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INTRODUCTION to the WORKSHOP Dr. G. Ortega 2021, May 11Th
INTRODUCTION to the WORKSHOP Dr. G. Ortega 2021, May 11th ESA UNCLASSIFIED - For Official Use 1 …the process of technology 1 I have a great idea! 2 I write a proposal 3 My proposal is approved 4 I execute the activity of the proposal 2 Welcome ! •Original idea of the TEC-MPA Section of ESA and materialized in 2021 •Is there any interest on Will the idea of the discussion ideas for technology pre-discussions work? prior we make any kind of proposal? •Number of registrations: 161 3 Objectives • Objective 1: Provide for an overview of the current state of technology ideas • Objective 2: Gather inputs from possible Bidders • Objective 3: Prioritize the upcoming research and development inputs to the ESA technology plans (TRP, GSTP) for the coming cycle 4 Scope of the Workshop • 1) Technology for the architecture design, analysis and technical assessment of space transportation vehicles for suborbital, orbital and exploration applications, including upper stages, (re)-entry, expendable, and reusable vehicles • 2) Technology for the development of tools and techniques for the feasibility and viability assessments, and quick design iterations of flight vehicles • 3) Technology for flight vehicles, flight physics, aerodynamics, thermodynamics and fluid dynamics engineering and the architecture design and analysis of suborbital, (re-)entry, space transportation, and exploration vehicles 5 Time Line 1 2 3 4 5 May June September October November Workshop Consolidation of Final list of the best Preparation of Introduction of the ideas ideas (including upcoming TDE ideas in ESA description) cycle internal system 6 The program 7 Can I take your idea and ….? •No, please •The ideas are provided to you with the aim of discussion •The information should not be used to move the ideas to non-ESA technology programs 8 I have another idea… •Can I please discuss with you privately? •Yes, of course. -
ISS About the Kit Objectives
EUROPE and THE INTERNATIONAL SPACE STATION: Living and Working in Space A ready-to-use kit brought to you by the Ecsite Space Group with the Support of the European Space Agency TABLE OF CONTENTS THE INTERNATIONAL SPACE STATION: LIVING AND WORKING IN SPACE p.3 About the ISS About the kit Objectives READY TO USE TOOLS p.4 1. Exhibition “The International Space Station: Living and Working in Space” p.4 2. Learning activities p.11 2.1 Paper rocket p.11 2.2 Landing your Eggonaut safely p.11 3. ESA Exhibition Panels p.12 ACCESS TO RESOURCES p.13 MAIN CONTRIBUTORS p.13 ABOUT THE ECSITE SPACE GROUP p.14 YOUR CONTACT AT ECSITE p.14 2 The ISS: Living and Working in Space Ecsite Space Group The International Space Station: Living and Working in Space About the International Space Station The International Space Station, ISS, is the world’s largest-ever international scientific venture. The partnership includes the USA, Russia, Canada, Japan, and Europe. Orbiting 400 kilometres above us, the ISS offers unique opportunities to observe our planet, carry out research in space and prepare for human exploration of the Solar System. ESA is responsible for two key elements of the International Space Station: the Columbus research laboratory, and the Automated Transfer Vehicle (ATV) that delivered precious supplies to the ISS during five flights from 2008 to 2015. A European Service Module based on ATV technology will provide four major system functions to NASA’s Orion spacecraft: propulsion, power, thermal control and vital resources for the astronauts, such as water and a breathable atmosphere. -
Out There Somewhere Could Be a PLANET LIKE OURS the Breakthroughs We’Ll Need to find Earth 2.0 Page 30
