NOAA's PRODUCT PROCESSING PLANS for the METOP MISSION

Total Page:16

File Type:pdf, Size:1020Kb

NOAA's PRODUCT PROCESSING PLANS for the METOP MISSION P5.29 NOAA’S PRODUCT PROCESSING PLANS FOR THE METOP MISSION Stacy L. Bunin* and Diane Holmes Mitretek Systems, Inc., Falls Church, Virginia Tom Schott NOAA/NESDIS, Washington, D.C 1. INTRODUCTION launched in June 2002 to replace NOAA-15. It was placed into a mid-morning orbit (10:00 AM). In November 1998, the National Oceanic and NOAA-17’s new mid-morning orbit allows for Atmospheric Administration (NOAA) and the increased temporal coverage and production of European Organization for the Exploitation of numerous imagery-based products, such as Meteorological Satellites (EUMETSAT) signed a aerosol and vegetation index, currently not Memorandum of Agreement for participation in the available from early morning orbits due to sun Initial Joint Polar System (IJPS). IJPS consists of angle constraints. The new channel 3a (1.6 two independent, but fully coordinated, polar micron) added to the NOAA-KLM series for satellite systems. In support of IJPS, NOAA will enhanced discrimination between snow/ice and operate the NOAA-N and -N’ satellites, which will clouds is also optimized in the mid-morning orbit. be flown in a polar orbit with an afternoon (2:00 Additionally, NOAA-17 at 10:00 AM allows for a P.M.) equatorial crossing time. EUMETSAT will transition to and validation of the NOAA heritage develop the Meteorological Operational (Metop) instruments and their derived products scheduled series of satellites to be flown in a polar orbit with for Metop-1. The planned launch dates for the a mid-morning (9:30 A.M.) equatorial crossing NOAA and Metop satellites during the IJPS era time. The mid-morning and afternoon satellites follows: will each carry a set of jointly provided common instruments, plus additional instruments specific to NOAA-N – June 2004 each orbit and operating agency. Through the use Metop-1 – July 2005 of these satellites, NOAA and EUMETSAT will NOAA-N’ – March 2008 support the generation of products and services Metop-2 – August 2010 for their respective user communities. This paper will focus on NOAA’s product processing plans in The first Metop satellite is planned to become the IJPS era, including the impacts of changes to operational in 2006 after an extensive checkout the current product suite and the new products to period. be generated from Metop data, which includes sea surface winds, advanced atmospheric soundings, and higher resolution products from Metop’s global 3. IJPS INSTRUMENTS 1-km Advanced Very High Resolution Radiometer (AVHRR) data. The core environmental instrument set used for product processing on the NOAA and Metop satellites in the IJPS era are listed below. In 2. CURRENT SATELLITE STATUS AND PLANS addition, sensors for search and rescue and data collection are also part of the core instrument Currently NESDIS has two operational polar- suite. orbiting satellites. NOAA-K, now designated NOAA-15, was launched into an early morning • Advanced Microwave Sounding Unit-A orbit (7:30 AM) in May 1998. NOAA-L, now (AMSU-A) is a microwave sounder with 15 designated NOAA-16, was launched into an channels in the 23-90 GHz range. This afternoon (2:00 PM) orbit in September 2000. instrument is used primarily for derivation of NOAA-M, now designated NOAA-17, was temperature soundings along with several surface and hydrological parameters. * Corresponding author address: Stacy L. • Advanced Very High Resolution Radiometer Bunin, Mitretek Systems; 3150 Fairview Park (AVHRR/3) is an imaging radiometer with six Drive South; Falls Church, Virginia 22042; e- channels (3 visible/near infrared and 3 mail: [email protected]. infrared) in the range of 0.6-12 microns. The Metop spacecraft will have the capability to • Infrared Atmospheric Sounding Interferometer record full resolution 1-km global imagery for (IASI) is a Michelson interferometer covering one complete orbital pass. The NOAA-N and the 3.6-15.5 micron range. IASI thinned –N’ satellites will continue to provide 4-km radiances will be used initially by NESDIS and global imagery as well as more 1-km Local its users in a manner similar to those Area Coverage (LAC) imagery due to the use generated from the Atmospheric Infrared of digital recorders on the spacecraft. In Sounder (AIRS) instrument aboard NASA’s addition to imagery this instrument supports Aqua satellite. Plans also include the the production of numerous ocean, land, and generation of atmospheric temperature and ice parameters along with hazard (fire, moisture soundings to complement the HIRS, volcano) detection and monitoring. MHS, and AMSU-based soundings. • High Resolution Infrared Radiation Sounder (HIRS/4) is a temperature sounder with 19 Data streams from all core instruments, regardless infrared channels in the 3-15 micron range, of platform, plus the SBUV/2, will continue to be and one visible channel. The HIRS/4 is an available at NESDIS in order to continue to meet upgrade from the HIRS/3 currently orbiting current and planned Level 1 data and Level 2 aboard the NOAA-KLM series of satellites. product generation, distribution and archive The HIRS/4 has a smaller field of view at 10- requirements. In addition, access to the data km, compared to 20-km on the HIRS/3 model. and/or products of the four new Metop instruments • Microwave Humidity Sounder (MHS) is a will be supported in order to enhance fulfillment of microwave sounder with five channels at 89, NESDIS requirements. 