dariway 1551 Adkins 1980 sgl up Delta Rae 1552 Adkins 1980 sgl tr Grinnell Bay 1553 Adkins 1980 sgl tr Joanne Lynn 1554 Adkins 1980 sdbl up Grandma Ellen 3066 Ainsworth 1993 sgl up Percy Ainsworth 3065 Ainsworth 1993 sgl tr Tufty Joe 3063 Ainsworth 1993 dbl tr Heidi Joy 2246 Akers/Laburnum 1987 dbl up Elaine Allen 1214 Allen 1974 sdbl up Susan Allen 1215 Allen 1974 sgl up Grandpa Jack 3789 Allso 1997 dbl up/tr Amazing Maisie 4632 Allsop 2001 s-dbl up/tr Amelia Rose 8018 Allsop 2012 sgl tr Arthur C. Boggis 4629 Allsop 2001 s-dbl up Beautiful Bobbie 3781 Allsop 1997 dbl tr Beloved Brian 5689 Allsop 2005 sgl up/tr Betty’s Buddies 8610 Allsop 2015 sgl up Captivating Kelly 3782 Allsop 1997 dbl tr Cheeky Chantelle 3783 Allsop 1997 dbl tr Cinque Port Liberty 4626 Allsop 2001 dbl up/tr Clara Agnes 5572 Allsop 2004 sgl up/tr Conner's Cascade 8019 Allsop 2012 sgl tr CutieKaren 4040 Allsop 1998 dbl tr Danielle’s Dream 4630 Allsop 2001 dbl tr Darling Danielle 3784 Allsop 1997 dbl tr Doodie Dane 3785 Allsop 1997 dbl gtr Dorothy Ann 4627 Allsop 2001 sgl tr Elaine's Gem 8020 Allsop 2012 sgl up Generous Jean 4813 -
Hered in These Proceedings with the Aim to Keep Track of These Very Interesting Days
Proceedings of GAIA-FUN-SSO 2014 Third “Gaia Follow-up Network for Solar System Objects” Workshop held at IMCCE/Paris Observatory 2014, November 24 – 26 Institut de mécanique céleste et de calcul des éphémérides Observatoire de Paris Legal Deposite – June 2015 ISBN 2-910015-73-4 Foreword The observation of Solar System Objects (SSO) by the Gaia space astrometry mission will be constrained by a scanning law. Much detection of interesting objects may occur with no possibility of further observations by the probe. These objects will then require complementary ground-based observations. Among them, previously unknown Near- Earth Objects, fast moving towards the Earth or going away from it could be found. Several objects discovered by Gaia could also be Inner-Earth Objects, as the probe will observe at rather low Solar elongations. In order to confirm from the ground the discoveries made in space and to follow interesting targets, a dedicated network is organized, the Gaia Follow-Up Network. This task is performed in the frame of the Coordination Unit 4 of the Gaia Data Processing and Analysis Consortium (DPAC), devoted to data processing of specific objects. The goal of the network is to improve the knowledge of the orbit of poorly observed targets by astrometric observations on alert. This activity is coordinated by a central node interacting with the Gaia data reduction pipeline all along the mission. In 2010 and 2012, we had organized the first two workshops in order to initiate the network and to meet the participants. In 2014, almost one year after the launch of Gaia, we organize the third Gaia-FUN-SSO workshop in Paris in order to discuss further the coordination of the network of observing stations, to discuss the prelaunch training observations which have been performed and to prepare the network for the operating phase of the alert mode which must begin in 2015. -
Astrometry and Spectra Classification of Near Earth Asteroids with Lijiang
Astronomy and Astrophysics in the Gaia sky Proceedings IAU Symposium No. 330, 2017 A. Recio-Blanco, P. de Laverny, A.G.A. Brown c International Astronomical Union 2018 & T. Prusti, eds. doi:10.1017/S174392131700624X Astrometry and Spectra Classification of Near Earth Asteroids with Lijiang 2.4m Telescope† X. L. Zhang1,2,B.Yang1,2, and J. M. Bai1,2 1 Yunnan Observatories, Chinese Academy of Sciences, Kunming 650011, China email: [email protected] 2 Key Laboratory of the Structure and Evolution of Celestial Objects, Chinese Academy of Sciences, Kunming 650011, China Abstract. The Lijiang 2.4m telescope of Yunnan Observatories is located at longitude E100◦0151, latitude N26◦4232 and height 3250m above sea level (IAU code O44). Because of low latitude of the site, long-focus system and planetary tracking mode of telescope, high accuracy posi- tioning and spectral classification of the near Earth objects (NEAs) especially in the Southern Hemisphere can be studied with the Lijiang 2.4m telescope. As a set of observational campaigns organized by the GAIA-FUN-SSO, astrometry of several near Earth asteroids including (367943) Duende and (99942) Apophis were made with Lijiang 2.4m telescope during 2013. From Decem- ber 12, 2015, spectra of three near earth asteroids were also observed with the YFOSC terminal attached to the Lijiang 2.4m telescope. This paper will give the detailed introduction of Lijiaing 2.4m telescope and observational results of near Earth asteroids obtained with it. Keywords. methods: observational, techniques: astrometry, spectrum classification. 