Space Activities 2018
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Issues Paper on Exploring Space Technologies for Sustainable Development and the Benefits of International Research Collaboration in This Context
United Nations Commission on Science and Technology for Development Inter-sessional Panel 2019-2020 7-8 November 2019 Geneva, Switzerland Issues Paper on Exploring space technologies for sustainable development and the benefits of international research collaboration in this context Draft Not to be cited Prepared by UNCTAD Secretariat1 18 October 2019 1 Contributions from the Governments of Austria, Belgium, Botswana, Brazil, Canada, Japan, Mexico, South Africa, Turkey, the United Kingdom, United States of America, as well as from the Economic and Social Commission for Asia and the Pacific, the Food and Agriculture Organization, the International Telecommunication Union, the United Nations Office for Disaster Risk Reduction and the World Food Programme are gratefully acknowledged. Contents Table of figures ....................................................................................................................................... 3 Table of boxes ......................................................................................................................................... 3 I. Introduction .................................................................................................................................... 4 II. Space technologies for the Sustainable Development Goals ......................................................... 5 1. Food security and agriculture ..................................................................................................... 5 2. Health applications .................................................................................................................... -
Electric Propulsion for Station Keeping and Electric Orbit Raising on Eutelsat Platforms
Electric Propulsion for Station Keeping and Electric Orbit Raising on Eutelsat Platforms 2015-b/IEPC-97 Presented at Joint Conference of 30th International Symposium on Space Technology and Science 34th International Electric Propulsion Conference and 6th Nano-satellite Symposium, Hyogo-Kobe, Japan July 4 – 10, 2015 C. Casaregola1 Eutelsat, Paris, 75015, France Abstract: With a fleet of 34 geostationary satellites and more than 30 years of service from space, Eutelsat is today Europe’s most long-standing satellite operator and one of the world’s leading satellite operators. The first two platforms using Electric Propulsion procured are SESAT-1 (EUTELSAT 16C) and KA-SAT, for which Electric Propulsion is limited to on-station operations. The successful demonstration of sustained capability of Electric Propulsion for these two platforms in addition to the extensive flight heritage with no significant anomalies demonstrated in the last decades on both commercial and scientific platforms, prove the high level of maturity reached by Electric Propulsion systems. Based on that and due to new attractive launch options, one full-electric platform - EUTELSAT 115 West B – has been procured and launched in March 2015. The launch of EUTELSAT 115 West B is a key milestone for telecom platforms as it makes Eutelsat the first Operator to use Electric Propulsion for a complete electric orbit raising. Two additional platforms – EUTELSAT 117 West B and EUTELSAT 172 B - are under procurement and will perform complete electric orbit raising as well. An overview of Eutelsat platforms using Electric Propulsion for station keeping and electric orbit raising is given in the paper. -
Douglas Missile & Space Systems Division
