A New View on the Solar Wind Interaction with the Moon
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Conceptual Design for a Sputter-Type Negative Ion Source Based
MOPO-03 Proceedings of ECRIS08, Chicago, IL USA CONCEPTUAL DESIGN OF A SPUTTER-TYPE NEGATIVE ION SOURCE BASED ON ELECTRON CYCLOTRON RESONANCE PLASMA HEATING O. Tarvainen and S. Kurennoy, Los Alamos National Laboratory, Los Alamos, NM 87545, U.S.A. Abstract PHYSICS ASPECTS OF H- ION BEAM A design for a negative ion source based on electron PRODUCTION cyclotron resonance plasma heating and ionization by Modern H- ion sources are based on two important ion surface sputtering is presented. The plasma chamber of formation processes, the volume [3] and the surface [4] the source is an rf-cavity designed for TE111 eigenmode at production. The relative importance of these processes 2.45 GHz. The desired mode is excited with a loop depends on the detailed design of the ion source. antenna. The ionization process takes place on a cesiated The volume production of H- is generally accepted to surface of a biased converter electrode (cathode). The ion be due to dissociative attachment (DA) of low energy beam is further “self-extracted” through the plasma electrons to rovibrationally (ν,,) excited molecules. Two region. The magnetic field of the source is optimized for electron populations are needed in order to optimize the both, plasma generation by electron cyclotron resonance volume production process: hot electrons (few eV) heating, and beam extraction. The source can be used for creating the excited molecular states i.e. ehot + H2 Æ e + a production of a variety of negative ions ranging from v’’ H2 (v’’ > 5) and cold electrons (less than 1 eV) hydrogen to heavy ions. -
General Disclaimer One Or More of the Following Statements May Affect
General Disclaimer One or more of the Following Statements may affect this Document This document has been reproduced from the best copy furnished by the organizational source. It is being released in the interest of making available as much information as possible. This document may contain data, which exceeds the sheet parameters. It was furnished in this condition by the organizational source and is the best copy available. This document may contain tone-on-tone or color graphs, charts and/or pictures, which have been reproduced in black and white. This document is paginated as submitted by the original source. Portions of this document are not fully legible due to the historical nature of some of the material. However, it is the best reproduction available from the original submission. Produced by the NASA Center for Aerospace Information (CASI) ^i e I !emote sousing sad eeolegio Studies of the llaistary Crusts Bernard Ray Hawke Prince-1 Investigator a EL r Z^ .99 University of Hawaii Hawaii Institute of Geophysics Planetary Geosciences Division Honolulu, Hawaii 96822 ^y 1i i W. December 1983 (NASA —CR-173215) REMOTE SENSING AND N84-17092 GEOLOGIC STUDIES OF THE PLANETARY CRUSTS Final Report ( Hawaii Inst. of Geophysics) 14 p HC A02/MF 101 CSCL 03B Unclas G3/91 11715 Gy -2- ©R1GNAL OF POOR QUALITY Table of Contents Page I. Remote Sensing and Geologic Studies cf Volcanic Deposits . • . 3 A. Spectral reflectance studies of dark-haloed craters. • . 3 B. Remote s^:sing studies of regions which were sites of ancient volcanisa . 3 C. [REEP basalt deposits in the Imbrium Region. -
Sputter Coating Technical Brief
Sputter Coating Technical Brief Document Number TB-SPUTTER Issue 2 (01/02) Introduction HP000107 Quorum Technologies Ltd main sales office: South Stour Avenue Ashford Kent U.K. Tel: ++44(0) 1233 646332 TN23 7RS Fax: ++44(0) 1233 640744 Email: [email protected] http:///www.quorumtech.com For further information regarding any of the other products designed and manufactured by Quorum Technologies, contact your local representative or directly to Quorum Technologies at the address above. Carbon and sputter coaters Plasma reactor for ashing and etching High vacuum bench top evaporators Cryo-SEM preparation systems Critical point dryers Freeze dryers for electron microscopy Service and Spares Disclaimer The components and packages described in this document are mutually compatible and guaranteed to meet or exceed the published performance specifications. No performance guarantees, however, can be given in circumstances where these component packages are used in conjunction with equipment supplied by companies other than Quorum Technologies. Quorum Technologies Limited, Company No. 04273003 Registered office: Unit 19, Charlwoods Road, East Grinstead, West Sussex, RH19 2HL, UK TB-SPUTTER Contents Contents Chapter 1 - Introduction .......................................................................................... 