157, and around 183 GHz supporting production of humidity profiles and other hydrological products. 4. DIRECT READOUT SERVICES • Space Environment Monitor (SEM-2) is a multi-channel charged-particle spectrometer. During the IJPS era, satellite data will continue to be available to direct broadcast local users In addition to the core instruments, the NOAA worldwide. The NOAA and Metop satellites will satellites will also carry: broadcast via High Resolution Picture Transmission (HRPT), which is AVHRR based for • Solar Backscatter-Ultraviolet Radiometer NOAA satellites. Initially the Metop satellites will (SBUV/2) is a spectral radiometer with 12 also only be AVHRR based, although the channels in the 252.0-322.3 nm in discrete capability exists for utilizing other Metop mode and 160-400 nm in scan mode, used for instrument data at a future date. generating total ozone and ozone profiles. While the NOAA satellites will continue to The Metop satellites will carry four new broadcast the 4-km AVHRR data via analog instruments: Automated Picture Transmission (APT) links, the Metop satellites will broadcast a new digital Low Resolution Picture Transmission (LRPT) data • Advanced Scatterometer (ASCAT) is a pulsed stream using the VHF band. LRPT includes C-band radar at 5.255 GH, and will be used to selected channels of AVHRR data, as well as generate ocean surface wind vector products. HIRS/4, AMSU-A, MHS, SEM, and the GRAS • Global Ozone Monitoring Experiment (GOME- positioning and timing data. 2) is a nadir-viewing spectrometer with four channels in the range of 0.240-0.790 microns. NESDIS plans are for using the GOME-2 to 5. IJPS PRODUCT PROCESSING derive total ozone and ozone profile products. • Global navigation satellite system Receiver for The products that will be generated during the Atmospheric Sounding (GRAS) is a radio IJPS era and their associated instrument datasets occultation receiver that uses signals from the are depicted in Figure 1. Operational snow and global navigation satellite systems. GRAS will ice, hazards, and significant event imagery are only initially be used by NESDIS for research generated by the NESDIS Office of Satellite Data applications including atmospheric Processing and Distribution’s (OSDPD) Satellite temperature and moisture profiles. Services Division on the Satellite Environmental Processing System (SATEPS). Aerosol, global vegetation, cloud imagery, sea surface Environment Center. Services during the IJPS era temperature, radiation budget, atmospheric include search and rescue and the data collection moisture and temperature soundings, ozone, and services. Products are made available to a wide microwave surface and hydrological products are variety of users via the SATEPS and CEMSCS generated by the Central Environmental Satellite servers, the Internet, the National Weather Service Computer System (CEMSCS) within OSDPD’s Gateway, the Global Telecommunications System, Information Processing Division. Other products or several other methods. include sea ice analyses generated by the National Ice Center and space environment products generated by NOAA’s Space IJPS Product Processing Level 1 Data Product Generation Levels 2 and 3 SATEPS CEMSCS Other Snow/ Hazards Aerosol Global Cloud Global Local Sea Space Ice Vegetation Imagery Sea Sea Ice Environ- Surface Surface (NIC) ment Temp Temp (SEC) •AVHRR •AVHRR •AVHRR •AVHRR •AVHRR •AVHRR •AVHRR •AVHRR •SEM-2 GAC GAC GAC GAC GAC GAC LAC LAC •HIRS/4 •AVHRR •AVHRR Significant HRPT HRPT Event Imagery Radiation Soundings Ozone MW TBD Data Search Budget Surface/ Day-2 Collection and Hydro Systems (DCS) Rescue •AVHRR (SAR) GAC •DCS •SAR •AVHRR •AVHRR •AVHRR •SBUV/2 •AMSU-A •ASCAT LAC GAC GAC •MHS •IASI •AVHRR •HIRS/4 •AMSU-A •GOME-2 HRPT •HIRS/4 •GRAS •MHS User Interfaces (Servers, Web Pages, GTS, NWS Gateway, etc.) Figure 1. IJPS Product Processing and Services. There will be a phased approached to product months and include products from AMSU-A, processing during the IJPS era based on mission HIRS/4, MHS, SEM, Metop’s HRPT AVHRR data, priorities. The highest priority is continuing the and the products based on the 4-km AVHRR data. morning mission and includes those products that Products based on the full global 1-km AVHRR are required to be generated, distributed, and data may also become operational at the archived on an operational basis at the transition transition. In addition, GOME-2 total ozone from an older spacecraft (i.e., from NOAA-16 to products are expected to become operational at NOAA-N or from NOAA-17 to Metop-1) in order to the time of the transition for continuity of the continue the fulfillment of existing requirements on NOAA-17 SBUV/2 products.
