Science and Space Health Priorities for Next Decade and Beyond
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Climate Change and Human Health: Risks and Responses
Climate change and human health RISKS AND RESPONSES Editors A.J. McMichael The Australian National University, Canberra, Australia D.H. Campbell-Lendrum London School of Hygiene and Tropical Medicine, London, United Kingdom C.F. Corvalán World Health Organization, Geneva, Switzerland K.L. Ebi World Health Organization Regional Office for Europe, European Centre for Environment and Health, Rome, Italy A.K. Githeko Kenya Medical Research Institute, Kisumu, Kenya J.D. Scheraga US Environmental Protection Agency, Washington, DC, USA A. Woodward University of Otago, Wellington, New Zealand WORLD HEALTH ORGANIZATION GENEVA 2003 WHO Library Cataloguing-in-Publication Data Climate change and human health : risks and responses / editors : A. J. McMichael . [et al.] 1.Climate 2.Greenhouse effect 3.Natural disasters 4.Disease transmission 5.Ultraviolet rays—adverse effects 6.Risk assessment I.McMichael, Anthony J. ISBN 92 4 156248 X (NLM classification: WA 30) ©World Health Organization 2003 All rights reserved. Publications of the World Health Organization can be obtained from Marketing and Dis- semination, World Health Organization, 20 Avenue Appia, 1211 Geneva 27, Switzerland (tel: +41 22 791 2476; fax: +41 22 791 4857; email: [email protected]). Requests for permission to reproduce or translate WHO publications—whether for sale or for noncommercial distribution—should be addressed to Publications, at the above address (fax: +41 22 791 4806; email: [email protected]). The designations employed and the presentation of the material in this publication do not imply the expression of any opinion whatsoever on the part of the World Health Organization concerning the legal status of any country, territory, city or area or of its authorities, or concerning the delimitation of its frontiers or boundaries. -
Potential European Contributions to Europa Lander Mission
The Europa Initiative for ESA’s M5 mission Report to OPAG Michel Blanc, Geraint Jones, Olga Prieto-Ballesteros, Veerle Sterken, Javier Gomez-Elvira, David Mimoun, Adam Masters, Sascha Kempf, Luciano Iess, John Cooper, Zita Martins, Ralph Lorenz, Jérémie lasue, Nicolas André, Bruce Bills, Gael Choblet, Geoff Collins, Philippe Garnier, Kevin Hand, Paul Hartogh, Krishan Khurana, Andrea Longobardo, Katrin Stephan, Federico Tosi, Steve Vance, Tim van Hoolst, Roland Wagner, Frances Westall, Martin Wolverk, William Desprats, Ryan Russell, Georges Balmino, Julien Laurent-Varin and the Europa Initiative team August 11th, 2016 1 EI WORKING SCHEME Europa M5 for an ESA contribution to the Europa Lander mission Initiative Penetrator Contribution to Cubesat? Orbiter or… NASA lander A – GLOBAL GEOPHYSICSMagnetospheric interactions CHARACTERIZE EUROPA AS A COMPLEX DYNAMICAL SYSTEM B – ExosphereOF COUPLED LAYERS(neutrals, dust, plumes) FROM CORE TO PLASMA ENVELOPE THROUGH OCEAN AND CRYOSPHERE dimension RESPONDING TO E – Geophysics (internalJUPITER SYSTEM FORCING: TIDAL, MAGNETOSPHERICstructure, incl. Characterization of the ocean) themes ASTROBIOLOGY CONTRIBUTE TO NASA’s LANDER SCIENCE Science AND PROVIDE AN ADDITIONAL ELEMENT (AWL) As resources permit « Spacecraft » dimension EI contribution to EUROPA LanDer : SubmitteD LOI’s Joint Europa Mission (Blanc/Prieto-Ballesteros) • Baseline: Carrier-Orbiter + lander joint NASA/ESA mission: – P1a: Carrier-Orbiter provided by ESA, operated by NASA; – P1b: Alternative option: Carrier-Orbiter provided and operated by NASA; science platform (+ sub-systems?) provided by ESA – Science platform open to both ESA member states and NASA • Option 1: Augmented surface science: Astrobiology Wet Laboratory (AWL) provided by ESA + Member States to enhance landing site exploration. • Option 2: Augmented orbital science - cubesat released from carrier. -
In SPACE November 2012
