Earth Observation Technologies at the European Space Agency (ESA)
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New Opportunities for Ice Sheet Observations
Remote Sens. 2015, 7, 9371-9389; doi:10.3390/rs70709371 OPEN ACCESS remote sensing ISSN 2072-4292 www.mdpi.com/journal/remotesensing Article The Sentinel-1 Mission: New Opportunities for Ice Sheet Observations Thomas Nagler 1,*, Helmut Rott 1,2, Markus Hetzenecker 1, Jan Wuite 1 and Pierre Potin 3 1 ENVEO IT GmbH, Technikerstrasse 21a, A-6020 Innsbruck, Austria; E-Mails: [email protected] (H.R.); [email protected] (M.H.); [email protected] (J.W.) 2 Institute for Meteorology and Geophysics, University of Innsbruck, A-6020 Innsbruck, Austria 3 European Space Agency/ESRIN, via Galileo Galilei, I-00044 Frascati, Italy; E-Mail: [email protected] * Author to whom correspondence should be addressed; E-Mail: [email protected]; Tel.: +43-512-507-48300; Fax: +43-512-507-48319. Academic Editors: Nicolas Baghdadi and Prasad S. Thenkabail Received: 28 May 2015 / Accepted: 14 July 2015 / Published: 22 July 2015 Abstract: The Sentinel satellite constellation series, developed by the European Space Agency, represents the dedicated space component of the European Copernicus program, committed to long-term operational services in a wide range of application domains. Here, we address the potential of the Sentinel-1 mission for mapping and monitoring the surface velocity of glaciers and ice sheets. We present an ice velocity map of Greenland, derived from synthetic aperture radar (SAR) data acquired in winter 2015 by Sentinel-1A, the first satellite of the Copernicus program in orbit. The map is assembled from about 900 SAR scenes acquired in Interferometric Wide swath (IW) mode, applying the offset tracking technique. -
Tianwen-1: China's Mars Mission
Tianwen-1: China's Mars Mission drishtiias.com/printpdf/tianwen-1-china-s-mars-mission Why In News China will launch its first Mars Mission - Tianwen-1- in July, 2020. China's previous ‘Yinghuo-1’ Mars mission, which was supported by a Russian spacecraft, had failed after it did not leave the earth's orbit and disintegrated over the Pacific Ocean in 2012. The National Aeronautics and Space Administration (NASA) is also going to launch its own Mars mission in July, the Perseverance which aims to collect Martian samples. Key Points The Tianwen-1 Mission: It will lift off on a Long March 5 rocket, from the Wenchang launch centre. It will carry 13 payloads (seven orbiters and six rovers) that will explore the planet. It is an all-in-one orbiter, lander and rover system. Orbiter: It is a spacecraft designed to orbit a celestial body (astronomical body) without landing on its surface. Lander: It is a strong, lightweight spacecraft structure, consisting of a base and three sides "petals" in the shape of a tetrahedron (pyramid- shaped). It is a protective "shell" that houses the rover and protects it, along with the airbags, from the forces of impact. Rover: It is a planetary surface exploration device designed to move across the solid surface on a planet or other planetary mass celestial bodies. 1/3 Objectives: The mission will be the first to place a ground-penetrating radar on the Martian surface, which will be able to study local geology, as well as rock, ice, and dirt distribution. It will search the martian surface for water, investigate soil characteristics, and study the atmosphere. -
INPE) MCTI Çp ' Acordo Operação Técnica COPERNICUS Entre ESA,AEB E INPE (0026237) SEI 01350.001611/2018-03 / Pg
ORIGINAL N° 1 Copernicus Space Component Technical Operating Arrangement ESA - Brazilian Space Agency and INPE (INPE) MCTI çp ' Acordo Operação Técnica COPERNICUS entre ESA,AEB E INPE (0026237) SEI 01350.001611/2018-03 / pg. 1 Table of Contents 1 INTRODUCTION....................................................................................... 4 1.1 Background....................................................................................................................... 4 1.2 Purpose and objectives ..................................................................................................... 4 1.3 Scope................................................................................................................................. 