DOCSLIB.ORG

THINK LOGISTICS – SPACE LOGISTICS ! Florian Loire Strategy for Civil Launchers

Total Page：16

File Type：pdf, Size：1020Kb

Download full-text PDF Read full-text
THINK LOGISTICS – SPACE LOGISTICS ! Florian Loire Strategy for Civil Launchers THINK LOGISTICS – SPACE LOGISTICS ! Florian Loire Strategy for civil launchers Space School - 25 June 2019 #spaceenablers 1 DISRUPTION IN THE SPACE MARKET COMPETITIVE LANDSCAPE THIS DOCUMENT AND ITS CONTENTS ARE PROPERTY OF ARIANEGROUP. IT SHALL NOT BE COMMUNICATED TO ANY THIRD PARTY WITHOUT THE OWNER’S WRITTEN CONSENT | ARIANEGROUP SAS – ALL RIGHTS RESERVED. SPACE LOGISTICS @ ESTACA - 25/06/2019 Existing Space Economy has real economic value to society Science & Meteorology …. Exploration Navigation/Positioning Earth Observation Telecommunications THIS DOCUMENT AND ITS CONTENTS ARE PROPERTY OF ARIANEGROUP. IT SHALL NOT BE COMMUNICATED TO ANY THIRD PARTY WITHOUT THE OWNER’S WRITTEN CONSENT | ARIANEGROUP SAS – ALL RIGHTS RESERVED. #space- enablers THE GOOD OLD DAYS: A FEW WELL SEGMENTED LAUNCH SERVICE MARKET SEGMENTS THIS DOCUMENT AND ITS CONTENTS ARE PROPERTY OF ARIANEGROUP. IT SHALL NOT BE COMMUNICATED TO ANY THIRD PARTY WITHOUT THE OWNER’S SPACE LOGISTICS @ ESTACA 07/12/2018 WRITTEN CONSENT | ARIANEGROUP SAS – ALL RIGHTS RESERVED. - ARIANE 5 THE EUROPEAN WORKHORSE WITH 104 LAUNCHES PERFORMED ARIANE 5 ES Fairing ARIANE 5 ECA Height: 17 m Launch weight: 760 t Ø 5.4 m Launch weight: 780 t Thrust: 1,340 t Thrust: 1,340 t Dual Launch System (SYLDA) Ø 4 m useful Last HM7B engine Still the Thrust: 6.5 t mission in benchmark 2018 Reignitable Aestus engine for GTO Thrust: 2.7 t missions 2 boosters Vulcain 2 engine Thrust: 136 t * All references to tons (t) are metric tons throughout THIS DOCUMENT AND ITS CONTENTS ARE PROPERTY OF ARIANEGROUP. IT SHALL NOT BE COMMUNICATED TO ANY THIRD PARTY WITHOUT THE OWNER’S WRITTEN CONSENT | ARIANEGROUP SASGMBH – ALL– ALL RIGHTS RIGHTS RESERVED. RESERVED. - 25/06/2019 REVOLUTION: LEO SMALLSATS CONSTELLATIONS THIS DOCUMENT AND ITS CONTENTS ARE PROPERTY OF ARIANEGROUP. IT SHALL NOT BE COMMUNICATED TO ANY THIRD PARTY WITHOUT THE OWNER’S WRITTEN CONSENT | ARIANEGROUP SAS – ALL RIGHTS RESERVED. SPACE LOGISTICS @ ESTACA - Source: bloomberg.com REVOLUTION: GEO SMALLSATS THIS DOCUMENT AND ITS CONTENTS ARE PROPERTY OF ARIANEGROUP. IT SHALL NOT BE COMMUNICATED TO ANY THIRD PARTY WITHOUT THE OWNER’S WRITTEN CONSENT | ARIANEGROUP SAS – ALL RIGHTS RESERVED. - Source: www.astranis.com REVOLUTION: IN ORBIT SERVICING Source: ESA.blog.int Source: Effective Space Solution THIS DOCUMENT AND ITS CONTENTS ARE PROPERTY OF ARIANEGROUP. IT SHALL NOT BE COMMUNICATED TO ANY THIRD PARTY WITHOUT THE OWNER’S WRITTEN CONSENT | ARIANEGROUP SAS – ALL RIGHTS RESERVED. SPACE LOGISTICS @ ESTACA - Institutional market complemented with Digital Economy financing …. New business models What Disruption is taking place? High Tech Industry Industrial optimization Geopolitical environment Acceleration of Innovation Cycles National interests of contributing nations New work methodologies Sovereignty and strategic / military interests (digitalization, Agile…) …. THIS DOCUMENT AND ITS CONTENTS ARE PROPERTY OF ARIANEGROUP. IT SHALL NOT BE COMMUNICATED TO ANY THIRD PARTY WITHOUT THE OWNER’S WRITTEN CONSENT | ARIANEGROUP SAS – ALL RIGHTS RESERVED. - QUICK EVOLUTION OF COMPETITIVE LANDSCAPE 1st launch Domestic competition 1st launch st in 2018 1 launch in 2017 MEDIUM / HEAVY LAUNCHERS in 2016 2021 Ariane 5 Soyuz Proton Falcon 9 Atlas V H-II Long March-3 GSLV Mk.II Ariane 6 Falcon Heavy New Glenn Vulcan OmegA Starship Angara H-III Soyuz 5 Long March-5 GSLV Mk.III Falcon 9 A5 Block 5 1st launch in 1st launch 2015 et 2016 SMALL LAUNCHERS in 2016 1st launch in 2018 Vega PSLV Dnepr Minotaur-C Rockot Long March-2 Soyuz-1 Vega C PSLV Angara 