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STI Program Bibliography
Scientific and Technical Information Program Affordable Heavy Lift Capability: 2000-2004 This custom bibliography from the NASA Scientific and Technical Information Program lists a sampling of records found in the NASA Aeronautics and Space Database. The scope of this topic includes technologies to allow robust, affordable access of cargo, particularly to low-Earth orbit. This area of focus is one of the enabling technologies as defined by NASA’s Report of the President’s Commission on Implementation of United States Space Exploration Policy, published in June 2004. Best if viewed with the latest version of Adobe Acrobat Reader Affordable Heavy Lift Capability: 2000-2004 A Custom Bibliography From the NASA Scientific and Technical Information Program October 2004 Affordable Heavy Lift Capability: 2000-2004 This custom bibliography from the NASA Scientific and Technical Information Program lists a sampling of records found in the NASA Aeronautics and Space Database. The scope of this topic includes technologies to allow robust, affordable access of cargo, particularly to low-Earth orbit. This area of focus is one of the enabling technologies as defined by NASA’s Report of the President’s Commission on Implementation of United States Space Exploration Policy, published in June 2004. OCTOBER 2004 20040095274 EAC trains its first international astronaut class Bolender, Hans, Author; Bessone, Loredana, Author; Schoen, Andreas, Author; Stevenin, Herve, Author; ESA bulletin. Bulletin ASE. European Space Agency; Nov 2002; ISSN 0376-4265; Volume 112, 50-5; In English; Copyright; Avail: Other Sources After several years of planning and preparation, ESA’s ISS training programme has become operational. Between 26 August and 6 September, the European Astronaut Centre (EAC) near Cologne gave the first ESA advanced training course for an international ISS astronaut class. -
Diplomarbeit
View metadata, citation and similar papers at core.ac.uk brought to you by CORE provided by OTHES DIPLOMARBEIT Titel der Diplomarbeit „Matthias Bernhard Braun auf seinem Weg nach Böhmen“ Verfasserin Anneliese Schallmeiner angestrebter akademischer Grad Magistra der Philosophie (Mag.phil.) Wien 2008 Studienkennzahl lt. Studienblatt: A 315 Studienrichtung lt. Studienblatt: Kunstgeschichte Betreuerin / Betreuer: Ao Prof. Dr. Walter Krause Inhalt Seite I. Einleitung 4 II. Biographischer Abriss und Forschungslage 8 1. Biographischer Abriss zu Matthias Bernhard Braun 8 2. Forschungslage 13 III. Matthias Bernhard Braun auf seinem Weg nach Böhmen 22 1. Stilanalytische Überlegungen 22 2. Von Stams nach Plass/Plasy – Die Bedeutung des Zisterzienserordens – 27 Eine Hypothese 2.1. Brauns Arbeiten für das Zisterzienserkloster in Plass/Plasy 32 2.1.1. Die Kalvarienberggruppe 33 2.1.2. Die Verkündigungsgruppe 36 2.1.3. Der Bozzetto zur Statuengruppe der hl. Luitgard auf der Karlsbrücke 39 3. Die Statuengruppen auf der Karlsbrücke in Prag 41 3.1. Die Statuengruppe der hl. Luitgard 47 3.1.1. Kompositionelle und ikonographische Vorbilder 50 3.1.2. Visionäre und mysthische Vorbilder 52 3.2. Die Statuengruppe des hl. Ivo 54 3.2.1. Kompositionelle Vorbilder 54 3.2.2. Die Statue des hl. Franz Borgia von Ferdinand Maximilian Brokoff als 55 mögliches Vorbild für die Statue des hl. Ivo 4. Die Statue des hl. Judas Thaddäus 57 5. Brauns Beitrag zur Ausstattung der St. Klemenskirche in Prag 59 5.1. Evangelisten und Kirchenväter 60 5.2. Die Beichtstuhlaufsatzfiguren 63 6. Die Bedeutung des Grafen Franz Anton von Sporck für den Weg von 68 Matthias Bernhard Braun nach Böhmen 6.1. -
Crustal and Time-Varying Magnetic Fields at the Insight Landing Site on Mars
