Curriculum Vitae --- Prof
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Mineralization Control Effect of Geochemical
International Journal of Research in Social Sciences Vol. 8 Issue 10, October 2018, ISSN: 2249-2496 Impact Factor: 7.081 Journal Homepage: http://www.ijmra.us, Email: [email protected] Double-Blind Peer Reviewed Refereed Open Access International Journal - Included in the International Serial Directories Indexed & Listed at: Ulrich's Periodicals Directory ©, U.S.A., Open J-Gage as well as in Cabell’s Directories of Publishing Opportunities, U.S.A 1 2 Mineralization Control Effect of 3 Geochemical Tectonic Macroscopic Frame of 4 China 5 Jin-zhong Gong* 6 Abstract: Due to the close relationship between rock geophysics and geochemistry, the 7 geochemical distribution of stream sediments in China is closely related to the tectonic 8 framework. Based on the transitional zones of macro element change, we can outline the 9 geochemical tectonic framework of China, and draw the four horizontal, three vertical and one 10 shield, and basically correspond to the geophysical tectonic framework. Four horizontal is: the 11 variation line of Si-K-Na-Mg content in the Tianshan-Yinshan-Yanshan, K-Na content in the 12 Kunlun mountain –Qinling -Dabie mountain, Si-K-Na content in the Gangdise - 13 Nangqingtanggula, Al-K-Ca-Mg content in Nanling. Three vertical is: the variation line of Al-Fe 14 content in Zhang Guangcai ridge - Qianshan, Greater Hinggan Si-Ca-K-Na- Taihang mountains 15 Ca-Mg - Wuling mountain Ca-Mg content, Helan mountain - Minshan Ca content. One shield 16 area is Yunnan - Guizhou plateau - Emeishan basalt rock area Al-Fe-Ti-Mn and the basic element 17 enrichment region. -
From the Sun to the Earth: August 25, 2018 Geomagnetic Storm Effects
https://doi.org/10.5194/angeo-2019-165 Preprint. Discussion started: 10 January 2020 c Author(s) 2020. CC BY 4.0 License. From the Sun to the Earth: August 25, 2018 geomagnetic storm effects Mirko Piersanti1, Paola De Michelis2, Dario Del Moro3, Roberta Tozzi2, Michael Pezzopane2, Giuseppe Consolini4, Maria Federica Marcucci4, Monica Laurenza4, Simone Di Matteo5, Alessio Pignalberi2, Virgilio Quattrociocchi4,6, and Piero Diego4 1INFN - University of Rome "Tor Vergata", Rome, Italy. 2Istituto Nazionale di Geofisica e Vulcanologia, Rome, Italy. 3University of Rome "Tor Vergata", Rome, Italy. 4INAF-Istituto di Astrofisica e Planetologia Spaziali, Rome, Italy. 5Catholic University of America at NASA Goddard Space Flight Center, Greenbelt, Maryland, USA 6Dpt. of Physical and Chemical Sciences, University of L’Aquila, L’Aquila, Italy Correspondence: Mirko Piersanti ([email protected]) Abstract. On August 25, 2018 the interplanetary counterpart of the August 20, 2018 Coronal Mass Ejection (CME) hit the Earth, giving rise to a strong G3 geomagnetic storm. We present a description of the whole sequence of events from the Sun to the ground as well as a detailed analysis of the observed effects on the Earth’s environment by using a multi instrumental approach. We studied the ICME propagation in the interplanetary space up to the analysis of its effects in the magnetosphere, 5 ionosphere and at ground. To accomplish this task, we used ground and space collected data, including data from CSES (China Seismo Electric Satellite), launched on February 11, 2018. We found a direct connection between the ICME impact point onto the magnetopause and the pattern of the Earth’s polar electrojects. -
The Annual Compendium of Commercial Space Transportation: 2017