September 2014 Out there somewhere could be A PLANET LIKE OURS The breakthroughs we’ll need to find Earth 2.0 Page 30 Faster comms with lasers/16 Real fallout from Ukraine crisis/36 NASA Glenn chief talks tech/18 A PUBLICATION OF THE AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS Engineering the future Advanced Composites Research The Wizarding World of Harry Potter TM Bloodhound Supersonic Car Whether it’s the world’s fastest car With over 17,500 staff worldwide, and 2,800 in or the next generation of composite North America, we have the breadth and depth of capability to respond to the world’s most materials, Atkins is at the forefront of challenging engineering projects. engineering innovation. www.na.atkinsglobal.com September 2014 Page 30 DEPARTMENTS EDITOR’S NOTEBOOK 2 New strategy, new era LETTER TO THE EDITOR 3 Skeptical about the SABRE engine INTERNATIONAL BEAT 4 Now trending: passive radars IN BRIEF 8 A question mark in doomsday comms Page 12 THE VIEW FROM HERE 12 Surviving a bad day ENGINEERING NOTEBOOK 16 Demonstrating laser comms CONVERSATION 18 Optimist-in-chief TECH HISTORY 22 Reflecting on radars PROPULSION & ENERGY 2014 FORUM 26 Electric planes; additive manufacturing; best quotes Page 38 SPACE 2014 FORUM 28 Comet encounter; MILSATCOM; best quotes OUT OF THE PAST 44 CAREER OPPORTUNITIES 46 Page 16 FEATURES FINDING EARTH 2.0 30 Beaming home a photo of a planet like ours will require money, some luck and a giant telescope rich with technical advances. by Erik Schechter COLLATERAL DAMAGE 36 Page 22 The impact of the Russia-Ukrainian conflict extends beyond the here and now. -
Soviet Steps Toward Permanent Human Presence in Space
SALYUT: Soviet Steps Toward Permanent Human Presence in Space December 1983 NTIS order #PB84-181437 Recommended Citation: SALYUT: Soviet Steps Toward Permanent Human Presence in Space–A Technical Mere- orandum (Washington, D. C.: U.S. Congress, Office of Technology Assessment, OTA- TM-STI-14, December 1983). Library of Congress Catalog Card Number 83-600624 For sale by the Superintendent of Documents, U.S. Government Printing Office, Washington, D.C. 20402 Foreword As the other major spacefaring nation, the Soviet Union is a subject of interest to the American people and Congress in their deliberations concerning the future of U.S. space activities. In the course of an assessment of Civilian Space Stations, the Office of Technology Assessment (OTA) has undertaken a study of the presence of Soviets in space and their Salyut space stations, in order to provide Congress with an informed view of Soviet capabilities and intentions. The major element in this technical memorandum was a workshop held at OTA in December 1982: it was the first occasion when a significant number of experts in this area of Soviet space activities had met for extended unclassified discussion. As a result of the workshop, OTA prepared this technical memorandum, “Salyut: Soviet Steps Toward Permanent Human Presence in Space. ” It has been reviewed extensively by workshop participants and others familiar with Soviet space activities. Also in December 1982, OTA wrote to the U. S. S. R.’s Ambassador to the United States Anatoliy Dobrynin, requesting any information concerning present and future Soviet space activities that the Soviet Union judged could be of value to the OTA assess- ment of civilian space stations. -
Year in Review 2013
SM_Dec_2013 cover Worldwide Satellite Magazine December 2013 SatMagazine 2013 YEAR IN REVIEW SatMagazine December 2013—Year In Review Publishing Operations Senior Contributors This Issue’s Authors Silvano Payne, Publisher + Writer Mike Antonovich, ATEME Mike Antonovich Robert Kubbernus Hartley G. Lesser, Editorial Director Tony Bardo, Hughes Eran Avni Dr. Ajey Lele Richard Dutchik Dave Bettinger Tom Leech Pattie Waldt, Executive Editor Chris Forrester, Broadgate Publications Don Buchman Hartley Lesser Jill Durfee, Sales Director, Editorial Assistant Karl Fuchs, iDirect Government Services Eyal Copitt Timothy Logue Simon Payne, Development Director Bob Gough, 21 Carrick Communications Rich Currier Jay Monroe Jos Heyman, TIROS Space Information Tommy Konkol Dybvad Tore Morten Olsen Donald McGee, Production Manager David Leichner, Gilat Satellite Networks Chris Forrester Kurt Peterhans Dan Makinster, Technical Advisor Giles Peeters, Track24 Defence Sima Fishman Jorge Potti Bert Sadtler, Boxwood Executive Search Simen K. Frostad Sally-Anne Ray David Gelerman Susan Sadaat Samer Halawi Bert Sadtler Jos Heyman Patrick Shay Jack Jacobs Mike Towner Casper Jensen Serge Van Herck Alexandre Joint Pattie Waldt Pradman Kaul Ali Zarkesh Published 11 times a year by SatNews Publishers 800 Siesta Way Sonoma, CA 95476 USA Phone: (707) 939-9306 Fax: (707) 838-9235 © 2013 SatNews Publishers We reserve the right to edit all submitted materials to meet our content guidelines, as well as for grammar or to move articles to an alternative issue to accommodate publication space requirements, or removed due to space restrictions. Submission of content does not constitute acceptance of said material by SatNews Publishers. Edited materials may, or may not, be returned to author and/or company for review prior to publication. -