4 Chapter 2 - Gaseous Condition .............................................................................. 5 Chapter 3 - Glow Discharge ................................................................................... -
A Self-Sputtering Ion Source: a New Approach to Quiescent Metal Ion Beams
Lawrence Berkeley National Laboratory Lawrence Berkeley National Laboratory Title A self-sputtering ion source: A new approach to quiescent metal ion beams Permalink https://escholarship.org/uc/item/24w7z1p2 Author Oks, Efim M. Publication Date 2010-03-31 Peer reviewed eScholarship.org Powered by the California Digital Library University of California Presented at the International Conference on Ion Sources on September 24, 2009 and submitted for publication to Review of Scientific Instruments received September 3, 2009, accepted November 13, 2009 A self-sputtering ion source: A new approach to quiescent metal ion beams Efim Oks1 and André Anders2* 1High Current Electronics Institute, Russian Academy of Sciences, 2/3 Academichesky Ave., Tomsk 634055, Russia 2Lawrence Berkeley National Laboratory, 1 Cyclotron Road, Berkeley, California 94720, USA *corresponding author, email [email protected] rev. version of November 05, 2009 ACKNOWLEDGMENT The work was supported by the US Department of Energy under Contract No DE-AC02-05CH11231 with the Lawrence Berkeley National Laboratory. DISCLAIMER This document was prepared as an account of work sponsored in part by the United States Government. While this document is believed to contain correct information, neither the United States Government nor any agency thereof, nor The Regents of the University of California, nor any of their employees, makes any warranty, express or implied, or assumes any legal responsibility for the accuracy, completeness, or usefulness of any information, apparatus, product, or process disclosed, or represents that its use would not infringe privately owned rights. Reference herein to any specific commercial product, process, or service by its trade name, trademark, manufacturer, or otherwise, does not necessarily constitute or imply its endorsement, recommendation, or favoring by the United States Government or any agency thereof, or The Regents of the University of California. -
Regolith Compaction and Its Implications for the Formation Mechanism of Lunar Swirls
EPSC Abstracts Vol. 13, EPSC-DPS2019-1608-1, 2019 EPSC-DPS Joint Meeting 2019 c Author(s) 2019. CC Attribution 4.0 license. Regolith Compaction and its Implications for the Formation Mechanism of Lunar Swirls Christian Wöhler (1), Megha Bhatt (2), Arne Grumpe (1), Marcel Hess (1), Alexey A. Berezhnoy (3), Vladislav V. Shevchenko (3) and Anil Bhardwaj (2) (1) Image Analysis Group, TU Dortmund University, Otto-Hahn-Str. 4, 44227 Dortmund, Germany, (2) Physical Research Laboratory, Ahmedabad, 380009, India, (3) Sternberg Astronomical Institute, Universitetskij pr., 13, Moscow State University, 119234 Moscow, Russia ([email protected]) Abstract The brightening of the regolith at Reiner Gamma could be a result of reduced space-weathering due to In this study we have examined spectral trends of magnetic shielding [3] and/or due to soil compaction Reiner Gamma (7.5°N, 59°W) using the Moon [5]. According to the model of [9], the spectral Mineralogy Mapper (M3) [1] observations. We variation due to soil compaction is a change in albedo derived maps of solar wind induced OH/H2O and a with negligible effect on spectral slope and compaction index map of the Reiner Gamma swirl. absorption band depths. To quantify soil compaction Our results suggest that the combination of soil at Reiner Gamma, we empirically defined the compaction and magnetic shielding can explain the compaction index c as a positive real number given observed spectral trends. These new findings support by c = M / RSE, where M is the reflectance the hypothesis of swirl formation by interaction modulation at 1.579 µm between a bright on-swirl between a comet and the uppermost regolith layer. -