Federal Aviation Administration The Annual Compendium of Commercial Space Transportation: 2017 January 2017 Annual Compendium of Commercial Space Transportation: 2017 i Contents About the FAA Office of Commercial Space Transportation The Federal Aviation Administration’s Office of Commercial Space Transportation (FAA AST) licenses and regulates U.S. commercial space launch and reentry activity, as well as the operation of non-federal launch and reentry sites, as authorized by Executive Order 12465 and Title 51 United States Code, Subtitle V, Chapter 509 (formerly the Commercial Space Launch Act). FAA AST’s mission is to ensure public health and safety and the safety of property while protecting the national security and foreign policy interests of the United States during commercial launch and reentry operations. In addition, FAA AST is directed to encourage, facilitate, and promote commercial space launches and reentries. Additional information concerning commercial space transportation can be found on FAA AST’s website: http://www.faa.gov/go/ast Cover art: Phil Smith, The Tauri Group (2017) Publication produced for FAA AST by The Tauri Group under contract. NOTICE Use of trade names or names of manufacturers in this document does not constitute an official endorsement of such products or manufacturers, either expressed or implied, by the Federal Aviation Administration. ii Annual Compendium of Commercial Space Transportation: 2017 GENERAL CONTENTS Executive Summary 1 Introduction 5 Launch Vehicles 9 Launch and Reentry Sites 21 Payloads 35 2016 Launch Events 39 2017 Annual Commercial Space Transportation Forecast 45 Space Transportation Law and Policy 83 Appendices 89 Orbital Launch Vehicle Fact Sheets 100 iii Contents DETAILED CONTENTS EXECUTIVE SUMMARY . -
Joint IAGA IASPEI Symposia J1 Earth and Planetary Core Structure and Evolution from Observations and Modelling Conveners
Joint IAGA IASPEI Symposia J1 Earth and planetary core structure and evolution from observations and modelling Conveners: Christopher Davies ([email protected]) Swarandeep Sahoo ([email protected]) Kimberly Moore ([email protected]) Christine Thomas ([email protected]) Recent advances in the theory and observation of planetary cores is providing profound insight into these remote and enigmatic regions. The Juno and Cassini missions have revealed the properties of Jupiter's magnetic and gravity fields in unprecedented detail, while results from forthcoming missions such as BepiColombo and InSight promise a step change in our knowledge of the interior structure and dynamics of terrestrial bodies within our solar system. Complementary theoretical developments have advanced our understanding of nucleation and crystallization of solids within planetary cores and how these processes influence the generation of global magnetic fields over geological timescales. Numerical simulations of the dynamo process are pushing towards the extreme conditions of rapidly rotating magnetic turbulence that are thought to characterize many planetary cores, promising new insights into the field generation process and the origin of observed magnetic secular variation. On Earth, novel seismic data processing techniques are being combined with vast datasets to illuminate core-mantle interactions and anomalous structures in the liquid and solid cores, while mineral physics calculations and experiments are now capable of estimating transport properties at the extreme pressure-temperature conditions of the core-mantle boundary. Observations of Earth's magnetic field magnitude and its secular variation have been used to infer various physical processes such as core flow patterns, inner core growth, thermal and compositional evolution of the core, and their fundamental origin. -
Annual Report 2017
ANNUAL REPORT 2017 Cover picture: Photo Credit ESA 2 Annual Report 2017 TABLE OF CONTENTS 1 Introduction.......................................................................................................................... 4 2 Year 2017 Review ............................................................................................................... 5 3 Reports of Industrial and Institutional Members ................................................................. 11 3.1 Austrian Academy of Sciences ....................................................................................... 11 3.2 AAC - Aerospace & Advanced Composites GmbH (AAC as spin-off from AIT) .............. 52 3.3 ENPULSION GMBH ....................................................................................................... 56 3.4 EOX IT Services GmbH .................................................................................................. 58 3.5 Fachhochschule Wiener Neustadt – University of Applied Sciences Wiener Neustadt (& research company FOTEC) ............................................................................................. 65 3.6 GeoVille Information Systems and Data Processing GmbH ............................................ 68 3.7 Joanneum Research Forschungsgesellschaft mbH ........................................................ 74 3.8 MAGNA STEYR FAHRZEUGTECHNIK AG & CO KG AEROSPACE ............................. 91 3.9 Ruag Space GmbH ....................................................................................................... -
