Bernard Marty Patrick Michel
Total Page:16
File Type:pdf, Size:1020Kb
Load more
Recommended publications
-
Using a Nuclear Explosive Device for Planetary Defense Against an Incoming Asteroid
Georgetown University Law Center Scholarship @ GEORGETOWN LAW 2019 Exoatmospheric Plowshares: Using a Nuclear Explosive Device for Planetary Defense Against an Incoming Asteroid David A. Koplow Georgetown University Law Center, [email protected] This paper can be downloaded free of charge from: https://scholarship.law.georgetown.edu/facpub/2197 https://ssrn.com/abstract=3229382 UCLA Journal of International Law & Foreign Affairs, Spring 2019, Issue 1, 76. This open-access article is brought to you by the Georgetown Law Library. Posted with permission of the author. Follow this and additional works at: https://scholarship.law.georgetown.edu/facpub Part of the Air and Space Law Commons, International Law Commons, Law and Philosophy Commons, and the National Security Law Commons EXOATMOSPHERIC PLOWSHARES: USING A NUCLEAR EXPLOSIVE DEVICE FOR PLANETARY DEFENSE AGAINST AN INCOMING ASTEROID DavidA. Koplow* "They shall bear their swords into plowshares, and their spears into pruning hooks" Isaiah 2:4 ABSTRACT What should be done if we suddenly discover a large asteroid on a collision course with Earth? The consequences of an impact could be enormous-scientists believe thatsuch a strike 60 million years ago led to the extinction of the dinosaurs, and something ofsimilar magnitude could happen again. Although no such extraterrestrialthreat now looms on the horizon, astronomers concede that they cannot detect all the potentially hazardous * Professor of Law, Georgetown University Law Center. The author gratefully acknowledges the valuable comments from the following experts, colleagues and friends who reviewed prior drafts of this manuscript: Hope M. Babcock, Michael R. Cannon, Pierce Corden, Thomas Graham, Jr., Henry R. Hertzfeld, Edward M. -
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. -
OSIRIS-Rex, Returning the Asteroid Sample
OSIRIS-REx, Returning the Asteroid Sample Thomas Ajluni Timothy Linn William Willcockson ASRC Federal Space & Defense Lockheed Martin Space Systems Lockheed Martin Space Systems 7000 Muirkirk Meadows Drive Company, P.O. Box 179 Company, P.O. Box 179 Suite 100, Beltsville, MD 20705 Denver, CO 80201 Denver, CO 80201 301.286.1831 303-977-0659 303-977-5094 [email protected] [email protected] [email protected] David Everett Ronald Mink Joshua Wood NASA Goddard Space Flight NASA Goddard Space Flight Lockheed Martin Space Systems Center, 8800 Greenbelt Road Center, 8800 Greenbelt Road Company, P.O. Box 179 Greenbelt, MD 20771 Greenbelt, MD 20771 Denver, CO 80201 301.286.1596 301.286.3524 303-977-3199 [email protected] [email protected] [email protected] Abstract—This paper addresses the technical aspects of the sample return system for the upcoming Origins, Spectral x attitude control Interpretation, Resource Identification, and Security-Regolith x propulsion Explorer (OSIRIS-REx) asteroid sample return mission. The x power overall mission design and current implementation are presented as an overview to establish a context for the x thermal control technical description of the reentry and landing segment of the x telecommunications mission. x command and data handling x structural support to ensure successful rendezvous The prime objective of the OSIRIS-REx mission is to sample a with Bennu primitive, carbonaceous asteroid and to return that sample to Earth in pristine condition for detailed laboratory analysis. x characterization of Bennu’s properties Targeting the near-Earth asteroid Bennu, the mission launches x delivery of the sampler to the surface, and return of in September 2016 with an Earth reentry date of September the spacecraft to the vicinity of the Earth 24, 2023. -
Chondrule-Like Material in Wild 2: a New Insight from Impact Experiments of Chondrule Fragments on Stardust Analogue Al Foil
