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Hayabusa2 and the Formation of the Solar System PPS02-25
PPS02-25 JpGU-AGU Joint Meeting 2017 Hayabusa2 and the formation of the Solar System *Sei-ichiro WATANABE1,2, Hayabusa2 Science Team2 1. Division of Earth and Planetary Sciences, Graduate School of Science, Nagoya University, 2. JAXA/ISAS Explorations of small solar system bodies bring us direct and unique information about the formation and evolution of the Solar system. Asteroids may preserve accretion processes of planetesimals or pebbles, a sequence of destructive events induced by the gas-driven migration of giant planets, and hydrothermal processes on the parent bodies. After successful small-body missions like Rosetta to comet 67P/Churyumov-Gerasimenko, Dawn to Vesta and Ceres, and New Horizons to Pluto, two spacecraft Hayabusa2 and OSIRIS-REx are now traveling to dark primitive asteroids.The Hayabusa2 spacecraft journeys to a C-type near-earth asteroid (162173) Ryugu (1999 JU3) to conduct detailed remote sensing observations and return samples from the surface. The Haybusa2 spacecraft developed by Japan Aerospace Exploration Agency (JAXA) was successfully launched on 3 Dec. 2014 by the H-IIA Launch Vehicle and performed an Earth swing-by on 3 Dec. 2015 to set it on a course toward its target. The spacecraft will reach Ryugu in the summer of 2018, observe the asteroid for 18 months, and sample surface materials from up to three different locations. The samples will be delivered to the Earth in Nov.-Dec. 2020. Ground-based observations have obtained a variety of optical reflectance spectra for Ryugu. Some reported the 0.7 μm absorption feature and steep slope in the short wavelength region, suggesting hydrated minerals. -
TINA Small Force-Controlled Robotic Arm for Exploration and Small Satellites
DLR.de/en TINA Small force-controlled robotic arm for exploration and small satellites Brief description The robotic arm TINA is a four-axis space demonstrator to investigate autonomous operations during exploration missions on Earth. Aims The aim of the research project is to demonstrate the technology needed for a small, force-controlled robotic arm for use in space. By selecting specific components, it is possible to use TINA in Parties involved microgravity conditions as well as on Earth. DLR Institute of Robotics and Mechatronics Applications Facts and figures - Exploration, rover - Degrees of freedom: up to 7 - Controller: hard real time - Small satellites - Size: up to 2 m long - Radiation hardness: - Weight: 1.6 kg per joint various levels possible - Data transmission: - Tools: different end effectors can be Spacewire selected - Data rate: 3kHz - Supply voltage: +20V to +70V @DLR_en DLR.de/en TINA Small force-controlled robotic arm for exploration and small satellites The design of TINA follows the ‘qualifiable’ philosophy of DEXHAND [1], which uses industrial-grade compo- nents with a similar performance to their space equivalents and follows the ECSS guidelines closely, or uses the industrial-grade versions of radiation-hardened electronic components. This philosophy ensures that the transition to a fully qualified design can be achieved with a minimum number of changes. It also provides an almost perfect version for thermal and EMI modelling. Another big advantage is the low price compared to the fully qualified, radiation-hardened version, which allows the construction of multiple test arms for grasp- ing, object handling and many other applications. Each joint is made up of a brushless DC motor in combination with a resolver for commutation and position sensing, a harmonic drive gearbox, a brake for safety reasons and a torque sensor to give TINA the ability to ‘feel’. -
New Voyage to Rendezvous with a Small Asteroid Rotating with a Short Period
