IAC-08-E1.1.4 REXUS and BEXUS – a Swedish-German Co-Operation for University Student Experiments on Rockets and Balloons
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Potential of Polarization/Raman Lidar to Separate Fine Dust, Coarse Dust
Atmos. Meas. Tech., 10, 3403–3427, 2017 https://doi.org/10.5194/amt-10-3403-2017 © Author(s) 2017. This work is distributed under the Creative Commons Attribution 3.0 License. Potential of polarization/Raman lidar to separate fine dust, coarse dust, maritime, and anthropogenic aerosol profiles Rodanthi-Elisavet Mamouri1,2 and Albert Ansmann3 1Cyprus University of Technology, Dep. of Civil Engineering and Geomatics, Limassol, Cyprus 2The Cyprus Institute, Energy, Environment, and Water Research Center, Nicosia, Cyprus 3Leibniz Institute for Tropospheric Research, Leipzig, Germany Correspondence to: Rodanthi-Elisavet Mamouri ([email protected]) Received: 26 April 2017 – Discussion started: 4 May 2017 Revised: 28 July 2017 – Accepted: 2 August 2017 – Published: 19 September 2017 Abstract. We applied the recently introduced polarization advantages in comparison to 355 and 1064 nm polarization lidar–photometer networking (POLIPHON) technique for lidar approaches and leads to the most robust and accurate the first time to triple-wavelength polarization lidar measure- POLIPHON products. ments at 355, 532, and 1064 nm. The lidar observations were performed at Barbados during the Saharan Aerosol Long- Range Transport and Aerosol-Cloud-Interaction Experiment (SALTRACE) in the summer of 2014. The POLIPHON 1 Introduction method comprises the traditional lidar technique to separate mineral dust and non-dust backscatter contributions and the Polarization lidar is a very powerful remote sensing tool for new, extended approach to separate even the fine and coarse aerosol and cloud research. The technique has been used for dust backscatter fractions. We show that the traditional and a long time to monitor and investigate cirrus cloud systems the advanced method are compatible and lead to a consis- (e.g., Sassen, 1991, 2005; Reichardt et al., 2002, 2008) and tent set of dust and non-dust profiles at simplified, less com- polar stratospheric cloud evolution (see, e.g., Browell et al., plex aerosol layering and mixing conditions as is the case 1990; Achtert and Tesche, 2014). -
We Help Earth Benefit from Space in Summary 2019 Contents
WE HELP EARTH BENEFIT FROM SPACE IN SUMMARY 2019 CONTENTS About this report 2019 HIGHLIGHTS This is an English summary of Swedish 3 Space Corporation’s (SSC) 2019 Annual and Sustainability Report. CEO STATEMENT The Swedish report, available at our web- 4 site, is the legally binding annual report. THIS IS SSC The report summarizes the 2019 fiscal 6 year and covers performance on issues most important to SSC's ability to deliver SSC GLOBAL PRESENCE value to stakeholders in a changing and complex business environment. This 8 summary serves as our United Nations Global Compact (UNGC) Communi- EVOLVING SPACE LANDSCAPE 9 cations on Progress. Visit: STRATEGIC APPROACH https://www.sscspace.com/about-ssc/finances/reports-archive/ 10 Copyright: Unless otherwise indicated, SSC has the copyright to images in this publication. FOCUS AREAS FOR PROFITABLE SUSTAINABLE GROWTH 12 EMPLOYEES - OUR GREATEST ASSET 14 MEET OUR PEOPLE 15 2019 HIGHLIGHTS 2019 HIGHLIGHTS 2019 was another year of exciting space missions and projects for the space sector as a whole, but also for SSC. The rapid development has allowed us to grow and take new steps to prepare for the future. MASER 14 and inauguration of SubOrbital Express as a service Our MASER 14 sounding rocket reached an altitude of approximately 250 kilometers and spent over six minutes in microgravity. The mission inaugurated SubOrbital Express, a service to enable research into microgravity applications, atmospheric physics or other scientific disciplines. In this microgravity environment, we conducted experiments on fluid drainage, X-ray radio graphy and dust formation. Read more: https://www.suborbitalexpress.com Inauguration of exciting antenna art in Inuvik The two SSC antennas at the Inuvik site are painted by the local artists Anick Jenks and Ron English. -
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. -
Beyond the Paths of Heaven the Emergence of Space Power Thought