ESO Call for Proposals – P109 Proposal Deadline: 23 September 2021, 12:00 Noon CEST * Call for Proposals
ESO Call for Proposals – P109 Proposal Deadline: 23 September 2021, 12:00 noon CEST * Call for Proposals ESO Period 109 Proposal Deadline: 23 September 2021, 12:00 noon Central European Summer Time Issued 26 August 2021 * Preparation of the ESO Call for Proposals is the responsibility of the ESO Observing Programmes Office (OPO). For questions regarding preparation and submission of proposals to ESO telescopes, please submit your enquiries through the ESO Helpdesk. The ESO Call for Proposals document is a fully linked pdf file with bookmarks that can be viewed with Adobe Acrobat Reader 4.0 or higher. Internal document links appear in red and external links appear in blue. Links are clickable and will navigate the reader through the document (internal links) or will open a web browser (external links). ESO Call for Proposals Editor: Dimitri A. Gadotti Approved: Xavier Barcons Director General v Contents I Phase 1 Instructions1 1 ESO Proposals Invited1 1.1 Important recent changes (since Periods 107 and 108)..................2 1.1.1 General.......................................2 1.1.2 Paranal.......................................3 1.1.3 La Silla.......................................5 1.1.4 Chajnantor.....................................5 1.2 Important reminders....................................6 1.2.1 General.......................................6 1.2.2 Paranal.......................................7 1.2.3 La Silla.......................................9 1.2.4 Chajnantor.....................................9 1.3 Changes foreseen in the upcoming Periods........................ 10 2 Getting Started 10 2.1 Support for VLTI programmes.............................. 11 2.2 Exposure Time Calculators................................ 11 2.3 The p1 proposal submission tool............................. 11 2.3.1 Important notes.................................. 12 2.4 Proposal Submission.................................... 13 3 Visitor Instruments 13 II Proposal Types, Policies, and Procedures 14 4 Proposal Types 14 4.1 Normal Programmes................................... -
International Space Exploration Coordination Group (ISECG) Provides an Overview of ISECG Activities, Products and Accomplishments in the Past Year
Annual Report 2012 of the International Space Exploration Coordination Group INTERNATIONAL SPACE EXPLORATION COORDINATION GROUP ISECG Secretariat Keplerlaan 1, PO Box 299, NL-2200 AG Noordwijk, The Netherlands +31 (0) 71 565 3325 [email protected] ISECG publications can be found on: http://www.globalspaceexploration.org/ 2 Table of Contents 1. Introduction 4 2. Executive Summary 4 3. Background 5 4. Activities 4.1. Overview 7 4.2. Activities on ISECG Level 7 4.3. Working Group Activities 8 4.3.1. Exploration Roadmap Working Group (ERWG) 8 4.3.2. International Architecture Working Group (IAWG) 9 4.3.3. International Objectives Working Group (IOWG) 10 4.3.4. Strategic Communications Working Group (SCWG) 10 Annex: Space Exploration Highlights of ISECG Member Agencies 12 1. Agenzia Spaziale Italiana (ASI), Italy 13 2. Centre National d’Etudes Spatiales (CNES), France 15 3. Canadian Space Agency (CSA), Canada 17 4. Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR), Germany 21 5. European Space Agency (ESA) 23 6. Japan Aerospace Exploration Agency (JAXA), Japan 28 7. Korea Aerospace Research Institute (KARI), Republic of Korea 30 8. National Aeronautics and Space Administration (NASA), USA 31 9. State Space Agency of Ukraine (SSAU), Ukraine 33 10. UK Space Agency (UKSA), United Kingdom 35 3 1 Introduction The 2012 Annual Report of the International Space Exploration Coordination Group (ISECG) provides an overview of ISECG activities, products and accomplishments in the past year. In the annex many of the ISECG participating agencies report on national space exploration highlights in 2012. 2 Executive Summary ISECG was established in response to the “The Global Exploration Strategy: The Framework for Coordination” (GES) developed by 14 space agencies1 and released in May 2007. -
