Mercury's Sodium Exosphere: an Ab Initio Calculation to Interpret
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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. -
Radiation Forces on Small Particles in the Solar System T
1CARUS 40, 1-48 (1979) Radiation Forces on Small Particles in the Solar System t JOSEPH A. BURNS Cornell University, 2 Ithaca, New York 14853 and NASA-Ames Research Center PHILIPPE L. LAMY CNRS-LAS, Marseille, France 13012 AND STEVEN SOTER Cornell University, Ithaca, New York 14853 Received May 12, 1978; revised May 2, 1979 We present a new and more accurate expression for the radiation pressure and Poynting- Robertson drag forces; it is more complete than previous ones, which considered only perfectly absorbing particles or artificial scattering laws. Using a simple heuristic derivation, the equation of motion for a particle of mass m and geometrical cross section A, moving with velocity v through a radiation field of energy flux density S, is found to be (to terms of order v/c) mi, = (SA/c)Qpr[(1 - i'/c)S - v/c], where S is a unit vector in the direction of the incident radiation,/" is the particle's radial velocity, and c is the speed of light; the radiation pressure efficiency factor Qpr ~ Qabs + Q~a(l - (cos a)), where Qabs and Q~c~ are the efficiency factors for absorption and scattering, and (cos a) accounts for the asymmetry of the scattered radiation. This result is confirmed by a new formal derivation applying special relativistic transformations for the incoming and outgoing energy and momentum as seen in the particle and solar frames of reference. Qpr is evaluated from Mie theory for small spherical particles with measured optical properties, irradiated by the actual solar spectrum. Of the eight materials studied, only for iron, magnetite, and graphite grains does the radiation pressure force exceed gravity and then just for sizes around 0. -
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. -
Section 22-3: Energy, Momentum and Radiation Pressure
Answer to Essential Question 22.2: (a) To find the wavelength, we can combine the equation with the fact that the speed of light in air is 3.00 " 108 m/s. Thus, a frequency of 1 " 1018 Hz corresponds to a wavelength of 3 " 10-10 m, while a frequency of 90.9 MHz corresponds to a wavelength of 3.30 m. (b) Using Equation 22.2, with c = 3.00 " 108 m/s, gives an amplitude of . 22-3 Energy, Momentum and Radiation Pressure All waves carry energy, and electromagnetic waves are no exception. We often characterize the energy carried by a wave in terms of its intensity, which is the power per unit area. At a particular point in space that the wave is moving past, the intensity varies as the electric and magnetic fields at the point oscillate. It is generally most useful to focus on the average intensity, which is given by: . (Eq. 22.3: The average intensity in an EM wave) Note that Equations 22.2 and 22.3 can be combined, so the average intensity can be calculated using only the amplitude of the electric field or only the amplitude of the magnetic field. Momentum and radiation pressure As we will discuss later in the book, there is no mass associated with light, or with any EM wave. Despite this, an electromagnetic wave carries momentum. The momentum of an EM wave is the energy carried by the wave divided by the speed of light. If an EM wave is absorbed by an object, or it reflects from an object, the wave will transfer momentum to the object. -
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. -
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. -
MONITORING of AERODYNAMIC PRESSURES for VENUS EXPRESS in the UPPER ATMOSPHERE DURING DRAG EXPERIMENTS BASED on TELEMETRY Sylvain