ARTICLES https://doi.org/10.1038/s41561-020-0537-x Crustal and time-varying magnetic fields at the InSight landing site on Mars Catherine L. Johnson 1,2 ✉ , Anna Mittelholz1, Benoit Langlais3, Christopher T. Russell4, Véronique Ansan 3, Don Banfield 5, Peter J. Chi 4, Matthew O. Fillingim 6, Francois Forget 7, Heidi Fuqua Haviland 8, Matthew Golombek9, Steve Joy 4, Philippe Lognonné 10, Xinping Liu4, Chloé Michaut 11, Lu Pan 12, Cathy Quantin-Nataf12, Aymeric Spiga 7,13, Sabine Stanley14,15, Shea N. Thorne 1, Mark A. Wieczorek 16, Yanan Yu4, Suzanne E. Smrekar9 and William B. Banerdt 9 Magnetic fields provide a window into a planet’s interior structure and evolution, including its atmospheric and space environ- ments. Satellites at Mars have measured crustal magnetic fields indicating an ancient dynamo. These crustal fields interact with the solar wind to generate transient fields and electric currents in Mars’s upper atmosphere. Surface magnetic field data play a key role in understanding these effects and the dynamo. Here we report measurements of magnetic field strength and direction at the InSight (Interior Exploration using Seismic Investigations, Geodesy and Heat Transport) landing site on Mars. We find that the field is ten times stronger than predicted by satellite-based models. We infer magnetized rocks beneath the surface, within ~150 km of the landing site, consistent with a past dynamo with Earth-like strength. Geological mapping and InSight seismic data suggest that much or all of the magnetization sources are carried in basement rocks, which are at least 3.9 billion years old and are overlain by between 200 m and ~10 km of lava flows and modified ancient terrain. -
Aerobraking to Lower Apogee in Earth Orbit with the Small Payload Orbit Transfer (SPORT™) Microsatellite Vehicle
View metadata, citation and similar papers at core.ac.uk brought to you by CORE provided by DigitalCommons@USU SSC01-XI-8 Aerobraking to Lower Apogee in Earth Orbit with the Small Payload ORbit Transfer (SPORT™) Microsatellite Vehicle Paul Gloyer AeroAstro, Inc. 160 Adams Lane, Waveland, MS 39576 228-466-9863, [email protected] Tony Robinson AeroAstro, Inc. 520 Huntmar Park Drive, Herndon, VA 20170 703-709-2240 x133, [email protected] Adeena Mignogna AeroAstro, Inc. 520 Huntmar Park Drive, Herndon, VA 20170 703-709-2240 x126, [email protected] Yasser Ahmad Astronautic Technology Sdn. Bhd. 520 Huntmar Park Drive, Herndon, VA 20170 703-709-2240 x138, [email protected] Abstract. AeroAstro, Inc. and Astronautic Technology Sdn. Bhd. (a Malaysian space company) are commercially developing the Small Payload ORbit Transfer (SPORT) vehicle, which uses advanced earth aerobraking technology to achieve efficient orbit transfer from Geosynchronous-Transfer Orbit (GTO) to Low Earth Orbit (LEO). After being delivered to GTO by a large launch vehicle, such as Ariane, SPORT uses its onboard propulsion system to adjust its perigee altitude to about 150 km. At this altitude, the large deployable aerobrake produces enough drag to reduce the apogee altitude from 36,000+ km to about 1,000 km in approximately 300 orbits. Upon reaching the target apogee altitude, the propulsion system is used to raise the perigee to the desired altitude, thereby allowing SPORT to release its payload. Aerobraking technology enables orbit transfer in a cost-effective manner, reducing the overall mass of the spacecraft by drastically reducing the amount of propellant required to achieve the maneuver. -
Re-Usable Launch and Payload Delivery System MDDP 2012/3
Group 2 Re-usable Launch and Payload Delivery System MDDP 2012/3 Re-usable Launch and Payload Delivery System MDDP Group 2 James Dobberson Robert Taylor Matthew Chapman Timothy West Mukudzei Muchengeti William Wou Group 2 Re-usable Launch and Payload Delivery System MDDP 2012/3 1. Contents 1. Contents ..................................................................................................................................... i 2. Executive Summary .................................................................................................................. ii 3. Introduction .............................................................................................................................. 1 4. Down Selection and Integration Methodology ......................................................................... 2 5. Presentation of System Concept and Operations ...................................................................... 5 6. System Investment Plan ......................................................................................................... 20 7. Numerical Analysis and Statement of Feasibility .................................................................. 23 8. Conclusions and Future Work ................................................................................................ 29 9. Launch Philosophy ................................................................................................................. 31 10. Propulsion .............................................................................................................................. -