1.2 Cyclone 4M Epsilon 2 Long March- 6 & 7 Electron LauncherOne Vector Alpha TODAY TOMORROW THIS DOCUMENT AND ITS CONTENTS ARE PROPERTY OF ARIANEGROUP. IT SHALL NOT BE COMMUNICATED TO ANY THIRD PARTY WITHOUT THE OWNER’S WRITTEN CONSENT | ARIANEGROUP SAS – ALL RIGHTS RESERVED. - 25/06/2019 2 TOWARDS SPACE LOGISTICS SERVICES THIS DOCUMENT AND ITS CONTENTS ARE PROPERTY OF ARIANEGROUP. IT SHALL NOT BE COMMUNICATED TO ANY THIRD PARTY WITHOUT THE OWNER’S WRITTEN CONSENT | ARIANEGROUP SAS – ALL RIGHTS RESERVED. - 25/06/2019 SPACE LOGISTICS CONCEPT ADAPTING END-TO-END TRANSPORTATION SERVICE TO CLIENT NEEDS Defining the nodes and flows of the space transportation network (Constellation) Satellite GEO Satellite Asteroids Mars Earth Sub-orbital/ HAPS Space Station(s) Moon To transport: For activities on nodes Enabling growth in market segments • Micro/small to large satellites Navigation Telecom Earth Observation • Cargo / payloads • Humans Safety & Security Human flight + cargo Science • Raw materials • Fuels Space Production Mining • … THIS DOCUMENT AND ITS CONTENTS ARE PROPERTY OF ARIANEGROUP. IT SHALL NOT BE COMMUNICATED TO ANY THIRD PARTY WITHOUT THE OWNER’S WRITTEN CONSENT | ARIANEGROUP SAS – ALL RIGHTS RESERVED. - 25/06/2019 THE DRIVERS FOR SPACE ECONOMY A (very) profitable business prospect Conventional Futuristic Conventional commercial customers Futuristic visions of scalability • Telecom broadcast • “Millions of people working and living in space” (Blue Origin) • Broadband • “Making life multi-planetary” (SpaceX) • Earth observation • “Moon Village” (ESA) • … • “Space belongs to everyone” (PTScientists) • “There are $20 trillion checks up there to be cashed” (Planetary Resources) Institutional enablers / customers • “The addressable market could be as large as $37 billion” (NASA, DoD, EC, ESA, CNES, DLR, …) (Bigelow) Enabled through cash available for investment • Customer contracts • Company investments Public Private • R&D contracts / Grants (institutional, • Private fortune Partnerships conventional commercial) • Equity raises through venture capital THIS DOCUMENT AND ITS CONTENTS ARE PROPERTY OF ARIANEGROUP. IT SHALL NOT BE COMMUNICATED TO ANY THIRD PARTY WITHOUT THE OWNER’S WRITTEN CONSENT | ARIANEGROUP SAS – ALL RIGHTS RESERVED. - 25/06/2019 What is our European answer ? Enabling Space Economy Identification of minimum bricks for an efficient transport service Simplification for customer by offering end-to-end service Increasing addressable market by offering extra service capabilities for increased societal return THIS DOCUMENT AND ITS CONTENTS ARE PROPERTY OF ARIANEGROUP. IT SHALL NOT BE COMMUNICATED TO ANY THIRD PARTY WITHOUT THE OWNER’S WRITTEN CONSENT | ARIANEGROUP SAS – ALL RIGHTS RESERVED. - ARIANE 6 UNPRECEDENTED FLEXIBILITY, MODULARITY AND COMPETITIVENESS Fairing ARIANE 62 Height: 14 or 20 m ARIANE 64 (2 BOOSTERS) Ø 5.4 m (4 BOOSTERS) Performance: Dual launch system Performance: 4.5-5 t GTO Ø 4.5 m useful 12 t* GTO Launch weight: 530 t* Launch weight: 860 t Thrust: 816 t Reignitable Vinci engine Thrust: 1,530 t Thrust: 18 t 2 or 4 P120C boosters (common with Vega C) Thrust: 459 t Vulcain 2.1 engine Thrust: 140 t * All references to tons (t) are metric tons throughout THIS DOCUMENT AND ITS CONTENTS ARE PROPERTY OF ARIANEGROUP. IT SHALL NOT BE COMMUNICATED TO ANY THIRD PARTY WITHOUT THE OWNER’S WRITTEN CONSENT | ARIANEGROUP SASGMBH – ALL– ALL RIGHTS RIGHTS RESERVED. RESERVED. - 25/06/2019 ARIANE 6 ALL COMMERCIAL AND INSTITUTIONAL MISSIONS ARIANE 64 PERFORMANCE MEO LEO 20 t GTO 12 t SSO THIS DOCUMENT AND ITS CONTENTS ARE PROPERTY OF ARIANEGROUP. IT SHALL NOT BE COMMUNICATED TO ANY THIRD PARTY WITHOUT THE OWNER’S WRITTEN CONSENT | ARIANEGROUP SASGMBH – ALL– ALL RIGHTS RIGHTS RESERVED. RESERVED. - 25/06/2019 LAUNCHERS ARE THE FIRST KEY ENABLER FOR