·, THE THOR HISTORY. MAY 1963 DOUGLAS REPORT SM-41860 APPROVED BY: W.H.. HOOPER CHIEF, THOR SYSTEMS ENGINEERING AEROSPACE SYSTEMS ENGINEERING DOUGLAS MISSILE & SPACE SYSTEMS DIVISION ABSTRACT This history is intended as a quick orientation source and as n ready-reference for review of the Thor and its sys tems. The report briefly states the development of Thor, sur'lli-:arizes and chronicles Thor missile and booster launch inGs, provides illustrations and descriptions of the vehicle systcn1s, relates their genealogy, explains sane of the per fon:iance capabilities of the Thor and Thor-based vehicles used, and focuses attention to the exploration of space by Douelas Aircraf't Company, Inc. (DAC). iii PREFACE The purpose of The Thor History is to survey the launch record of the Thor Weapon, Special Weapon, and Space Systems; give a systematic account of the major events; and review Thor's participation in the military and space programs of this nation. The period covered is from December 27, 1955, the date of the first contract award, through May, 1963. V �LE OF CONTENTS Page Contract'Award . • • • • • • • • • • • • • • • • • • • • • • • • • 1 Background • • • • • • • • • • • • • • • • • • • • • • • • • • • • l Basic Or�anization and Objectives • • • • • • • • • • • • • • • • 1 Basic Developmenta� Philosophy . • • • • • • • • • • • • • • • • • 2 Early Research and Development Launches • • • ·• • • • • • • • • • 4 Transition to ICBM with Space Capabilities--Multi-Stage Vehicles . 6 Initial Lunar and Space Probes ••••••• • • • • • • • -
OUFTI-1 Environmental Impact Assessment
Date: 11/02/2016 Issue: 1 Rev: 1 Page: 1 of 11 OUFTI-1 Environmental Impact Assessment Reference 3_OUF_ENV_IMPACT_1.0 Issue/Rev Issue 1 Rev 0 Date 11/02/2016 Distribution OUFTI-1 team OUFTI-1 Environmental Impact Assessment Date: 11/02/2016 Issue: 1 Rev: 1 Page: 2 of 11 AUTHORS Name Email Telephone X. Werner [email protected] +32 4 366 37 38 S. De Dijcker [email protected] +32 4 366 37 38 RECORD OF REVISIONS Iss/Rev Date Author Section/page Change description 1/0 11/02/2016 X.Werner, All Initial issue S. De Dijcker Copyright University of Liège [2016]. OUFTI-1 Environmental Impact Assessment Date: 11/02/2016 Issue: 1 Rev: 1 Page: 3 of 11 TABLE OF CONTENTS Authors ....................................................................................................................................... 2 Record of revisions ..................................................................................................................... 2 1. Activities and Objectives ................................................................................................... 4 1.1. Project description ....................................................................................................... 4 1.2. Soyuz launch vehicle ................................................................................................... 5 1.3. Arianespace ................................................................................................................. 7 1.4. Conclusion .................................................................................................................. -
Rafael Space Propulsion
Rafael Space Propulsion CATALOGUE A B C D E F G Proprietary Notice This document includes data proprietary to Rafael Ltd. and shall not be duplicated, used, or disclosed, in whole or in part, for any purpose without written authorization from Rafael Ltd. Rafael Space Propulsion INTRODUCTION AND OVERVIEW PART A: HERITAGE PART B: SATELLITE PROPULSION SYSTEMS PART C: PROPELLANT TANKS PART D: PROPULSION THRUSTERS Satellites Launchers PART E: PROPULSION SYSTEM VALVES PART F: SPACE PRODUCTION CAPABILITIES PART G: QUALITY MANAGEMENT CATALOGUE – Version 2 | 2019 Heritage PART A Heritage 0 Heritage PART A Rafael Introduction and Overview Rafael Advanced Defense Systems Ltd. designs, develops, manufactures and supplies a wide range of high-tech systems for air, land, sea and space applications. Rafael was established as part of the Ministry of Defense more than 70 years ago and was incorporated in 2002. Currently, 7% of its sales are re-invested in R&D. Rafael’s know-how is embedded in almost every operational Israel Defense Forces (IDF) system; the company has a special relationship with the IDF. Rafael has formed partnerships with companies with leading aerospace and defense companies worldwide to develop applications based on its proprietary technologies. Offset activities and industrial co-operations have been set-up with more than 20 countries world-wide. Over the last decade, international business activities have been steadily expanding across the globe, with Rafael acting as either prime-contractor or subcontractor, capitalizing on its strengths at both system and sub-system levels. Rafael’s highly skilled and dedicated workforce tackles complex projects, from initial development phases, through prototype, production and acceptance tests. -