MONITORING OF AERODYNAMIC PRESSURES FOR VENUS EXPRESS IN THE UPPER ATMOSPHERE DURING DRAG EXPERIMENTS BASED ON TELEMETRY Sylvain Damiani(1,2), Mathias Lauer(1), and Michael Müller(1) (1) ESA/ESOC; Robert-Bosch-Str. 5, 64293 Darmstadt, Germany; +49 6151900; [email protected] (2)GMV GmbH; Robert-Bosch-Str. 7, 64293 Darmstadt, Germany; +49 61513972970; [email protected] Abstract: The European Space Agency Venus Express spacecraft has to date successfully completed nine Aerodynamic Drag Experiment Campaigns designed in order to probe the planet's upper atmosphere over the North pole. The daily monitoring of the campaign is based on housekeeping telemetry. It consists of reducing the spacecraft dynamics in order to obtain a timely evolution of the aerodynamic torque over a pericenter passage, from which estimations of the accommodation coefficient, the dynamic pressure and the atmospheric density can be extracted. The observed surprising density fluctuations on short timescales justify the use of a conservative method to decide on the continuation of the experiments. Keywords: Venus Express, Drag Experiments, Attitude Dynamics, Aerodynamic Torque. 1. Introduction The European Space Agency's Venus Express spacecraft has been orbiting around Venus since 2006, and its mission has now been extended until 2014. During the extended mission, it has already successfully accomplished 9 Aerodynamic Drag Experiment campaigns until September 2012. Each campaign aims at probing the planet’s atmospheric density at high altitude and next to the North pole by lowering the orbit pericenter (down to 165 km of altitude), and observing its perturbations on both the orbit and the attitude of the probe. -
Forces, Light and Waves Mechanical Actions of Radiation
Forces, light and waves Mechanical actions of radiation Jacques Derouard « Emeritus Professor », LIPhy Example of comets Cf Hale-Bopp comet (1997) Exemple of comets Successive positions of a comet Sun Tail is in the direction opposite / Sun, as if repelled by the Sun radiation Comet trajectory A phenomenon known a long time ago... the first evidence of radiative pressure predicted several centuries later Peter Arpian « Astronomicum Caesareum » (1577) • Maxwell 1873 electromagnetic waves Energy flux associated with momentum flux (pressure): a progressive wave exerts Pressure = Energy flux (W/m2) / velocity of wave hence: Pressure (Pa) = Intensity (W/m2) / 3.10 8 (m/s) or: Pressure (nanoPa) = 3,3 . I (Watt/m2) • NB similar phenomenon with acoustic waves . Because the velocity of sound is (much) smaller than the velocity of light, acoustic radiative forces are potentially stronger. • Instead of pressure, one can consider forces: Force = Energy flux x surface / velocity hence Force = Intercepted power / wave velocity or: Force (nanoNewton) = 3,3 . P(Watt) Example of comet tail composed of particles radius r • I = 1 kWatt / m2 (cf Sun radiation at Earth) – opaque particle diameter ~ 1µm, mass ~ 10 -15 kg, surface ~ 10 -12 m2 – then P intercepted ~ 10 -9 Watt hence F ~ 3,3 10 -18 Newton comparable to gravitational attraction force of the sun at Earth-Sun distance Example of comet tail Influence of the particles size r • For opaque particles r >> 1µm – Intercepted power increases like the cross section ~ r2 thus less strongly than gravitational force that increases like the mass ~ r3 Example of comet tail Influence of the particles size r • For opaque particles r << 1µm – Solar radiation wavelength λ ~0,5µm – r << λ « Rayleigh regime» – Intercepted power varies like the cross section ~ r6 thus decreases much stronger than gravitational force ~ r3 Radiation pressure most effective for particles size ~ 1µm Another example Ashkin historical experiment (1970) A. -
INFLUENCE of SOLAR RADIATION PRESSURE on ORBITAL ECCENTRICITY of a GRAVITY-GRADIENT-ORIENTED LENTICULAR SATELLITE by William M
NASA TECHNICAL NOTE NASA TN D-2715 e- e- - -- (5- / --I -=e3-m INFLUENCE OF SOLAR RADIATION PRESSURE ON ORBITAL ECCENTRICITY OF A GRAVITY-GRADIENT-ORIENTED LENTICULAR SATELLITE by William M. Adams, Jr., and Ward F. Hodge Langley Research Center Langley Station, Hampton, Va. NATIONAL AERONAUTICS AND SPACE ADMINISTRATION WASHINGTON, D. C. 0 MARCH 1965 / t 1 TECH LIBRARY KAFB, "I I llllll11111 llllI11111111111111111l11 lilt 1111 0079733 INFLUENCE OF SOLAR RADIATION PRESSURE ON ORBITAL ECCENTRICITY OF A GRAVITY-GRADIENT-ORIENTED LENTICULAR SATELLITE By William M. Adams, Jr., and Ward F. Hodge Langley Research Center Langley Station, Hampton, Va. NATIONAL AERONAUTICS AND SPACE ADMINISTRATION For sole by the Office of Technical Services, Deportment of Commerce, Woshington, D.C. 20230 -- Price $1.00 ... ~ I I INFLUENCE OF SOLAR RADIATION PRESSURE ON ORBITAL ECCENTRICITY OF A GRAVITY-GRADIENT-ORIENTED LENTICULAR SATEUITE By William M. Adams, Jr., and Ward F. HoQe Langley Research Center A method is presented for calculating the perturbations of the orbital elements of a low-density