Aerospace Review Mandated by the Government of Canada Volume 2 Reaching Higher: Canada’s Interests and Future in SPACE November 2012 www.aerospacereview.ca Cover satellite image: ©MacDonald, Dettwiler and Associates Ltd. (MDA) For additional copies of this publication, please contact: Publishing and Depository Services Public Works and Government Services Canada Ottawa ON K1A 0S5 Telephone (toll-free): 1-800-635-7943 (Canada and U.S.) Telephone (local): 613-941-5995 TTY: 1-800-465-7735 Fax (toll-free): 1-800-565-7757 (Canada and U.S.) Fax (local): 613-954-5779 Email: [email protected] Website: publications.gc.ca This publication is available upon request in accessible formats (Braille and large print). Contact: Multimedia Services Communications and Marketing Branch Industry Canada Email: [email protected] This publication is also available online at aerospacereview.ca Permission to Reproduce Except as otherwise specifically noted, the information in this publication may be reproduced, in part or in whole and by any means, without charge or further permission from Industry Canada, provided that due diligence is exercised in ensuring the accuracy of the information reproduced; that Industry Canada is identified as the source institution; and that the reproduction is not represented as an official version of the information reproduced, nor as having been made in affiliation with, or with the endorsement of, Industry Canada. For permission to reproduce the information in this publication for commercial redistribution, -
Mars Exploration: an Overview of Indian and International Mars Missions Nayamavalsa Scariah1, Dr
Taurian Innovative Journal/Volume 1/ Issue 1 Mars exploration: An overview of Indian and International Mars Missions NayamaValsa Scariah1, Dr. Mili Ghosh2, Dr.A.P.Krishna3 Birla Institute of Technology, Mesra, Ranchi Abstract- Mars is the fourth planet from the sun. It is 1. Introduction also known as red planet because of its iron oxide content. There are lots of missions have been launched to Mars is also known as red planet, because of the mars for better understanding of our neighboring planet. reddish iron oxide prevalent on its surface gives it a There are lots of unmanned spacecraft including reddish appearance. It is the fourth planet from sun. orbiters, landers and rovers have been launched into mars since early 1960. Sputnik was the first satellite The term sol is used to define duration of solar day on launched in 1957 by Soviet Union. After seven failure Mars. A mean Martian solar day or sol is 24 hours 39 missions to Mars, Mariner 4 was the first satellite which minutes and 34.244 seconds. Many space missions to reached the Martian orbiter successfully. The Viking 1 Mars have been planned and launched for Mars was the first lander reached on Mars on 1975. India exploration (Table:1) but most of them failed without successfully launched a spacecraft, Mangalyan (Mars completing the task specially in early attempts th Orbiter Mission) on 5 November, 2013, with five whereas some NASA missions were very payloads to Mars. India was the first nation to successful(such as the twin Mars Exploration Rovers, successfully reach Mars on its first attempt. -
Venona Special Studies
- 1 - Venona Project Special Studies Transcribed by Students of the Mercyhurst College Institute for Intelligence Studies Arranged by John Earl Haynes, Library of Congress, 2010 COVER NAMES IN NEW YORK TRAFFIC p. 2 UNIDENTIFIED COVER NAMES IN NEW YORK TRAFFIC p. 86 COVER NAMES IN SAN FRANCISCO TRAFFIC p. 92 COVER NAMES IN WASHINGTON TRAFFIC p. 123 ADDITIONAL COVERNAMES AND RELATED INFORMATION IN DIPLOMATIC TRAFFIC p. 127 REVISED TRANSLATION OF MESSAGE ON ANTENNA-LIBERAL'S WIFE ETHEL p. 135 THE COVERNAMES "ANTENNA" AND "LIBERAL" IN . MESSAGES p. 139 ESSAGES IN . INVOLVING THE COVERNAME"ENORMOZ" AND THE NAMES OF NUCLEAR PHYSICISTS, ETC. p. 147 UNDATED REPORT OF MEREDITH GARDNER p. 155 DEVELOPMENT OF THE “G--“HOMER” [“GOMER”] CASE p. 158 THE KOMAR (KRAVCHENKO) AFFAIR IN . MESSAGES p. 161 REVISED TRANSLATION OF TWO . MESSAGES ON CHANGES IN COVERNAMES p. 170 THE COVERNAME "KARAS" IN. TRAFFIC p. 178 THE COVERNAMES "TÉNOR", "BAS", AND "CHETÁ" (? IN . TRAFFIC p. 181 - 2 - Special Study Cover Names in New York Traffic - 3 - cover-name Message number Date Publication reference S/ or 3/NBF/ 19 N.Y. to M. 812 29053 JKI 06 T1022 1B-1910 0027A ABRAM N.Y. to M. 992 24063 JKR 14 T872√ 1B-7518 0005A JACK SOBLE 1086 06073 JKV 48 T873√ 2A-0011 1957 29113 NNNNNN T939√ 625 04054 JHD 48 T916√ 851 15064 JIJ 40 T10.1√ 1146 10084 JHM 41 T123√ 1251 02094 JHN 12 T301√ (to ChEKh) 0005B 1353 23094 JHO 42 T289√ 1449 12104 JIL 37 T106√ 1754 14124 JHZ 49 T6√ 48 11015 JHV 37 (NSA)T1941 AVGUR 2A-0013 1638 (AUGUR) N.Y. -
