Russian and Chinese Responses to U.S. Military Plans in Space
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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. -
China's Space Industry and International Collaboration
China’s Space Industry and International Collaboration Presenter: Ju Jin Title: Minister Counselor,the Embassy of P.R.China Date: Feb 27,2008 Brief History • 52 years since 1956, first space institute established • Learning from Soviet Union until 1960 • U.S.A.’s close door policy until now • China’s self-reliance Policy Major Achievements • 12 series of Long March Launching Rockets • >100 Launches • >80 satellites in remote sensing, telecommunication, GPS, scientific experiment • Manned space flights——Shenzhou 5 (2003) and Shenzhou 6 (2005) • Lunar Exploration Project——Chang’e 1 (2007) LM-2F Launch Vehicle • Stages 1 & 2 & 4 strap-on boosters • 58.3 meters long • Launch Mass: 480 tons • Total Thrust : 600 tons • Reliability & Safety Index: 0.97 & 0.997 • 10 Sub-Systems Manned Space Flight--Shenzhou 6 Manned Space Flight--Shenzhou 6 Lunar Probe Project--Change-1 First Lunar Surface Photos Lunar Probe Project—Change 1 • 3 Years • 17,000 Scientists and Engineers • Young Team averaged in the age of 30s • 100% China-Made • Technology Breakthroughs – All-direction Antenna – Ultra-violet Sensor International Exchange and Cooperation: Main Activities Over the recent years, China has signed cooperation agreements on the peaceful use of outer space and space project cooperation agreements with Argentina, Brazil, Canada, France, Malaysia, Pakistan, Russia, Ukraine, the ESA and the European Commission, and has established space cooperation subcommittee or joint commission mechanisms with Brazil, France, Russia and Ukraine. China and the ESA z Sino-ESA Double Star Satellite Exploration of the Earth's Space Plan. z "Dragon Program," involving cooperation in Earth observation satellites, having so far conducted 16 remote-sensing application projects in the fields of agriculture, forestry, water conservancy, meteorology, oceanography and disasters. -
Kazakhstan Missile Chronology
Kazakhstan Missile Chronology Last update: May 2010 As of May 2010, this chronology is no longer being updated. For current developments, please see the Kazakhstan Missile Overview. This annotated chronology is based on the data sources that follow each entry. Public sources often provide conflicting information on classified military programs. In some cases we are unable to resolve these discrepancies, in others we have deliberately refrained from doing so to highlight the potential influence of false or misleading information as it appeared over time. In many cases, we are unable to independently verify claims. Hence in reviewing this chronology, readers should take into account the credibility of the sources employed here. Inclusion in this chronology does not necessarily indicate that a particular development is of direct or indirect proliferation significance. Some entries provide international or domestic context for technological development and national policymaking. Moreover, some entries may refer to developments with positive consequences for nonproliferation. 2009-1947 March 2009 On 4 March 2009, Kazakhstan signed a contract to purchase S-300 air defense missile systems from Russia. According to Ministry of Defense officials, Kazakhstan plans to purchase 10 batteries of S-300PS by 2011. Kazakhstan's Air Defense Commander Aleksandr Sorokin mentioned, however, that the 10 batteries would still not be enough to shield all the most vital" facilities designated earlier by a presidential decree. The export version of S- 300PS (NATO designation SA-10C Grumble) has a maximum range of 75 km and can hit targets moving at up to 1200 m/s at a minimum altitude of 25 meters. -
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. -
Praxis Manned Spaceflight Log 1961±2006