6 1.4 References......................................................................................................................... 6 2 EUROPEAN ACCESS TO BRAZILIAN EO MISSIONS AND CALIBRATION DATA AND PARTNER IN-SITU DATA ............................................................. 7 3 ARRANGEMENT OF TECHNICAL INTERFACES ....................................... 8 3.1 Technical Arrangement Types.......................................................................................... 8 4 INTERNATIONALARCHIVING AND DISSEMINATION CENTRES, MIRRORSITE ................................................................................................ 9 4.1 Invohred Entities............................................................................................................... 9 4.2 INPE Activity -
Atmospheric Dynamics Mission. the Phase-A Studies Were All Completed in June 1999
ESA SP-1233 (4) July 1999 Reports for Mission Selection THE FOUR CANDIDATE EARTH EXPLORER CORE MISSIONS Atmospheric Dynamics Mission ESA SP-1233 (4) – The Four Candidate Earth Explorer Core Missions – ATMOSPHERIC DYNAMICS _________________________________________________________________ Report prepared by: Earth Sciences Division Scientific Co-ordinator: Paul Ingmann Earth Observation Preparatory Programme Technical Co-ordinator: Joachim Fuchs Cover: Richard Francis & Carel Haakman Published by: ESA Publications Division c/o ESTEC, Noordwijk, The Netherlands Editor: Bruce Battrick Copyright: © 1999 European Space Agency ISBN 92-9092-528-0 Price: 70 DFl CONTENTS 1 INTRODUCTION................................................................................................................................5 2 BACKGROUND AND SCIENTIFIC JUSTIFICATION...............................................................9 2.1 GLOBAL WIND PROFILE MEASUREMENTS FOR CLIMATE AND NWP........................................9 2.2 THE NEED FOR ATMOSPHERIC WIND FIELDS FOR ATMOSPHERIC ANALYSES .........................10 2.3 POTENTIAL IMPROVEMENT OF NWP BY ENHANCED WIND OBSERVATIONS ...........................14 2.4 THE NEED FOR ATMOSPHERIC WIND FIELDS FOR CLIMATE STUDIES......................................22 2.5 FUTURE STUDIES AND PERSPECTIVES AIMING AT IMPROVING THE WIND FIELD KNOWLEDGE IN THE POST-2000 TIME FRAME ................................................................................................31 2.6 CONCLUSIONS ON NWP AND CLIMATE STUDIES ......................................................................33 -
Campaigns / the Living Planet Programme / Observing the Earth / Our Activities / ESA
Campaigns / The Living Planet Programme / Observing the Earth / Our Activities / ESA → EUROPEAN SPACE ABOUT US OUR ACTIVITIES CONNECT WITH US FOR MEDIA FOR EDUCATORS FOR KIDS AGENCY ESA OBSERVING THE EARTH LIVING PLANET CAMPAIGNS About Campaigns ESA > Our Activities > Observing the Earth > The Living Planet Programme > Campaigns Recent campaigns Cryovex DomeC-air DOMEX-3 IceSAR-2012 Campaigns blog KaSAR SMOS-ice Services Subscribe Campaigns photo gallery Contact us ARCTIC TREK FOR CRYOSAT A short video from Cold Facts explains why going to the Arctic to collect snow and ice measurements ensures confidence in the data from ESA’s CryoSat mission Campaigns data Archive LATEST NEWS Focus on Gabon forests for Biomass 03 March 2016 Gabon on the radar 22 July 2015 Revealing mountains hiding under ice 29 April 2015 Ice venturers yield results for CryoSat 18 March 2015 Plant power from above 03 February 2015 http://www.esa.int/Our_Activities/Observing_the_Earth/The_Living_Planet_Programme/Campaigns[19/04/2016 12:58:52] Campaigns / The Living Planet Programme / Observing the Earth / Our Activities / ESA Air quality under new scrutiny 28 October 2014 News Archive LATEST ARTICLES MOST-VIEWED ARTICLES MOST-VIEWED IMAGES MOST-VIEWED VIDEOS · Sentinel-1 sees rice paddy drop in… · Live updates: Rosetta mission… · Welcome to a comet · Europe’s solar eclipse seen f… · Interstellar dust intercepted at S… · Touchdown! Rosetta’s Philae p… · ROLIS descent image · Rosetta’s twelve-year journey… · Nansen gives birth to two icebergs · Pioneering Philae completes m… · First comet panoramic · Ambition the film · First light for ExoMars · Rosetta to deploy lander on 1… · OSIRIS spots Philae drifting … · Reconstructing Philae’s flight · Busy spacecraft and experiment sch… · Black hole-star pair orbiting… · Comet panoramic – lander orie… · Timelapse: Canary Islands to … FAQ JOBS AT ESA SITE MAP CONTACTS TERMS AND CONDITIONS http://www.esa.int/Our_Activities/Observing_the_Earth/The_Living_Planet_Programme/Campaigns[19/04/2016 12:58:52]. -
