Russian and Chinese Responses to U.S. Military Plans in Space
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Capture and Reuse of Carbon Dioxide (CO2) for a Plastics Circular Economy: a Review
processes Review Capture and Reuse of Carbon Dioxide (CO2) for a Plastics Circular Economy: A Review Laura Pires da Mata Costa 1 ,Débora Micheline Vaz de Miranda 1, Ana Carolina Couto de Oliveira 2, Luiz Falcon 3, Marina Stella Silva Pimenta 3, Ivan Guilherme Bessa 3,Sílvio Juarez Wouters 3,Márcio Henrique S. Andrade 3 and José Carlos Pinto 1,* 1 Programa de Engenharia Química/COPPE, Universidade Federal do Rio de Janeiro, Cidade Universitária, CP 68502, Rio de Janeiro 21941-972, Brazil; [email protected] (L.P.d.M.C.); [email protected] (D.M.V.d.M.) 2 Escola de Química, Universidade Federal do Rio de Janeiro, Cidade Universitária, CP 68525, Rio de Janeiro 21941-598, Brazil; [email protected] 3 Braskem S.A., Rua Marumbi, 1400, Campos Elíseos, Duque de Caxias 25221-000, Brazil; [email protected] (L.F.); [email protected] (M.S.S.P.); [email protected] (I.G.B.); [email protected] (S.J.W.); [email protected] (M.H.S.A.) * Correspondence: [email protected]; Tel.: +55-21-3938-8709 Abstract: Plastic production has been increasing at enormous rates. Particularly, the socioenvi- ronmental problems resulting from the linear economy model have been widely discussed, espe- cially regarding plastic pieces intended for single use and disposed improperly in the environment. Nonetheless, greenhouse gas emissions caused by inappropriate disposal or recycling and by the Citation: Pires da Mata Costa, L.; many production stages have not been discussed thoroughly. Regarding the manufacturing pro- Micheline Vaz de Miranda, D.; Couto cesses, carbon dioxide is produced mainly through heating of process streams and intrinsic chemical de Oliveira, A.C.; Falcon, L.; Stella transformations, explaining why first-generation petrochemical industries are among the top five Silva Pimenta, M.; Guilherme Bessa, most greenhouse gas (GHG)-polluting businesses. -
50 Satellite Formation-Flying and Rendezvous
Parkinson, et al.: Global Positioning System: Theory and Applications — Chap. 50 — 2017/11/26 — 19:03 — page 1 1 50 Satellite Formation-Flying and Rendezvous Simone D’Amico1) and J. Russell Carpenter2) 50.1 Introduction to Relative Navigation GNSS has come to play an increasingly important role in satellite formation-flying and rendezvous applications. In the last decades, the use of GNSS measurements has provided the primary method for determining the relative position of cooperative satellites in low Earth orbit. More recently, GNSS data have been successfully used to perform formation-flying in highly elliptical orbits with apogees at tens of Earth radii well above the GNSS constellations. Current research aims at dis- tributed precise relative navigation between tens of swarming nano- and micro-satellites based on GNSS. Similar to terrestrial applications, GNSS relative navigation benefits from a high level of common error cancellation. Furthermore, the integer nature of carrier phase ambiguities can be exploited in carrier phase differential GNSS (CDGNSS). Both aspects enable a substantially higher accuracy in the estimation of the relative motion than can be achieved in single-spacecraft navigation. Following historical remarks and an overview of the state-of-the-art, this chapter addresses the technology and main techniques used for spaceborne relative navigation both for real-time and offline applications. Flight results from missions such as the Space Shuttle, PRISMA, TanDEM-X, and MMS are pre- sented to demonstrate the versatility and broad range of applicability of GNSS relative navigation, from precise baseline determination on-ground (mm-level accuracy), to coarse real-time estimation on-board (m- to cm-level accuracy). -
ISS Presentation by Sergey Seyvald