Csa 2020-21 Dp
Canadian Space Agency 2020–21 Departmental Plan The Honourable Navdeep Bains, P.C., M.P. Minister of Innovation, Science and Industry © Her Majesty the Queen in Right of Canada, represented by the Minister of Industry, 2020 Catalogue Number: ST96-10E-PDF ISSN: 2371-7777 Table of Contents From the Minister ............................................................................. 1 Plans at a glance .............................................................................. 3 Core responsibilities: planned results and resources ............................. 5 Canada in Space ........................................................................ 5 Internal Services: planned results .................................................... 15 Spending and human resources ........................................................ 17 Planned spending ..................................................................... 17 Planned human resources.......................................................... 19 Estimates by vote ..................................................................... 19 Condensed future-oriented statement of operations ...................... 20 Corporate information ..................................................................... 23 Organizational profile ................................................................ 23 Raison d’être, mandate and role: who we are and what we do ....... 23 Operating context .................................................................... 23 Reporting framework ............................................................... -
Lunar Life Sciences Payload Assessment
Lunar Surface Science Workshop 2020 (LPI Contrib. No. 2241) 5077.pdf LUNAR LIFE SCIENCES PAYLOAD ASSESSMENT. S. C. Sun1, F. Karouia2, M. P. Lera3, M. P. Parra1, H. E. Ray4, A. J. Ricco1, S. M. Spremo1. 1NASA Ames Research Center, 2Blue Marble Space Institute of Science, 3KBR, 4ASRC Federal Space and Defense, Inc. Introduction: The Moon provides a unique site to ISS, including systems that integrate into EXPRESS study living organisms. The fractional gravity and (EXpedite the PRocessing of ExperimentS for Space) unique radiation environment have similarities to Mars Racks or are external space exposure research facilities. and will help us understand how life will respond to These same systems can be the basis for future payload conditions on the red planet. Martian and lunar envi- systems for experiments to be performed beyond Low ronments can be simulated on the ground but not to high Earth Orbit. Such facilities would need to be adapted to fidelity. Altered gravity and increased radiation are dif- be compatible with the new research platforms and ficult to replicate simultaneously, which makes study- function in the harsher radiation environment found out- ing their combined effect difficult. The International side the magnetosphere. If Gateway and a lunar based- Space Station, and previously, the Space Shuttle, pro- lab could provide EXPRESS-compatible interfaces, lev- vided a microgravity environment, and could simulate eraging hardware developed for ISS would be more fea- fractional-g only via an onboard centrifuge. Because sible. the ISS and Space Shuttle orbits were within the Earth’s Gaps in Capabilities: Many of the payload systems magnetosphere, experiments on those platforms have that have been developed require human tending. -
Robot Operating System - the Complete Reference (Volume 4) Part of the Studies in Computational Intelligence Book Series (SCI, Volume 831)