1. Introduction Knowledge of asteroids and comets, the relic of planet building blocks, directly sheds light on the formation of terrestrial planets, and the origin and evolution of the Solar System. -
An Innovative Solution to NASA's NEO Impact Threat Mitigation Grand
Final Technical Report of a NIAC Phase 2 Study December 9, 2014 NASA Grant and Cooperative Agreement Number: NNX12AQ60G NIAC Phase 2 Study Period: 09/10/2012 – 09/09/2014 An Innovative Solution to NASA’s NEO Impact Threat Mitigation Grand Challenge and Flight Validation Mission Architecture Development PI: Dr. Bong Wie, Vance Coffman Endowed Chair Professor Asteroid Deflection Research Center Department of Aerospace Engineering Iowa State University, Ames, IA 50011 email: [email protected] (515) 294-3124 Co-I: Brent Barbee, Flight Dynamics Engineer Navigation and Mission Design Branch (Code 595) NASA Goddard Space Flight Center Greenbelt, MD 20771 email: [email protected] (301) 286-1837 Graduate Research Assistants: Alan Pitz (M.S. 2012), Brian Kaplinger (Ph.D. 2013), Matt Hawkins (Ph.D. 2013), Tim Winkler (M.S. 2013), Pavithra Premaratne (M.S. 2014), Sam Wagner (Ph.D. 2014), George Vardaxis, Joshua Lyzhoft, and Ben Zimmerman NIAC Program Executive: Dr. John (Jay) Falker NIAC Program Manager: Jason Derleth NIAC Senior Science Advisor: Dr. Ronald Turner NIAC Strategic Partnerships Manager: Katherine Reilly Contents 1 Hypervelocity Asteroid Intercept Vehicle (HAIV) Mission Concept 2 1.1 Introduction ...................................... 2 1.2 Overview of the HAIV Mission Concept ....................... 6 1.3 Enabling Space Technologies for the HAIV Mission . 12 1.3.1 Two-Body HAIV Configuration Design Tradeoffs . 12 1.3.2 Terminal Guidance Sensors/Algorithms . 13 1.3.3 Thermal Protection and Shield Issues . 14 1.3.4 Nuclear Fuzing Mechanisms ......................... 15 2 Planetary Defense Flight Validation (PDFV) Mission Design 17 2.1 The Need for a PDFV Mission ............................ 17 2.2 Preliminary PDFV Mission Design by the MDL of NASA GSFC . -
Optimal Flight to Near-Earth Asteroids with Using Electric Propulsion and Gravity Maneuvers
OPTIMAL FLIGHT TO NEAR-EARTH ASTEROIDS WITH USING ELECTRIC PROPULSION AND GRAVITY MANEUVERS A. V. Chernov Keldysh Institute of Applied Mathematics, Miusskaya Sq. 4, Moscow, 125047, Russia, E-mail: [email protected] ABSTRACT Optimal space flight to near-Earth asteroid for using low thrust and gravity assist maneuver near Mars or Venus is investigated in this paper. The main deflection asteroids from the Earth and prevention their possible collision is investigated. The deflection is attention is given a case of the ideal low thrust. Besides realized by means of impact-kinetic effect of the optimal trajectories with the constrained low trust spacecraft on the asteroid and changing the asteroid appropriate to electric engine SPT-140 and solar orbit. The effectiveness of this method for preventing batteries as energy sources are received in vicinity of the optimal trajectories for ideal thrust. asteroid-Earth collision is estimated by means of optimal space flights, which are found. The flight of spacecraft (SC) is realized by means of using electric 2. THE PROBLEM STATEMENT propulsion system. To increase effectiveness the optimal gravity maneuvers of spacecraft near Mars and At first the SC with mass M0 moves along an initial Venus are using. Criterion of the space flight circular near-Earth parking orbit with radius R0. The optimization is maximal deflection of the asteroid from geocentric motion is realized by means of high thrust the Earth at the moment of asteroid-Earth nearest engine with the gas exhaust velocity c1. At moment t1 approach. For determination of optimal trajectories the the SC is applied the velocity impulse ∆V and the SC is maximum Pontrjagin principle is used. -