JSC ISS Corporate Presentation 27.04.2010 0 27.04.2010 All rights reserved - Ó JSC ISS - All rights reserved 1 ISS LOCATION ISS 27.04.2010 All rights reserved - Ó JSC ISS - All rights reserved 2 MORE THAN 50 YEARS EXPERIENCE IN SPACE • June 04, 1959 the affiliate of OKB-1 is established in Krasnoyarsk-26 • August 18, 1964 the first launch of in-house developed and manufactured Launcher 11K65 (COSMOS) A.G.Kozlov N.A.Testoyedov and three small-size satellites of COSMOS General General family (38, 39 and 40) Designer Designer and and General General Director Director • August 01, 1977 (1996-2006) (present time) establishment of NPO PM • 1997 NPO PM is renamed to academician M. F. M.F.Reshetnev Reshetnev’s NPO PM General Designer and General Director (1959- • March 03, 2008 1996) establishment of ISS-RESHETNEV COMPANY 27.04.2010 All rights reserved - Ó JSC ISS - All rights reserved 3 COMPANY STRUCTURE INTEGRATED STRUCTURE Joint - Stock Company «Academician M.F. Reshetnev» Information Satellite Systems» General Designer and General Director of JSC «ISS» Shareholders NPP «Geophizika-Cosmos», SIC «Polyus», Tomsk «GONETS», Moscow Moscow Reaction wheels, Battery electronic, Data relay service provider ADCS sensors Power Processing Unit based on LEO system Gonets. NPP «Kvant» ,Moscow «TTS – NPO PM», Zheleznogorsk NPP KP «Kvant», Rostov-na-Donu Solar arrays and batteries. EEE-parts screening and tests ADCS optical sensors «NPO PM – MKB», Zheleznogorsk SPS, Omsk «Sibpromproekt», Zheleznogorsk R&D in space and SADA, ADPM, control units Design and construction industrial facilities. space application on the ground «NPO PM – Razvitie», Zheleznogorsk Ground antenna systems 27.04.2010 4 COMPANY ORGANISATION General Designer & General Director N. -
ODQN 15-2, April 2011
National Aeronautics and Space Administration Orbital Debris Quarterly News Volume 15, Issue 2 April 2011 United Nations Discusses Space Inside... Debris and Long-Term Sustainability 14th NASA/DoD ODWG Meeting 2 of Activities in Outer Space NASA/DoD Meeting Space Debris has been an agenda item for In 2010 the subject of long-term sustainability on Active Debris each annual meeting of the Scientific and Technical of activities in outer space was added to the Removal 2 Subcommittee of the United Nations’ Committee Subcommittee’s agenda, and a working group was Kessler Receives 2011 on the Peaceful Uses of Outer Space (COPUOS) formed under a multi-year work plan. At the 2011 Dirk Brouwer Award 2 since 1994. In 1999 the Subcommittee produced meeting of the Subcommittee, terms of reference Russian Launch its first major assessment on the topic, Technical for the working group were established. The Vehicle Stage Reenters Report on Space Debris (Orbital Debris Quarterly objective of the Working Group will be “to examine Over U.S. 3 News, April 1999, pp. 7, 9), followed in 2007 with the and propose measures to ensure the safe and U.S. Commercial Earth establishment of space debris mitigation guidelines sustainable use of outer space for peaceful purposes, Obs Spacecraft Executes (Orbital Debris Quarterly News, April 2007, pp. 1-2). for the benefit of all countries. The Working Group Controlled Reentry 3 During its 48th session in February 2011, the will prepare a report on the long-term sustainability Subcommittee continued its deliberations on space of outer space activities containing a consolidated New Chapter on debris with numerous special presentations, including set of current practices and operating procedures, Space Waste 3 those by the United States, France, the Russian technical standards and policies associated with the Update on LEO Federation, the European Space Agency (ESA), safe conduct of space activities. -
The Start of the Manned Space Race by Andrew J
The Start of the Manned Space Race by Andrew J. LePage November 1998 Introduction of Sputnik 1 and 2 in October and November of 1957 changed everything. At the same time NACA and the USAF were studying manned spaceflight (see The Beginnings of The first Sputnik launches were to affect the manned America's Man in Space Program in the October space program in several ways. The impact the 1998 issue of SpaceViews), comparable efforts were launch of Sputnik 1 had on the West led Soviet quietly taking place independently in the Soviet Primer Nikita Khrushchev to exploit space missions Union . As with virtually every other aspect of the for their propaganda value. Development of more Soviet Union's early space program, Chief Designer advanced and spectacular missions like the manned Sergei P. Korolev and his OKB-1 (Experimental satellite program were immediately approved and Design Bureau No. 1) lead the way. All during the placed on the fast track. Also at the insistence of 1950s when Korolev and his colleague, Mikhail K. Khrushchev, Sputnik 2 was launched with a dog on Tikhonravov of NII-4 (Scientific Research Institute board. While thermal control problems marred the No. 4), were pushing their original Earth satellite mission, it did demonstrate that weightlessness would proposal, it also included plans to send probes to the not be a major hazard for a human (see Sputnik 2: Moon and men into orbit. When the satellite The First Animal in Space in the November 1997 proposal was finally adopted by the Soviet issue of SpaceViews). As a result, Korolev scrapped government on January 30, 1956, the lunar probe and his initial, more conservative approach and moved manned satellite projects were also given the green ahead with a much more aggressive plan. -