Orbiter Processing Facility
National Aeronautics and Space Administration Space Shuttle: Orbiter Processing From Landing To Launch he work of preparing a space shuttle for the same facilities. Inside is a description of an flight takes place primarily at the Launch orbiter processing flow; in this case, Discovery. Complex 39 Area. TThe process actually begins at the end of each acts Shuttle Landing Facility flight, with a landing at the center or, after landing At the end of its mission, the Space Shuttle f at an alternate site, the return of the orbiter atop a Discovery lands at the Shuttle Landing Facility on shuttle carrier aircraft. Kennedy’s Shuttle Landing one of two runway headings – Runway 15 extends Facility is the primary landing site. from the northwest to the southeast, and Runway There are now three orbiters in the shuttle 33 extends from the southeast to the northwest fleet: Discovery, Atlantis and Endeavour. Chal- – based on wind currents. lenger was destroyed in an accident in January After touchdown and wheelstop, the orbiter 1986. Columbia was lost during approach to land- convoy is deployed to the runway. The convoy ing in February 2003. consists of about 25 specially designed vehicles or Each orbiter is processed independently using units and a team of about 150 trained personnel, NASA some of whom assist the crew in disembarking from the orbiter. the orbiter and a “white room” is mated to the orbiter hatch. The The others quickly begin the processes necessary to “safe” the hatch is opened and a physician performs a brief preliminary orbiter and prepare it for towing to the Orbiter Processing Fa- medical examination of the crew members before they leave the cility. -
Launch Vehicle Control Center Architectures
Launch Vehicle Control Center Architectures Michael D. Watson1, Amy Epps2, and Van Woodruff3 NASA Marshall Space Flight Center, Huntsville, AL 35812 Michael Jacob Vachon4 NASA Johnson Space Center, Houston, TX 77058 Julio Monreal5 European Space Agency, Launchers Directorate, Paris, France Marl Levesque6 United Launch Alliance, Vandenberg AFB and Randall Williams7 and Tom McLaughlin8 Aerospace Corporation, El Segundo, CA 90245 Launch vehicles within the international community vary greatly in their configuration and processing. Each launch site has a unique processing flow based on the specific launch vehicle configuration. Launch and flight operations are managed through a set of control centers associated with each launch site. Each launch site has a control center for launch operations; however flight operations support varies from being co-located with the launch site to being shared with the space vehicle control center. There is also a nuance of some having an engineering support center which may be co-located with either the launch or flight control center, or in a separate geographical location altogether. A survey of control center architectures is presented for various launch vehicles including the NASA Space Launch System (SLS), United Launch Alliance (ULA) Atlas V and Delta IV, and the European Space Agency (ESA) Ariane 5. Each of these control center architectures shares some similarities in basic structure while differences in functional distribution also exist. The driving functions which lead to these factors are considered and a model of control center architectures is proposed which supports these commonalities and variations. I. INTRODUCTION Launch vehicles in both Europe and the United States have been operating successfully for several decades. -
Building KSC's Launch Complex 39
National Aeronautics and Space Administration Building KSC’s Launch Complex 39 n the beginning, there was sand and adjacent to the VAB would house the Apollo I palmettos and water. Yet out of this idyllic spacecraft and the Launch Control Center. setting would grow the most unique structures -- The launcher-transporter would incorporate engineering milestones -- that would set the stage three major facilities: a pedestal for the space for the future in space. vehicle, an umbilical tower to service the upper The Kennedy Space Center of the 21st reaches of the space vehicle, and a rail transport- century began life in the early 1960s when new er. An arming tower would stand about midway Facts facilities were needed to launch the moon-bound between the