ESA Bulletin No. 125, February 2006
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Giotto Steals a Ride
NEWS COM8ARYPROBE------------------------------------- JAPANESE UNIVERSITIES---- Giotto steals a ride MurmUrS of complaint Washington Munich this is a bargain", says GEM project scien JAPAN's national university professors are THE Earth lost a minute fraction of its tist Gerhard Schwehm. Schwehm said that all employees of the government, which orbital velocity earlier this week as the the second flyby would be a unique oppor puts them in an odd position when they European Space Agency (ESA) Giotto tunity to expand knowledge of comets. It want to protest to the government about space probe stole a little of the Earth's will be especially interesting, he said, to university conditions. But last month, the energy to help it on its way to a rendezvous study the interaction of the coma of the Association of National Universities finally with the comet Grigg Skjellerup. It was comet and the solar wind, as well as to succeeded, after years of trying, in winning the first time the manoeuvre, the same compare the distribution and optical funds from the Ministry of Education, "gravity assist" that helped the NASA properties of dust around Comet Grigg Culture and Science to set up a committee Voyager probe on its journey from Jupiter Skjellerup with that around Comet to study their own financial difficulties. out to Saturn and Neptune, had been exe Halley, which had at least 100 times more The association represents all the 93 cuted using the gravitation field of Earth. of it. national universities directly supported by According to ESA researcher Trevor Giotto was one of five spacecraft to the government and has responsibility for Morley, Giotto will gain 3.1 km/sec in approach Comet Halley in 1986, but it setting up the general entrance examination. -
Rosetta Craft Makes Historic Comet Rendezvous European Space Agency's Comet-Chasing Mission Arrives After 10-Year Journey
NATURE | NEWS Rosetta craft makes historic comet rendezvous European Space Agency's comet-chasing mission arrives after 10-year journey. Elizabeth Gibney 06 August 2014 ESA/Rosetta/MPS for OSIRIS Team MPS/UPD/LAM/IAA/SSO/INTA/UPM/DASP/IDA Comet 67P/Churyumov–Gerasimenko, as seen by Rosetta from a distance of 285 kilometres. No one can deny that it was an epic trip. The European Space Agency's comet-chasing Rosetta spacecraft has arrived at its quarry, after launching more than a decade ago and travelling 6.4 billion kilometres through the Solar System. That makes it the first spacecraft to rendezvous with a comet, and takes the mission a step closer to its next, more ambitious goal of making the first ever soft landing on a comet. Speaking from mission control in Darmstadt, Germany, Matt Taylor, Rosetta project scientist for the European Space Agency (ESA), called the space mission “the sexiest there’s ever been”. Rosetta is now within 100 kilometres of its target, comet 67P/Churyumov–Gerasimenko (or 67P for short), which in July was discovered to be shaped like a rubber duck. After a six-minute thruster burn, at 11:29 a.m. local time on 6 August, ESA scientists confirmed that Rosetta had moved into the same orbit around the Sun as the comet. Rosetta is now moving at a walking pace relative to the motion of 67P — though both are hurtling through space at 15 kilometres per second. Unlike NASA’s Deep Impact and Stardust craft, and ESA’s Giotto mission, which flew by their target comets at high speed, Rosetta will now stay with the comet, taking a ring-side seat as 67P approaches the Sun, and eventually swings around it in August 2015. -
Stardust Comet Flyby
NATIONAL AERONAUTICS AND SPACE ADMINISTRATION Stardust Comet Flyby Press Kit January 2004 Contacts Don Savage Policy/Program Management 202/358-1727 NASA Headquarters, Washington DC Agle Stardust Mission 818/393-9011 Jet Propulsion Laboratory, Pasadena, Calif. Vince Stricherz Science Investigation 206/543-2580 University of Washington, Seattle, WA Contents General Release ……………………………………......………….......................…...…… 3 Media Services Information ……………………….................…………….................……. 5 Quick Facts …………………………………………..................………....…........…....….. 6 Why Stardust?..................…………………………..................………….....………......... 