Space) Barriers for 50 Years: the Past, Present, and Future of the Dod Space Test Program
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Ultraviolet and Extreme Ultraviolet Spectroscopy of the Solar Corona at the Naval Research Laboratory
F222 Vol. 54, No. 31 / November 1 2015 / Applied Optics Research Article Ultraviolet and extreme ultraviolet spectroscopy of the solar corona at the Naval Research Laboratory 1, 1 1 2 1 1 J. D. MOSES, * Y.-K. KO, J. M. LAMING, E. A. PROVORNIKOVA, L. STRACHAN, AND S. TUN BELTRAN 1Space Science Division, Naval Research Laboratory, 4555 Overlook Avenue S.W., Washington DC 20375, USA 2University Corporation for Atmospheric Research, P.O. Box 3000, Boulder, Colorado 80307, USA *Corresponding author: [email protected] Received 8 June 2015; revised 3 August 2015; accepted 17 August 2015; posted 18 August 2015 (Doc. ID 242463); published 17 September 2015 We review the history of ultraviolet and extreme ultraviolet spectroscopy with a specific focus on such activities at the Naval Research Laboratory and on studies of the extended solar corona and solar-wind source regions. We describe the problem of forecasting solar energetic particle events and discuss an observational technique designed to solve this problem by detecting supra-thermal seed particles as extended wings on spectral lines. Such seed particles are believed to be a necessary prerequisite for particle acceleration by heliospheric shock waves driven by a coronal mass ejection. OCIS codes: (300.2140) Emission; (300.6540) Spectroscopy, ultraviolet; (350.1270) Astronomy and astrophysics; (350.6090) Space optics. http://dx.doi.org/10.1364/AO.54.00F222 1. INTRODUCTION with the launch of the Solar and Heliospheric Observatory [3] Many activities of the sun that affect the terrestrial environment (SoHO) in 1995, and the Solar Terrestrial Relations Observatory [4] (STEREO) in 2006. -
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 ••••••• • • • • • • • -
Kein Folientitel
The Solar Origins of Space Weather STP-10/CEDAR 2001 Joint Meeting June 17 to 22, 2001 Longmont, Colorado Rainer Schwenn Max-Planck-Institut für Aeronomie Katlenburg-Lindau Space Weather! Northern lights, Aurora! Space “storms” may cause severe damage to, e.g., power systems on earth! The Sun as the driver of Space Weather Major geomagnetic storms may cause •bright aurorae, down to low latitudes, •damage to high voltage lines in arctic regions, •anomalous corrosion of oil pipelines in arctic regions, •damage to long distance communication cables, •malfunction of magnetic compasses, •damage to satellites and satellite systems, •effects on biological systems. The Sun’s huge atmosphere, the “corona” Eclipse and LASCO-C2 coronagraph images processed and merged by Serge Koutchmy The Sun’s corona, well-known from eclipses The eclipse of 30.6.1973, recorded and processed by S. Koutchmy. The corona evaporates the “solar wind” Never seen before: the „smoke clouds“ near the equatorial plane are due to inhomogeneities in the solar wind, which thus becomes visible Note further: • The moving star field, • Our milky way which the sun traverses righ at Christmas, • A little comet plunging into the sun and evaporating Christmas 1996: LASCO-C3 shows the sun (though occulted) as a star amongst others in its own galaxy, the milky way! Tw o types of coron a and so wind lar Coronal “holes” were discovered in green light and in X-rays Yohkoh SXT 3-5 Million K Tw o types of coron a and so wind lar Coronal holes are apparent in all “hot” coronal emission lines EIT: 19.5 nm 1.5 Million K The two states of corona and solar wind Note the coronal hole edges: they transform nicely into stream boundaries The corona of the active sun (1998), viewed by EIT and LASCO-C1/C2 The “quiet” Sun and its minimum corona LASCO C1/C2, on 1.2. -
FASTSAT a Mini-Satellite Mission…..A Way Ahead”
Proposed Abstract: Under the combined Category and Title: “FASTSAT a Mini-Satellite Mission…..A Way Ahead” Authors: Mark E. Boudreaux, Joseph Casas, Timothy A. Smith The Fast Affordable Science and Technology Spacecraft (FASTSAT) is a mini-satellite weighing less than 150 kg. FASTSAT was developed as government-industry collaborative research and development flight project targeting rapid access to space to provide an alternative, low cost platform for a variety of scientific, research, and technology payloads. The initial spacecraft was designed to carry six instruments and launch as a secondary “rideshare” payload. This design approach greatly reduced overall mission costs while maximizing the on-board payload accommodations. FASTSAT was designed from the ground up to meet a challenging short schedule using modular components with a flexible, configurable layout to enable a broad range of payloads at a lower cost and shorter timeline than scaling down a more complex spacecraft. The integrated spacecraft along with its payloads were readied for launch 15 months from authority to proceed. As an ESPA-class spacecraft, FASTSAT is compatible with many different launch vehicles, including Minotaur I, Minotaur IV, Delta IV, Atlas V, Pegasus, Falcon 1/1e, and Falcon 9. These vehicles offer an array of options for launch sites and provide for a variety of rideshare possibilities. FASTSAT a Mini Satellite Mission …..A Way Ahead 15th Annual Space & Missile Defense Conference Session Track 1.2 : Operations for Small, Tactical Satellites Mark Boudreaux/NASA -