Recommended publications
  • 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).
    [Show full text]
  • 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.
    [Show full text]
  • → Space for Europe European Space Agency
    number 149 | February 2012 bulletin → space for europe European Space Agency The European Space Agency was formed out of, and took over the rights and The ESA headquarters are in Paris. obligations of, the two earlier European space organisations – the European Space Research Organisation (ESRO) and the European Launcher Development The major establishments of ESA are: Organisation (ELDO). The Member States are Austria, Belgium, Czech Republic, Denmark, Finland, France, Germany, Greece, Ireland, Italy, Luxembourg, the ESTEC, Noordwijk, Netherlands. Netherlands, Norway, Portugal, Romania, Spain, Sweden, Switzerland and the United Kingdom. Canada is a Cooperating State. ESOC, Darmstadt, Germany. In the words of its Convention: the purpose of the Agency shall be to provide for ESRIN, Frascati, Italy. and to promote, for exclusively peaceful purposes, cooperation among European States in space research and technology and their space applications, with a view ESAC, Madrid, Spain. to their being used for scientific purposes and for operational space applications systems: Chairman of the Council: D. Williams → by elaborating and implementing a long-term European space policy, by Director General: J.-J. Dordain recommending space objectives to the Member States, and by concerting the policies of the Member States with respect to other national and international organisations and institutions; → by elaborating and implementing activities and programmes in the space field; → by coordinating the European space programme and national programmes, and by integrating the latter progressively and as completely as possible into the European space programme, in particular as regards the development of applications satellites; → by elaborating and implementing the industrial policy appropriate to its programme and by recommending a coherent industrial policy to the Member States.
    [Show full text]
  • Esa Broch Envisat 2.Xpr Ir 36
    ENVISAT-1 Mission & System Summary ENVISAT-1 ENVISAT-1 Mission & System Summary Issue 2 Table of contents Table Table of contents 1 Introduction 3 Mission 4 System 8 Satellite 16 Payload Instruments 26 Products & Simulations 62 FOS 66 PDS 68 Overall Development and Verification Programme 74 Industrial Organization 78 Introduction Introduction 3 The impacts of mankind’s activities on the Earth’s environment is one of the major challenges facing the The -1 mission constists of three main elements: human race at the start of the third millennium. • the Polar Platform (); • the -1 Payload; The ecological consequences of human activities is of • the -1 Ground Segment. major concern, affecting all parts of the globe. Within less than a century, induced climate changes The development was initiated in 1989 as may be bigger than what those faced by humanity over a multimission platform; the -1 payload the last 10000 years. The ‘greenhouse effect’, acid rain, complement was approved in 1992 with the final the hole in the ozone layer, the systematic destruction decision concerning the industrial consortium being of forests are all triggering passionate debates. taken in March 1994. The -1 Ground Concept was approved in September 1994. This new awareness of the environmental and climatic changes that may be affecting our entire planet has These decisions resulted in three parallel industrial considerably increased scientific and political awareness developments, together producing the overall -1 of the need to analyse and understand the complex system. interactions between the Earth’s atmosphere, oceans, polar and land surfaces. The development, integration and test of the various elements are proceeding leading to a launch of the The perspective being able to make global observations -1 satellite planned for the end of this decade.