Satellite Systems
Chapter 18 REST-OF-WORLD (ROW) SATELLITE SYSTEMS For the longest time, space exploration was an exclusive club comprised of only two members, the United States and the Former Soviet Union. That has now changed due to a number of factors, among the more dominant being economics, advanced and improved technologies and national imperatives. Today, the number of nations with space programs has risen to over 40 and will continue to grow as the costs of spacelift and technology continue to decrease. RUSSIAN SATELLITE SYSTEMS The satellite section of the Russian In the post-Soviet era, Russia contin- space program continues to be predomi- ues its efforts to improve both its military nantly government in character, with and commercial space capabilities. most satellites dedicated either to civil/ These enhancements encompass both military applications (such as communi- orbital assets and ground-based space cations and meteorology) or exclusive support facilities. Russia has done some military missions (such as reconnaissance restructuring of its operating principles and targeting). A large portion of the regarding space. While these efforts have Russian space program is kept running by attempted not to detract from space-based launch services, boosters and launch support to military missions, economic sites, paid for by foreign commercial issues and costs have lead to a lowering companies. of Russian space-based capabilities in The most obvious change in Russian both orbital assets and ground station space activity in recent years has been the capabilities. decrease in space launches and corre- The influence of Glasnost on Russia's sponding payloads. Many of these space programs has been significant, but launches are for foreign payloads, not public announcements regarding space Russian. -
UHD with Asiasat
UHD with AsiaSat Alan WONG Manager, Sales Solutions 23 Jun 2016 AsiaSat Proprietary & Confidential AsiaSat Proprietary & Confidential Contents • Brief Introduction of AsiaSat • Hands-on Satellite Transmission • Our Engagement with UHD • How we see UHD? • AsiaSat UHD Platform • Next Step AsiaSat Proprietary & Confidential UHD with AsiaSat 2 Brief Introduction of AsiaSat Our Background Our Satellite Fleet Our Facilities Our People AsiaSat Proprietary & Confidential AsiaSat Corporate Video AsiaSat Proprietary & Confidential UHD with AsiaSat 4 Our Background Head-quartered in Hong Kong Established in 1988 Listing in Hong Kong Stock Exchange Regional Satellite Operator • Asia’s leading satellite operator, aiming to provide highest quality satellite communications services in the region Coverage • Across 50 countries in Asia-Pacific • Reaching 2/3 of world's population Customer Profile • International and Regional TV Broadcasters • Telecommunications Service Providers • News Agencies • Corporations and Governments AsiaSat Proprietary & Confidential UHD with AsiaSat 5 Our Satellite Fleet C-band Ku-band For more details of our satellite fleet, please visit our web site (http://www.asiasat.com/technology/satellite-fleet). AsiaSat Proprietary & Confidential UHD with AsiaSat 6 Our Earth Stations Tai Po Earth Station Stanley Earth Station For more details of our facilities, please visit our web site (http://www.asiasat.com/aboutus/facilities). AsiaSat Proprietary & Confidential UHD with AsiaSat 7 Tai Po Earth Station AsiaSat Tai Po Earth Station is Antennas Services • 1x 1.3m (C) • Uplink Service located at the Tai Po Industrial • 2x 9.0m (C) • Downlink Service Estate in the New Territories, • 3x 7.3m (C) • Occasional Service Hong Kong. • 2x 6.3m (C) • Conditional Access • 1x 6.1m (C) Service • 4x 7.3m (Ku) • Compression Service • 2x 6.3m (Ku) • Playout Service The Station is a two level building • 1x 4.9m (Ku) • Monitoring Service of 5,551 sq.m. -
GB-ASTRA 3B-Comsatbw-21Mai V