52nd Lunar and Planetary Science Conference 2021 (LPI Contrib. No. 2548) 1925.pdf CHONDRULE-LIKE MATERIAL IN WILD 2: A NEW INSIGHT FROM IMPACT EXPERIMENTS OF CHONDRULE FRAGMENTS ON STARDUST ANALOGUE AL FOIL. M. Van Ginneken1 and P. J. Wozniakiewicz1, 1Centre for Astrophysics and Planetary Science, School of Physical Sciences, University of Kent, United Kingdom ([email protected]; [email protected]) Introduction: NASA’s Stardust mission was the shape of craters depends mainly on the physical first mission to bring back to Earth material from a properties of the impactor [19]. Solid grains or dense celestial body, i.e. the Jupiter Family Comet (JFC) consolidated aggregates similar to chondrule fragments 81P/Wild 2 (hereafter Wild 2) [1]. Cometary dust was will result in bowl-shaped craters, the depth of which captured via impact into a collector that was deployed depending on the density of the material, whereas loose during a fly-by through the coma of Wild 2 at a relative aggregates of submicron particles result in complex speed of 6 km s-1. The collector consisted of silica features. Simulation of Stardust impacts using silicate aerogel secured into a metal frame by aluminum 1100 grains have shown that about 50% of silicate dominated foil (hereafter Al foil). A major result of the mission was impactors are retained as residue, which can be analysed the discovery that, contrary to expectations, Wild 2 was and provide precious chemical information [20]. not predominantly composed of presolar grains and low Studies of residues in a small (ø < 10 µm) or large temperature outer solar nebula material, but rather high (ø > 10 µm) craters on Stardust foil have shown that temperature (>>1000 °C) material typical of primitive these can give information on the bulk chemistry of the meteorites [1 - 3]. -
The Hera Mission
Dr. Patrick Michel Hera Investigation Team PI Université Côte d’Azur Observatoire de la Côte d’Azur CNRS, Lagrange Laboratory Nice, France The Hera Mission ESA UNCLASSIFIED - For Official Use Hera main aspects Role of space missions at ESA in NEO hazard mitigation • Understanding the problem (deflection modeling and simulations) 2001 • Ground versus space solutions analyses • Assessment of space component options 2002- • 6 parallel phase-0 studies (3 space telescopes, 3 rendezvous) Euneos Nero Earthguard 1 2004 • ESA’s NEO Mission Advisory Panel (NEOMAP) established • Kinetic impactor validation ranked highest importance 2004- • Don Quijote mission selected and studied up to phase-A level 2006 • SANCHO / Proba-IP orbiter up to phase A level studies, small deep-space Don Quijote Ishtar Simone 2008- mission to investigate impactor’s result 2009 • AIDA proposed by NASA: USA/impactor + ESA/impact assessment • ESA phase 0 and phase A studies on the observer spacecraft "AIM” (GSP) 2011- Proba-IP 2016 • Phase B1 study and “consolidation phase” for mission definition (GSTP) • HERA: impact observer spacecraft reformulation and optimization AIM 2017- • Phase B1 implementation + payload + technology breadboards (GSTP+SSA) Several concepts 2019 • DART phase-C kick-off on 15 May 2018 Hera iterated AIDA: An International Planetary Defense Mission U.S. National Research Council Committee “Defending Planet Earth: Near-Earth Object Surveys and Hazard Mitigation Strategies” Recommendation: “If [U.S.] Congress chooses to fund mitigation research at an appropriately high level, the first priority for a space mission in the mitigation area is an experimental test of a kinetic impactor along with a characterization, monitoring, and verification system, such as the Don Quixote mission that was previously considered, but not funded, by the European Space Agency. -
Space Sector Brochure