Extragalactic Sources of Rapidly Variable High Energy Gamma Radiation
Dario Hrupec Extragalactic sources of rapidly variable high energy gamma radiation Doctoral Thesis submitted to the Department of Physics, Faculty of Science, University of Zagreb, for the academic degree of Doctor of Natural Sciences (Physics) Zagreb 2008. This thesis was done at Ruder Boˇskovi´c Institute under the supervision of Professor Daniel Ferenc from the University of California at Davis. ii Acknowledgments I would like to thank my mentor Dr. Daniel Ferenc from the University of California at Davis for his great professional and personal support during my work on this thesis. I have received precious inspiration from him. Finally, he encouraged me to read a lot. It was an invaluable advice. I am thankful to my co-mentor Dr. Silvio Pallua from the Faculty of Science at Zagreb for his support and for the thesis review. I am also thankful to Dr. Kreˇsimir Pavlovski from the Faculty of Science at Zagreb for the thesis review. I am particularly thankful to him for his valuable support. In addition, his terminological arguments impressed me a lot. Many thanks to Dr. Matko Milin from Faculty of Science at Zagreb for the time he spent on reading and commenting my thesis. I really appreciate his being my committee member. I owe many thanks to Dr. Eckart Lorenz from the University of California at Davis and ETH-Zurich who made possible my observations with the Cerenkovˇ telescope 1 (CT1) at La Palma in 2003. His donation of two Cerenkovˇ telescopes to Ruder Boˇskovi´c Institute established a base for the Cosmic Ray Observatory At The Eastern Adriatic (CROATEA) and also for my work in astroparticle physics in Croatia. -
Galileo FOC-M7 SAT 19-20-21-22
LAUNCH KIT December 2017 VA240 Galileo FOC-M7 SAT 19-20-21-22 VA240 Galileo FOC-M7 SAT 19-20-21-22 ARIANESPACE’S SECOND ARIANE 5 LAUNCH FOR THE GALILEO CONSTELLATION AND EUROPE For its 11th launch of the year, and the sixth Ariane 5 liftoff from the Guiana Space Center (CSG) in French Guiana during 2017, Arianespace will orbit four more satellites for the Galileo constellation. This mission is being performed on behalf of the European Commission under a contract with the European Space Agency (ESA). For the second time, an Ariane 5 ES version will be used to orbit satellites in Europe’s own satellite navigation system. At the completion of this flight, designated Flight VA240 in Arianespace’s launcher family numbering system, 22 Galileo spacecraft will have been launched by Arianespace. Arianespace is proud to deploy its entire family of launch vehicles to address Europe’s needs and guarantee its independent access to space. Galileo, an iconic European program Galileo is Europe’s own global navigation satellite system. Under civilian control, Galileo offers guaranteed high-precision positioning around the world. Its initial services began in December CONTENTS 2016, allowing users equipped with Galileo-enabled devices to combine Galileo and GPS data for better positioning accuracy. The complete Galileo constellation will comprise a total of 24 operational satellites (along with > THE LAUNCH spares); 18 of these satellites already have been orbited by Arianespace. ESA transferred formal responsibility for oversight of Galileo in-orbit operations to the GSA VA240 mission (European GNSS Agency) in July 2017. Page 3 Therefore, as of this launch, the GSA will be in charge of the operation of the Galileo satellite Galileo FOC-M7 satellites navigation systems on behalf of the European Union. -
GLONASS Spacecraft