March 2019 Issue 24
Issue 24 March 2019 DAMPE HXMT EP QUESS WCOM GECAM CSES XPNAV XTP SVOM SPORT eXTP ASO-S MIT SMILE Overview on China's Space Science Missions - see articles on page 18 and 21. illustrations - credit: CNSA/NSSC/CAS/IHEP/CNES/CSNO/NAO/ESA/ATGMedialab/NASA Content Chinese Space Quarterly Report preview issue no 25/26: April - June 2018 ............. page 02 • UNISPACE50+ of the United Nations in Vienna Wu Ji and Chinese Space Science ............ page 18 • 4th CCAF 2018 in Wuhan • Chang'e 4 - full mission report Overview on China's Space Science Missions ............ page 21 • visit to Landspace facility in Huzhou 2019 in Chinese Space ............ page 25 • 3rd/4th Quarterly Reports 2018 All about the Chinese Space Programme GO TAIKONAUTS! Chinese Space Quarterly Report April - June 2018 by Jacqueline Myrrhe and Chen Lan SPACE TRANSPORTATION (PRSS-1) (One Arrow-Double Star) and the smaller, experimental PakTES-1A, built by Pakistan’s space agency SUPARCO CZ-5 (Space and Upper Atmospheric Research Commission) - with In mid-April, the SASTIND (State Administration of Science, assistance from the Space Advisory Company of South Africa. Technology and Industry for National Defence) closed the The launch marks CZ-2C’s return to the international commercial investigation into the CZ-5 Y2 failure. It publicly confirmed the launch service market after a break of nearly 20 years. findings of last summer: a quality issue in the structure of the turbopump in the YF-77 cryogenic engines of the core first stage. YUANWANG The Y3 rocket is being manufactured and will be launched by Yuanwang 3 the end of 2018. -
LIMADOU-CSES M. Ricci
LIMADOU-CSES M. Ricci (Resp.), B. Spataro CSES (China Seismo-Electromagnetic Satellite) is a scientific space mission dedicated to monitoring electromagnetic field and waves, plasma and particle perturbations of the atmosphere, ionosphere and magnetosphere induced by natural sources and anthropocentric emitters and to study their correlations with the occurrence of seismic events. More in general, CSES mission will investigate the structure and the dynamics of the topside ionosphere, the coupling mechanisms with the lower and higher plasma layers and the temporal variations of the geomagnetic field, in quiet and disturbed conditions. Data collected by the mission will also allow studying solar- terrestrial interactions and phenomena of solar physics, namely Coronal Mass Ejections (CMEs), solar flares and cosmic ray solar modulation. The satellite mission is part of a collaboration program between the China National Space Administration (CNSA) and the Italian Space Agency (ASI), and developed by China Earthquake Administration (CEA) and INFN, together with several Chinese and Italian Universities and research Institutes. Italy participates to the CSES mission with the LIMADOU project funded by ASI in collaboration with the Universities of Roma Tor Vergata, Uninettuno, Trento, Bologna and Perugia, as well as the INFN-LNF, INGV (Italian National Institute of Geophysics and Volcanology) and INAF-IAPS (Italian National Institute of Astrophysics and Planetology). This program has been selected in Italy to be funded by the Ministry of Education, University and Research (MIUR) in the context of the programs "Premiali". The launch of CSES, the first of a series of several planned satellite missions, took place successfully on February 2nd, 2018 from the Jiuquan, Gansu Cosmodrome (Inner Mongolia). -