SPACE SPACE REVOLUTIONIZING THE WAY TO SPACE SPACECRAFT TECHNOLOGIES PROPULSION Moog provides components and subsystems for cold gas, chemical, and electric Moog is a proven leader in components, subsystems, and systems propulsion and designs, develops, and manufactures complete chemical propulsion for spacecraft of all sizes, from smallsats to GEO spacecraft. systems, including tanks, to accelerate the spacecraft for orbit-insertion, station Moog has been successfully providing spacecraft controls, in- keeping, or attitude control. Moog makes thrusters from <1N to 500N to support the space propulsion, and major subsystems for science, military, propulsion requirements for small to large spacecraft. and commercial operations for more than 60 years. AVIONICS Moog is a proven provider of high performance and reliable space-rated avionics hardware and software for command and data handling, power distribution, payload processing, memory, GPS receivers, motor controllers, and onboard computing. POWER SYSTEMS Moog leverages its proven spacecraft avionics and high-power control systems to supply hardware for telemetry, as well as solar array and battery power management and switching. Applications include bus line power to valves, motors, torque rods, and other end effectors. Moog has developed products for Power Management and Distribution (PMAD) Systems, such as high power DC converters, switching, and power stabilization. MECHANISMS Moog has produced spacecraft motion control products for more than 50 years, dating back to the historic Apollo and Pioneer programs. Today, we offer rotary, linear, and specialized mechanisms for spacecraft motion control needs. Moog is a world-class manufacturer of solar array drives, propulsion positioning gimbals, electric propulsion gimbals, antenna positioner mechanisms, docking and release mechanisms, and specialty payload positioners. -
Stardust Sample Return
National Aeronautics and Space Administration Stardust Sample Return Press Kit January 2006 www.nasa.gov Contacts Merrilee Fellows Policy/Program Management (818) 393-0754 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, Wash. Contents General Release ............................................................................................................... 3 Media Services Information ……………………….................…………….................……. 5 Quick Facts …………………………………………..................………....…........…....….. 6 Mission Overview …………………………………….................……….....……............…… 7 Recovery Timeline ................................................................................................ 18 Spacecraft ………………………………………………..................…..……...........……… 20 Science Objectives …………………………………..................……………...…..........….. 28 Why Stardust?..................…………………………..................………….....………............... 31 Other Comet Missions .......................................................................................... 33 NASA's Discovery Program .................................................................................. 36 Program/Project Management …………………………........................…..…..………...... 40 1 2 GENERAL RELEASE: NASA PREPARES FOR RETURN OF INTERSTELLAR CARGO NASA’s Stardust mission is nearing Earth after a 2.88 billion mile round-trip journey -
The Power of Sample Return Missions - Stardust and Hayabusa
The Molecular Universe Proceedings IAU Symposium No. 280, 2011 c International Astronomical Union 2011 Jos´e Cernicharo & Rafael Bachiller, eds. doi:10.1017/S174392131102504X The Power of Sample Return Missions - Stardust and Hayabusa Scott A. Sandford1 1 Astrophysics Branch, NASA-Ames Research Center, Mail Stop 245-6, Moffett Field, CA 94035 USA email: [email protected] Abstract. Sample return missions offer opportunities to learn things about other objects in our Solar System (and beyond) that cannot be determined by observations using in situ spacecraft. This is largely because the returned samples can be studied in terrestrial laboratories where the analyses are not limited by the constraints - power, mass, time, precision, etc. - imposed by normal spacecraft operations. In addition, the returned samples serve as a scientific resource that is available far into the future; the study of the samples can continue long after the original spacecraft mission is finished. This means the samples can be continually revisited as both our scientific understanding and analytical techniques improve with time. These advantages come with some additional