7 Other Comet Missions ....................................................................................... 10 NASA's Discovery Program ............................................................................... 12 Mission Overview …………………………………….................……….....……........…… 15 Spacecraft ………………………………………………..................…..……........……… 25 Science Objectives …………………………………..................……………...…........….. 34 Program/Project Management …………………………...................…..…..………...... 37 1 2 GENERAL RELEASE: NASA COMET HUNTER CLOSING ON QUARRY Having trekked 3.2 billion kilometers (2 billion miles) across cold, radiation-charged and interstellar-dust-swept space in just under five years, NASA's Stardust spacecraft is closing in on the main target of its mission -- a comet flyby. "As the saying goes, 'We are good to go,'" said project manager Tom Duxbury at NASA's Jet -
SPICE for ESA Missions
SPICE for ESA Missions Marc Costa Sitjà RHEA Group for ESA SPICE and Auxiliary Data Engineer PSIDA, Saint Louis, MO, EEUU 21/09/2017 Issue/Revision: 1.0 Reference: Presentation Reference Status: Issued ESA UNCLASSIFIED - Releasable to the Public SPICE in a nutshell Ø SPICE is an information system that uses ancillary data to provide Solar System geometry information to scientists and engineers for planetary missions in order to plan and analyze scientific observations from space-born instruments. SPICE was originally developed and maintained by the Navigation and Ancillary Information Facility (NAIF) team of the Jet Propulsion Laboratory (NASA). Ø “Ancillary data” are those that help scientists and engineers determine: ● where the spacecraft was located ● how the spacecraft and its instruments were oriented (pointed) ● what was the location, size, shape and orientation of the target being observed ● what events were occurring on the spacecraft or ground that might affect interpretation of science observations Ø SPICE provides users a large suite of SW used to read SPICE ancillary data files to compute observation geometry. Ø SPICE is open, very well tested, extensively used and provides tons of resources to learn it and implement it. Ø SPICE is the recommended means of archiving ancillary data by NASA’s PDS and by the IPDA Ø The ancillary data (kernels) comes from: The S/C, MOC/SGS, S/C manufacturer and Instrument teams, Science Organizations. Author Name | Presentation Reference | ESAC | 23/11/2015 | Slide 2 ESA UNCLASSIFIED - Releasable to the Public SPICE in a nutshell Components Data Files Contents Producers Source* • MOC provides data, SGS • Fdyn & S Spacecraft and target generates kernels. -
Appendix 1: Venus Missions
Appendix 1: Venus Missions Sputnik 7 (USSR) Launch 02/04/1961 First attempted Venus atmosphere craft; upper stage failed to leave Earth orbit Venera 1 (USSR) Launch 02/12/1961 First attempted flyby; contact lost en route Mariner 1 (US) Launch 07/22/1961 Attempted flyby; launch failure Sputnik 19 (USSR) Launch 08/25/1962 Attempted flyby, stranded in Earth orbit Mariner 2 (US) Launch 08/27/1962 First successful Venus flyby Sputnik 20 (USSR) Launch 09/01/1962 Attempted flyby, upper stage failure Sputnik 21 (USSR) Launch 09/12/1962 Attempted flyby, upper stage failure Cosmos 21 (USSR) Launch 11/11/1963 Possible Venera engineering test flight or attempted flyby Venera 1964A (USSR) Launch 02/19/1964 Attempted flyby, launch failure Venera 1964B (USSR) Launch 03/01/1964 Attempted flyby, launch failure Cosmos 27 (USSR) Launch 03/27/1964 Attempted flyby, upper stage failure Zond 1 (USSR) Launch 04/02/1964 Venus flyby, contact lost May 14; flyby July 14 Venera 2 (USSR) Launch 11/12/1965 Venus flyby, contact lost en route Venera 3 (USSR) Launch 11/16/1965 Venus lander, contact lost en route, first Venus impact March 1, 1966 Cosmos 96 (USSR) Launch 11/23/1965 Possible attempted landing, craft fragmented in Earth orbit Venera 1965A (USSR) Launch 11/23/1965 Flyby attempt (launch failure) Venera 4 (USSR) Launch 06/12/1967 Successful atmospheric probe, arrived at Venus 10/18/1967 Mariner 5 (US) Launch 06/14/1967 Successful flyby 10/19/1967 Cosmos 167 (USSR) Launch 06/17/1967 Attempted atmospheric probe, stranded in Earth orbit Venera 5 (USSR) Launch 01/05/1969 Returned atmospheric data for 53 min on 05/16/1969 M. -
Achievements of Hayabusa2: Unveiling the World of Asteroid by Interplanetary Round Trip Technology