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WWW.OEAW.AC.AT REPORT 2017 REPORT ANNUAL WWW.IWF.OEAW.AC.AT ANNUAL REPORT 2017 COVER IMAGE NASA's Cassini spacecraft has been on an epic road trip, as this graphic of its orbits around the Saturn system shows. This picture traces Cassini's orbits from Saturn orbit insertion in June 2004 through the end of the mission in September 2017. Saturn is in the center, with the orbit of its largest moon Titan in red and the orbits of its six other inner satellites in white. Cassini's prime mission is shown in green. Its first mission extension is shown in orange. The completed orbits of its second mission extension are shown in purple. Orbits after Cassini's 15th anniversary of launch, on 15 October 2012, appear in dark gray. These include orbits that pass inside Saturn's innermost ring, which started in April 2017 (Credit: NASA/JPL-Caltech). TABLE OF CONTENTS INTRODUCTION .....................................................................................................................................5 EARTH & MOON ...................................................................................................................................... 7 GRAVITY FIELD ................................................................................................................................... 7 SATELLITE LASER RANGING .........................................................................................................9 NEAR-EARTH SPACE ............................................................................................................................ -
The High-Energy Particle Detector (HEPD) on Board the CSES Mission
Space Weather of the Heliosphere: Processes and Forecasts Proceedings IAU Symposium No. 335, 2017 c International Astronomical Union 2018 C. Foullon & O.E. Malandraki, eds. doi:10.1017/S1743921317008328 The High-Energy Particle Detector (HEPD) on Board the CSES Mission Vincenzo Vitale1, for the CSES/HEPD collaboration 1 Agenzia Spaziale Italiana (ASI) Science Data Center and INFN, Sezione di Roma “Tor Vergata” I-00133 Roma, Italy email: [email protected] Abstract. The High-Energy Particle Detector (HEPD) will measure electrons, protons and light nuclei fluxes, in low Earth orbit. This detector consists of a high precision silicon tracker, a versatile trigger system, a range-calorimeter and an anti-coincidence system. It is one of the instruments on board the China Seismo-Electromagnetic Satellite (CSES). HEPD can detect multi-MeV particles trapped within the geomagnetic field. When operated at large latitudes HEPD can also detect un-trapped solar particles and low energy cosmic rays. A detailed de- scription of the HEPD will be given. 1. Introduction The High-Energy Particle Detector (HEPD) is a space experiment for the detection of electrons from 3 to 100 MeV, protons from 30 to 300 MeV and light nuclei up to few hundreds of MeV. HEPD will be flown on the CSES satellite (Shen et al. 2011), together with several other instrument, for the study of the low Earth orbit (LEO) electromagnetic environment (ionosphere, magnetosphere and Van Allen belts). The CSES satellite will have a 98 degrees inclination Sun-synchronous circular orbit, an altitude of 500 km and an expected lifetime is 5 of years. -
Lectures on Geothermal Areas in China
GEOTHERMAL TRAINING PROGRAMME Reports 2008 Orkustofnun, Grensásvegur 9, Number 7 IS-108 Reykjavík, Iceland LECTURES ON GEOTHERMAL AREAS IN CHINA Wang Kun Department of Geothermal Management Tianjin Bureau of Land, Resources and Real Estate Management Heping District, Tianjin 300042 P.R. CHINA [email protected] Lectures given in August 2008 United Nations University, Geothermal Training Programme Reykjavík, Iceland Published in December 2008 ISBN 978-9979-68-253-0 ISSN 1670-7400 Wang Kun ii Lectures PREFACE The UNU Visiting Lecturer in 2008 was Dr. Wang Kun, Senior Engineer and Deputy Director of the Geothermal Management Department at Tianjin Bureau of Land, Resources and Real Estate Management (TBLRREM), Tianjin, China. TBLRREM is responsible for the geothermal development, monitoring and utilization in Tianjin. Tianjin is the leading province in geothermal in China. In 2007, the space heating area was approximately 12 