From the Heliosphere Into the Sun Programme Book Incuding All
511th WE-Heraeus-Seminar From the Heliosphere into the Sun –SailingagainsttheWind– Programme book incuding all abstracts Physikzentrum Bad Honnef, Germany January 31 – February 3, 2012 http://www.mps.mpg.de/meetings/heliocorona/ From the Heliosphere into the Sun A meeting dedicated to the progress of our understanding of the solar wind and the corona in the light of the upcoming Solar Orbiter mission This meeting is dedicated to the processes in the solar wind and corona in the light of the upcoming Solar Orbiter mission. Over the last three decades there has been astonishing progress in our understanding of the solar corona and the inner heliosphere driven by remote-sensing and in-situ observations. This period of time has seen the first high-resolution X-ray and EUV observations of the corona and the first detailed measurements of the ion and electron velocity distribution functions in the inner heliosphere. Today we know that we have to treat the corona and the wind as one single object, which calls for a mission that is fully designed to investigate the interwoven processes all the way from the solar surface to the heliosphere. The meeting will provide a forum to review the advances over the last decades, relate them to our current understanding and to discuss future directions. We will concentrate one day on in- situ observations and related models of the inner heliosphere, and spend another day on remote sensing observations and modeling of the corona – always with an eye on the symbiotic nature of the two. On the third day we will direct our view towards the future. -
The Strutjet Rocket Based Combined Cycle Engine A. Siebenhaar And
J The Strutjet Rocket Based Combined Cycle Engine A. Siebenhaar and M.J. Bulman GenCorp Aerojet Sacramento, CA And D.K. Bonnar Boeing Company Huntington Beach, Ca TABLE OF CONTENTS 1C) In_.roduc_o;', 2 0 Struuet t n_ine 2.1 FIo_ Path Description 2.2 Engine Architecture 2.2.1 FIo_path Elements 2.2.2 Turbo Machine D . Propellant Supply & Thermal Management 2.2.3 Engine C)cle 2.2.4 Structural Concept 2.3 Strutjet Operating Modes 2.3.1 Ducted Rocket Mode 2.3.2 Ramjet Mode 2.3.3 Scramjet Mode 2.3.4 Scram Rocket and Ascent Rocket Modes 2.4 Optimal Propulsion System Selection 2.4.1 Boost Mode Selection 2.4.2 Engine Design Point Selection 2.4.3 Ascent Rocket Transition Point Selection 3.0 Strutjet Vehicle Inte_ation 3.1 Strutjet Reference Mission 3.2 Engine-Vehicle Considerations 33 Vehicle Pitching Moment 3.4 Engine Performance 3.5 Reduced Operating Cost Through Robustness 3.6 Vehicle Comparisons 4.0 Available Hydrocarbon'and Hydrogen Test Data and plan_d Future Test Activities 4.1 Storable Hydrocarbon System Tests 4.2 CD'ogenic H.xdrogen System Tests 4.3 Planned Flight Tests 5.0 Maturit2. Of Required Su'utjet Technologies 6.0 Summar) and Conclusions 7.0 References J List of Tables 1. Comparison of Rocket and Strut.let Turbopumps 2. Sensitixitx to Engine Robustness 3. Vehicle Design Features and System Robustness 4. All-Rocket Vehicle Mass Breakdown 5. Strutjet Vehicle Mass Breakdown 6. Design Parameters for the All-Rocket and the RBCC-SSTO Vehicle 7. -
Highlights in Space 2010
International Astronautical Federation Committee on Space Research International Institute of Space Law 94 bis, Avenue de Suffren c/o CNES 94 bis, Avenue de Suffren UNITED NATIONS 75015 Paris, France 2 place Maurice Quentin 75015 Paris, France Tel: +33 1 45 67 42 60 Fax: +33 1 42 73 21 20 Tel. + 33 1 44 76 75 10 E-mail: : [email protected] E-mail: [email protected] Fax. + 33 1 44 76 74 37 URL: www.iislweb.com OFFICE FOR OUTER SPACE AFFAIRS URL: www.iafastro.com E-mail: [email protected] URL : http://cosparhq.cnes.fr Highlights in Space 2010 Prepared in cooperation with the International Astronautical Federation, the Committee on Space Research and the International Institute of Space Law The United Nations Office for Outer Space Affairs is responsible for promoting international cooperation in the peaceful uses of outer space and assisting developing countries in using