difficulties, however. In particular, sample return missions must deal with the additional difficulties of proximity operations near the objects they are to sample, and they must be capable of successfully making a round trip between the Earth and the sampled object. Such missions therefore need to take special precautions against unique hazards and be designed to successfully complete relatively extended mission durations. Despite these difficulties, several recent missions have managed to successfully complete sam- ple returns from a number of Solar System objects. These include the Stardust mission (samples from Comet 81P/Wild 2), the Hayabusa mission (samples from asteroid 25143 Itokawa), and the Genesis mission (samples of solar wind). -
European Component of the AIDA Mission to a Binary Asteroid: Characterization and Interpretation of the Impactof the DART Mission
Available online at www.sciencedirect.com ScienceDirect Advances in Space Research 62 (2018) 2261–2272 www.elsevier.com/locate/asr European component of the AIDA mission to a binary asteroid: Characterization and interpretation of the impactof the DART mission Patrick Michel a,⇑, Michael Kueppers b, Holger Sierks c, Ian Carnelli d, Andy F. Cheng e, Karim Mellab f, Mikael Granvik g, Antti Kestila¨ h, Tomas Kohout g,i, Karri Muinonen g,j, Antti Na¨sila¨ k, Antti Penttila g, Tuomas Tikka l, Paolo Tortora m, Vale´rie Ciarletti n, Alain He´rique o, Naomi Murdoch p, Erik Asphaug q, Andy Rivkin e, Olivier Barnouin e, Adriano Campo Bagatin r, Petr Pravec s, Derek C. Richardson t, Stephen R. Schwartz a,q, Kleomenis Tsiganis u, Stephan Ulamec v, Ozgu¨r Karatekin w a Universite´ Coˆte d’Azur, Observatoire de la Coˆte d’Azur, CNRS, Laboratoire Lagrange, CS 34229, 06304 Nice Cedex 4, France b ESA/ESAC, Camino bajo del Castillo, s/n Urbanizacio´n Villafranca del Castillo Villanueva de la Canada, E-28692 Madrid, Spain c Max-Planck Institute for Solar System Research, Justus-von-Liebig-Weg 3, 37077 Go¨ttingen, Germany d ESA/Hq, 8-10 rue Mario Nikis, 75738 Paris Cedex 15, France e The Johns Hopkins University Applied Physics Laboratory, 11100 Johns Hopkins Road, Laurel, 20723 MD, USA f ESA/ESTEC, Keplerlaan 1, 2201 AZ Noordwijk, The Netherlands g Department of Physics, University of Helsinki, Gustaf Ha¨llstro¨min katu 2a, FI-00560 Helsinki, Finland h Aalto University, 02150 Espoo, Finland i Institute of Geology, The Czech Academy of Sciences, Rozvojova´ 269, CZ-165 00 Prague 6 - Lysolaje, Czech Republic j Finnish Geospatial Research Institute FGI, National Land Survey, Geodeetinrinne 2, FI-02430 Masala, Finland k VTT Technical Research Centre of Finland, 02150 Espoo, Finland l Reaktor Space Lab, Mannerheimintie 2, 00100 Helsinki, Finland m University of Bologna, Department of Industrial Engineering, Via Fontanelle 40, 47121 Forlı`, FC, Italy n UVSQ (UPSay), UPMC (Sorbonne Univ.), CNRS/INSU, LATMOS-IPSL, 11 Boulevard d’Alembert, 78280 Guyancourt, France o Univ. -
Dawn Mission to Vesta and Ceres Symbiosis Between Terrestrial Observations and Robotic Exploration
Earth Moon Planet (2007) 101:65–91 DOI 10.1007/s11038-007-9151-9 Dawn Mission to Vesta and Ceres Symbiosis between Terrestrial Observations and Robotic Exploration C. T. Russell Æ F. Capaccioni Æ A. Coradini Æ M. C. De Sanctis Æ W. C. Feldman Æ R. Jaumann Æ H. U. Keller Æ T. B. McCord Æ L. A. McFadden Æ S. Mottola Æ C. M. Pieters Æ T. H. Prettyman Æ C. A. Raymond Æ M. V. Sykes Æ D. E. Smith Æ M. T. Zuber Received: 21 August 2007 / Accepted: 22 August 2007 / Published online: 14 September 2007 Ó Springer Science+Business Media B.V. 2007 Abstract The initial exploration of any planetary object requires a careful mission design guided by our knowledge of that object as gained by terrestrial observers. This process is very evident in the development of the Dawn mission to the minor planets 1 Ceres and 4 Vesta. This mission was designed to verify the basaltic nature of Vesta inferred both from its reflectance spectrum and from the composition of the howardite, eucrite and diogenite meteorites believed to have originated on Vesta. Hubble Space Telescope observations have determined Vesta’s size and shape, which, together with masses inferred from gravitational perturbations, have provided estimates of its density. These investigations have enabled the Dawn team to choose the appropriate instrumentation and to design its orbital operations at Vesta. Until recently Ceres has remained more of an enigma. Adaptive-optics and HST observations now have provided data from which we can begin C. T. Russell (&) IGPP & ESS, UCLA, Los Angeles, CA 90095-1567, USA e-mail: [email protected] F. -