A BOOST FOR SPACE COMMUNICATIONS SATELLITES For its first launch of the year, Arianespace will orbit two communications satellites: ASTRA 3B for the Luxembourg-based operator SES ASTRA, and COMSATBw-2 for Astrium as part of a contract with the German Ministry of Defense. The choice of Arianespace by leading space communications operators and manufacturers is clear international recognition of the company’s excellence in launch services. Because of its reliability and availability, the Arianespace launch system continues to set the global standard. Ariane 5 is the only commercial satellite launcher now on the market capable of simultaneously launching two payloads. Over the last two decades, Arianespace and SES have developed an exceptional relationship. ASTRA 3B will be the 33rd satellite from the SES group (Euronext Paris and Luxembourg Bourse: SESG) to have chosen the European launcher. SES ASTRA operates the leading direct-to-home TV broadcast system in Europe, serving more than 125 million households via DTH and cable networks. ASTRA 3B was built by Astrium using a Eurostar E 3000 platform, and will weigh approximately 5,500 kg at launch. Fitted with 60 active Ku-band transponders and four Ka-band transponders, ASTRA 3B will be positioned at 23.5 degrees East. It will deliver high-power broadcast services across all of Europe, and offers a design life of 15 years. Astrium chose Arianespace for the launch of two military communications satellites, COMSATBw-1 and COMSATBw-2, as part of a satellite communications system supplied to the German Ministry of Defense. The first satellite in this family, COMSATBw-1, was launched by Arianespace in October 2009. -
Design for Demise Analysis for Launch Vehicles
A first design for demise analysis for launch vehicles Henrik Simon, Stijn Lemmens Space debris: Inactive, manmade objects in space Source: ESA Overview Introduction Fundamentals Modelling approach Results and discussion Summary and outlook What is the motivation and task? INTRODUCTION Motivation . Mitigation: Prevention of creation and limitation of long-term presence . Guidelines: LEO removal within 25 years . LEO removal within 25 years after mission end . Casualty risk limit for re-entry: 1 in 10,000 Rising altitude Decay & re-entry above 2000 km Source: NASA Source: NASA Solution: Design for demise Source: ESA Scope of the thesis . Typical design of upper stages . General Risk assessment . Design for demise solutions to reduce the risk ? ? ? Risk A Risk B Risk C Source: CNES How do we assess the risk and simulate the re-entry? FUNDAMENTALS Fundamentals: Ground risk assessment Ah = + 2 Ai � ℎ = =1 � Source: NASA Source: NASA 3.5 m 5.0 m 2 2 ≈ ≈ Fundamentals: Re-entry simulation tools SCARAB: Spacecraft-oriented approach . CAD-like modelling . 6 DoF flight dynamics . Break-up / fragmentation computed How does a rocket upper stage look like? MODELLING Modelling approach . Research on typical design: . Elongated . Platform . Solid Rocket Motor . Lack of information: . Create common intersection . Deliberately stay top-level and only compare effects Modelling approach Modelling approach 12 Length [m] 9 7 5 3 2 150 300 500 700 800 1500 2200 Mass [kg] How much is the risk and how can we reduce it? SIMULATIONS Example of SCARAB re-entry simulation 6x Casualty risk of all reference cases Typical survivors Smaller Smaller fragments fragments Pressure tanks Pressure tanks Main tank Engine Main structure + tanks Design for Demise . -
1998 Year in Review
Associate Administrator for Commercial Space Transportation (AST) January 1999 COMMERCIAL SPACE TRANSPORTATION: 1998 YEAR IN REVIEW Cover Photo Credits (from left): International Launch Services (1998). Image is of the Atlas 2AS launch on June 18, 1998, from Cape Canaveral Air Station. It successfully orbited the Intelsat 805 communications satellite for Intelsat. Boeing Corporation (1998). Image is of the Delta 2 7920 launch on September 8, 1998, from Vandenberg Air Force Base. It successfully orbited five Iridium communications satellites for Iridium LLP. Lockheed Martin Corporation (1998). Image is of the Athena 2 awaiting its maiden launch on January 6, 1998, from Spaceport Florida. It successfully deployed the NASA Lunar Prospector. Orbital Sciences Corporation (1998). Image is of the Taurus 1 launch from Vandenberg Air Force Base on February 10, 1998. It successfully orbited the Geosat Follow-On 1 military remote sensing satellite for the Department of Defense, two Orbcomm satellites and the Celestis 2 funerary payload for Celestis Corporation. Orbital Sciences Corporation (1998). Image is of the Pegasus XL launch on December 5, 1998, from Vandenberg Air Force Base. It successfully orbited the Sub-millimeter Wave Astronomy Satellite for the Smithsonian Astrophysical Observatory. 