Beyond the Paths of Heaven The Emergence of Space Power Thought A Comprehensive Anthology of Space-Related Master’s Research Produced by the School of Advanced Airpower Studies Edited by Bruce M. DeBlois, Colonel, USAF Professor of Air and Space Technology Air University Press Maxwell Air Force Base, Alabama September 1999 Library of Congress Cataloging-in-Publication Data Beyond the paths of heaven : the emergence of space power thought : a comprehensive anthology of space-related master’s research / edited by Bruce M. DeBlois. p. cm. Includes bibliographical references and index. 1. Astronautics, Military. 2. Astronautics, Military—United States. 3. Space Warfare. 4. Air University (U.S.). Air Command and Staff College. School of Advanced Airpower Studies- -Dissertations. I. Deblois, Bruce M., 1957- UG1520.B48 1999 99-35729 358’ .8—dc21 CIP ISBN 1-58566-067-1 Disclaimer Opinions, conclusions, and recommendations expressed or implied within are solely those of the authors and do not necessarily represent the views of Air University, the United States Air Force, the Department of Defense, or any other US government agency. Cleared for public release: distribution unlimited. ii Contents Chapter Page DISCLAIMER . ii OVERVIEW . ix PART I Space Organization, Doctrine, and Architecture 1 An Aerospace Strategy for an Aerospace Nation . 3 Stephen E. Wright 2 After the Gulf War: Balancing Space Power’s Development . 63 Frank Gallegos 3 Blueprints for the Future: Comparing National Security Space Architectures . 103 Christian C. Daehnick PART II Sanctuary/Survivability Perspectives 4 Safe Heavens: Military Strategy and Space Sanctuary . 185 David W. Ziegler PART III Space Control Perspectives 5 Counterspace Operations for Information Dominance . -
Suborbital Platforms and Range Services (SPARS)
Suborbital Capabilities for Science & Technology Small Missions Workshop @ Johns Hopkins University June 10, 2019 Mike Hitch, Giovanni Rosanova Goddard Space Introduction Flight Center AGENDAWASP OPIS ▪ Purpose ▪ History & Importance of Suborbital Carriers to Science ▪ Suborbital Platforms ▪ Sounding Rockets ▪ Balloons (brief) ▪ Aircraft ▪ SmallSats ▪ WFF Engineering ▪ Q & A P-3 Maintenance 12-Jun-19 Competition Sensitive – Do Not Distribute 2 Goddard Space Purpose of the Meeting Flight Center Define theWASP OPISutility of Suborbital Carriers & “Small” Missions ▪ Sounding rockets, balloons and aircraft (manned and unmanned) provide a unique capability to scientists and engineers to: ▪ Allow PIs to enhance and advance technology readiness levels of instruments and components for very low relative cost ▪ Provide PIs actual science flight opportunities as a “piggy-back” on a planned mission flight at low relative cost ▪ Increase experience for young and mid-career scientists and engineers by allowing them to get their “feet wet” on a suborbital mission prior to tackling the much larger and more complex orbital endeavors ▪ The Suborbital/Smallsat Platforms And Range Services (SPARS) Line Of Business (LOB) can facilitate prospective PIs with taking advantage of potential suborbital flight opportunities P-3 Maintenance 12-Jun-19 Competition Sensitive – Do Not Distribute 3 Goddard Space Value of Suborbital Research – What’s Different? Flight Center WASP OPIS Different Risk/Mission Assurance Strategy • Payloads are recovered and refurbished. • Re-flights are inexpensive (<$1M for a balloon or sounding rocket vs >$10M - 100M for a ELV) • Instrumentation can be simple and have a large science impact! • Frequent flight opportunities (e.g. “piggyback”) • Development of precursor instrument concepts and mature TRLs • While Suborbital missions fully comply with all Agency Safety policies, the program is designed to take Higher Programmatic Risk – Lower cost – Faster migration of new technology – Smaller more focused efforts, enable Tiger Team/incubator experiences. -
Measurements of Auroral Particles by Means of Sounding Rockets of Mother-Daughter Type A
MEASUREMENTS OF AURORAL PARTICLES BY MEANS OF SOUNDING ROCKETS OF MOTHER-DAUGHTER TYPE A. Falck KGI REPORT 192 NOVEMBER 1985 KIRUNA U-OI'HYSICAL INSTITITK MKINA N\X|1>I\ MEASUREMENTS OF AURORAL PARTICLES BY MEANS OF SOUNDING ROCKETS OF MOTHER-DAUGHTER TYPE by A. Falck Kiruna Geophysical Institute P.O. Box 704, S-981 27 KIRUNA, Sweden KGI Report 192 November 1985 Printed in Sweden Kiruna Geophysical Institute Kiruna 19^5 ISSN 034/-f 405 Contents Page 1. Presentation of the S17 payioads 3 1.1 The scientific objective of the sounding rockets S17 3 1.2 S17 experiments 3 1.3 Physical characteristics of the payioads 3 1.4 Physical characteristics of the Nike-Tomahawk rocket 5 1.5 Nominal characteristics of flight events 7 1.6 Attitude measurements 8 1.7 Separation of the two payload units 20 1.8 Telemetry and data analyzing technique 33 2. Description of the instrumentation for the particle experiments in the S17 payioads 38 2.1 General theory of CEM - detectors 38 2.2 Calibration of th* CEM - detectors 42 2.3 Solid state detectors in SI7 payioads 44 2.4 Mounting of the detectors 48 2.5 The efficiency of channel multipliers 48 3. Review of the geophysical conditions during the SI7 flights and presentation of some supporting observations 51 j.1 The auroral situation during S17 flights 51 :• 2 Magnetic activity 51 .'.3 Other supporting observations 56 .4 The lowlightlevel-TV-system 56 'K Particle fluxes and electric currents coupling the magnetosphere and the ionosphere during a magnetospheric substorm 66 4.1 Review of some substorm terminology and definitions 66 4.2 Reference and comparisons of SI7-2 measure- ments with the results of the IMS-study 75 4.3 Comparison of simultaneous particle observa- tions at low ionospheric altitude (S17-1) and at the magnetic equatorial region (ATS-6) 91 4.4 Summary and conclusions 99 5. -