Mars Aerocapture/Aerobraking Aeroshell Configurations by Abraham Chavez
Mars Aerocapture/Aerobraking Aeroshell Configurations by Abraham Chavez This presentation provides a review of those studies and a starting point for considering Aerocapture/Aerobraking technology as a way to reduce mass and cost, to achieve the ambitious science returns currently desired What is Aerocapture: is first of all a very rapid process, requiring a heavy heat shield resulting in high g-forces, Descent into a relatively dense atmosphere is suffciently rapid that the deceleration causes severe heating requiring What is Aerobraking: is a very gradual process that has the advantage that small reductions in spacecraft velocity are achieved by drag of the solar arrays in the outer atmosphere, thus no additional mass for a heat shield is necessary. an aeroshell. Sasakawa International Center for Space Architecture, University of Houston College of Architecture Aerocapture vs Aerobraking Entry targeting burn Atmospheric entry Atmospheric Drag Aerocapture Reduces Orbit Period Periapsis Energy raise dissipation/ maneuver Autonomous Aerobraking (propulsive) guidance Target ~300 Passes Jettison Aeroshell Hyperbolic Through Upper orbit Approach Atmosphere Controlled exit Orbit Insertion Pros Cons Burn Uses very little fuel--significant mass Needs protective aeroshell savings for larger vehicles Pros Cons Establishes orbit quickly (single pass) One-shot maneuver; no turning back, Little spacecraft design impact Still need ~1/2 propulsive fuel load much like a lander Gradual adjustments; can pause Hundreds of passes = more chance of Has -
Curriculum Vitae Reto Gieré
Curriculum Vitae Reto Gieré Department of Earth and Environmental Science and Center of Excellence in Environmental Toxicology University of Pennsylvania 240 S. 33rd Street, Hayden Hall Philadelphia, PA 19104-6316, USA Office Phone: 215-898-6907 E-mail: [email protected] Department: https://www.sas.upenn.edu/earth Journal of Petrology: http://petrology.oupjournals.org European Journal of Mineralogy: https://www.european-journal-of-mineralogy.net April 2021 Education 1995 Habilitation (Venia Docendi) in Earth Sciences, Universität Basel, Switzerland 1990 Ph.D. in Earth Sciences, ETH Zürich, Switzerland Thesis title: "Quantification of element mobility at a tonalite/dolomite contact (Adamello Massif, Provincia di Trento, Italy)". Supervisors: V. Trommsdorff (ETH Zürich), H.J. Greenwood (UBC Vancouver), and F. Oberli (ETH Zürich) 1988–1989 Visiting Graduate Student, University of British Columbia, Vancouver (Canada). Graduate studies in Thermodynamics. Advisors: H.J. Greenwood, T.H. Brown 1984 Diploma in Earth Sciences, ETH Zürich, Switzerland Thesis title: "Geology and petrography of the eastern Bergell contact aureole" (in German language). Supervisors: V. Trommsdorff (ETH Zürich), V. Dietrich (ETH Zürich), A. Montrasio (Università degli Studi, Milano) Language skills Fluent in five languages: English, German, French, Italian, Romansh Current Position Since 2015 Professor, Department of Earth and Environmental Science, and Member of the Center of Excellence in Environmental Toxicology, University of Pennsylvania, Philadelphia, USA Previous -
Envision – Front Cover