SPACE LOGISTICS A competitive and continuously improving launcher Development of alternative vs launch vehicles targeting the same family is the first key building block timeframe ICARUS new lightweight upper stage (by 2025) Vega-C 2020 Ariane 6 maiden flight 2020 maiden flight FOC 2023 Prometheus THIS DOCUMENT AND ITS CONTENTS ARE PROPERTY OF ARIANEGROUP. IT SHALL NOT BE COMMUNICATED TO ANY THIRD PARTY WITHOUT THE OWNER’S WRITTEN CONSENT | ARIANEGROUP SAS – ALL RIGHTS RESERVED. - 25/06/2019 MISSION VERSATILITY IS KEY COMPETITIVE ADVANTAGE A family of innovative dispensers and future AG kickstage to answer several market needs and improve Ariane 6 market capture Multi-payload for GTO and M/LEO constellation GEO dispatching • Dual launch towards GTO • Deploying (big) constellations • Transportation of stack of small • Replenishing in multiple planes sats to GEO • Galileo 1st and 2nd generation Dispenser(s) MLS Rideshare • A regular piggyback Launch Service for light Satellites Enabling complex and long • Offering affordable tickets to any duration missions Orbit, to all segments of the light Satellites market • From the spare capacity of the • Exploration (lunar and cargo) Launcher, after the primary Kick Stage(s) • Large Science missions A62 A64 passenger mission THIS DOCUMENT AND ITS CONTENTS ARE PROPERTY OF ARIANEGROUP. IT SHALL NOT BE COMMUNICATED TO ANY THIRD PARTY WITHOUT THE OWNER’S WRITTEN CONSENT | ARIANEGROUP SAS – ALL RIGHTS RESERVED. - 25/06/2019 18 LUNAR EXPLORATION Total Government Investment Global interest converging towards 2013-2017 2018-2022 2023-2027 the Moon $67B $81B $93B 2017 $15B (74% from US ) 2008-2017 -> 6 Mars missions 53% 25% 10% 9% 3% transportation orbital Mars other deep Moon 2018-2027 -> Mars missions 10 infrastructure exploration space exploration exploration 44% 26% 14% 9% 7% 2008-2017 -> 8 Lunar missions transportation orbital Moon other deep Mars infrastructure exploration space exploration exploration 2018-2027 -> 50 Lunar missions 2027 $20B (64% from US ) Lunar Surface End-to-End Services (ISRU) Ariane 6 + Lander + ~300kg A flagship missions for Europe, payload transportation to the by Europe, for strategic lunar
Load more

Recommended publications
  • Call for M5 Missions
    ESA UNCLASSIFIED - For Official Use M5 Call - Technical Annex Prepared by SCI-F Reference ESA-SCI-F-ESTEC-TN-2016-002 Issue 1 Revision 0 Date of Issue 25/04/2016 Status Issued Document Type Distribution ESA UNCLASSIFIED - For Official Use Table of contents: 1 Introduction .......................................................................................................................... 3 1.1 Scope of document ................................................................................................................................................................ 3 1.2 Reference documents .......................................................................................................................................................... 3 1.3 List of acronyms ..................................................................................................................................................................... 3 2 General Guidelines ................................................................................................................ 6 3 Analysis of some potential mission profiles ........................................................................... 7 3.1 Introduction ............................................................................................................................................................................. 7 3.2 Current European launchers ...........................................................................................................................................