Book Robot Operating System - The Complete Reference (Volume 4) Part of the Studies in Computational Intelligence book series (SCI, volume 831) Several authors CISTER-TR-190702 2019 Book CISTER-TR-190702 Robot Operating System - The Complete Reference (Volume 4) Robot Operating System - The Complete Reference (Volume 4) Several authors CISTER Research Centre Rua Dr. António Bernardino de Almeida, 431 4200-072 Porto Portugal Tel.: +351.22.8340509, Fax: +351.22.8321159 E-mail: https://www.cister-labs.pt Abstract This is the fourth volume of the successful series Robot Operating Systems: The Complete Reference, providing a comprehensive overview of robot operating systems (ROS), which is currently the main development framework for robotics applications, as well as the latest trends and contributed systems. The book is divided into four parts: Part 1 features two papers on navigation, discussing SLAM and path planning. Part 2 focuses on the integration of ROS into quadcopters and their control. Part 3 then discusses two emerging applications for robotics: cloud robotics, and video stabilization. Part 4 presents tools developed for ROS; the first is a practical alternative to the roslaunch system, and the second is related to penetration testing. This book is a valuable resource for ROS users and wanting to learn more about ROS capabilities and features. © 2019 CISTER Research Center 1 www.cister-labs.pt Studies in Computational Intelligence 831 Anis Koubaa Editor Robot Operating System (ROS) The Complete Reference (Volume 4) Studies in Computational Intelligence Volume 831 Series Editor Janusz Kacprzyk, Polish Academy of Sciences, Warsaw, Poland [email protected] The series “Studies in Computational Intelligence” (SCI) publishes new develop- ments and advances in the various areas of computational intelligence—quickly and with a high quality. -
Actual Problems Актуальные Проблемы
АКАДЕМИЯ НАУК АВИАЦИИ И ВОЗДУХОПЛАВАНИЯ РОССИЙСКАЯ АКАДЕМИЯ КОСМОНАВТИКИ ИМ. К.Э.ЦИОЛКОВСКОГО ACADEMY OF AVIATION AND AERONAUTICS SCIENCES RUSSIAN ASTRONAUTICS ACADEMY OF K.E.TSIOLKOVSKY'S NAME СССР 7 195 ISSN 1727-6853 12.04.1961 АКТУАЛЬНЫЕ ПРОБЛЕМЫ АВИАЦИОННЫХ И АЭРОКОСМИЧЕСКИХ СИСТЕМ процессы, модели, эксперимент 2(39) 2014 RUSSIAN-AMERICAN SCIENTIFIC JOURNAL ACTUAL PROBLEMS OF AVIATION AND AEROSPACE SYSTEMS processes, models, experiment УРНАЛ УЧНЫЙ Ж О-АМЕРИКАНСКИЙ НА ОССИЙСК Р Казань Daytona Beach А К Т УА Л Ь Н Ы Е П Р О Б Л Е М Ы А В И А Ц И О Н Н Ы Х И А Э Р О К О С М И Ч Е С К И Х С И С Т Е М Казань, Дайтона Бич Вып. 2 (39), том 19, 1-206, 2014 СОДЕРЖАНИЕ CONTENTS Г.В.Новожилов 1 G.V.Novozhilov К 120-летию авиаконструктора To the 120-th Anniversary of Сергея Владимировича Ильюшина Sergey Vladimirovich Ilyushin А.Болонкин 14 A.Bolonkin Использование энергии ветра Utilization of wind energy at high больших высот altitude Эмилио Спедикато 46 Emilio Spedicato О моделировании взаимодействия About modelling interaction of Earth Земли с крупным космическим with large space object: the script with объектом: сценарий взрыва Фаэтона explosion of Phaeton and the sub- и последующей эволюции sequent evolution of Mankind (part II) Человечества (часть II) М.В.Левский 76 M.V.Levskii Оптимальное по времени The time-optimal control of motion of a управление движением spacecraft with inertial executive космического аппарата с devices инерционными исполнительными органами В.А.Афанасьев, А.С.Мещанов, 99 V.A.Afanasyev, A.S.Meshchanov, Е.Ю.Самышева -
Frequency Response and Bode Plots
1 Frequency Response and Bode Plots 1.1 Preliminaries The steady-state sinusoidal frequency-response of a circuit is described by the phasor transfer function Hj( ) . A Bode plot is a graph of the magnitude (in dB) or phase of the transfer function versus frequency. Of course we can easily program the transfer function into a computer to make such plots, and for very complicated transfer functions this may be our only recourse. But in many cases the key features of the plot can be quickly sketched by hand using some simple rules that identify the impact of the poles and zeroes in shaping the frequency response. The advantage of this approach is the insight it provides on how the circuit elements influence the frequency response. This is especially important in the design of frequency-selective circuits. We will first consider how to generate Bode plots for simple poles, and then discuss how to handle the