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Secretariat GENERAL ST/SG/SER.E/320 23 May 1997 ENGLISH ORIGINAL: RUSSIAN
UNITED NATIONS ST Distr. Secretariat GENERAL ST/SG/SER.E/320 23 May 1997 ENGLISH ORIGINAL: RUSSIAN COMMITTEE ON THE PEACEFUL USES OF OUTER SPACE INFORMATION FURNISHED IN CONFORMITY WITH THE CONVENTION ON REGISTRATION OF OBJECTS LAUNCHED INTO OUTER SPACE Note verbale dated 15 April 1997 from the Permanent Mission of the Russian Federation to the United Nations (Vienna) addressed to the Secretary-General The Permanent Mission of the Russian Federation to the United Nations (Vienna) presents its compliments to the Secretary-General of the United Nations and, in accordance with article IV of the Convention on Registration of Objects Launched into Outer Space,* has the honour to transmit information concerning space objects launched by the Russian Federation from April to December 1996 and conce rning Russian space objects which ceased to exist within those same periods of time and are no longer in Earth orbit (see annex). *General Assembly resolution 3235 (XXIX), annex, of 12 November 1974. V.97-23994T ST/SG/SER.E/320 Page 2 ST/SG/SER.E/320 Page 3 ST/SG/SER.E/320 Page 4 ST/SG/SER.E/320 Page 5 ST/SG/SER.E/320 Page 6 ST/SG/SER.E/320 Page 7 ST/SG/SER.E/320 Page 8 ST/SG/SER.E/320 Page 9 Annex* REGISTRATION DATA ON SPACE OBJECTS LAUNCHED BY THE RUSSIAN FEDERATION IN APRIL 1996 1. In April 1996, the Russian Federation launched the following space objects: Basic orbit characteristics Date of Apogee Perigee Inclination Period No. Name of space object launching (km) (km) (degrees) (minutes) General purpose of space object 2985 Priroda 23 April 347 220 51.6 89.9 The Priroda module is intended for the per- (launched by a Proton carrier rocket formance of research and experiments by the crew from the Baikonur launch site) of the Mir orbital station, partly under the programme of cooperation between the Russian Federation and the United States of America 2986 Cosmos-2332 24 April 1 585 304 83 104 The space object is intended for assignments on (launched by a Cosmos carrier rocket behalf of the Ministry of Defence of the Russian from the Plesetsk launch site) Federation 2. -
L AUNCH SYSTEMS Databk7 Collected.Book Page 18 Monday, September 14, 2009 2:53 PM Databk7 Collected.Book Page 19 Monday, September 14, 2009 2:53 PM
databk7_collected.book Page 17 Monday, September 14, 2009 2:53 PM CHAPTER TWO L AUNCH SYSTEMS databk7_collected.book Page 18 Monday, September 14, 2009 2:53 PM databk7_collected.book Page 19 Monday, September 14, 2009 2:53 PM CHAPTER TWO L AUNCH SYSTEMS Introduction Launch systems provide access to space, necessary for the majority of NASA’s activities. During the decade from 1989–1998, NASA used two types of launch systems, one consisting of several families of expendable launch vehicles (ELV) and the second consisting of the world’s only partially reusable launch system—the Space Shuttle. A significant challenge NASA faced during the decade was the development of technologies needed to design and implement a new reusable launch system that would prove less expensive than the Shuttle. Although some attempts seemed promising, none succeeded. This chapter addresses most subjects relating to access to space and space transportation. It discusses and describes ELVs, the Space Shuttle in its launch vehicle function, and NASA’s attempts to develop new launch systems. Tables relating to each launch vehicle’s characteristics are included. The other functions of the Space Shuttle—as a scientific laboratory, staging area for repair missions, and a prime element of the Space Station program—are discussed in the next chapter, Human Spaceflight. This chapter also provides a brief review of launch systems in the past decade, an overview of policy relating to launch systems, a summary of the management of NASA’s launch systems programs, and tables of funding data. The Last Decade Reviewed (1979–1988) From 1979 through 1988, NASA used families of ELVs that had seen service during the previous decade. -
Architecture of Afterlife: Future Cemetery in Metropolis
ARCHITECTURE OF AFTERLIFE: FUTURE CEMETERY IN METROPOLIS A DARCH PROJECT SUBMITTED TO THE GRADUATE DIVISION OF THE UNIVERSITY OF HAWAI‘I AT MĀNOA IN PARTIAL FULFILLMENT OF THE REQUIREMENTS FOR THE DEGREE OF DOCTOR OF ARCHITECTURE MAY 2017 BY SHIYU SONG DArch Committee: Joyce Noe, Chairperson William Chapman Brian Takahashi Key Words: Conventional Cemetery, Contemporary Cemetery, Future Cemetery, High-technology Innovation Architecture of Afterlife: Future Cemetery in Metropolis Shiyu Song April 2017 We certify that we have read this Doctorate Project and that, in our opinion, it is satisfactory in scope and quality in partial fulfillment for the degree of Doctor of Architecture in the School of Architecture, University of Hawai‘i at Mānoa. Doctorate Project Committee ___________________________________ Joyce Noe ___________________________________ William Chapman ___________________________________ Brian Takahashi Acknowledgments I dedicate this thesis to everyone in my life. I would like to express my deepest appreciation to my committee chair, Professor Joyce Noe, for her support, guidance and insight throughout this doctoral project. Many thanks to my wonderful committee members William Chapman and Brian Takahashi for their precious and valuable guidance and support. Salute to my dear professor Spencer Leineweber who inspires me in spirit and work ethic. Thanks to all the professors for your teaching and encouragement imparted on me throughout my years of study. After all these years of study, finally, I understand why we need to study and how important education is. Overall, this dissertation is an emotional research product. As an idealist, I choose this topic as a lesson for myself to understand life through death. The more I delve into the notion of death, the better I appreciate life itself, and knowing every individual human being is a bless; everyday is a present is my best learning outcome. -