Colorado Space Grant Consortium
CO_FY16_Year2_APD Colorado Space Grant Consortium Lead Institution: University of Colorado Boulder Director: Chris Koehler Telephone Number: 303.492.3141 Consortium URL: http://spacegrant.colorado.edu Grant Number: NNX15AK04H Lines of Business (LOBs): NASA Internships, Fellowships, and Scholarships; Stem Engagement; Institutional Engagement; Educator Professional Development A. PROGRAM DESCRIPTION The National Space Grant College and Fellowship Program consists of 52 state-based, university- led Space Grant Consortia in each of the 50 states plus the District of Columbia and the Commonwealth of Puerto Rico. Annually, each consortium receives funds to develop and implement student fellowships and scholarships programs; interdisciplinary space-related research infrastructure, education, and public service programs; and cooperative initiatives with industry, research laboratories, and state, local, and other governments. Space Grant operates at the intersection of NASA’s interest as implemented by alignment with the Mission Directorates and the state’s interests. Although it is primarily a higher education program, Space Grant programs encompass the entire length of the education pipeline, including elementary/secondary and informal education. The Colorado Space Grant Consortium is a Designated Consortium funded at a level of $760,000 for fiscal year 2016. B. PROGRAM GOALS • Population of students engaged in COSGC hands-on programs (awardees and non- awardees) will be at least 40% women and 23.7% from ethnic minority populations underrepresented in STEM fields. • Maintain student hands-on programs at all 8 COSGC Minority Serving Institutions and engaged at least 30 students on MSI campuses. • 30% of COSGC NASA funds will be awarded directly to students. • Award 80 scholarships to support students working on hands-on projects. -
Espinsights the Global Space Activity Monitor
ESPInsights The Global Space Activity Monitor Issue 2 May–June 2019 CONTENTS FOCUS ..................................................................................................................... 1 European industrial leadership at stake ............................................................................ 1 SPACE POLICY AND PROGRAMMES .................................................................................... 2 EUROPE ................................................................................................................. 2 9th EU-ESA Space Council .......................................................................................... 2 Europe’s Martian ambitions take shape ......................................................................... 2 ESA’s advancements on Planetary Defence Systems ........................................................... 2 ESA prepares for rescuing Humans on Moon .................................................................... 3 ESA’s private partnerships ......................................................................................... 3 ESA’s international cooperation with Japan .................................................................... 3 New EU Parliament, new EU European Space Policy? ......................................................... 3 France reflects on its competitiveness and defence posture in space ...................................... 3 Germany joins consortium to support a European reusable rocket......................................... -
Esrange Launching Programme