Astronomical Observability of the Cassini Entry Into Saturn
1 7/25/2017 Astronomical Observability of the Cassini Entry into Saturn Ralph D. Lorenz Johns Hopkins Applied Physics Laboratory Laurel, MD 20723, USA [email protected] Abstract The Cassini spacecraft will enter Saturn's atmosphere on 15 th September 2017. This event may be visible from Earth as a 'meteor' flash, and entry dynamics simulations and results from observation of spacecraft entries at Earth are summarized to develop expectations for astronomical observability. 2 1. Cassini End of Mission Scenario Cassini was originally designed to perform a 4-year exploration of the Saturnian system, after arrival in 2004 and delivering the Huygens probe to Titan. Robust design and a rich scientific return have permitted and motivated two mission extensions, first to 2010 and later to 2017. At this point, systems and instruments, although generally performing very well, are well beyond their qualification lifetimes. Electrical power has been slowly declining (restricting the number of instruments that can operate simultaneously), but most importantly the propellants for manoeuvres and attitude control have been depleted. Planetary protection considerations require the radioisotope-powered spacecraft to be disposed of in a controlled manner that will preclude the contamination of Saturn moons that have potentially habitable environments, notably Titan and Enceladus. As with Galileo at Jupiter in 2003, the chosen plan is to direct the spacecraft to enter the primary planet's atmosphere. The endgame part of Cassini's orbital tour (the "Grand Finale") was designed (e.g. Yam et al., 2009) with a series of orbits with apoapsis near Titan's orbit, permitting continued observations towards the summer solstice, and periapsis initially outside the F-ring, with a gravity assist from a final close Titan encounter (T126, in April 2017) shifting the periapsis to within the D-ring, i.e. -
Ceres Is the Largest Object in the Asteroid Belt, Which Lies Mainly
Dactyl, the moon of Ida, is shown below in a close-up and at its true size relative to Ida. Dactyl was the Ceres and the Asteroid Belt first asteroid moon to be discovered. Ceres is the largest object in the The best photos of Ceres (below left) and Vesta (below right) as As of 2008, only the asteroid belt, which lies mainly of 2008, from the Hubble Space Telescope (courtesy NASA/ESA) handful of asteroids between Mars and Jupiter. shown here have had Ida and Dactyl, from NASA’s Galileo Asteroids are made of various their pictures taken combinations of rocks, metals and by spacecraft flying carbon compounds that have past them. If you’re Steins, Ceres is much smaller than the Moon, which is shown below reading this panel from ESA’s Rosetta Eros, from NEAR never been captured by any after 2011, you’ve planet’s gravity. Asteroids have on the same scale as Ceres and Vesta above. Nonetheless, Shoemaker Ceres is sometimes referred to as a dwarf planet, hopefully seen better (NASA/JHUAPL) not changed much for billions of along with Pluto and a growing list of other objects. photos of Vesta, the years, making them important third-largest object in records of the formation of the the asteroid belt, solar system. The solar system taken by the Mathilde, from contains millions of asteroids Dawn spacecraft. And if you’re reading NEAR Shoemaker ranging down to the size of large (NASA/JHUAPL) this panel after 2015, boulders, as well as smaller hopefully there are objects called meteoroids.