1998 YEAR IN REVIEW INTRODUCTION INTRODUCTION In 1998, U.S. launch service providers conducted In addition, 1998 saw continuing demand for 22 launches licensed by the Federal Aviation launches to deploy the world’s first low Earth Administration (FAA), an increase of 29 percent orbit (LEO) communication systems. In 1998, over the 17 launches conducted in 1997. Of there were 17 commercial launches to LEO, 14 these 22, 17 were for commercial or international of which were for the Iridium, Globalstar, and customers, resulting in a 47 percent share of the Orbcomm LEO communications constellations. -
Small Satellite Launchers
SMALL SATELLITE LAUNCHERS NewSpace Index 2020/04/20 Current status and time from development start to the first successful or planned orbital launch NEWSPACE.IM Northrop Grumman Pegasus 1990 Scorpius Space Launch Demi-Sprite ? Makeyev OKB Shtil 1998 Interorbital Systems NEPTUNE N1 ? SpaceX Falcon 1e 2008 Interstellar Technologies Zero 2021 MT Aerospace MTA, WARR, Daneo ? Rocket Lab Electron 2017 Nammo North Star 2020 CTA VLM 2020 Acrux Montenegro ? Frontier Astronautics ? ? Earth to Sky ? 2021 Zero 2 Infinity Bloostar ? CASIC / ExPace Kuaizhou-1A (Fei Tian 1) 2017 SpaceLS Prometheus-1 ? MISHAAL Aerospace M-OV ? CONAE Tronador II 2020 TLON Space Aventura I ? Rocketcrafters Intrepid-1 2020 ARCA Space Haas 2CA ? Aerojet Rocketdyne SPARK / Super Strypi 2015 Generation Orbit GoLauncher 2 ? PLD Space Miura 5 (Arion 2) 2021 Swiss Space Systems SOAR 2018 Heliaq ALV-2 ? Gilmour Space Eris-S 2021 Roketsan UFS 2023 Independence-X DNLV 2021 Beyond Earth ? ? Bagaveev Corporation Bagaveev ? Open Space Orbital Neutrino I ? LIA Aerospace Procyon 2026 JAXA SS-520-4 2017 Swedish Space Corporation Rainbow 2021 SpinLaunch ? 2022 Pipeline2Space ? ? Perigee Blue Whale 2020 Link Space New Line 1 2021 Lin Industrial Taymyr-1A ? Leaf Space Primo ? Firefly 2020 Exos Aerospace Jaguar ? Cubecab Cab-3A 2022 Celestia Aerospace Space Arrow CM ? bluShift Aerospace Red Dwarf 2022 Black Arrow Black Arrow 2 ? Tranquility Aerospace Devon Two ? Masterra Space MINSAT-2000 2021 LEO Launcher & Logistics ? ? ISRO SSLV (PSLV Light) 2020 Wagner Industries Konshu ? VSAT ? ? VALT -
1 Before the Federal Communications Commission Washington, D.C
Federal Communications Commission DA 06-4 Before the Federal Communications Commission Washington, D.C. 20554 In the Matter of ) ) AFRISPACE, INC. ) IB File No. SAT-LOA-20050311- ) 00061 Application for Authority to Launch and ) Operate a Replacement Satellite, AfriStar-2, ) Call Sign: S2666 at 21° E.L. and to Co-locate It with AfriStar-1 ) ) ORDER AND AUTHORIZATION Adopted: January 03, 2006 Released: January 03, 2006 By the Chief, International Bureau: I. INTRODUCTION 1. By this Order, we authorize AfriSpace, Inc. (AfriSpace)1 to launch and operate the AfriStar-2 satellite in the geostationary-satellite orbit (GSO) at the 21° East Longitude (E.L.) orbital location. AfriStar-2 is controlled from the United States and is capable of providing Broadcasting-Satellite Service (sound) (BSS (sound)) to Africa and Europe on a non-common carrier basis. We authorize AfriStar-2 to operate downlinks within 2.6 megahertz of spectrum in each polarization with a center frequency of 1479.5 MHz. We also authorize AfriSpace to utilize feeder links and telecommand links for the AfriStar-2 satellite in the 7025-7075 MHz frequency band, to operate its telemetry link for the AfriStar-2 satellite at a center frequency of 1491.7 MHz, and to co-locate the AfriStar-2 satellite at 21° E.L. with the AfriStar-1 satellite currently in orbit. In addition, we grant AfriSpace a waiver of the Commission’s rule regarding transponder saturation flux densities for the AfriStar-2 satellite.2 These authorizations give AfriSpace the capability to continue to provide service to existing customers despite unanticipated technical difficulties experienced by the AfriStar-1 satellite and to serve new customers, conditioned on AfriSpace complying with the applicable laws, regulations, rules, and licensing procedures of any countries it proposes to serve.