space science and technology. United Nations Office for Outer Space Affairs P. O. Box 500, 1400 Vienna, Austria Tel: (+43-1) 26060-4950 Fax: (+43-1) 26060-5830 E-mail: [email protected] URL: www.unoosa.org United Nations publication Printed in Austria USD 15 Sales No. E.11.I.3 ISBN 978-92-1-101236-1 ST/SPACE/57 *1180239* V.11-80239—January 2011—775 UNITED NATIONS OFFICE FOR OUTER SPACE AFFAIRS UNITED NATIONS OFFICE AT VIENNA Highlights in Space 2010 Prepared in cooperation with the International Astronautical Federation, the Committee on Space Research and the International Institute of Space Law Progress in space science, technology and applications, international cooperation and space law UNITED NATIONS New York, 2011 UniTEd NationS PUblication Sales no. -
Jaxa Today 10.Pdf
Japan Aerospace Exploration Agency April 2016 No. 10 Special Features Japan’s Technical Prowess Technical excellence and team spirit are manifested in such activities as the space station capture of the HTV5 spacecraft, development of the H3 Launch Vehicle, and reduction of sonic boom in supersonic transport International Cooperation JAXA plays a central role in international society and contributes through diverse joint programs, including planetary exploration, and the utilization of Earth observation satellites in the environmental and disaster management fields Contents No. 10 Japan Aerospace Exploration Agency Special Feature 1: Japan’s Technical Prowess 1−3 Welcome to JAXA TODAY Activities of “Team Japan” Connecting the Earth and Space The Japan Aerospace Exploration Agency (JAXA) is positioned as We review some of the activities of “Team the pivotal organization supporting the Japanese government’s Japan,” including the successful capture of H-II Transfer Vehicle 5 (HTV5), which brought overall space development and utilization program with world- together JAXA, NASA and the International Space Station (ISS). leading technology. JAXA undertakes a full spectrum of activities, from basic research through development and utilization. 4–7 In 2013, to coincide with the 10th anniversary of its estab- 2020: The H3 Launch Vehicle Vision JAXA is currently pursuing the development lishment, JAXA defined its management philosophy as “utilizing of the H3 Launch Vehicle, which is expected space and the sky to achieve a safe and affluent society” and to become the backbone of Japan’s space development program and build strong adopted the new corporate slogan “Explore to Realize.” Under- international competitiveness. We examine the H3’s unique features and the development program’s pinned by this philosophy, JAXA pursues a broad range of pro- objectives. -
Cubesat-Based Science Missions for Geospace and Atmospheric Research
National Aeronautics and Space Administration NATIONAL SCIENCE FOUNDATION (NSF) CUBESAT-BASED SCIENCE MISSIONS FOR GEOSPACE AND ATMOSPHERIC RESEARCH annual report October 2013 www.nasa.gov www.nsf.gov LETTERS OF SUPPORT 3 CONTACTS 5 NSF PROGRAM OBJECTIVES 6 GSFC WFF OBJECTIVES 8 2013 AND PRIOR PROJECTS 11 Radio Aurora Explorer (RAX) 12 Project Description 12 Scientific Accomplishments 14 Technology 14 Education 14 Publications 15 Contents Colorado Student Space Weather Experiment (CSSWE) 17 Project Description 17 Scientific Accomplishments 17 Technology 18 Education 18 Publications 19 Data Archive 19 Dynamic Ionosphere CubeSat Experiment (DICE) 20 Project Description 20 Scientific Accomplishments 20 Technology 21 Education 22 Publications 23 Data Archive 24 Firefly and FireStation 26 Project Description 26 Scientific Accomplishments 26 Technology 27 Education 28 Student Profiles 30 Publications 31 Cubesat for Ions, Neutrals, Electrons and MAgnetic fields (CINEMA) 32 Project Description 32 Scientific Accomplishments 32 Technology 33 Education 33 Focused Investigations of Relativistic Electron Burst, Intensity, Range, and Dynamics (FIREBIRD) 34 Project Description 34 Scientific Accomplishments 34 Education 34 2014 PROJECTS 35 Oxygen Photometry of the Atmospheric Limb (OPAL) 36 Project Description 36 Planned Scientific Accomplishments 36 Planned Technology 36 Planned Education 37 (NSF) CUBESAT-BASED SCIENCE MISSIONS FOR GEOSPACE AND ATMOSPHERIC RESEARCH [ 1 QB50/QBUS 38 Project Description 38 Planned Scientific Accomplishments 38 Planned -
University of Florida Thesis Or Dissertation Formatting Template