general second-order response. Before doing this, however, it may be helpful to review some properties of transfer functions, the decibel scale, and properties of the log function. Poles, Zeroes, and Stability The s-domain transfer function is always a rational polynomial function of the form Ns() smm as12 a s m asa Hs() K K mm12 10 (1.1) nn12 n Ds() s bsnn12 b s bsb 10 As we have seen already, the polynomials in the numerator and denominator are factored to find the poles and zeroes; these are the values of s that make the numerator or denominator zero. If we write the zeroes as zz123,, zetc., and similarly write the poles as pp123,, p , then Hs( ) can be written in factored form as ()()()s zsz sz Hs() K 12 m (1.2) ()()()s psp12 sp n 1 © Bob York 2009 2 Frequency Response and Bode Plots The pole and zero locations can be real or complex. -
Interstellar Travel and the Fermi Paradox
Interstellar Travel If aliens haven’t visited us, could we go to them? In this lecture we will have some fun speculating about future interstellar travel by humans. Please keep in mind that, as we discussed earlier, this cannot be considered a solution for the problems that we have on Earth, for the simple reason that the expense per person is utterly prohibitive and will remain so in any conceivable future scenario. Nonetheless, given enough time it could be that we have the capacity to move out into the galaxy. Incidentally, we will leave discussions of really far-out concepts such as wormholes to a future class. Interstellar distances The major barrier to interstellar travel is the staggering distance between stars. The closest one to the Sun is Proxima Centauri, which is 4.3 light years away but not a likely host to planets. There are, however, a few possibilities within roughly 10 light years, so that is a good target. How far is 10 light years? By definition it is how far light travels in 10 years, but let’s put this into a more familiar context. A moderately brisk walking pace is 5 km/hr, and since one light year is about 10 trillion kilometers, you would need about 20 trillion hours, or about 2.3 billion years, to walk that distance. The fastest cars sold commercially go about 400 km/hr, so you would need about three billion hours or a bit less than thirty million years. The speed of the Earth in its orbit, which is comparable to the speed of the fastest spacecraft we have constructed (all unmanned, of course), is about 30 km/s and even at that rate it would take about a hundred thousand years to travel ten light years. -
Standard for Terminology V2
Joint Monitoring Programme for Ambient Noise North Sea 2018 – 2020 Standard for Terminology WP 3 Deliverable/Task: 3.1 Authors: L. Wang, S Robinson Affiliations: NPL Version 2.0 Date: March 2020 INTERREG North Sea Region Jomopans Project Full Title Joint Monitoring Programme for Ambient Noise North Sea Project Acronym Jomopans Programme Interreg North Region Programme Programme Priority Priority 3 Sustainable North Sea Region Colophon Name Niels Kinneging (Project Manager) Organization Name Rijkswaterstaat Email [email protected] Phone +31 6 5321 5242 This report should be cited: JOMOPANS standard: Terminology for ambient ocean noise monitoring Cover picture: UK Crown copyright 2 INTERREG North Sea Region Jomopans Table of contents 1 General acoustic terms ......................................................................................................... 5 1.1 Definitions of basic quantities and metrics ............................................................................ 5 1.2 Levels used in underwater acoustics ...................................................................................11 2 Metrics for ambient noise monitoring in JOMOPANS ..........................................................14 2.1 Metrics for use in JOMOPANS ............................................................................................14 2.2 Other common metrics not used in JOMOPANS .................................................................14 3 Terminology used in acoustic modelling ..............................................................................15