    [Show full text]
  • The EUMETSAT Polar System 13+ Successful Years of Global Observations for Operational Weather Prediction and Climate Monitoring K
    Article The EUMETSAT Polar System 13+ Successful Years of Global Observations for Operational Weather Prediction and Climate Monitoring K. Dieter Klaes, Jörg Ackermann, Craig Anderson, Yago Andres, Thomas August, Régis Borde, Bojan Bojkov, Leonid Butenko, Alessandra Cacciari, Dorothée Coppens, Marc Crapeau, Stephanie Guedj, Olivier Hautecoeur, Tim Hultberg, Rüdiger Lang, Stefanie Linow, Christian Marquardt, Rosemarie Munro, Carlo Pettirossi, Gabriele Poli, Francesca Ticconi, Olivier Vandermarcq, Mayte Vasquez, and Margarita Vazquez-Navarro ABSTRACT: After successful launch in November 2018 and successful commissioning of Metop-C, all three satellites of the EUMETSAT Polar System (EPS) are in orbit together and operational. EPS is part of the Initial Joint Polar System (IJPS) with the United States (NOAA) and provides the service in the midmorning orbit. The Metop satellites carry a mission payload of sounding and imaging instruments, which allow provision of support to operational meteorology and climate monitoring, which are the main mission objectives for EPS. Applications include numerical weather prediction, atmospheric composition monitoring, and marine meteorology. Climate monitoring is supported through the generation of long time series through the program duration of 20+ years. The payload was developed and contributed by partners, including NOAA, CNES, and ESA. EUMETSAT and ESA developed the space segment in cooperation. The system has proven its value since the first satellite Metop-A, with enhanced products at high reliability
    [Show full text]
  • Synthetic Aperture Radar in Europe: ERS, Envisat, and Beyond
    SYNTHETIC APERTURE RADAR IN EUROPE Synthetic Aperture Radar in Europe: ERS, Envisat, and Beyond Evert Attema, Yves-Louis Desnos, and Guy Duchossois Following the successful Seasat project in 1978, the European Space Agency used advanced microwave radar techniques on the European Remote Sensing satellites ERS-1 (1991) and ERS-2 (1995) to provide global and repetitive observations, irrespective of cloud or sunlight conditions, for the scientific study of the Earth’s environment. The ERS synthetic aperture radars (SARs) demonstrated for the first time the feasibility of a highly stable SAR instrument in orbit and the significance of a long-term, reliable mission. The ERS program has created opportunities for scientific discovery, has revolutionized many Earth science disciplines, and has initiated commercial applica- tions. Another European SAR, the Advanced SAR (ASAR), is expected to be launched on Envisat in late 2000, thus ensuring the continuation of SAR data provision in C band but with important new capabilities. To maximize the use of the data, a new data policy for ERS and Envisat has been adopted. In addition, a new Earth observation program, The Living Planet, will follow Envisat, offering opportunities for SAR science and applications well into the future. (Keywords: European Remote Sensing satellite, Living Planet, Synthetic aperture radar.) INTRODUCTION In Europe, synthetic aperture radar (SAR) technol- Earth Watch component of the new Earth observation ogy for polar-orbiting satellites has been developed in program, The Living Planet, and possibly the scientific the framework of the Earth observation programs of Earth Explorer component will include future SAR the European Space Agency (ESA).
    [Show full text]
  • Civilian Satellite Remote Sensing: a Strategic Approach
    Civilian Satellite Remote Sensing: A Strategic Approach September 1994 OTA-ISS-607 NTIS order #PB95-109633 GPO stock #052-003-01395-9 Recommended citation: U.S. Congress, Office of Technology Assessment, Civilian Satellite Remote Sensing: A Strategic Approach, OTA-ISS-607 (Washington, DC: U.S. Government Printing Office, September 1994). For sale by the U.S. Government Printing Office Superintendent of Documents, Mail Stop: SSOP. Washington, DC 20402-9328 ISBN 0-16 -045310-0 Foreword ver the next two decades, Earth observations from space prom- ise to become increasingly important for predicting the weather, studying global change, and managing global resources. How the U.S. government responds to the political, economic, and technical0 challenges posed by the growing interest in satellite remote sensing could have a major impact on the use and management of global resources. The United States and other countries now collect Earth data by means of several civilian remote sensing systems. These data assist fed- eral and state agencies in carrying out their legislatively mandated pro- grams and offer numerous additional benefits to commerce, science, and the public welfare. Existing U.S. and foreign satellite remote sensing programs often have overlapping requirements and redundant instru- ments and spacecraft. This report, the final one of the Office of Technolo- gy Assessment analysis of Earth Observations Systems, analyzes the case for developing a long-term, comprehensive strategic plan for civil- ian satellite remote sensing, and explores the elements of such a plan, if it were adopted. The report also enumerates many of the congressional de- cisions needed to ensure that future data needs will be satisfied.