lenticular satellite due to solar radiation pressure. The necessary calculations are performed by means of the digital computer. Typ- ical results are presented for seven orbital inclinations ranging from 0' to ll3O for a perfectly absorptive satellite initially in a nearly circular 2,000- nautical-mile orbit. The information obtained indicates that the change in eccentricity caused by solar radiation pressure becomes large enough for all the inclinations con- sidered to cause attitude-control problems with the gravity-gradient stabiliza- tion system. A nearly circular orbit appears necessary for lenticular satel- lites since the ability of gravity gradient attitude control systems to damp the pitching libration induced by elliptic orbital motion is still in doubt. -
Reviewing Martian Atmospheric Noble Gas Measurements: from Martian Meteorites to Mars Missions
geosciences Review Reviewing Martian Atmospheric Noble Gas Measurements: From Martian Meteorites to Mars Missions Thomas Smith 1,* , P. M. Ranjith 1, Huaiyu He 1,2,3,* and Rixiang Zhu 1,2,3 1 State Key Laboratory of Lithospheric Evolution, Institute of Geology and Geophysics, Chinese Academy of Sciences, 19 Beitucheng Western Road, Box 9825, Beijing 100029, China; [email protected] (P.M.R.); [email protected] (R.Z.) 2 Institutions of Earth Science, Chinese Academy of Sciences, Beijing 100029, China 3 College of Earth and Planetary Sciences, University of Chinese Academy of Sciences, Beijing 100049, China * Correspondence: [email protected] (T.S.); [email protected] (H.H.) Received: 10 September 2020; Accepted: 4 November 2020; Published: 6 November 2020 Abstract: Martian meteorites are the only samples from Mars available for extensive studies in laboratories on Earth. Among the various unresolved science questions, the question of the Martian atmospheric composition, distribution, and evolution over geological time still is of high concern for the scientific community. Recent successful space missions to Mars have particularly strengthened our understanding of the loss of the primary Martian atmosphere. Noble gases are commonly used in geochemistry and cosmochemistry as tools to better unravel the properties or exchange mechanisms associated with different isotopic reservoirs in the Earth or in different planetary bodies. The relatively low abundance and chemical inertness of noble gases enable their distributions and, consequently, transfer mechanisms to be determined. In this review, we first summarize the various in situ and laboratory techniques on Mars and in Martian meteorites, respectively, for measuring noble gas abundances and isotopic ratios. -
Statistical Studies on Mars Atmospheric Sputtering by Precipitating Pickup O+: Preparation for the MAVEN Mission Yung-Ching Wang, Janet G
Statistical studies on Mars atmospheric sputtering by precipitating pickup O+: Preparation for the MAVEN mission Yung-Ching Wang, Janet G. Luhmann, Xiaohua Fang, François Leblanc, Robert E. Johnson, Yingjuan Ma, Wing-Huen Ip To cite this version: Yung-Ching Wang, Janet G. Luhmann, Xiaohua Fang, François Leblanc, Robert E. Johnson, et al.. Statistical studies on Mars atmospheric sputtering by precipitating pickup O+: Preparation for the MAVEN mission. Journal of Geophysical Research. Planets, Wiley-Blackwell, 2015, 120 (1), pp.34-50. 10.1002/2014JE004660. hal-01076673 HAL Id: hal-01076673 https://hal.archives-ouvertes.fr/hal-01076673 Submitted on 13 Jan 2021 HAL is a multi-disciplinary open access L’archive ouverte pluridisciplinaire HAL, est archive for the deposit and dissemination of sci- destinée au dépôt et à la diffusion de documents entific research documents, whether they are pub- scientifiques de niveau recherche, publiés ou non, lished or not. The documents may come from émanant des établissements d’enseignement et de teaching and research institutions in France or recherche français ou étrangers, des laboratoires abroad, or from public or private research centers. publics ou privés. JournalofGeophysicalResearch: Planets RESEARCH ARTICLE Statistical studies on Mars atmospheric sputtering 10.1002/2014JE004660 by precipitating pickup O+: Preparation Key Points: for the MAVEN mission • Sputtering loss rates are controlled by Yung-Ching Wang1,2, Janet G. Luhmann1, Xiaohua Fang3, François Leblanc4, the environments 5 6 2,7 • Solar