Achievements of Hayabusa2: Unveiling the World of Asteroid by Interplanetary Round Trip Technology Yuichi Tsuda Project Manager, Hayabusa2 Japan Aerospace ExplorationAgency 58th COPUOS, April 23, 2021 Lunar and Planetary Science Missions of Japan 1980 1990 2000 2010 2020 Future Plan Moon 2007 Kaguya 1990 Hiten SLIM Lunar-A × Venus 2010 Akatsuki 2018 Mio 1998 Nozomi × Planets Mercury (Mars) 2010 IKAROS Venus MMX Phobos/Mars 1985 Suisei 2014 Hayabusa2 Small Bodies Asteroid Ryugu 2003 Hayabusa 1985 Sakigake Asteroid Itokawa Destiny+ Comet Halley Comet Pheton 2 Hayabusa2 Mission ✓ Sample return mission to a C-type asteroid “Ryugu” ✓ 5.2 billion km interplanetary journey. Launch Earth Gravity Assist Ryugu Arrival MINERVA-II-1 Deployment Dec.3, 2014 Sep.21, 2018 Dec.3, 2015 Jun.27, 2018 MASCOT Deployment Oct.3, 2018 Ryugu Departure Nov.13.2019 Kinetic Impact Earth Return Second Dec.6, 2020 Apr.5, 2019 Target Markers Orbiting Touchdown Sep.16, 2019 Jul,11, 2019 First Touchdown Feb.22, 2019 MINERVA-II-2 Orbiting MD [D VIp srvlxp #534<# Oct.2, 2019 Hayabusa2 Spacecraft Overview Deployable Xband Xband Camera (DCAM3) HGA LGA Xband Solar Array MGA Kaba nd Ion Engine HGA Panel RCS thrusters ×12 ONC‐T, ONC‐W1 Star Trackers Near Infrared DLR MASCOT Spectrometer (NIRS3) Lander Thermal Infrared +Z Imager (TIR) Reentry Capsule +X MINERVA‐II Small Carry‐on +Z LIDAR ONC‐W2 +Y Rovers Impactor (SCI) +X Sampler Horn Target +Y Markers ×5 Launch Mass: 609kg Ion Engine: Total ΔV=3.2km/s, Thrust=5-28mN (variable), Specific Impulse=2800- 3000sec. (4 thrusters, mounted on two-axis gimbal) Chemical RCS: Bi-prop. -
Jjmonl 1603.Pmd
alactic Observer GJohn J. McCarthy Observatory Volume 9, No. 3 March 2016 GRAIL - On the Trail of the Moon's Missing Mass GRAIL (Gravity Recovery and Interior Laboratory) was a NASA scientific mission in 2011/12 to map the surface of the moon and collect data on gravitational anomalies. The image here is an artist's impres- sion of the twin satellites (Ebb and Flow) orbiting in tandem above a gravitational image of the moon. See inside, page 4 for information on gravitational anomalies (mascons) or visit http://solarsystem. nasa.gov/grail. The John J. McCarthy Observatory Galactic Observer New Milford High School Editorial Committee 388 Danbury Road Managing Editor New Milford, CT 06776 Bill Cloutier Phone/Voice: (860) 210-4117 Production & Design Phone/Fax: (860) 354-1595 www.mccarthyobservatory.org Allan Ostergren Website Development JJMO Staff Marc Polansky It is through their efforts that the McCarthy Observatory Technical Support has established itself as a significant educational and Bob Lambert recreational resource within the western Connecticut Dr. Parker Moreland community. Steve Barone Jim Johnstone Colin Campbell Carly KleinStern Dennis Cartolano Bob Lambert Mike Chiarella Roger Moore Route Jeff Chodak Parker Moreland, PhD Bill Cloutier Allan Ostergren Cecilia Dietrich Marc Polansky Dirk Feather Joe Privitera Randy Fender Monty Robson Randy Finden Don Ross John Gebauer Gene Schilling Elaine Green Katie Shusdock Tina Hartzell Paul Woodell Tom Heydenburg Amy Ziffer In This Issue "OUT THE WINDOW ON YOUR LEFT" ............................... 4 SUNRISE AND SUNSET ...................................................... 13 MARE HUMBOLDTIANIUM AND THE NORTHEAST LIMB ......... 5 JUPITER AND ITS MOONS ................................................. 13 ONE YEAR IN SPACE ....................................................... 6 TRANSIT OF JUPITER'S RED SPOT .................................... -
In Situ Observations of Cometary Nuclei 211
Keller et al.: In Situ Observations of Cometary Nuclei 211 In Situ Observations of Cometary Nuclei H. U. Keller Max-Planck-Institut für Aeronomie D. Britt University of Central Florida B. J. Buratti Jet Propulsion Laboratory N. Thomas Max-Planck-Institut für Aeronomie (now at University of Bern) It is only through close spacecraft encounters that cometary nuclei can be resolved and their properties determined with complete confidence. At the time of writing, only two nuclei (those of Comets 1P/Halley and 19P/Borrelly) have been observed, both by rapid flyby missions. The camera systems onboard these missions have revealed single, solid, dark, lumpy, and elongated nuclei. The infrared systems gave surface temperatures well above the free