    [Show full text]
  • Simulation of the Yield and Accuracy of Wind Profile Measurements From
    431 Simulation of the yield and accuracy of wind profile measurements from the Atmospheric Dynamics Mission (ADM-Aeolus). David G.H. Tan and Erik Andersson Research Department Submitted to Q. J. R. Meteorol. Soc. January 2004 Series: ECMWF Technical Memoranda A full list of ECMWF Publications can be found on our web site under: http://www.ecmwf.int/publications/ Contact: [email protected] ­c Copyright 2004 European Centre for Medium Range Weather Forecasts Shinfield Park, Reading, RG2 9AX, England Literary and scientific copyrights belong to ECMWF and are reserved in all countries. This publication is not to be reprinted or translated in whole or in part without the written permission of the Director. Appropriate non-commercial use will normally be granted under the condition that reference is made to ECMWF. The information within this publication is given in good faith and considered to be true, but ECMWF accepts no liability for error, omission and for loss or damage arising from its use. Yield and accuracy of ADM-Aeolus wind measurements Abstract The European Space Agency’s ADM-Aeolus mission will for the first time provide wind profile measure- ments from space. In this study we carry out global simulations to predict the yield and accuracy of future ADM-Aeolus wind profile measurements, using realistic clouds and climatological aerosol distributions. Based on an assessment of wind analysis accuracy we argue that the main Aeolus impacts are to be expected (1) in the jet streams over the oceans, especially away from main air traffic routes, and in the African/Asian subtropical jet; (2) in the lower troposphere, e.g.
    [Show full text]
  • The European Space Agency
    THE EUROPEAN SPACE AGENCY UNITED SPACE IN EUROPE ESA facts and figures . Over 50 years of experience . 22 Member States . Eight sites/facilities in Europe, about 2300 staff . 5.75 billion Euro budget (2017) . Over 80 satellites designed, tested and operated in flight Slide 2 Purpose of ESA “To provide for and promote, for exclusively peaceful purposes, cooperation among European states in space research and technology and their space applications.” Article 2 of ESA Convention Slide 3 Member States ESA has 22 Member States: 20 states of the EU (AT, BE, CZ, DE, DK, EE, ES, FI, FR, IT, GR, HU, IE, LU, NL, PT, PL, RO, SE, UK) plus Norway and Switzerland. Seven other EU states have Cooperation Agreements with ESA: Bulgaria, Cyprus, Latvia, Lithuania, Malta and Slovakia. Discussions are ongoing with Croatia. Slovenia is an Associate Member. Canada takes part in some programmes under a long-standing Cooperation Agreement. Slide 4 Activities space science human spaceflight exploration ESA is one of the few space agencies in the world to combine responsibility in nearly all areas of space activity. earth observation launchers navigation * Space science is a Mandatory programme, all Member States contribute to it according to GNP. All other programmes are Optional, funded ‘a la carte’ by Participating States. operations technology telecommunications Slide 5 ESA’s locations Salmijaervi (Kiruna) Moscow Brussels ESTEC (Noordwijk) ECSAT (Harwell) EAC (Cologne) Washington Houston Maspalomas ESA HQ (Paris) ESOC (Darmstadt) Oberpfaffenhofen Santa Maria
    [Show full text]
  • Maria Cristina Falvella Strategic Perspectives and European Affairs Italian Space Agency
    Space activities in Italy: - National strategies and way forward Maria Cristina Falvella Strategic perspectives and European affairs Italian Space Agency Workshop on European Space Governance - Madrid , March 23° 2015 A long tradition in space activities o’40: The Italian Space Community began to organize itself o ‘50: Edoardo Amaldi and Luigi Broglio started the first aerospace projects o 1964: first Italian satellite into orbit from Wallops Island (USA) o 1966: the first Italian satellite launched from Italian equatorial Malindi Base (Kenya) Italian Space Agency : National History o 1963 - National Institute for Space Researches (IRS): the first formal space coordination activities o 1979 - first National Space Plan o 1988 - Institution of the Italian Space Agency (ASI) Italian Space Agency International History • Italy is a founding Member State of the