    [Show full text]
  • PRESS RELEASE Safran Appointments
    PRESS RELEASE Safran appointments June 28, 2021 Two appointments to Safran's Executive Committee Effective July 1, 2021, Stéphane Cueille is named CEO of Safran Electrical & Power. He takes over from Alain Sauret, who is retiring. Olivier Andriès, CEO of Safran, said, “I would like to sincerely thank Alain Sauret, who joined the Group almost 40 years ago at our legacy company, Labinal. He went on to transform the company into a world-class center of electrical system excellence. Safran Electrical & Power is today a cornerstone of our decarbonized aviation roadmap.” Holding the rank of Ingénieur de l’Armement (defense scientist), Stéphane Cueille was seconded to Snecma1 from 1998 to 2001 to work on ceramic matrix composites (CMC). He returned to the French defense procurement agency DGA in 2001, taking various management positions in the aircraft propulsion sector. In 2005 he was placed in charge of the Missiles-Space unit in the industrial affairs department (S2IE). In 2008, he returned to Snecma, starting in the turbine blade quality department at the Gennevilliers plant. He was subsequently named repair general manager in Snecma’s Military Engine division, then director of the turbine blade center of excellence. / Safran Mereis / Capa/ Safran/ MereisCapa/ Safran / In May 2013 he was appointed Managing Director of Aircelle Ltd, the UK subsidiary of Aircelle2 based in Burnley. In January 2015 he was named head of Safran Tech, the Stéphanie Group's Research & Technology (R&T) center, and then in 2016 was appointed Senior Executive Vice President R&T and Christophe Innovation, also becoming a member of the Safran Executive © Committee.
    [Show full text]
  • 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 ••••••• • • • • • • •
    [Show full text]
  • PRESS-KIT-VV19-08122021-EN.Pdf
    www.arianespace.com www.avio.com www.avio Arianespace’s seventh launch of 2021 with the second Vega of the year will place its satellite passengers into Sun-synchronous orbit. The launcher will be carrying a total payload of approximately 1 029 kg. The launch will be performed in Kourou, French Guiana. MISSION DESCRIPTION 2 PLÉIADES NEO 4 SATELLITE 3 Liftoff is planned on at exactly: FOUR AUXILIARY PAYLOADS 4 - 5 09:47 p.m. Washington, D.C. time, 10:47 p.m. Kourou time, VEGA LAUNCHER 6 01:47 a.m. Universal time (UTC), August 17, LAUNCH CAMPAIGN 7 03:47 a.m. Paris time, August 17, 10:47 a.m. Tokyo time, August 17. FLIGHT SEQUENCES 7 STAKEHOLDERS OF A LAUNCH 8 The nominal duration of the mission (from liftoff to separation of the satellites) is: 1 hour, 44 minutes and 59 seconds. Satellite: Pléiades Neo 4 Customer: Airbus Defence and Space - Intelligence Satellites: Four auxiliary payloads Cyrielle BOUJU [email protected] +33 (0)6 32 65 97 48 For Pléiades Neo For the four auxiliary payloads Francesco DE LORENZO • Perigee altitude: 614 km • Perigee altitude: 540 km [email protected] • Apogee altitude: 625 km • Apogee altitude: 554 km + 39 (0)6 97285317 • Inclination : 97.89 degrees • Inclination : 97.55 degrees First Pléiades Neo constellation satellites have been achieved within only five years, thanks to the hard work of over 500 people, across seven sites in Europe, to deliver first-class 14 km swath imagery at 30 cm native resolution, capable to daily collect up to 2 million km² and image the entire Earth landmass five times per year.