B-180466 Polar Orbiting Weather Satellite Programs
U-180466 l’ht! Honorable Frank E. Moss Chai rmnn, Committee on Aeronautical .r- Cf ‘ind Space Sciences ;>, r-,rr*Id- l~llll~llllllllllllllllllluu~llllllllllllllll United States Senate LM095911 f?- Dear Ilr. Chairman: Your January 1.6, 19 74, letter asked us to obtain cost and other data ~ on both the Department of the Air Force and the joint Natioual Aeronauticsn and Space Administration (NASA)/National Oceanic and Atmospheric Adminis- *76 tration (NOAA) polar orbiting weather satellite programs. L .-__,__ cs&~yl”.^-b -.,I-*Ii*--... --:- -*-“a .-,. We interviewed officials in NASA, NOM, the Department of the Air Force and the Office of Management and Budget (OHU). At these meetings they told us of the existence of two classified studies which provided some comparative analyses of the technical cfrar; cteristics and costs of the NASA and Air Force operational weather satellite systems and the follow-on sys tems in development . We then met with your staff on February 13, 1974, and orally presented the information, At that meeting your staff as ed us for 11 written re- port, We have not independently verified the d :ta; however, we have dis- cussed the matters in this report with the agent y officials. We plan to discuss briefly the history of I he NASA/NOM and Air Force satellite sys terns, compare tl~e characteristics Ilf both systems, provide cost comparisons of the operational- and develop~oental satellite --.-.systems, and furnish information on plans to obtain some mcasurc of commonality of bcltll sys terns. --_.III STORY _-- OF NASA/NOM --_-PKOCRhM The purpose of the joint NASA/NOAA weather satellite system is to provide systematic, +;Lobal cloud cover observations and other meteorologi- cal observations to incrt*&x: man’s ability to -forecast wc;lthcrI m--...YII-._conditions. -
History of NOAA's Polar Observational Environmental Satellites the First
History of NOAA’s Polar Observational Environmental Satellites The first weather satellite in a series of spacecraft originally known as the Television Infrared Observation Satellites (TIROS) was launched on April 1, 1960. By the mid 1970’s NOAA and NASA agreed to produce the series operationally based on the TIROS-N generation of satellites. TIROS-N, a research and development spacecraft serving as a prototype for the operational follow-on series, NOAA-A through NOAA-N Prime was on launched October 13, 1978. Beginning with NOAA-E, launched in 1983, the basic satellite was “stretched” to permit accommodation of additional research instruments. This became known as the Advanced TIROS-N configuration. Some of the additional instruments flown include: Search and Rescue; Earth Radiation Budget Experiment, and the Solar Backscatter Ultraviolet spectrometer. Three of those instruments, Search and Rescue Repeater, Search and Rescue Processor and Solar Backscatter Ultraviolet Radiometer, became part of the operational program. The primary sounding instrumentation has remained essentially unchanged until the addition of Advanced Microwave Sounding Units-A and -B on NOAA-K (15). The Microwave Humidity Sounder replaces the AMSU-B on NOAA-N Prime performing essentially the same science. The satellite design life throughout the series has been two years. The lifetime is a cost/risk tradeoff since more years normally result in a more expensive satellite. To mitigate that risk, the NOAA-N Prime satellite uses the most reliable NASA-approved flight parts, Class S, and considerable redundancy in critical subsystem components. The instruments are not redundant, but they have a three-year design life in order to enhance their expected operational reliability. -
Exploration of Mars by the European Space Agency 1