Observational Investigation of the 2013 Near-Earth Encounter By
Observational Investigation of the 2013 Near-Earth Encounter by Asteroid (367943) Duende Nicholas A. Moskovitz a, Conor James Benson b, Daniel Scheeres b, Thomas Endicott c, David Polishook d, Richard Binzel e, Francesca DeMeo e, William Ryan f, Eileen Ryan f, Mark Willman g, Carl Hergenrother h, Arie Verveer i, Tim Lister j, Peter Birtwhistle k, Amanda Sickafoose `;e;o, Takahiro Nagayama m, Alan Gilmore n, Pam Kilmartin n, Susan Bennechi o, Scott Sheppard p, Franck Marchis q, Thomas Augusteijn r, Olesja Smirnova r aLowell Observatory, 1400 West Mars Hill Road, Flagstaff, AZ 86001 (U.S.A) bUniversity of Colorado Boulder, Boulder, CO 80305 cUniversity of Massachusetts Boston, Boston, MA 02125 dWeizmann Institute of Science, 234 Herzl St. Rehovot 7610001, Israel arXiv:1911.00609v1 [astro-ph.EP] 1 Nov 2019 eMassachusetts Institute of Technology, EAPS, Cambridge, MA 02139 f New Mexico Institute of Mining and Technology, Socorro, NM 87801 gInstitute for Astronomy, University of Hawaii, Hilo, HI 96720 hUniversity of Arizona, LPL, Tucson, AZ 85721 iPerth Observatory, Bickley, WA 6076 (Australia) Preprint submitted to Icarus 5 November 2019 jLas Cumbres Observatory Global Telescope Network, Goleta, CA 93117 kGreat Shefford Observatory, Berkshire (England) `South African Astronomical Observatory (South Africa) mKagoshima University (Japan) nUniversity of Canterbury, Mt John University Observatory, Lake Tekapo (New Zealand) oPlanetary Science Institute, 1700 E. Fort Lowell Rd., Tucson, AZ 85719 pDepartment of Terrestrial Magnetism, Carnegie Institution for Science, Washington, DC 20015 qSETI Institute, Carl Sagan Center, 189 Bernardo Ave., Mountain View CA 94043 rNordic Optical Telescope, La Palma (Spain) Copyright c 2019 Nicholas A. Moskovitz Number of pages: 50 Number of tables: 5 Number of figures: 12 2 Proposed Running Head: The 2013 Near-Earth Encounter of Asteroid Duende Please send Editorial Correspondence to: Nicholas A. -
Planetary Defense
NIAC (NASA Innovative Advanced Concepts) Phase 2 Study (2012 – 2014) An Innovative Solution to NASA's NEO Impact Threat Mitigation Grand Challenge and Flight Validation Mission Architecture Development Bong Wie (PI) Asteroid Deflection Research Center Iowa State University Brent Barbee (Co-I) NASA Goddard Space Flight Center Graduate Students: Alan Pitz, Brian Kaplinger, Matt Hawkins, Tim Winkler, Pavithra Premaratne, George Vardaxis, Joshua Lyzhoft, Ben Zimmerman Asteroid Deflection Research Center Presented at NASA SBAG Meeting, January 6-7, 2015 Asteroid Deflection IOWA STATE UNIVERSITY 1 Research Center 2006 NEO Report by NASA 2010 NEO Report by NRC Asteroid Deflection Research Center IOWA STATE UNIVERSITY Asteroid Deflection 2 Research Center 2006 NEO Report by NASA 2010 NEO Report by NRC Sufficient Warning Time for Deflection Asteroid Deflection Research Center IOWA STATE UNIVERSITY Asteroid Deflection 3 Research Center Study Justification (1/2) 17 m (diameter) An Airburst of 17-m Chelyabinsk 10,000 tons Meteor on Feb. 15, 2013 18.6 km/s impact 440 kt of TNT (30 Hiroshima bombs) Airburst @23.3 km 1,500 people were injured; 7,200 buildings damaged What if it were a 17 m nickel-iron meteorite? Asteroid Deflection Research Center IOWA STATE UNIVERSITY Asteroid Deflection 4 Research Center Study Justification (2/2) • Asteroid 2012 DA14 (367943 Duende), discovered on Feb. 23, 2012, had a close encounter with Earth (27,700-km near-miss) on Feb. 15, 2013. • What if the 30-m DA14 were predicted to collide with Earth with its impact damage of 150 Hiroshima nuclear bombs (or 2.3 Mt of TNT)? Asteroid Deflection Research Center IOWA STATE UNIVERSITY Asteroid Deflection 5 Research Center Study Justification (2/2) • Asteroid 2012 DA14 (367943 Duende), discovered on Feb.