Mm2 in Tianjin alone. Seventy geoscientists and engineers from China have graduated from the UNU-GTP and many of these are from Tianjin. Dr. Wang Kun is a former UNU-GTP Fellow (1998) and specialized in reservoir engineering. She obtained her BSc in numerical mathematics at Nankai University in Tianjin 1989, and her PhD in geology at Peking University 2005. She worked as a senior engineer at the Design Institute of Geothermal Exploration and Development until 2001, when she moved to the TBLRREM. Wang Kun is one of the leading geothermal reservoir engineers in China. She gave a series of lectures on geothermal development and resource management in China. Her lectures were excellent and well attended by members of the geothermal community in Iceland as well as the UNU Fellows and MSc Fellows. -
Changes to the Database for May 1, 2021 Release This Version of the Database Includes Launches Through April 30, 2021
Changes to the Database for May 1, 2021 Release This version of the Database includes launches through April 30, 2021. There are currently 4,084 active satellites in the database. The changes to this version of the database include: • The addition of 836 satellites • The deletion of 124 satellites • The addition of and corrections to some satellite data Satellites Deleted from Database for May 1, 2021 Release Quetzal-1 – 1998-057RK ChubuSat 1 – 2014-070C Lacrosse/Onyx 3 (USA 133) – 1997-064A TSUBAME – 2014-070E Diwata-1 – 1998-067HT GRIFEX – 2015-003D HaloSat – 1998-067NX Tianwang 1C – 2015-051B UiTMSAT-1 – 1998-067PD Fox-1A – 2015-058D Maya-1 -- 1998-067PE ChubuSat 2 – 2016-012B Tanyusha No. 3 – 1998-067PJ ChubuSat 3 – 2016-012C Tanyusha No. 4 – 1998-067PK AIST-2D – 2016-026B Catsat-2 -- 1998-067PV ÑuSat-1 – 2016-033B Delphini – 1998-067PW ÑuSat-2 – 2016-033C Catsat-1 – 1998-067PZ Dove 2p-6 – 2016-040H IOD-1 GEMS – 1998-067QK Dove 2p-10 – 2016-040P SWIATOWID – 1998-067QM Dove 2p-12 – 2016-040R NARSSCUBE-1 – 1998-067QX Beesat-4 – 2016-040W TechEdSat-10 – 1998-067RQ Dove 3p-51 – 2017-008E Radsat-U – 1998-067RF Dove 3p-79 – 2017-008AN ABS-7 – 1999-046A Dove 3p-86 – 2017-008AP Nimiq-2 – 2002-062A Dove 3p-35 – 2017-008AT DirecTV-7S – 2004-016A Dove 3p-68 – 2017-008BH Apstar-6 – 2005-012A Dove 3p-14 – 2017-008BS Sinah-1 – 2005-043D Dove 3p-20 – 2017-008C MTSAT-2 – 2006-004A Dove 3p-77 – 2017-008CF INSAT-4CR – 2007-037A Dove 3p-47 – 2017-008CN Yubileiny – 2008-025A Dove 3p-81 – 2017-008CZ AIST-2 – 2013-015D Dove 3p-87 – 2017-008DA Yaogan-18 -
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WWW.OEAW.AC.AT REPORT 2016 REPORT ANNUAL WWW.IWF.OEAW.AC.AT ANNUAL REPORT 2016 COVER IMAGE Topographic image of a dust particle collected and analyzed by the atomic force microscope MIDAS (insert) aboard ESA's Rosetta mission (Credit: ESA/Rosetta/IWF for the MIDAS team IWF/ESA/LATMOS/Universiteit Leiden/Universität Wien). TABLE OF CONTENTS INTRODUCTION .....................................................................................................................................5 EARTH & MOON ...................................................................................................................................... 7 GRAVITY FIELD ................................................................................................................................... 7 SATELLITE LASER RANGING .........................................................................................................9 NEAR-EARTH SPACE ............................................................................................................................. 11 SOLAR SYSTEM .......................................................................................................................................17 SUN & SOLAR WIND ........................................................................................................................17 MERCURY .......................................................................................................................................... 18 VENUS & MARS ...............................................................................................................................