DESIGN OF A REPRESENTATIVE LEO SATELLITE AND HYPERVELOCITY IMPACT TEST TO IMPROVE THE NASA STANDARD BREAKUP MODEL By SHELDON COLBY CLARK A THESIS PRESENTED TO THE GRADUATE SCHOOL OF THE UNIVERSITY OF FLORIDA IN PARTIAL FULFILLMENT OF THE REQUIREMENTS FOR THE DEGREE OF MASTER OF SCIENCE UNIVERSITY OF FLORIDA 2013 1 © 2013 Sheldon C. Clark 2 To my family - forever first and foremost - for making me who I am today and supporting me unconditionally through all of my endeavors. To my friends, colleagues, and advisors who have accompanied me on my journey – I am forever grateful. 3 ACKNOWLEDGMENTS I would like to thank all those who have given me the opportunity to grow to the person I am today. I thank my parents and family for their unconditional love and support. I am grateful to Dr. Norman Fitz-Coy for the learning opportunities he has provided and the guidance he has shared with me. I also thank my longtime friends, my colleagues in the Space Systems Group, and my peers at the University of Florida for their support and help through the years. 4 TABLE OF CONTENTS page ACKNOWLEDGMENTS .................................................................................................. 4 LIST OF TABLES ............................................................................................................ 7 LIST OF FIGURES .......................................................................................................... 8 LIST OF ABBREVIATIONS .......................................................................................... -
The Insurance Institute of London
The Insurance Institute of London CII CPD accredited - demonstrates the quality of an event and that it meets CII/PFS member CPD scheme requirements. This webinar will count as 1 hour of CPD and can be included as part of your CPD requirement should you consider it relevant to your professional development needs. It is recommended that you keep any evidence of the CPD activity you have completed and upload copies to the recording tool as the CII may ask to see this if your record is selected for review. MHI Launch Services - key essence of MHI’s quality management - Ref. B01038001405 February 17, 2021 © MITSUBISHI HEAVY INDUSTRIES, LTD. All Rights Reserved. MHI PROPRIETARY INFORMATION MHI PROPRIETARY INFORMATION 1. Introduction of MHI & Insurance Activities for our products 2. Launch Services 2.1 current work force H-IIA/B 2.2 Next gen, flagship H3 - Under Development - 3. MHI Quality Management Overview 4. Overcoming anomalies 4.1 Launch Operation case, H-IIB F8 4.2 Development case, H3 main engine(LE-9) 5. Conclusion © MITSUBISHI HEAVY INDUSTRIES, LTD. All Rights Reserved. PROPRIETARY INFORMATION 3 1. Introduction of MHI & Insurance Activities for our products MHI PROPRIETARY Introduction of MHI INFORMATION Power Systems Foundation July 7, 1884 Capital (USD) 2,415 MUSD As of Mar. 2019 Employees Thermal Power Plant Compressor CO2 Recovery Plants Desalination Plant (consolidated) 80,744 As of Mar. 2019 Industry & Infrastructure Sales (consolidated) 38,055 MUSD As of Mar. 2020 EBITDA 115.1 Dubai Metro Intelligent Transport Systems Overseas offices 7 Aircraft, Defense & Space Currency rate: USD 1 = JPY 110 Boeing – 787 Space Jet Defense Aircraft Launch Vehicle (Composite main wings) (H-IIA/-IIB) © MITSUBISHI HEAVY INDUSTRIES, LTD. -
Corporate Profile
2013 : Epsilon Launch Vehicle 2009 : International Space Station 1997 : M-V Launch Vehicle 1955 : The First Launched Pencil Rocket Corporate Profile Looking Ahead to Future Progress IHI Aerospace (IA) is carrying out the development, manufacture, and sales of rocket projectiles, and has been contributing in a big way to the indigenous space development in Japan. We started research on rocket projectiles in 1953. Now we have become a leading comprehensive manufacturer carrying out development and manufacture of rocket projectiles in Japan, and are active in a large number of fields such as rockets for scientific observation, rockets for launching practical satellites, and defense-related systems, etc. In the space science field, we cooperate with the Japan Aerospace Exploration Agency (JAXA) to develop and manufacture various types of observational rockets named K (Kappa), L (Lambda), and S (Sounding), and the M (Mu) rockets. With the M rockets, we have contributed to the launch of many scientific satellites. In 2013, efforts resulted in the successful launch of an Epsilon Rocket prototype, a next-generation solid rocket which inherited the 2 technologies of all the aforementioned rockets. In the practical satellite booster rocket field, We cooperates with the JAXA and has responsibilities in the solid propellant field including rocket boosters, upper-stage motors in development of the N, H-I, H-II, and H-IIA H-IIB rockets. We have also achieved excellent results in development of rockets for material experiments and recovery systems, as well as the development of equipment for use in a space environment or experimentation. In the defense field, we have developed and manufactured a variety of rocket systems and rocket motors for guided missiles, playing an important role in Japanese defense.