DMAAC – February 1973
LUNAR TOPOGRAPHIC ORTHOPHOTOMAP (LTO) AND LUNAR ORTHOPHOTMAP (LO) SERIES (Published by DMATC) Lunar Topographic Orthophotmaps and Lunar Orthophotomaps Scale: 1:250,000 Projection: Transverse Mercator Sheet Size: 25.5”x 26.5” The Lunar Topographic Orthophotmaps and Lunar Orthophotomaps Series are the first comprehensive and continuous mapping to be accomplished from Apollo Mission 15-17 mapping photographs. This series is also the first major effort to apply recent advances in orthophotography to lunar mapping. Presently developed maps of this series were designed to support initial lunar scientific investigations primarily employing results of Apollo Mission 15-17 data. Individual maps of this series cover 4 degrees of lunar latitude and 5 degrees of lunar longitude consisting of 1/16 of the area of a 1:1,000,000 scale Lunar Astronautical Chart (LAC) (Section 4.2.1). Their apha-numeric identification (example – LTO38B1) consists of the designator LTO for topographic orthophoto editions or LO for orthophoto editions followed by the LAC number in which they fall, followed by an A, B, C or D designator defining the pertinent LAC quadrant and a 1, 2, 3, or 4 designator defining the specific sub-quadrant actually covered. The following designation (250) identifies the sheets as being at 1:250,000 scale. The LTO editions display 100-meter contours, 50-meter supplemental contours and spot elevations in a red overprint to the base, which is lithographed in black and white. LO editions are identical except that all relief information is omitted and selenographic graticule is restricted to border ticks, presenting an umencumbered view of lunar features imaged by the photographic base. -
Deposition Lecture Day 2 Deposition
Deposition Lecture Day 2 Deposition PVD - Physical Vapor Deposition E-beam Evaporation Thermal Evaporation (wire feed vs boat) Sputtering CVD - Chemical Vapor Deposition PECVD LPCVD MVD ALD MBE Plating Parylene Coating Vacuum Systems, pumps and support equipment Differences, Pros and Cons for depositing various materials Physical vs. Chemical Deposition Metallization - depositing metal layers or thin films - E-beam & Thermal Evaporation, Sputtering, Plating - Contact layer, mask/protection layer, interface layers Dielectric Deposition - depositing dielectric layers or thin films -CVD, e-beam, sputtering - insulating/capacitor layer, mask/protecting layer, interface layers *Dielectric = an electrical insulator that can be polarized by an applied electric field. ~energy storing capacity → capacitor Environment of the Deposition *Cleanroom is not enough! Must also be in vacuum! Purity of the deposited film depends on the quality of the vacuum, and on the purity of the source material. Cryo pumps Evaporation is a common method of thin-film deposition. The source material is evaporated in a vacuum. The vacuum allows vapor particles to travel directly to the target object (substrate), where they condense back to a solid state. Evaporation is used in microfabrication, and to make macro-scale products such as metallized plastic film. Any evaporation system includes a vacuum pump. It also includes an energy source that evaporates the material to be deposited. Many different energy sources exist: ● In the thermal method, metal material (in the form of wire, pellets, shot) is fed onto heated semimetal (ceramic) evaporators known as "boats" due to their shape. A pool of melted metal forms in the boat cavity and evaporates into a cloud above the source. -
Intrusives and Lava Tubes: Potential Lunar Swirl Source Bodies? S