EnVision – Front Cover ESA M5 proposal - downloaded from ArXiV.org Proposal Name: EnVision Lead Proposer: Richard Ghail Core Team members Richard Ghail Jörn Helbert Radar Systems Engineering Thermal Infrared Mapping Civil and Environmental Engineering, Institute for Planetary Research, Imperial College London, United Kingdom DLR, Germany Lorenzo Bruzzone Thomas Widemann Subsurface Sounding Ultraviolet, Visible and Infrared Spectroscopy Remote Sensing Laboratory, LESIA, Observatoire de Paris, University of Trento, Italy France Philippa Mason Colin Wilson Surface Processes Atmospheric Science Earth Science and Engineering, Atmospheric Physics, Imperial College London, United Kingdom University of Oxford, United Kingdom Caroline Dumoulin Ann Carine Vandaele Interior Dynamics Spectroscopy and Solar Occultation Laboratoire de Planétologie et Géodynamique Belgian Institute for Space Aeronomy, de Nantes, Belgium France Pascal Rosenblatt Emmanuel Marcq Spin Dynamics Volcanic Gas Retrievals Royal Observatory of Belgium LATMOS, Université de Versailles Saint- Brussels, Belgium Quentin, France Robbie Herrick Louis-Jerome Burtz StereoSAR Outreach and Systems Engineering Geophysical Institute, ISAE-Supaero University of Alaska, Fairbanks, United States Toulouse, France EnVision Page 1 of 43 ESA M5 proposal - downloaded from ArXiV.org Executive Summary Why are the terrestrial planets so different? Venus should be the most Earth-like of all our planetary neighbours: its size, bulk composition and distance from the Sun are very similar to those of Earth. -
Energy, Power, and Transport
Frontispiece Advanced Lunar Base In this panorama of an advanced lunar base, the main habitation modules in the background to the right are shown being covered by lunar soil for radiation protection. The modules on the far right are reactors in which lunar soil is being processed to provide oxygen. Each reactor is heated by a solar mirror. The vehicle near them is collecting liquid oxygen from the reactor complex and will transport it to the launch pad in the background, where a tanker is just lifting off. The mining pits are shown just behind the foreground figure on the left. The geologists in the foreground are looking for richer ores to mine. Artist: Dennis Davidson NASA SP-509, vol. 2 Space Resources Energy, Power, and Transport Editors Mary Fae McKay, David S. McKay, and Michael B. Duke Lyndon B. Johnson Space Center Houston, Texas 1992 National Aeronautics and Space Administration Scientific and Technical Information Program Washington, DC 1992 For sale by the U.S. Government Printing Office Superintendent of Documents, Mail Stop: SSOP, Washington, DC 20402-9328 ISBN 0-16-038062-6 Technical papers derived from a NASA-ASEE summer study held at the California Space Institute in 1984. Library of Congress Cataloging-in-Publication Data Space resources : energy, power, and transport / editors, Mary Fae McKay, David S. McKay, and Michael B. Duke. x, 174 p. : ill. ; 28 cm.—(NASA SP ; 509 : vol. 2) 1. Outer space—Exploration—United States. 2. Natural resources. 3. Space industrialization—United States. I. McKay, Mary Fae. II. McKay, David S. III. Duke, Michael B. -
Forgotten Baroque Borderland
Originalveröffentlichung in: Wasilewska, Joanna (Hrsg.): Poland - China : art and cultural heritage, Kraków 2011, S. 63-72 , Abb. 1-8 Jan K. Ostrowski Jagiellonian University, Krakow Forgotten Baroque Borderland Manuals on European modern art concentrate extensively on Italy, Flanders, Holland and France. Much less attention is paid to Spain, Germany, Austria, England and Rus sia. Poland receives at best one or two pages with a short and usually superficial de scription of arbitrarily chosen works from its largest centers, such as Krakow and War saw. The present article does not intend to question such a traditional artistic hierarchy. It is only an attempt to draw the attention of foreign art historians to certain artistic phenomena of high quality, or rather to a large artistic region about which one can find hardly any information in international literature on art. First of all, I propose a few definitions and explanations. Ihe notion of Poland of the sixteenth to the eighteenth century includes the present territories of Poland, Lithua nia, Belarus and Ukraine. Analogically, Lithuania embraced present tiny Lithuania, much greater Belarus and even some parts of Greater Russia. The Polish-Lithuanian union was dominated by a Polish-speaking and Roman Catholic population, while a large Eastern portion of the country preserved up to the end a majority which spoke Ruthenian (not Russian!) and belonged to the Eastern Church (not necessarily Ortho dox). In a few words, the territory situated roughly between the present Eastern border of Poland and the Dneper-Dvina line presented in the sixteenth-eighteenth centuries (and even later) an extremely complicated ethnic, religious and cultural picture. -