    [Show full text]
  • Ariane 5 Second Launch of 2020 Is a Success
    Ariane 5 Second Launch of 2020 is a Success Kourou, February 18, 2020 For its second launch of the year, Ariane 5, placed two telecommunications satellites in orbit: JCSAT-17 for SKY Perfect JSAT Corporation and GEO- KOMPSAT-2B for the Korea Aerospace Research Institute (KARI) This was the 252nd launch for Ariane, which marked its 40th anniversary on December 24, 2019 Nine more Ariane 5 launches are scheduled up to 2023 For its second launch of the year from the European Spaceport in Kourou, French Guiana, the Ariane 5 launcher placed two telecommunications satellites in geostationary transfer orbit (GTO): the JCSAT-17 satellite for SKY Perfect JSAT Corporation and the GEO-KOMPSAT-2B satellite for the Korea Aerospace Research Institute (KARI). The total performance required of the launcher was 10109kg; including 9236 kg for the two satellites which were injected into an orbit inclined 6° to the equator. “2020 has only just begun and Ariane 5 has achieved its second success in two months. With Ariane 6’s maiden flight planned for this year, nine more Ariane 5 launches are scheduled to fly up to 2023. This will ensure smooth transition between the two launchers, offering the same level of reliability, but with increased payload capacity,” said André-Hubert Roussel, CEO of ArianeGroup. “I want to thank all the teams at ArianeGroup and those of our subsidiary and launch operator Arianespace, as well as those of all our industrial partners, for their commitment. Their expertise and their talent have guaranteed the permanent success of the Ariane launchers over 40 years and will continue to do so in the years to come.
    [Show full text]
  • ESPA Ring Datasheet
    PAYLOAD ADAPTERS | ESPA ESPA THE EVOLVED SECONDARY PAYLOAD ADAPTER ESPA mounts to the standard NSSL (formerly EELV) interface bolt pattern (Atlas V, Falcon 9, Delta IV, OmegA, Vulcan, Courtesy of Lockheed Martin New Glenn) and is a drop-in component in the launch stack. Small payloads mount to ESPA ports featuring either a Ø15-inch bolt circle with 24 fasteners or a 4-point mount with pads at each corner of a 15-inch square; both of these interfaces have become small satellite standards. ESPA is qualified to carry 567 lbs (257 kg), and a Heavy interface Courtesy of NASA (with Ø5/16” fastener hardware) has been introduced with a capacity of 991 lbs (450 kg). All small satellite mass capabilities require the center of gravity (CG) to be within 20 inches (50.8 cm) of the ESPA port surface. Alternative configurations can be accommodated. ESPA GRANDE ESPA Grande is a more capable version of ESPA with Ø24-inch ports; the ring height is typically 42 inches. The Ø24-inch port has been qualified by test to Courtesy of ORBCOMM & Sierra Nevada Corp. carry small satellites up to 1543 lb (700 kg). ESPA ESPA IS ADAPTABLE TO UNIQUE MISSION REQUIREMENTS • The Air Force’s STP-1 mission delivered multiple small satellites on an Atlas V. • NASA’s Lunar Crater Observation and Sensing Satellite (LCROSS): ESPA was the spacecraft hub for the LCROSS shepherding satellite in 2009. • ORBCOMM Generation 2 (OG2) launched stacks of two and three ESPA Grandes on two different Falcon 9 missions and in total deployed 17 satellites.
    [Show full text]
  • Orbital Fueling Architectures Leveraging Commercial Launch Vehicles for More Affordable Human Exploration
    ORBITAL FUELING ARCHITECTURES LEVERAGING COMMERCIAL LAUNCH VEHICLES FOR MORE AFFORDABLE HUMAN EXPLORATION by DANIEL J TIFFIN Submitted in partial fulfillment of the requirements for the degree of: Master of Science Department of Mechanical and Aerospace Engineering CASE WESTERN RESERVE UNIVERSITY January, 2020 CASE WESTERN RESERVE UNIVERSITY SCHOOL OF GRADUATE STUDIES We hereby approve the thesis of DANIEL JOSEPH TIFFIN Candidate for the degree of Master of Science*. Committee Chair Paul Barnhart, PhD Committee Member Sunniva Collins, PhD Committee Member Yasuhiro Kamotani, PhD Date of Defense 21 November, 2019 *We also certify that written approval has been obtained for any proprietary material contained therein. 2 Table of Contents List of Tables................................................................................................................... 5 List of Figures ................................................................................................................. 6 List of Abbreviations ....................................................................................................... 8 1. Introduction and Background.................................................................................. 14 1.1 Human Exploration Campaigns ....................................................................... 21 1.1.1. Previous Mars Architectures ..................................................................... 21 1.1.2. Latest Mars Architecture .........................................................................