ESRANGE SPACE CENTER EASP LAUNCHING PROGRAMME 16 AUGUST 2021 Jan Feb Mar Apr May Jun Jul Aug Sep Oct Nov Dec Rx/Bx TW SSC Cust Conf 2020 HEMERA SB 2020-2 Student balloon 1 balloon 1 balloon Mini-BOOSTER HEMERA SB 2020-1 3 balloons 2020 1 balloons SPIDER 2 1 IM rocket EOSTRE 1 balloon STERN 2020-2 LEONIS 1 rocket CNES 2021 BEXUS 30/31 STORT SF3 LTU IWC 16 MAPHEUS-11 4 balloons 2 balloons 1 Imp. Orion 1 Balloon 1 IM/IM rocket STORT SF1&2 TEXUS 57 BOLT-1 2Imp. Orion 1 VSB-30 rocket 1 S-31/IO rocket NO parachute test 2021 3-6 drops BROR test HADT 2021 REXUS 27/28 2 balloons STORT TF1 2 Imp. Orion rockets LTU IWC 17 1 IO rocket 1 Balloon HEMERA-2 MAPHEUS-9/10 CNES Pre-campaign 1 balloon 2 IM/IM rockets NASA summer 2022 / SUNRISE-3 REXUS 29/30 4 balloons BEXUS 32/33 2 Imp. Orion rockets SERA 4 2 balloons 1 rocket HADT 2022 TEXUS 58/59 (ESA) 2 balloons 2 VSB-30 rockets MIRIAM-2 MAIUS 2 HEMERA LSB-1 2022 1 IM/IO rocket 1 VSB-30 rocket 1 balloon BROR HIFLIER 1 1 IM/IO rocket 1 S-31/IO rocket S1X-M15 DLR ESBO STUDIO MAPHEUS-12 1 VSB-30 rocket 1 balloon 1 VSB-30 rocket STERN 2022-1 HyEnd 25th ESA-PAC symposium HEMERA-3 1 rocket Biarritz, France 1 balloon PERFORMED DECIDED TENTATIVE SCHEDULE UNDER CONSIDERATION NON-ESC LAUNCH PRE-TEST/OTHER EASTER ESRANGE SPACE CENTER EASP LAUNCHING PROGRAMME 16 AUGUST 2021 Jan Feb Mar Apr May Jun Jul Aug Sep Oct Nov Dec Rx/Bx TW 26th ESA-PAC symposium HEMERA2-1 BEXUS 34/35 Switzerland 1 balloon 2 balloons REXUS 31/32 2 Imp. -
Methods of Oabservation at Sea Meteorological Soundings in The
WORLD METEOROLOGICAL ORGANIZATION WORLD METEOROLOGICAL ORGANIZATION TECHNICAL NOTE No. 2 TECHNICAL NOTE No. 60 METHODS OF OABSERVATION AT SEA METEOROLOGICAL SOUNDINGS IN THE PARTUPPER I – SEA SURFACEATMOSPHERE TEMPERATURE by W.W. KELLOGG WMO-No.WMO-No. 153. 26. TP. 738 Secretariat of the World Meteorological Organization – Geneva – Switzerland THE WMO The WOTld :Meteol'ological Organization (Wl\IO) is a specialized agency of the United Nations of which 125 States and Territories arc Members. It was created: to facilitate international co~operation in the establishment of networks of stations and centres to provide meteorological services and observationsI to promote the establishment and maintenance of systems for the rapid exchange of meteorological information, to promote standardization of meteorological observations and ensure the uniform publication of observations and statistics. to further the application of rneteol'ology to Rviatioll, shipping, agricultul"C1 and other human activities. to encourage research and training in meteorology. The machinery of the Organization consists of: The World Nleteorological Congress, the supreme body of the o.rganization, brings together the delegates of all Members once every four years to determine general policies for the fulfilment of the purposes of the Organization, to adopt Technical Regulations relating to international meteorological practice and to determine the WMO programme, The Executive Committee is composed of 21 dil'cetors of national meteorological services and meets at least once a yeae to conduct the activities of the Organization and to implement the decisions taken by its Members in Congress, to study and make recommendations Oll matters affecting international meteorology and the opel'ation of meteorological services. -
Importance Oi Thermistor Mount Configuration to Meteorological
James F. Morrissey importance oi and Andrew S. Carten, Jr. thermistor mount configuration A. F. Cambridge Research Laboratories to meteorological rocket Bedford, Mass. temperature measurements Abstract tions. Thus, we are receiving more data than ever be- A description is given of the original rocketsonde ther- fore—thanks to more successful firings and improved mistor mount, consisting of a 10-mil bead suspended signal reception—but data quality has stayed at a low between two metal posts. The difficulties encountered to medium level. Recent evidence, described later in this with this mount and the subsequent development of article, confirms our belief that caution is in order. the superior "thin-film" mount are also described. The Today's rocketsonde is, for the most part, a more uncertainties associated with the use of the latter mount rugged version of the standard radiosonde. This is only are outlined along with their effect on data acceptance. natural, considering both the effort which has gone into A different approach to the original problem is de- refining radiosonde and associated ground equipment scribed, which employs longer leads for dissipation of design and the success which has crowned that effort. heat conducted to the bead. The uncertainty associated In choosing a sensor for the rocketsonde, it was recog- with the long lead is shown to be minimal. Preliminary nized that the small bead thermistor has the necessary results of a series of 10 rocket flights are presented. response time to provide useful measurements to about These results tend to confirm the advantages of the 60 km. A 10-mil diameter bead, aluminized to minimize long lead mount. -
Japan's Technical Prowess International Cooperation
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 Japan’s Technical Prowess 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.