Praxis Manned Space¯ight Log 1961±2006 Tim Furniss and David J. Shayler with Michael D. Shayler Praxis Manned Spaceflight Log 1961±2006 Published in association with PPraxisraxis PPublishiublishingng Chichester, UK Tim Furniss David J. Shayler Space¯ight Correspondent Astronautical Historian Flight International Astro Info Service Bideford Halesowen Devon West Midlands UK UK Michael D. Shayler Editor and Designer Astro Info Service Birmingham UK SPRINGER±PRAXIS BOOKS IN SPACE EXPLORATION SUBJECT ADVISORY EDITOR: John Mason B.Sc., M.Sc., Ph.D. ISBN 10: 0-387-34175-7 Springer Berlin Heidelberg New York ISBN 13: 978-0-387-34175-0 Springer Berlin Heidelberg New York Springer is part of Springer-Science + Business Media (springer.com) Library of Congress Control Number: 2006937359 Apart from any fair dealing for the purposes of research or private study, or criticism or review, as permitted under the Copyright, Designs and Patents Act 1988, this publication may only be reproduced, stored or transmitted, in any form or by any means, with the prior permission in writing of the publishers, or in the case of reprographic reproduction in accordance with the terms of licences issued by the Copyright Licensing Agency. Enquiries concerning reproduction outside those terms should be sent to the publishers. # Praxis Publishing Ltd, Chichester, UK, 2007 Printed in Germany The use of general descriptive names, registered names, trademarks, etc. in this publication does not imply, even in the absence of a speci®c statement, that such names are exempt from the relevant protective laws and regulations and therefore free for general use. Cover design: Jim Wilkie Project Copy Editor: Mike Shayler Typesetting: Originator Publishing Services, Gt Yarmouth, Norfolk, UK Printed on acid-free paper Contents Authors' Preface ...................................... -
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. -
Moscow Defense Brief 1/2005
CONTENTS War And People #1(3), 2005 Militant Islam in Russia – Potential for Conflict PUBLISHER 2 Centre for Arms Trade Analysis of Strategies and Financial Results of Russian Arms Trade With Foreign Technolog ies States in 2004 9 CAST Director & Editor Russian Arms Trade with Southeast Asia and The Republic Ruslan Pukhov of Korea 13 Advisory Editor Konstantin Makienko Defense Industry Researcher Ukraine’s Defense Industry: A Mirror of the Nation 19 Ruslan Aliev Researcher Russian Armed Forces Sergei Pokidov The Russian Military: Still Saving for a Rainy Day 23 Researcher Dmitry Vasiliev Space Editorial Office Russia, Moscow, 119334, Leninsky prospect, 45, suite 480 Russian-Indian Cooperation in Space 27 phone: +7 095 135 1378 fax: +7 095 775 0418 Armed Conflicts http://www.mdb.cast.ru/ To subscribe contact US Armor in Operation “Iraqi Freedom” 32 phone +7 095 135 1378 or e-mail: [email protected] Facts & Figures E-mail the editors: [email protected] Largest identified transfers of Russian arms in 2004 36 Moscow Defense Brief is published by the Centre for Analysis of Strategies and Technologies Identified contracts signed in 2004 37 All rights reserved. No part of this publication may be reproduced in any form or by any means, electronic, Our Authors mechanical or photocopying, recording or other wise, without reference to Moscow Defense Brief. Please note that, while the Publisher has taken all reasonable care in the compilation of this publication, the Publisher cannot accept responsibility for any errors or omissions in this publication or -
Limitations of Spacecraft Redundancy: a Case Study Analysis
44th International Conference on Environmental Systems Paper Number 13-17 July 2014, Tucson, Arizona Limitations of Spacecraft Redundancy: A Case Study Analysis Robert P. Ocampo1 University of Colorado Boulder, Boulder, CO, 80309 Redundancy can increase spacecraft safety by providing the crew or ground with multiple means of achieving a given function. However, redundancy can also decrease spacecraft safety by 1) adding additional failure modes to the system, 2) increasing design “opaqueness”, 3) encouraging operational risk, and 4) masking or “normalizing” design flaws. Two Loss of Crew (LOC) events—Soyuz 11 and Challenger STS 51-L—are presented as examples of these limitations. Together, these case studies suggest that redundancy is not necessarily a fail-safe means of improving spacecraft safety. I. Introduction A redundant system is one that can achieve its intended function through multiple independent pathways or Aelements 1,2. In crewed spacecraft, redundancy is typically applied to systems that are critical for safety and/or mission success3,4. Since no piece of hardware can be made perfectly reliable, redundancy—in theory—allows for the benign (e.g. non-catastrophic) failure of critical elements. Redundant elements can be 1) similar or dissimilar to each other, 2) activated automatically (“hot spare”) or manually (“cold spare”), and 3) located together or separated geographically5-7. U.S. spacecraft have employed redundancy on virtually all levels of spacecraft design, from component to subsystem7,8. Redundancy has a successful history of precluding critical and catastrophic failures during human spaceflight. A review of NASA mission reports, from Mercury to Space Shuttle, indicates that redundancy has saved the crew or extended the mission over 160 times, or roughly once per flight9. -