    [Show full text]
  • Hi-Rel Solutions for Space Launch Vehicles a Single Network for All
    © Airbus Safran Launchers 2016 © A Single Network for All Data Traffic Hi-Rel Solutions for Space Launch Vehicles www.tttech.com/space We are delighted that our network solution based on Deterministic Ethernet is providing a very powerful platform “ simplifying the electronic architectures of launch vehicles worldwide! Georg Kopetz, Member of the Executive Board, TTTech Computertechnik AG ” Over the last 25 years, space launch vehicle designs have utilized several different solutions for their on-board data handling. For the safety-critical command and control data, the very robust MIL-1553 bus served as a standard solution, originally designed as a military avionic data bus. For redundancy purposes, this widespread standard enforces two MIL-1553 buses running in parallel. This fact creates the first challenge, namely managing redundant fieldbuses in software and in parallel separate channels for additional data, e.g. telemetry. The second challenge arises from increasing data rates: MIL-1553 is limited to 1 Mbit/s, while there actually is both a need for higher control data rates and an interest in new types of sensors like video cameras. Adding more field buses would be possible, but would increase both weight and software complexity as well as qualification efforts. Finally, despite the need for higher bandwidth and a simplified network, no system cost increase can be tolerated, as in recent years the market for launch vehicles has become extremely competitive. This has led launch vehicle manufacturers worldwide to look for automotive or industrial solutions in order to reduce the cost of the electronics used throughout their vehicles. © Airbus Safran Launchers 2015 After several years of research funded by the ► French space agency (CNES) and afterwards by PROJECT ▼ the European Space Agency (ESA), architectures Launcher avionics A GLANCE AT based on TTEthernet are considered a great fit ► CHALLENGE for launch vehicles.
    [Show full text]
  • Space Coast Is Getting Busy: 6 New Rockets Coming to Cape Canaveral, KSC
    4/16/2019 Space Coast is getting busy: 6 new rockets coming to Cape Canaveral, KSC Space Coast is getting busy: 6 new rockets coming to Cape Canaveral, Kennedy Space Center Emre Kelly, Florida Today Published 4:04 p.m. ET April 11, 2019 | Updated 7:53 a.m. ET April 12, 2019 COLORADO SPRINGS, Colo. – If schedules hold, the Space Coast will live up to its name over the next two years as a half-dozen new rockets target launches from sites peppered across the Eastern Range. Company, government and military officials here at the 35th Space Symposium, an annual space conference, have reaffirmed their plans to launch rockets ranging from more traditional heavy-lift behemoths to smaller vehicles that take advantage of new manufacturing technologies. Even if some of these schedules slip, at least one thing is apparent to several spaceflight experts here: The Eastern Range is seeing an unprecedented growth in commercial space companies and efforts. Space Launch System: 2020 NASA's Space Launch System rocket launches from Kennedy Space Center's pad 39B in this rendering by the agency. (Photo: NASA) NASA's long-awaited SLS, a multibillion-dollar rocket announced in 2011, is slated to become the most powerful launch vehicle in history if it can meet a stringent late 2020 deadline. The 322-foot-tall rocket is expected to launch on its first flight – Exploration Mission 1 – from Kennedy Space Center with an uncrewed Orion capsule for a mission around the moon, which fits in with the agency's wider goal of putting humans on the surface by 2024.