Hayabusa2 Extended Mission: New Voyage to Rendezvous with a Small Asteroid Rotating with a Short Period M. Hirabayashi1, Y. Mimasu2, N. Sakatani3, S. Watanabe4, Y. Tsuda2, T. Saiki2, S. Kikuchi2, T. Kouyama5, M. Yoshikawa2, S. Tanaka2, S. Nakazawa2, Y. Takei2, F. Terui2, H. Takeuchi2, A. Fujii2, T. Iwata2, K. Tsumura6, S. Matsuura7, Y. Shimaki2, S. Urakawa8, Y. Ishibashi9, S. Hasegawa2, M. Ishiguro10, D. Kuroda11, S. Okumura8, S. Sugita12, T. Okada2, S. Kameda3, S. Kamata13, A. Higuchi14, H. Senshu15, H. Noda16, K. Matsumoto16, R. Suetsugu17, T. Hirai15, K. Kitazato18, D. Farnocchia19, S.P. Naidu19, D.J. Tholen20, C.W. Hergenrother21, R.J. Whiteley22, N. A. Moskovitz23, P.A. Abell24, and the Hayabusa2 extended mission study group. 1Auburn University, Auburn, AL, USA ([email protected]) 2Japan Aerospace Exploration Agency, Kanagawa, Japan 3Rikkyo University, Tokyo, Japan 4Nagoya University, Aichi, Japan 5National Institute of Advanced Industrial Science and Technology, Tokyo, Japan 6Tokyo City University, Tokyo, Japan 7Kwansei Gakuin University, Hyogo, Japan 8Japan Spaceguard Association, Okayama, Japan 9Hosei University, Tokyo, Japan 10Seoul National University, Seoul, South Korea 11Kyoto University, Kyoto, Japan 12University of Tokyo, Tokyo, Japan 13Hokkaido University, Hokkaido, Japan 14University of Occupational and Environmental Health, Fukuoka, Japan 15Chiba Institute of Technology, Chiba, Japan 16National Astronomical Observatory of Japan, Iwate, Japan 17National Institute of Technology, Oshima College, Yamaguchi, Japan 18University of Aizu, Fukushima, Japan 19Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA, USA 20University of Hawai’i, Manoa, HI, USA 21University of Arizona, Tucson, AZ, USA 22Asgard Research, Denver, CO, USA 23Lowell Observatory, Flagstaff, AZ, USA 24NASA Johnson Space Center, Houston, TX, USA 1 Highlights 1. -
Accounting Report for the Third Quarter of Fiscal Year Ending March 2012 (April 1, 2011 - December 31, 2011)
TRANSLATION - FOR REFERENCE ONLY - February 1, 2012 Company: JVC KENWOOD Corporation Representative: Hisayoshi Fuwa, President and CEO (Code: 6632; First Section of the Tokyo Stock Exchange) Contact: Satoshi Fujita, Executive Officer and CFO (Tel: +81-45-444-5232) (E-mail: [email protected]) Accounting Report for the Third Quarter of Fiscal Year Ending March 2012 (April 1, 2011 - December 31, 2011) Consolidated Financial Highlights for the Third Quarter of Fiscal Year Ending March 2012 (April 1, 2011 - December 31, 2011) Operating Results (Millions of yen) 1st Quarter to 3rd Quarter (For reference) April 1, 2011 YoY April 1, 2010 to Dec.31, 2011 to Dec.31, 2010 (%) Net sales 236,542 267,182 89 Operating profit (loss) 8,791 9,416 - Ordinary income (loss) 6,511 6,530 - Net income (loss) 4,409 2,193 - Sales by Segments (Millions of yen) 1st Quarter to 3rd Quarter (For reference) YoY April 1, 2011 April 1, 2010 to Dec.31, 2011 to Dec.31, 2010 (%) Car Electronics 77,707 80,558 96 Professional Systems 67,142 67,210 100 Home & Mobile Electronics 59,274 79,167 75 Entertainment 28,139 33,742 83 Others 4,279 6,502 66 Total 236,542 267,182 89 Major Products in Each Segment Car Electronics Car Audio, Car AV Systems and Car Navigation Systems Land Mobile Radio Equipment, Video Surveillance Equipment, Professional Systems Commercial Audio, Video and Display Equipment Home & Mobile Electronics Video Cameras, LCD TVs, Projectors, Pure Audio and AV Accessories Entertainment Music and video software, such as CDs and DVDs Radio Frequency ID Systems, Weather Satellite Data Reception Systems, Other Other projects Electronic Devices, Recording Media, Interior Furniture, etc. -
SPACE RESEARCH in POLAND Report to COMMITTEE
SPACE RESEARCH IN POLAND Report to COMMITTEE ON SPACE RESEARCH (COSPAR) 2020 Space Research Centre Polish Academy of Sciences and The Committee on Space and Satellite Research PAS Report to COMMITTEE ON SPACE RESEARCH (COSPAR) ISBN 978-83-89439-04-8 First edition © Copyright by Space Research Centre Polish Academy of Sciences and The Committee on Space and Satellite Research PAS Warsaw, 2020 Editor: Iwona Stanisławska, Aneta Popowska Report to COSPAR 2020 1 SATELLITE GEODESY Space Research in Poland 3 1. SATELLITE GEODESY Compiled by Mariusz Figurski, Grzegorz Nykiel, Paweł Wielgosz, and Anna Krypiak-Gregorczyk Introduction This part of the Polish National Report concerns research on Satellite Geodesy performed in Poland from 2018 to 2020. The activity of the Polish institutions in the field of satellite geodesy and navigation are focused on the several main fields: • global and regional GPS and SLR measurements in the frame of International GNSS Service (IGS), International Laser Ranging Service (ILRS), International Earth Rotation and Reference Systems Service (IERS), European Reference Frame Permanent Network (EPN), • Polish geodetic permanent network – ASG-EUPOS, • modeling of ionosphere and troposphere, • practical utilization of satellite methods in local geodetic applications, • geodynamic study, • metrological control of Global Navigation Satellite System (GNSS) equipment, • use of gravimetric satellite missions, • application of GNSS in overland, maritime and air navigation, • multi-GNSS application in geodetic studies. Report -