Exploration of Mars by the European Space Agency Alejandro Cardesín ESA Science Operations Mars Express, ExoMars 2016 IAC Winter School, November 20161 Credit: MEX/HRSC History of Missions to Mars Mars Exploration nowadays… 2000‐2010 2011 2013/14 2016 2018 2020 future … Mars Express MAVEN (ESA) TGO Future ESA (ESA- Studies… RUSSIA) Odyssey MRO Mars Phobos- Sample Grunt Return? (RUSSIA) MOM Schiaparelli ExoMars 2020 Phoenix (ESA-RUSSIA) Opportunity MSL Curiosity Mars Insight 2020 Spirit The data/information contained herein has been reviewed and approved for release by JPL Export Administration on the basis that this document contains no export‐controlled information. Mars Express 2003-2016 … First European Mission to orbit another Planet! First mission of the “Rosetta family” Up and running since 2003 Credit: MEX/HRSC First European Mission to orbit another Planet First European attempt to land on another Planet Original mission concept Credit: MEX/HRSC December 2003: Mars Express Lander Release and Orbit Insertion Collission trajectory Bye bye Beagle 2! Last picture Lander after release, release taken by VMC camera Insertion 19/12/2003 8:33 trajectory Credit: MEX/HRSC Beagle 2 was found in January 2015 ! Only 6km away from landing site OK Open petals indicate soft landing OK Antenna remained covered Lessons learned: comms at all time! Credit: MEX/HRSC Mars Express: so many missions at once Mars Mission Phobos Mission Relay Mission Credit: MEX/HRSC Mars Express science investigations Martian Moons: Phobos & Deimos: Ionosphere, surface, -
Metop Second Generation Payload
MetOp Second Generation Payload Marc Loiselet, Ville Kangas, Ilias Manolis, Franco Fois, Salvatore d’Addio European Space Agency, ESA/ESTEC, Keplerlaan 1, 2200 AG Noordwijk, The Netherlands E-mail: [email protected] MetOp-Second Generation Satellite Instruments Instrument Provider The ESA MetOp Second Generation (MetOp-SG) Programme was approved at the ESA Council Meeting at Ministerial level in Naples in Sat-A METimage DLR via EUMETSAT November 2012. IASI-NG CNES via EUMETSAT MetOp-SG is a follow-on to the current, first generation series of MetOp satellites, which is now established as a cornerstone of the global MWS ESA – MetOp-SG network of meteorological satellites. RO ESA – MetOp-SG The MetOp-SG programme is being implemented in collaboration with EUMETSAT. 3MI ESA – MetOp-SG ESA will develop the prototype MetOp-SG satellites (including associated instruments) and procure, on behalf of EUMETSAT, the recurrent Sentinel-5 ESA – GMES satellites (and associated instruments). The overall MetOp-SG space segment architecture consists of two series of satellites (Sat-A, Sat-B), each carrying different suites of instruments and operating in LEO polar orbit. The planned launches of the first of each series of satellites Sat-B SCA ESA – MetOp-SG are at the beginning of 2021 and at end 2022, respectively. MWI ESA – MetOp-SG RO ESA – MetOp-SG More information can be found in the “MetOp Second Generation – Overview” presentation from Graeme Mason, Hubert Barré, Maurizio ICI ESA – MetOp-SG Betto, ESA-ESTEC, The Netherlands. Argos-4 CNES via EUMETSAT Payload ESA is responsible for instrument design of six instruments, namely the MicroWave Sounder (MWS), Scatterometer (SCA), the Radio Occultation (RO), the MicroWave Imaging (MWI), the Ice Cloud Imager (ICI), and the Multi-viewing, Multi-channel, Multi-polarisation imager (3MI). -
European Astronaut Selection ESA Prepares for the Missions of the 21 St Century
European Astronaut Selection ESA prepares for the missions of the 21 st century With the selection of its first astronauts ESA’s human spaceflight activities in 1978 and the first Spacelab mission are now entering a new era, with ESA in 1983, the European Space Agency astronauts working aboard the (ESA) took its first steps into human International Space Station (ISS), spaceflight. The advent of the Columbus Columbus starting operations, and orbital laboratory project required a the new ‘ATV’ cargo ship delivering second selection of astronauts in 1992. fresh supplies to the Station. The exploration of the Solar System will be one of humanity’s most exciting adventures in the near future. All of the world’s spacefaring nations are preparing for this huge enterprise, and an astronaut corps is essential for Europe, thanks to ESA, to take part in this endeavour. Now is the time for ESA to seek new talents to reinforce its astronaut team, to prepare for