sublimation tempera- ture of water ice and close to blackbody temperatures. The observed nuclei were much more similar than they were different. In both cases, significant topography was evident, possibly reflecting the objects’ sublimation histories. Dust emission was restricted to active regions and jets in the inner comae were prevalent. Active regions may have been slightly brighter than inert areas but the reflectance was still very low. No activity from the nightside was found. In this chapter, the observations are presented and comparisons are made between Comets Halley and Borrelly. A paradigm for the structure of cometary nuclei is also described that implies that the nonvolatile component defines the characteristics of nuclei and that high porosity, large- scale inhomogeneity, and moderate tensile strength are common features. 1. INTRODUCTION It is important to emphasize that prior to the spacecraft encounters with Comet 1P/Halley in 1986, the existence of The nuclei of most comets are too small to be resolved a nucleus was merely inferred from coarse observations. -
Abstract Book
\ Abstract Book 50th ESLAB Symposium: “From Giotto to Rosetta” 14 – 18 March 2016 Leiden, The Netherlands 2 Table of Contents Programme .................................................................................................................................................. 4 Monday 14 March 2016 ............................................................................................................................ 5 Tuesday 15 March 2016 ............................................................................................................................ 7 Wednesday 16 March 2016 ...................................................................................................................... 9 Thursday 17 March 2016 ........................................................................................................................ 11 Friday 18 March 2016 ............................................................................................................................. 13 Poster Sessions........................................................................................................................................ 14 Abstracts .................................................................................................................................................... 23 Oral Presentations ............................................................................................................................... 23 Posters .................................................................................................................................................. -
Analysis of MIRO/Rosetta Data
Analysis of MIRO/Rosetta Data Dissertation zur Erlangung des mathematisch-naturwissenschaftlichen Doktorgrades “Doctor rerum naturalium” der Georg-August-Universität Göttingen im Promotionsprogramm PROPHYS der Georg-August University School of Science (GAUSS) vorgelegt von David Marshall aus Norwich, Vereinigtes Königreich Göttingen, 2018 Betreuungsausschuss Dr. Paul Hartogh Max-Planck-Institut für Sonnensystemforschung, Göttingen Prof. Dr. Stefan Dreizler Institut für Astrophysik, Georg-August-Universität Göttingen Mitglieder der Prüfungskommision Referent: Dr. Paul Hartogh Max-Planck-Institut für Sonnensystemforschung, Göttingen Korreferent: Prof. Dr. Stefan Dreizler Institut für Astrophysik, Georg-August-Universität Göttingen Weitere Mitglieder der Prüfungskommission: Prof. Dr. Ulrich Christensen Max-Planck-Institut für Sonnensystemforschung, Göttingen Prof. Dr. Ariane Frey II. Physikalisches Institut, Georg-August-Universität Göttingen Prof. Dr. Thorsten Hohage Institut für Numerische und Angewandte Mathematik, Georg-August-Universität Göttin- gen Prof. Dr. Andreas Pack Geowissenschaftliches Zentrum, Georg-August-Universität Göttingen Tag der mündlichen Prüfung: 19.12.2018 Bibliografische Information der Deutschen Nationalbibliothek Die Deutsche Nationalbibliothek verzeichnet diese Publikation in der Deutschen Nationalbibliografie; detaillierte bibliografische Daten sind im Internet über http://dnb.d-nb.de abrufbar. ISBN 978-3-944072-65-4 uni-edition GmbH 2019 http://www.uni-edition.de c David Marshall This work is distributed under a Creative Commons Attribution 3.0 License Printed in Germany Contents Summary9 Zusammenfassung 11 1 Introduction 13 1.1 Comets................................... 13 1.2 Observational history: from the stone age to the space age........ 16 1.3 The Rosetta mission............................. 21 1.4 67P/Churyumov-Gerasimenko....................... 24 1.5 The Microwave Instrument for the Rosetta orbiter............. 28 1.6 MIRO aims, results and spectra....................... 32 1.7 Thesis aims................................ -