    [Show full text]
  • Igor AFANASYEV, Dmitry VORONTSOV Cosmonautics | Event
    cosmonautics | event Andrey Morgunov Igor AFANASYEV, Dmitry VORONTSOV AANGARA’SNGARA’S FFIRSTIRST BBLASTOFFLASTOFF At 16.04 hrs Moscow time on 9 July 2014, the Plesetsk space launch centre saw the launching facility in February 2014 to the first launch of the Angara-1.2PP launch vehicle of the advanced space rocket practice its fuelling and the nose fairing was family being developed by the Khrunichev state space research and production fitted on the rocket in March. The successful ground tests were followed by the prelaunch centre. The maiden blastoff conducted as part of the Angara flight test programme preparations. was aimed at testing the solutions embodied in the design of the URM-1 and URM-2 The date of the launch was put off for versatile rocket modules and the Angara’s launch and technical facilities as well. 27 June 2014 due to extra checks required. In this connection, orbiting an actual spacecraft had not been considered, with On 9 June, Khrunichev hosted a session of an inseparable full-scale mock-up used as payload. The flight was suborbital to the Chief Designers Council, dedicated to prevent cluttering near-Earth orbit with space junk. the preparation of the Angara to its flight tests. The session pronounced the rocket fit To say the Angara’s first launch had been In spite of the hurdles, the developer, for the trials. anticipated for a long time would be an nevertheless, got in the stretch with the Angara The LV had been taken out of the assembly understatement: it was slated for 2005 under programme.
    [Show full text]
  • Omega-3 Fatty Acids Fact Sheet for Consumers
    Omega-3 Fatty Acids Fact Sheet for Consumers What are omega-3 fatty acids and what do they do? Omega-3 fatty acids are found in foods, such as fish and flaxseed, and in dietary supplements, such as fish oil. The three main omega-3 fatty acids are alpha-linolenic acid (ALA), eicosapentaenoic acid (EPA), and docosahexaenoic acid (DHA). ALA is found mainly in plant oils such as flaxseed, soybean, and canola oils. DHA and EPA are found in fish and other seafood. ALA is an essential fatty acid, meaning that your body can’t make it, so you must get it from the foods and beverages you consume. Your body can convert some ALA into EPA and then to DHA, but only in very small amounts. Therefore, getting EPA and DHA from foods (and dietary supplements if you take them) is the only practical way to increase levels of these omega-3 fatty acids in your body. Omega-3s are important components of the membranes that surround each cell in your body. DHA levels are especially high in retina (eye), brain, and sperm cells. Omega-3s also provide calories to give your body energy and have many functions in your heart, blood vessels, lungs, immune system, and endocrine system (the network of hormone-producing glands). How much omega-3s do I need? Omega-3s are found in foods Experts have not established recommended amounts for omega-3 fatty acids, except such as fatty fish and plant oils. for ALA. Average daily recommended amounts for ALA are listed below in grams (g).
    [Show full text]
  • The European Launchers Between Commerce and Geopolitics
    The European Launchers between Commerce and Geopolitics Report 56 March 2016 Marco Aliberti Matteo Tugnoli Short title: ESPI Report 56 ISSN: 2218-0931 (print), 2076-6688 (online) Published in March 2016 Editor and publisher: European Space Policy Institute, ESPI Schwarzenbergplatz 6 • 1030 Vienna • Austria http://www.espi.or.at Tel. +43 1 7181118-0; Fax -99 Rights reserved – No part of this report may be reproduced or transmitted in any form or for any purpose with- out permission from ESPI. Citations and extracts to be published by other means are subject to mentioning “Source: ESPI Report 56; March 2016. All rights reserved” and sample transmission to ESPI before publishing. ESPI is not responsible for any losses, injury or damage caused to any person or property (including under contract, by negligence, product liability or otherwise) whether they may be direct or indirect, special, inciden- tal or consequential, resulting from the information contained in this publication. Design: Panthera.cc ESPI Report 56 2 March 2016 The European Launchers between Commerce and Geopolitics Table of Contents Executive Summary 5 1. Introduction 10 1.1 Access to Space at the Nexus of Commerce and Geopolitics 10 1.2 Objectives of the Report 12 1.3 Methodology and Structure 12 2. Access to Space in Europe 14 2.1 European Launchers: from Political Autonomy to Market Dominance 14 2.1.1 The Quest for European Independent Access to Space 14 2.1.3 European Launchers: the Current Family 16 2.1.3 The Working System: Launcher Strategy, Development and Exploitation 19 2.2 Preparing for the Future: the 2014 ESA Ministerial Council 22 2.2.1 The Path to the Ministerial 22 2.2.2 A Look at Europe’s Future Launchers and Infrastructure 26 2.2.3 A Revolution in Governance 30 3.
    [Show full text]