missions to the ISS, the Moon and beyond. T The Selection | How? When? Where? h e S e l e c t i o n How can I apply? You can apply online via the ESA web portal (www.esa.int/ astronautselection). Registration is in two steps: • pre-registration: provide identity information and a JAR-FCL 3, Class 2 medi- cal examination certificate, from an Aviation Medical Examiner who has been certified by his/her national Aviation Medical Authority; • a password then allows you to access the application form. T The Selection | How? When? Where? h e S e l e • initial selection according to basic criteria; c t i What are the o • psychological tests for selected candidates; n • second round of psychological tests and interviews; steps in the • medical tests; selection • job interview. -
Space Almanac 2007
2007 Space Almanac The US military space operation in facts and figures. Compiled by Tamar A. Mehuron, Associate Editor, and the staff of Air Force Magazine 74 AIR FORCE Magazine / August 2007 Space 0.05g 60,000 miles Geosynchronous Earth Orbit 22,300 miles Hard vacuum 1,000 miles Medium Earth Orbit begins 300 miles 0.95g 100 miles Low Earth Orbit begins 60 miles Astronaut wings awarded 50 miles Limit for ramjet engines 28 miles Limit for turbojet engines 20 miles Stratosphere begins 10 miles Illustration not to scale Artist’s conception by Erik Simonsen AIR FORCE Magazine / August 2007 75 US Military Missions in Space Space Support Space Force Enhancement Space Control Space Force Application Launch of satellites and other Provide satellite communica- Ensure freedom of action in space Provide capabilities for the ap- high-value payloads into space tions, navigation, weather infor- for the US and its allies and, plication of combat operations and operation of those satellites mation, missile warning, com- when directed, deny an adversary in, through, and from space to through a worldwide network of mand and control, and intel- freedom of action in space. influence the course and outcome ground stations. ligence to the warfighter. of conflict. US Space Funding Millions of constant Fiscal 2007 dollars 60,000 50,000 40,000 30,000 20,000 10,000 0 Fiscal Year 59 62 65 68 71 74 77 80 83 86 89 92 95 98 01 04 Fiscal Year NASA DOD Other Total Fiscal Year NASA DOD Other Total 1959 1,841 3,457 240 5,538 1983 13,051 18,601 675 32,327 1960 3,205 3,892 -
Development and Testing of Metop-Sg Solar Array Drive Mechaism
DEVELOPMENT AND TESTING OF METOP-SG SOLAR ARRAY DRIVE MECHAISM Aksel Elkjaer (1) (2), Lars Helge Surdal (1) (1) Kongsberg Defence & Aerospace (KDA), PO1003, N-3601 Kongsberg, NORWAY (2) Norwegian University of Science and Technology (NTNU), NO-7491 Trondheim, NORWAY, Email: [email protected] ABSTRACT The following sections are grouped into two chapters; §2 Design Drivers presents specific technical This paper presents the development process of the requirements and the design developments that occurred KARMA5-SG Solar Array Drive Mechanism (SADM) during preliminary and critical design reviews. The for delivery to MetOp-SG satellites. The mechanism second chapter, §3 Test Results, details test setups, development is recounted with respect to key design results and non-conformances. drivers and experiences from their subsequent test verification are shared. Design drivers relating to structural, thermal and driveline performance are detailed in the context of a flight program development. Practical experiences from testing are reported and specific challenges from non-conformances are highlighted. A description of test setups and results for functional, vibration and thermal requirements are presented. The purpose of the paper is to share practices and offer lessons learned. 1 INTRODUCTION Delivery to flight programs entails demanding programmatic constraints. As such technology maturity Figure 1. KARMA5-SG MetOp-SG SADM is prioritised to assure schedule constraints. Nevertheless, system development leads to eventual 2 DESIGN DRIVERS changes that impact design decisions and success rests The purpose of the SADM is to provide precise and on the collaboration of all stakeholders. This paper smooth positioning of the solar array whilst transferring provides experiences from the development of MetOp- the electrical power it generates into the satellite.