The Orbital-Hub: Low Cost Platform for Human Spaceflight After ISS
67th International Astronautical Congress (IAC), Guadalajara, Mexico, 26-30 September 2016. Copyright ©2016 by the International Astronautical Federation (IAF). All rights reserved. IAC-16, B3,1,9,x32622 The Orbital-Hub: Low Cost Platform for Human Spaceflight after ISS O. Romberga, D. Quantiusa, C. Philpota, S. Jahnkea, W. Seboldta, H. Dittusb, S. Baerwaldeb, H. Schlegelc, M. Goldd, G. Zamkad, R. da Costae, I. Retate, R. Wohlgemuthe, M. Langee a German Aerospace Center (DLR), Institute of Space Systems, Bremen, Germany, [email protected] b German Aerospace Center (DLR), Executive Board, Space Research and Technology, Cologne, Germany, c European Space Agency (ESA) Contractor, Johnson Space Center, Houston, USA, d Bigelow Aerospace, Las Vegas / Washington, USA, e Airbus DS, Bremen, Germany Abstract The International Space Station ISS demonstrates long-term international cooperation between many partner governments as well as significant engineering and programmatic achievement mostly as a compromise of budget, politics, administration and technological feasibility. A paradigm shift to use the ISS more as an Earth observation platform and to more innovation and risk acceptance can be observed in the development of new markets by shifting responsibilities to private entities and broadening research disciplines, demanding faster access by users and including new launcher and experiment facilitator companies. A review of worldwide activities shows that all spacefaring nations are developing their individual programmes for the time after ISS. All partners are basically still interested in LEO and human spaceflight as discussed by the ISECG. ISS follow-on activities should comprise clear scientific and technological objectives combined with the long term view on space exploration. -
Sixty Years of Australia in Space
Journal & Proceedings of the Royal Society of New South Wales, vol. 153, part 1, 2020, pp. 46–57. ISSN 0035-9173/20/010046-12 Sixty years of Australia in space Kerrie Dougherty Space Humanities Department, International Space University, Strasbourg, France Email: [email protected] Abstract Australia’s involvement in space activities commenced in 1957, at the beginning of the Space Age, with space tracking and sounding rocket launches at Woomera. By 1960, Australia was considered one of the leading space-active nations and in 1967 became one of the earliest countries to launch its own satellite. Yet by 1980, Australia’s space prominence had dwindled, with the country lacking both a national space agency and a coherent national space policy. Despite attempts in the latter part of the 1980s to develop an Australian space industry, the lack of a coherent and consistent national space policy and an effective co-ordinating body, left Australia constantly “punching below its weight” in global space activities until the Twenty First Century. This paper will briefly examine the often-contradictory history of Australian space activities from 1957 to the announcement of the Australian Space Agency in 2017, providing background and context for the later papers in this issue. Introduction Launchpad: the Woomera or 60,000 years the Indigenous people of Rocket Range FAustralia have looked to the sky, using “If the Woomera Range did not already exist, the stars to determine their location, find the proposal that Australia should engage in their way across the land and mark the a program of civil space research would be passage of the seasons and the best times unrealistic”. -
An Overview of Hayabusa2 Mission and Asteroid 162173 Ryugu