Technologies for Future Venus Exploration
September 9, 2009 WHITE PAPER TO THE NRC DECADAL SURVEY INNER PLANETS SUB–PANEL ON TECHNOLOGIES FOR FUTURE VENUS EXPLORATION by Tibor Balint1 & James Cutts1 (818) 354-1105 & (818) 354-4120 [email protected] & [email protected] and Mark Bullock2, James Garvin3, Stephen Gorevan4, Jeffery Hall1, Peter Hughes3, Gary Hunter4, Satish Khanna1, Elizabeth Kolawa1, Viktor Kerzhanovich1, Ethiraj Venkatapathy5 1Jet Propulsion Laboratory, California Institute of Technology; 2Southwest Research Institute; 3NASA–Goddard Space Flight Center; 3Honeybee Robotics; 4NASA–Glenn Research Center; 5NASA–Ames Research Center ABSTRACT The purpose of this white paper is to provide an overview to the NRC Decadal Survey Inner Planets Sub–Panel on key technologies required for future Venus exploration missions. It covers both heritage technologies and identifies new technologies to enable future missions in all three mission classes. The technologies will focus on mission enabling and enhancing capabilities for in situ missions, because most orbiter related sub–systems are considered heritage technologies. This white paper draws heavily on the recently completed Venus Flagship Mission study that identified key technologies required to implement its Design Reference Mission and other important mission options. The highest priority technologies and capabilities for the Venus Flagship Design Reference mission consist of: surface sample acquisition and handling; mechanical implementation of a rotating pressure vessel; a rugged–terrain landing system; and a large scale environmental test chamber to test these technologies under relevant Venus–like conditions. Other longer–term Venus Flagship Mission options will require additional new capabilities, namely a Venus–specific Radioisotope Power System; active refrigeration, high temperature electronics and advanced thermal insulation. -
1950 Da, 205, 269 1979 Va, 230 1991 Ry16, 183 1992 Kd, 61 1992
Cambridge University Press 978-1-107-09684-4 — Asteroids Thomas H. Burbine Index More Information 356 Index 1950 DA, 205, 269 single scattering, 142, 143, 144, 145 1979 VA, 230 visual Bond, 7 1991 RY16, 183 visual geometric, 7, 27, 28, 163, 185, 189, 190, 1992 KD, 61 191, 192, 192, 253 1992 QB1, 233, 234 Alexandra, 59 1993 FW, 234 altitude, 49 1994 JR1, 239, 275 Alvarez, Luis, 258 1999 JU3, 61 Alvarez, Walter, 258 1999 RL95, 183 amino acid, 81 1999 RQ36, 61 ammonia, 223, 301 2000 DP107, 274, 304 amoeboid olivine aggregate, 83 2000 GD65, 205 Amor, 251 2001 QR322, 232 Amor group, 251 2003 EH1, 107 Anacostia, 179 2007 PA8, 207 Anand, Viswanathan, 62 2008 TC3, 264, 265 Angelina, 175 2010 JL88, 205 angrite, 87, 101, 110, 126, 168 2010 TK7, 231 Annefrank, 274, 275, 289 2011 QF99, 232 Antarctic Search for Meteorites (ANSMET), 71 2012 DA14, 108 Antarctica, 69–71 2012 VP113, 233, 244 aphelion, 30, 251 2013 TX68, 64 APL, 275, 292 2014 AA, 264, 265 Apohele group, 251 2014 RC, 205 Apollo, 179, 180, 251 Apollo group, 230, 251 absorption band, 135–6, 137–40, 145–50, Apollo mission, 129, 262, 299 163, 184 Apophis, 20, 269, 270 acapulcoite/ lodranite, 87, 90, 103, 110, 168, 285 Aquitania, 179 Achilles, 232 Arecibo Observatory, 206 achondrite, 84, 86, 116, 187 Aristarchus, 29 primitive, 84, 86, 103–4, 287 Asporina, 177 Adamcarolla, 62 asteroid chronology function, 262 Adeona family, 198 Asteroid Zoo, 54 Aeternitas, 177 Astraea, 53 Agnia family, 170, 198 Astronautica, 61 AKARI satellite, 192 Aten, 251 alabandite, 76, 101 Aten group, 251 Alauda family, 198 Atira, 251 albedo, 7, 21, 27, 185–6 Atira group, 251 Bond, 7, 8, 9, 28, 189 atmosphere, 1, 3, 8, 43, 66, 68, 265 geometric, 7 A- type, 163, 165, 167, 169, 170, 177–8, 192 356 © in this web service Cambridge University Press www.cambridge.org Cambridge University Press 978-1-107-09684-4 — Asteroids Thomas H.