49th Lunar and Planetary Science Conference 2018 (LPI Contrib. No. 2083) 2587.pdf INTRUSIVES AND LAVA TUBES: POTENTIAL LUNAR SWIRL SOURCE BODIES? S. M. Tikoo1 and D. J. Hemingway2, 1Department of Earth and Planetary Sciences, Rutgers University, Piscataway Township, NJ ([email protected]), 2Department of Earth and Planetary Science, University of California, Berkeley, CA. Introduction: Lunar swirls are enigmatic albedo ferromagnetic grains or create new ones. This process features that appear in several regions across the lunar is exemplified by heating experiments on lunar sam- surface (e.g., ref. [1]) and consist of bright and dark ples or their analogs in a controlled oxygen fugacity markings alternating over length scales of typically 1– environment. Heating synthetic mare basalts in a re- 5 km. Most swirls are not readily associated with con- ducing atmosphere ~1 log unit below the iron-wustite spicuous geological features, such as impact craters buffer (i.e., IW-1; the oxygen fugacity conditions in- (e.g., the archetypal swirl at Reiner Gamma lies atop a ferred for a majority of lunar rocks studied thus far) to relatively smooth mare plain) but instead appear to be temperatures in excess of 600°C has produced subsoli- surficial in nature. Swirls are most plausibly the result dus reduction of ilmenite and the associated growth of metal (Fig. 1) [6]. of electrostatically or magnetically-driven sorting of regolith fines [2,3] or solar wind interactions with lo- calized remanent crustal magnetism (e.g., ref. [4]). In either scenario, the complex geometry of the albedo pattern must be a function of the structure of the near surface magnetic field. -
Landed Science at a Lunar Crustal Magnetic Anomaly
Landed Science at a Lunar Crustal Magnetic Anomaly David T. Blewett, Dana M. Hurley, Brett W. Denevi, Joshua T.S. Cahill, Rachel L. Klima, Jeffrey B. Plescia, Christopher P. Paranicas, Benjamin T. Greenhagen, Lauren Jozwiak, Brian A. Anderson, Haje Korth, George C. Ho, Jorge I. Núñez, Michael I. Zimmerman, Pontus C. Brandt, Sabine Stanley, Joseph H. Westlake, Antonio Diaz-Calderon, R. Ter ik Daly, and Jeffrey R. Johnson Space Science Branch, Johns Hopkins University Applied Physics Lab, USA Lunar Science for Landed Missions Workshop – January, 2018 1 Lunar Magnetic Anomalies • The lunar crust contains magnetized areas, a few tens to several hundred kilometers across, known as "magnetic anomalies". • The crustal fields are appreciable: Strongest anomalies are ~10-20 nT at 30 km altitude, perhaps a few hundred to 1000 nT at the surface. Lunar Prospector magnetometer Btot map (Richmond & Hood 2008 JGR) over LROC WAC 689-nm mosaic 2 Lunar Magnetic Anomalies: Formation Hypotheses • Magnetized basin ejecta: ambient fields amplified by compression as impact-generated plasma converged on the basin antipode (Hood and co-workers) Lunar Prospector magnetometer Btot (Richmond & Hood 2008 JGR) over LROC WAC 689- nm mosaic 3 Lunar Magnetic Anomalies: Formation Hypotheses • Magnetized basin ejecta: ambient fields amplified by compression as impact-generated plasma converged on the basin antipode (Hood and co-workers) • Magnetic field impressed on the surface by plasma interactions when a cometary coma struck the Moon (Schultz) Lunar Prospector magnetometer Btot (Richmond & Hood 2008 JGR) over LROC WAC 689- nm mosaic 4 Lunar Magnetic Anomalies: Formation Hypotheses • Magnetized basin ejecta: ambient fields amplified by compression as impact-generated plasma converged on the basin antipode (Hood and co-workers) • Magnetic field impressed on the surface by plasma interactions when a cometary coma struck the Moon (Schultz) • Magmatic intrusion or impact melt magnetized in an early lunar dynamo field (e.g., Purucker et al. -
Lunar Sourcebook : a User's Guide to the Moon
4 LUNAR SURFACE PROCESSES Friedrich Hörz, Richard Grieve, Grant Heiken, Paul Spudis, and Alan Binder The Moon’s surface is not affected by atmosphere, encounters with each other and with larger planets water, or life, the three major agents for altering throughout the lifetime of the solar system. These terrestrial surfaces. In addition, the lunar surface has orbital alterations are generally minor, but they not been shaped by recent geological activity, because ensure that, over geological periods, collisions with the lunar crust and mantle have been relatively cold other bodies will occur. and rigid throughout most of geological time. When such a collision happens, two outcomes are Convective internal mass transport, which dominates possible. If “target” and “projectile” are of comparable the dynamic Earth, is therefore largely absent on the size, collisional fragmentation and annihilation Moon, and so are the geological effects of such occurs, producing a large number of much smaller internal motions—volcanism, uplift, faulting, and