Asteroid Science 2019 (LPI Contrib. No. 2189) 2086.pdf AN OVERVIEW OF HAYABUSA2 MISSION AND ASTEROID 162173 RYUGU. S. Watanabe1,2, M. Hira- bayashi3, N. Hirata4, N. Hirata5, M. Yoshikawa2, S. Tanaka2, S. Sugita6, K. Kitazato4, T. Okada2, N. Namiki7, S. Tachibana6,2, M. Arakawa5, H. Ikeda8, T. Morota6,1, K. Sugiura9,1, H. Kobayashi1, T. Saiki2, Y. Tsuda2, and Haya- busa2 Joint Science Team10, 1Nagoya University, Nagoya 464-8601, Japan ([email protected]), 2Institute of Space and Astronautical Science, JAXA, Japan, 3Auburn University, U.S.A., 4University of Aizu, Japan, 5Kobe University, Japan, 6University of Tokyo, Japan, 7National Astronomical Observatory of Japan, Japan, 8Research and Development Directorate, JAXA, Japan, 9Tokyo Institute of Technology, Japan, 10Hayabusa2 Project Summary: The Hayabusa2 mission reveals the na- Combined with the rotational motion of the asteroid, ture of a carbonaceous asteroid through a combination global surveys of Ryugu were conducted several times of remote-sensing observations, in situ surface meas- from ~20 km above the sub-Earth point (SEP), includ- urements by rovers and a lander, an active impact ex- ing global mapping from ONC-T (Fig. 1) and TIR, and periment, and analyses of samples returned to Earth. scan mapping from NIRS3 and LIDAR. Descent ob- Introduction: Asteroids are fossils of planetesi- servations covering the equatorial zone were performed mals, building blocks of planetary formation. In partic- from 3-7 km altitudes above SEP. Off-SEP observa- ular carbonaceous asteroids (or C-complex asteroids) tions of the polar regions were also conducted. Based are expected to have keys identifying the material mix- on these observations, we constructed two types of the ing in the early Solar System and deciphering the global shape models (using the Structure-from-Motion origin of water and organic materials on Earth [1]. -
ESTEC White Paper Spinning in and Spinning Off: Ways to Strengthen the Ties Between ESTEC and the Dutch Knowledge Infrastructure
ESTEC White Paper Spinning in and spinning off: Ways to strengthen the ties between ESTEC and the Dutch knowledge infrastructure The High Tech Systems and Materials top team More information can be obtained from: Office top team High Tech Systems and Materials Boerhaavelaan 40 Postbus 190 2700 AD Zoetermeer The Netherlands www.htsm.nl www.hollandhightech.nl Projectmanagement DB Huisstijlmedia Design Bruikman Reclame, Den Haag The Hague, May 2012 ESTEC White Paper Spinning in and spinning off: Ways to strengthen the ties between ESTEC and the Dutch knowledge infrastructure by the High Tech Systems and Materials top team Table of contents Summary and conclusions . 3 1. The role of ESTEC in the Netherlands . .5 . 1 .1 The space industry in a global context . 5 1 .2 The Netherlands from a European perspective . 6. 1 .3 ESTEC’s position in Europe and the Netherlands . 8 1 .4 Looking ahead: the risks and rewards of the budgetary outlook . 9 2. Spinning in and off: stronger linkages between ESTEC and the Netherlands . 11 . 2 .1 Economic and societal applications from space data . 11 2 .2 Technology transfer and valorization . 13 2 .3 Stronger ties between academia, research institutes and ESTEC . 15 2 .4 Sharing and maintaining research facilities . 16 . 2 .5 Improving ESTEC’s visibility in the Dutch knowledge infrastructure . 17 Appendix 1: Technology crossovers from space to other roadmaps in the top sector HTSM and other . 18 . Appendix 2: Acknowledgements . 20 . Appendix 3: Top team High Tech Systems and Materials . 21. 2 | ESTEC White Paper High Tech Systems and Materials Top Team Summary and conclusions In the Proposal for an Innovation Contract for the Top Sector High Tech Systems and Materials (HTSM) (December 2011, see www .htsm .nl), the HTSM top team concludes that ESTEC, the European Space Agency (ESA) technology and research site in the Netherlands, is an important contributor to this top sector’s innovation ecosystem . -
Planetary Science in the Eyes of Giant Telescopes
Planetary Science in the Eyes of Giant Telescopes Franck Marchis (Carl Sagan Center at the SETI Ins<tute) Feeding the Giants Workshop, Ischia, Italy, August 30 2011, Outline ELTs = Extremely Large Telescopes (E-ELT, TMT, GMT) • Solar System Exploraon – Why Exploring the Solar System with ELTs – Space Mission Programs: Why, Who, Where, When? • Poten<al of the ELTs for Solar System Science – High Angular imaging coupled with spectroscopy in the NIR to explore Io, Titan, and TNOs – Low res UV-NIR spectroscopic combined with All-sky surveys 402 Years of Telescopes Why Planetary Science and the ELTs? • Long heritage of telescopic observaons for the study of the Solar System • Started in 1609 with Galileo Galilei – First publicaon in modern astronomy based on telescope data – Discoveries in the field of Planetary Science • Galilean Moons • Roughness of the Moon surface • Disk appearance of planets & phase of Venus • In 2009, 40% of Keck PR and 25% of Keck AO publicaons are based on Planetary Science results • Strong Public Interest for Planetary Science Toys in Japan Pluto protests 51 Years of Space Missions • First aempts to reach Mars (1960) and Venus (1961) • ~200 solar, lunar and interplanetary missions • More reliable technologies -> more space missions • More accessible technologies -> more countries have access to space (e.g. Japan, China, India,…) • Could the ELTs contribute to Planetary Science in this context? 51 Years of Space Missions (2009) Naonal Geographic 51 Years of Space Missions Inner Solar System NEA 51 Years of Space Missions -
India and China Space Programs: from Genesis of Space Technologies to Major Space Programs and What That Means for the Internati
University of Central Florida STARS Electronic Theses and Dissertations, 2004-2019 2009 India And China Space Programs: From Genesis Of Space Technologies To Major Space Programs And What That Means For The Internati Gaurav Bhola University of Central Florida Part of the Political Science Commons Find similar works at: https://stars.library.ucf.edu/etd University of Central Florida Libraries http://library.ucf.edu This Masters Thesis (Open Access) is brought to you for free and open access by STARS. It has been accepted for inclusion in Electronic Theses and Dissertations, 2004-2019 by an authorized administrator of STARS. For more information, please contact [email protected]. STARS Citation Bhola, Gaurav, "India And China Space Programs: From Genesis Of Space Technologies To Major Space Programs And What That Means For The Internati" (2009). Electronic Theses and Dissertations, 2004-2019. 4109. https://stars.library.ucf.edu/etd/4109 INDIA AND CHINA SPACE PROGRAMS: FROM GENESIS OF SPACE TECHNOLOGIES TO MAJOR SPACE PROGRAMS AND WHAT THAT MEANS FOR THE INTERNATIONAL COMMUNITY by GAURAV BHOLA B.S. University of Central Florida, 1998 A dissertation submitted in partial fulfillment of the requirements for the degree of Master of Arts in the Department of Political Science in the College of Arts and Humanities at the University of Central Florida Orlando, Florida Summer Term 2009 Major Professor: Roger Handberg © 2009 Gaurav Bhola ii ABSTRACT The Indian and Chinese space programs have evolved into technologically advanced vehicles of national prestige and international competition for developed nations. The programs continue to evolve with impetus that India and China will have the same space capabilities as the United States with in the coming years. -
Space Debris
IADC-11-04 April 2013 Space Debris IADC Assessment Report for 2010 Issued by the IADC Steering Group Table of Contents 1. Foreword .......................................................................... 1 2. IADC Highlights ................................................................ 2 3. Space Debris Activities in the United Nations ................... 4 4. Earth Satellite Population .................................................. 6 5. Satellite Launches, Reentries and Retirements ................ 10 6. Satellite Fragmentations ................................................... 15 7. Collision Avoidance .......................................................... 17 8. Orbital Debris Removal ..................................................... 18 9. Major Meetings Addressing Space Debris ........................ 20 Appendix: Satellite Break-ups, 2000-2010 ............................ 22 IADC Assessment Report for 2010 i Acronyms ADR Active Debris Removal ASI Italian Space Agency CNES Centre National d’Etudes Spatiales (France) CNSA China National Space Agency CSA Canadian Space Agency COPUOS Committee on the Peaceful Uses of Outer Space, United Nations DLR German Aerospace Center ESA European Space Agency GEO Geosynchronous Orbit region (region near 35,786 km altitude where the orbital period of a satellite matches that of the rotation rate of the Earth) IADC Inter-Agency Space Debris Coordination Committee ISRO Indian Space Research Organization ISS International Space Station JAXA Japan Aerospace Exploration Agency LEO Low