Reentry Motion and Aerodynamics of the MUSES-C Sample Return Capsule
Trans. Japan Soc. Aero. Space Sci. Vol. 51, No. 172, pp. 65–70, 2008 Reentry Motion and Aerodynamics of the MUSES-C Sample Return Capsule By Nobuaki ISHII,1Þ Tetsuya YAMADA,1Þ Koju HIRAKI2Þ and Yoshifumi INATANI1Þ 1ÞThe Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan 2ÞKyushu Institute of Technology, Kita-Kyushu, Japan (Received June 21st, 2006) The Hayabusa spacecraft (MUSES-C) carries a small capsule for bringing asteroid samples back to the earth. The initial spin rate of the reentry capsule together with the flight path angle of the reentry trajectory is a key parameter for the aerodynamic motion during the reentry flight. The initial spin rate is given by the spin-release mechanism attached between the capsule and the mother spacecraft, and the flight path angle can be modified by adjusting the earth approach orbit. To determine the desired values of both parameters, the attitude motion during atmospheric flight must be clarified, and angles of attack at the maximum dynamic pressure and the parachute deployment must be assessed. In previous studies, to characterize the aerodynamic effects of the reentry capsule, several wind-tunnel tests were conducted using the ISAS high-speed flow test facilities. In addition to the ground test data, the aerodynamic properties in hypersonic flows were analyzed numerically. Moreover, these data were made more accurate using the results of balloon drop tests. This paper summarized the aerodynamic properties of the reentry capsule and simulates the attitude motion of the full- configuration capsule during atmospheric flight in three dimensions with six degrees of freedom. The results show the best conditions for the initial spin rates and flight path angles of the reentry trajectory. -
The Soviet Space Program
C05500088 TOP eEGRET iuf 3EEA~ NIE 11-1-71 THE SOVIET SPACE PROGRAM Declassified Under Authority of the lnteragency Security Classification Appeals Panel, E.O. 13526, sec. 5.3(b)(3) ISCAP Appeal No. 2011 -003, document 2 Declassification date: November 23, 2020 ifOP GEEAE:r C05500088 1'9P SloGRET CONTENTS Page THE PROBLEM ... 1 SUMMARY OF KEY JUDGMENTS l DISCUSSION 5 I. SOV.IET SPACE ACTIVITY DURING TfIE PAST TWO YEARS . 5 II. POLITICAL AND ECONOMIC FACTORS AFFECTING FUTURE PROSPECTS . 6 A. General ............................................. 6 B. Organization and Management . ............... 6 C. Economics .. .. .. .. .. .. .. .. .. .. .. ...... .. 8 III. SCIENTIFIC AND TECHNICAL FACTORS ... 9 A. General .. .. .. .. .. 9 B. Launch Vehicles . 9 C. High-Energy Propellants .. .. .. .. .. .. .. .. .. 11 D. Manned Spacecraft . 12 E. Life Support Systems . .. .. .. .. .. .. .. .. 15 F. Non-Nuclear Power Sources for Spacecraft . 16 G. Nuclear Power and Propulsion ..... 16 Te>P M:EW TCS 2032-71 IOP SECl<ET" C05500088 TOP SECRGJ:. IOP SECREI Page H. Communications Systems for Space Operations . 16 I. Command and Control for Space Operations . 17 IV. FUTURE PROSPECTS ....................................... 18 A. General ............... ... ···•· ................. ····· ... 18 B. Manned Space Station . 19 C. Planetary Exploration . ........ 19 D. Unmanned Lunar Exploration ..... 21 E. Manned Lunar Landfog ... 21 F. Applied Satellites ......... 22 G. Scientific Satellites ........................................ 24 V. INTERNATIONAL SPACE COOPERATION ............. 24 A. USSR-European Nations .................................... 24 B. USSR-United States 25 ANNEX A. SOVIET SPACE ACTIVITY ANNEX B. SOVIET SPACE LAUNCH VEHICLES ANNEX C. SOVIET CHRONOLOGICAL SPACE LOG FOR THE PERIOD 24 June 1969 Through 27 June 1971 TCS 2032-71 IOP SLClt~ 70P SECRE1- C05500088 TOP SEGR:R THE SOVIET SPACE PROGRAM THE PROBLEM To estimate Soviet capabilities and probable accomplishments in space over the next 5 to 10 years.' SUMMARY OF KEY JUDGMENTS A. -
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.