UN-COPUOS 1959: Prof. Edoardo Amaldi proposes the institution of an European body for civil space research 1964: Italy is a founding Member State of • ELDO, European Launcher Development Organization • ESRO, European Space Research Organization 1975: Italy is a founding Member State of the European Space Agency (ESA) Italian Space Agency www.asi.it ASI is a public Agency, monitored by the Italian Ministry of Education, University and Research ASI Mission ■ Elaboration of national space strategies through the drafting of the National Space Plan ■ Promotion and financing of Scientific and Technological Space Research ■ Support of Space Education and Training of students and young professionals
    [Show full text]
  • 10. Spacecraft Configurations MAE 342 2016
    2/12/20 Spacecraft Configurations Space System Design, MAE 342, Princeton University Robert Stengel • Angular control approaches • Low-Earth-orbit configurations – Satellite buses – Nanosats/cubesats – Earth resources satellites – Atmospheric science and meteorology satellites – Navigation satellites – Communications satellites – Astronomy satellites – Military satellites – Tethered satellites • Lunar configurations • Deep-space configurations Copyright 2016 by Robert Stengel. All rights reserved. For educational use only. 1 http://www.princeton.edu/~stengel/MAE342.html 1 Angular Attitude of Satellite Configurations • Spinning satellites – Angular attitude maintained by gyroscopic moment • Randomly oriented satellites and magnetic coil – Angular attitude is free to vary – Axisymmetric distribution of mass, solar cells, and instruments Television Infrared Observation (TIROS-7) Orbital Satellite Carrying Amateur Radio (OSCAR-1) ESSA-2 TIROS “Cartwheel” 2 2 1 2/12/20 Attitude-Controlled Satellite Configurations • Dual-spin satellites • Attitude-controlled satellites – Angular attitude maintained by gyroscopic moment and thrusters – Angular attitude maintained by 3-axis control system – Axisymmetric distribution of mass and solar cells – Non-symmetric distribution of mass, solar cells – Instruments and antennas do not spin and instruments INTELSAT-IVA NOAA-17 3 3 LADEE Bus Modules Satellite Buses Standardization of common components for a variety of missions Modular Common Spacecraft Bus Lander Congiguration 4 4 2 2/12/20 Hine et al 5 5 Evolution
    [Show full text]
  • Reaping the Full Benefits of Copernicus After 2020 -The Ambitions of the European Space Industry
    Reaping the full benefits of Copernicus after 2020 -The ambitions of the European space industry- Key elements on the Copernicus programme Introduction: what Copernicus is Copernicus is a user-driven program and the result of a common ambition (EU, European Space Agency and the Member States) to build a European autonomous capacity in the field of earth observation, providing reliable, up-to-date, free, full and open information in six thematic areas (“services”): land monitoring, marine monitoring, atmospheric monitoring, climate change, emergency management and security. The programme is composed of a space (Sentinels & contributing missions), in-situ (ground- based, sea-borne or air-borne monitoring systems) and service component. Copernicus space segment: a long-term & complex infrastructure Initially deployed since 2014, the constellation of Sentinels consists of the following satellites1: Sentinel-1 All-weather, day and night radar imagery for land and ocean services Sentinel-2 High-resolution optical imagery for land services Sentinel-3 High-accuracy optical, radar and altimetry data for marine and land services Sentinel-4 and Data for atmospheric composition monitoring from geostationary Sentinel-5 orbit and polar orbit (instruments carried on the next generation of meteorological satellites, i.e Meteosat Third Generation (MTG) and MetOp Second Generation) Sentinel-5 Bridge the gap between Envisat (Sciamachy data in particular) and Precursor Sentinel-5 Sentinel-6 Radar altimetry data to measure global sea-surface height, primarily for operational oceanography and for climate studies Rationale for Copernicus continuation and evolution Users want “more Copernicus”! The intense use (> 120 000 registered users2) and increased awareness for the potential of Copernicus have generated great expectations for an evolved Copernicus system.
    [Show full text]