assembly building and the pads. Saturn V rockets. The Apollo Saturn would carry a number of Initial plans called for a launch complex hazardous explosives: the launch escape system comprising a Vertical Assembly Building (VAB), (the tower on top of the vehicle that lifted the a launcher-transporter, an arming area and a spacecraft away from the launch vehicle in case launch pad. The VAB would consist of assembly of an emergency), retrorockets to separate the bay areas for each of the stages, with a high-bay stages, ullage rockets to force fuel to the bottom unit approximately 110 meters in height for final of tanks, and the launch vehicle’s destruct system. assembly and checkout of the vehicle. Buildings These plans would be modified during NASA NASA Launch Pad 39A is under construction (foreground) with the imposing Vertical Assembly Building rising from the sand in the background. -
European Service Module (ESM)
ArianeGroup to deliver key propulsion system components for the Orion spacecraft for the Artemis III Moon mission Lampoldshausen, Bremen, 28 September 2020 Airbus Defence and Space has placed several propulsion contracts with ArianeGroup for the third European Service Module (ESM) for NASA’s Artemis Moon mission ArianeGroup will be delivering several key components, including the attitude control system, as well as providing propulsion system integration and testing services These contracts follow on from the decisions taken at ESA’s Space 19+ Conference ArianeGroup has just signed several agreements with Airbus Defence and Space for the adaptation and construction of the third European Service Module (ESM) flight model for the Orion spacecraft. ArianeGroup will therefore: provide integration and testing services for the propulsion sub-system, as well as for certain parts of the thermal sub-system and the corresponding electronic sub-systems deliver several major components of the propulsion sub-system: notably 24 attitude control engines, two high-pressure regulators, various fuel valves, four fuel tanks, and two high- pressure helium tanks for pressurizing the fuel tanks in zero-gravity conditions provide technical support during system integration and acceptance of the Orion spacecraft’s ESM in the United States Airbus DS is prime contractor on behalf of the European Space Agency (ESA) for the ESM service module, Europe’s contribution to NASA’s Orion MPCV (Multi-Purpose Crew Vehicle) spacecraft. “When the first astronauts of the Artemis mission walk on the surface of the Moon in 2024, it will be in part thanks to the expertise of ArianeGroup in Germany and in France. -
When Artemis Talks, Johannes Kepler Listens 27 January 2011
When Artemis talks, Johannes Kepler listens 27 January 2011 be shared between Artemis and NASA's Tracking and Data Relay Satellite System (TDRSS). The first ATV mission was also supported by Artemis, in 2008. Working in parallel with TDRSS, Artemis was used as the main relay while ATV was attached to the Station and provided back up for commands and telemetry during rendezvous, docking, undocking and reentry. Artemis will provide communications between Johannes Kepler and the ATV Control Centre (ATV-CC) in Toulouse, France. Hovering some 36 000 km above the equator at 21.4ºE, Artemis will route telemetry and commands to and from the control centre whenever the satellite sees the International Space Station or ATV. During every ATV-2 orbit, there is close to 40 minutes of continuous contact. Credit: ESA Credits: ESA/J.Huart After Ariane 5 lofts ATV Johannes Kepler into Artemis will again provide dedicated support to ATV space on 15 February, ESA's Artemis data relay throughout the free-flying phase of its mission up to satellite will be ready for action. the docking with the Station. TDRSS is the backup to Artemis during the attached phase, while Artemis Artemis will provide communications between will back up TDRSS during the other phases and in Johannes Kepler and the ATV Control Centre (ATV- emergency situations. CC) in Toulouse, France. Hovering some 36 000 km above the equator at 21.4ºE, Artemis will route Such was the case on 11 September 2008, when telemetry and commands to and from the control the Artemis Mission Control Centre provided centre whenever the satellite sees the International emergency support to ATV-1 after Hurricane Ike Space Station or ATV.