INNO V AT IO N The task of designing and developing the GLONASS GLONASS spacecraft fell to the Scientific Production Association of Applied Mechan ics (Nauchno Proizvodstvennoe Ob"edinenie Spacecraft Prikladnoi Mekaniki or NPO PM) , located near Krasnoyarsk in Siberia. This major aero Nicholas L. Johnson space industrial complex was established in 1959 as a division of Sergei Korolev 's Kaman Sciences Corporation Expe1imental Design Bureau (Opytno Kon struktorskoe Byuro or OKB). (Korolev , among other notable achievements , led the Fourteen years after the launch of the effort to develop the Soviet Union's first first test spacecraft, the Russian Global Nav launch vehicle - the A launcher - which igation Satellite System (Global 'naya Navi placed Sputnik 1 into orbit.) The founding gatsionnaya Sputnikovaya Sistema or and current general director and chief GLONASS) program remains viable and designer is Mikhail Fyodorovich Reshetnev, essentially on schedule despite the economic one of only two still-active chief designers and political turmoil surrounding the final from Russia's fledgling 1950s-era space years of the Soviet Union and the emergence program. of the Commonwealth of Independent States A closed facility until the early 1990s, (CIS). By the summer of 1994, a total of 53 NPO PM has been responsible for all major GLONASS spacecraft had been successfully Russian operational communications, navi Despite the significant economic hardships deployed in nearly semisynchronous orbits; gation, and geodetic satellite systems to associated with the breakup of the Soviet Union of the 53 , nearly 12 had been normally oper date. Serial (or assembly-line) production of and the transition to a modern market economy, ational since the establishment of the Phase I some spacecraft, including Tsikada and Russia continues to develop its space programs, constellation in 1990. -
The Annual Compendium of Commercial Space Transportation: 2012
Federal Aviation Administration The Annual Compendium of Commercial Space Transportation: 2012 February 2013 About FAA About the FAA Office of Commercial Space Transportation The Federal Aviation Administration’s Office of Commercial Space Transportation (FAA AST) licenses and regulates U.S. commercial space launch and reentry activity, as well as the operation of non-federal launch and reentry sites, as authorized by Executive Order 12465 and Title 51 United States Code, Subtitle V, Chapter 509 (formerly the Commercial Space Launch Act). FAA AST’s mission is to ensure public health and safety and the safety of property while protecting the national security and foreign policy interests of the United States during commercial launch and reentry operations. In addition, FAA AST is directed to encourage, facilitate, and promote commercial space launches and reentries. Additional information concerning commercial space transportation can be found on FAA AST’s website: http://www.faa.gov/go/ast Cover art: Phil Smith, The Tauri Group (2013) NOTICE Use of trade names or names of manufacturers in this document does not constitute an official endorsement of such products or manufacturers, either expressed or implied, by the Federal Aviation Administration. • i • Federal Aviation Administration’s Office of Commercial Space Transportation Dear Colleague, 2012 was a very active year for the entire commercial space industry. In addition to all of the dramatic space transportation events, including the first-ever commercial mission flown to and from the International Space Station, the year was also a very busy one from the government’s perspective. It is clear that the level and pace of activity is beginning to increase significantly. -
The Navy Navigation Satellite System (Transit)
ROBERT J. DANCHIK THE NAVY NAVIGATION SATELLITE SYSTEM (TRANSIT) This article provides an update on the status of the Navy Navigation Satellite System (TRANSIT). Some insights are provided on the evolution of the system into its current configuration, as well as a discussion of future plans. BACKGROUND sign goal was never achieved for long in those early In 1958, research scientists at APL solved the orbit days because the satellites had short operational life of the first Russian satellite, Sputnik-I, by analysis of times. The failures largely resulted from inadequate the observed Doppler shift of its transmitted signal. component quality and the large number of wiring in This led immediately to the concept of satellite navi terconnections. However, after OSCAR 2 10 and OS gation and the development of the U.S. Navy Navi CAR 12 were launched in 1966 and 1967, respectively, gation Satellite