fragments. If the target object is very large compared subduction—that both create and destroy surfaces on to the projectile, it behaves as an “infinite halfspace,” Earth. The great contrast between the ancient, stable and the result is an impact crater in the target body. Moon and the active, dynamic Earth is most clearly For collisions in the asteroid belt, many of the shown by the ages of their surfaces. Nearly 80% of the resulting collisional fragments or crater ejecta escape entire solid surface of Earth is <200 m.y. old. In the gravitational field of the impacted object; many of contrast, >99% of the lunar surface formed more than these fragments are then further perturbed into 3 b.y. -
Magnetron Sputtering of Polymeric Targets: from Thin Films to Heterogeneous Metal/Plasma Polymer Nanoparticles
materials Article Magnetron Sputtering of Polymeric Targets: From Thin Films to Heterogeneous Metal/Plasma Polymer Nanoparticles OndˇrejKylián 1,* , Artem Shelemin 1, Pavel Solaˇr 1, Pavel Pleskunov 1, Daniil Nikitin 1 , Anna Kuzminova 1, Radka Štefaníková 1, Peter Kúš 2, Miroslav Cieslar 3, Jan Hanuš 1, Andrei Choukourov 1 and Hynek Biederman 1 1 Department of Macromolecular Physics, Faculty of Mathematics and Physics, Charles University, V Holešoviˇckách 2, 180 00 Prague 8, Czech Republic 2 Department of Surface and Plasma Science, Faculty of Mathematics and Physics, Charles University, V Holešoviˇckách 2, 180 00 Prague 8, Czech Republic 3 Department of Physics of Materials, Faculty of Mathematics and Physics, Charles University, Ke Karlovu 5, 121 16 Prague 2, Czech Republic * Correspondence: [email protected] Received: 25 June 2019; Accepted: 23 July 2019; Published: 25 July 2019 Abstract: Magnetron sputtering is a well-known technique that is commonly used for the deposition of thin compact films. However, as was shown in the 1990s, when sputtering is performed at pressures high enough to trigger volume nucleation/condensation of the supersaturated vapor generated by the magnetron, various kinds of nanoparticles may also be produced. This finding gave rise to the rapid development of magnetron-based gas aggregation sources. Such systems were successfully used for the production of single material nanoparticles from metals, metal oxides, and plasma polymers. In addition, the growing interest in multi-component heterogeneous nanoparticles has led to the design of novel systems for the gas-phase synthesis of such nanomaterials, including metal/plasma polymer nanoparticles. In this featured article, we briefly summarized the principles of the basis of gas-phase nanoparticles production and highlighted recent progress made in the field of the fabrication of multi-component nanoparticles. -
The Choice of the Location of the Lunar Base N93-17431
155 PRECEDING PhGE ,,=,_,,c,;_''_'" t¢OT F|Lf_D THE CHOICE OF THE LOCATION OF THE LUNAR BASE N93-17431 V. V. Y__hevchenko P.. K _ AsO_nomtca/In./lute Moscow U_ Moscow 119899 USSR The development of modern methods of remote sensing of the lunar suuface and data from lunar studies by space vehicles make it possgale to assess scientifically the e:qOediowy of the locationof the lunar base in a definite region on the Moon. The prefimlnary choice of the site is important for tackling a range of problems assocfated with ensuring the activity of a manned lunar base and with fulfilh'ng the research program. Based on astronomical dat_ we suggest the Moon's western _, specifically the western part of Oceanus Proceliarurtg where natural scientifically interesting objects have been identifle_ as have surface rocks with enlaanced contents of ilmenite, a poss_le source of oxygen. A comprehensive et_tluation of the region shows timt, as far as natural features are concernetg it is a key one for solving the main problems of the Moon's orlgln and evolution. INTRODUCTION final period of shaping the lunar crust's upper horizons (this period coincided with the final equalization of the Moon's periods The main criteria for choosing a site for the first section of a of orbital revolution and axial rotation), the impact of terrestrial manned lunar base are (1)the most favorable conditions for gravitation on the internal structure of the Moon increased. transport operations, (2)the presence of natural objects of Between 4 and 3 b.y.