EUSAR 2021 Program
Program 13th European Conference on Synthetic Aperture Radar Online Event March 29 - April 1, 2021 The given times in the program www.eusar.de schedule are according to the German Local Time (CEST) Check at: https://www.worldtimebuddy.com/ Organized by Technically sponsored by EUREL • URSI • DGON Welcome Message of the General Chairman Dear SAR community/EUSAR partners and friends, At this point I would like to thank everybody for your long lasting loyalty in attending the EUSAR confer- A warm welcome to all EUSAR members and ences since more than two decades. followers! Best regards, take care and stay healthy, I´m happy to confirm that the postponed EUSAR Conference will take place from March 29 - April 1, 2021 as a virtual digital conference. In these times of crisis, in particular, the EUSAR board members would like to continue to offer our community a platform for intensive scientific and professional exchange. We feel responsible to give especially all authors the pos- sibility for publishing and presenting their submitted outstanding papers and posters, what means one of © Matthias Weiß the conference values. Besides this, the discussions Michael Loercher, HENSOLDT of the attending industry, research and public sector EUSAR 2021 Conference Chairman leaders inventing and providing ideas and sugges- tions for tomorrow’s innovative technology develop- ments to protect our global world. Please note already in your calendars, that the next EUSAR Conference 2022, hosted from Hensoldt AG, will take place in April 2022 in Leipzig. © Hensoldt EUSAR 2021 Welcome Message of the Technical Chairman It’s a great pleasure to welcome you to the At the closing session on the last day of the confer- 13th European Conference on Synthetic Aperture ence a Best Paper Award, a Best Poster Award, and Radar (EUSAR) 2021 which will be the first virtual three Best Students Awards will be presented. -
Report of the in Situ Resources Utilization Workshop
i i NASA Conference Publication 3017 Report of the In Situ Resources Utilization Workshop Edited by Kyle Fairchild and Wendell W. Mendell NASA Lyndon B. Johnson Space Center Houston, Texas Proceedings of a workshop cosponsored by National Aeronautics and Space Administration, Department of Energy, Large Scale Programs Institute, United Technologies Corporation, Kraft Foods, and Disney Imagineering, and hosted by United Technologies Corporation Lake Buena Vista, Florida January 28-30, 1987 National Aeronautics and Space Administration Scientific and Technical Information Division 1988 PREFACE This report contains the results of a workshop that investigated potential joint development of the key technologies and mechanisms required to enable the permanent habitation of space. Fifty representatives from the public and private sectors met at the United Technologies Center, Lake Buena Vista, Florida, January 28 to 30, 1987, to begin a joint public/private assessment of new technology requirements of future space options, to share knowledge on those required technologies that may exist in the private sector, and to investigate potential joint technology development opportunities. This report also provides input to a NASA technology development plan and docu- ments possibilities for collaborative technology development among the public 9 private, and academic sectors. This workshop represents the first "nucleation" phase of a continuing process. The participant list represents only a small fraction of all organ- izations that will contribute to future development of space technologies and activities. We attempted to assemble a representative cross section of business, academic, and government organizations to investigate the feasi- bility of potential technological collaborations and the organizational structures that would enable most effective collaboration.