System (TRANSIT) by APL, under the enough data on the failure mechanisms became avail sponsorship of the Navy's Special Projects Office, to able to APL to achieve the desired advances in reli provide position fixes for the Fleet Ballistic Missile ability. The integrated circuit introduced in OSCAR Weapon System submarines. (The articles in Ref. 1, 10 significantly extended the satellite lifetime by im a previous issue of the fohns Hopkins APL Techni proving component reliability and reducing the num cal Digest devoted to TRANSIT, give the principles ber of interconnections. Subsequently, the last major of operation and early history of the system.) Now, design change made to the solar cell interconnections, 26 years after its conception, the system is mature. -
Redalyc.Status and Trends of Smallsats and Their Launch Vehicles
Journal of Aerospace Technology and Management ISSN: 1984-9648 [email protected] Instituto de Aeronáutica e Espaço Brasil Wekerle, Timo; Bezerra Pessoa Filho, José; Vergueiro Loures da Costa, Luís Eduardo; Gonzaga Trabasso, Luís Status and Trends of Smallsats and Their Launch Vehicles — An Up-to-date Review Journal of Aerospace Technology and Management, vol. 9, núm. 3, julio-septiembre, 2017, pp. 269-286 Instituto de Aeronáutica e Espaço São Paulo, Brasil Available in: http://www.redalyc.org/articulo.oa?id=309452133001 How to cite Complete issue Scientific Information System More information about this article Network of Scientific Journals from Latin America, the Caribbean, Spain and Portugal Journal's homepage in redalyc.org Non-profit academic project, developed under the open access initiative doi: 10.5028/jatm.v9i3.853 Status and Trends of Smallsats and Their Launch Vehicles — An Up-to-date Review Timo Wekerle1, José Bezerra Pessoa Filho2, Luís Eduardo Vergueiro Loures da Costa1, Luís Gonzaga Trabasso1 ABSTRACT: This paper presents an analysis of the scenario of small satellites and its correspondent launch vehicles. The INTRODUCTION miniaturization of electronics, together with reliability and performance increase as well as reduction of cost, have During the past 30 years, electronic devices have experienced allowed the use of commercials-off-the-shelf in the space industry, fostering the Smallsat use. An analysis of the enormous advancements in terms of performance, reliability and launched Smallsats during the last 20 years is accomplished lower prices. In the mid-80s, a USD 36 million supercomputer and the main factors for the Smallsat (r)evolution, outlined. -
A Value Proposition for Lunar Architectures Utilizing On-Orbit Propellant Refueling
A VALUE PROPOSITION FOR LUNAR ARCHITECTURES UTILIZING ON-ORBIT PROPELLANT REFUELING By James Jay Young In Partial Fulfillment of the Requirements for the Degree of Doctor of Philosophy in the School of Aerospace Engineering Georgia Institute of Technology May 2009 Copyright © 2009 by James J. Young A VALUE PROPOSITION FOR LUNAR ARCHITECTURES UTILIZING ON-ORBIT PROPELLANT REFUELING Approved by: Dr. Alan W. Wilhite, Chairman Dr. Douglas Stanley School of Aerospace Engineering School of Aerospace Engineering Georgia Institute of Technology Georgia Institute of Technology Dr. Trina M. Chytka Dr. Daniel P. Schrage Vehicle Analysis Branch School of Aerospace Engineering NASA Langley Research Center Georgia Institute of Technology Dr. Carlee A. Bishop Electronics Systems Laboratory Georgia Tech Research Institute Date Approved: October 29, 2008 ACKNOWLEDGEMENTS As I sit down to acknowledge all the people who have helped me throughout my career as a student I realized that I could spend pages thanking everyone. I may never have reached all of my goals without your endless support. I would like to thank all of you for helping me achieve me goals. I would like to specifically thank my thesis advisor, Dr. Alan Wilhite, for his guidance throughout this process. I would also like to thank my committee members, Dr. Carlee Bishop, Dr. Trina Chytka, Dr. Daniel Scharge, and Dr. Douglas Stanley for the time they dedicated to helping me complete my dissertation. I would also like to thank Dr. John Olds for his guidance during my first two years at Georgia Tech and introducing me to the conceptual design field. I must also thank all of the current and former students of the Space Systems Design Laboratory for helping me overcome any technical challenges that I encountered during my research.