Fast Solar Wind Monitor (BMSW): Description and First Results
Space Sci Rev (2013) 175:165–182 DOI 10.1007/s11214-013-9979-4 Fast Solar Wind Monitor (BMSW): Description and First Results Jana Šafránková · Zdenekˇ Nemeˇ cekˇ · Lubomír Prechˇ · Georgy Zastenker · Ivo Cermákˇ · Lev Chesalin · Arnošt Komárek · Jakub Vaverka · Martin Beránek · Jiríˇ Pavl˚u · Elena Gavrilova · Boris Karimov · Arkadii Leibov Received: 4 September 2012 / Accepted: 19 March 2013 / Published online: 6 April 2013 © Springer Science+Business Media Dordrecht 2013 Abstract Monitoring of solar wind parameters is a key problem of the Space Weather pro- gram. The paper presents a description of a novel fast solar wind monitor (Bright Monitor of the Solar Wind, BMSW) and the first results of its measurements of plasma moments with a time resolution ranging from seconds to 31 ms. The method of the fast monitoring is based on simultaneous measurements of the total ion flux and ion integral energy spectrum by six nearly identical Faraday cups (FCs). Three of them are dedicated to determination of the ion flow direction, whereas other three equipped with control grids supplied by a re- tarding potential are used for a determination of the density, temperature, and speed of the plasma flow. The paper introduces not only the measuring methods, the FCs design, and modes of operation, but brings the examples of time series of measurements and their com- parison with the observations of other spacecraft as well as the first results of an analysis of frequency spectra of solar wind fluctuations within the ion kinetic scale, examples of rapid measurements at the ramp of an interplanetary shock and investigations of fast variations of alpha particle content. -
1998 Year in Review
Associate Administrator for Commercial Space Transportation (AST) January 1999 COMMERCIAL SPACE TRANSPORTATION: 1998 YEAR IN REVIEW Cover Photo Credits (from left): International Launch Services (1998). Image is of the Atlas 2AS launch on June 18, 1998, from Cape Canaveral Air Station. It successfully orbited the Intelsat 805 communications satellite for Intelsat. Boeing Corporation (1998). Image is of the Delta 2 7920 launch on September 8, 1998, from Vandenberg Air Force Base. It successfully orbited five Iridium communications satellites for Iridium LLP. Lockheed Martin Corporation (1998). Image is of the Athena 2 awaiting its maiden launch on January 6, 1998, from Spaceport Florida. It successfully deployed the NASA Lunar Prospector. Orbital Sciences Corporation (1998). Image is of the Taurus 1 launch from Vandenberg Air Force Base on February 10, 1998. It successfully orbited the Geosat Follow-On 1 military remote sensing satellite for the Department of Defense, two Orbcomm satellites and the Celestis 2 funerary payload for Celestis Corporation. Orbital Sciences Corporation (1998). Image is of the Pegasus XL launch on December 5, 1998, from Vandenberg Air Force Base. It successfully orbited the Sub-millimeter Wave Astronomy Satellite for the Smithsonian Astrophysical Observatory. 1998 YEAR IN REVIEW INTRODUCTION INTRODUCTION In 1998, U.S. launch service providers conducted In addition, 1998 saw continuing demand for 22 launches licensed by the Federal Aviation launches to deploy the world’s first low Earth Administration (FAA), an increase of 29 percent orbit (LEO) communication systems. In 1998, over the 17 launches conducted in 1997. Of there were 17 commercial launches to LEO, 14 these 22, 17 were for commercial or international of which were for the Iridium, Globalstar, and customers, resulting in a 47 percent share of the Orbcomm LEO communications constellations. -
Annexe: Summary of Soviet and Russian Space Science Missions
Contents Introduction by the authors ..................................... ix Acknowledgments ............................................ xi Glossary .................................................. xiii Terminological and translation notes ..............................xv Reference notes .............................................xvii List of tables ............................................... xix List of illustrations ......................................... xxiii List of figures .............................................xxvii 1 Early space science ........................................... 1 Space science by balloon....................................... 3 Scientific flights into the atmosphere: the Akademik series..............14 Scientific test flights with animals ................................20 The idea of a scientific Earth satellite .............................23 Scientific objectives of the first Earth satellites . ....................25 Key people .................................................25 Instead, Prosteishy Sputnik .....................................27 PS2......................................................29 Object D: the first large scientific satellite in orbit....................33 Early space science: what was learned? ............................37 References .................................................39 2 Deepening our understanding ....................................43 Following Sputnik: the MS series ................................43 Cosmos 5 and Starfish: introducing Yuri Galperin -
Yakutia) “…The Republic of Sakha (Yakutia) Is the Largest Region in the Russian Federation and One of the Richest in Natural Resources
Investor's Guide to the Republic of Sakha (Yakutia) “…The Republic of Sakha (Yakutia) is the largest region in the Russian Federation and one of the richest in natural resources. Needless to say, the stable and dynamic development of Yakutia is of key importance to both the Far Eastern Federal District and all of Russia…” President of the Russian Federation Vladimir Putin “One of the fundamental priorities of the Government of the Republic of Sakha (Yakutia) is to develop comfortable conditions for business and investment activities to ensure dynamic economic growth” Head of the Republic of Sakha (Yakutia) Egor Borisov 2 Contents Welcome from Egor Borisov, Head of the Republic of Sakha (Yakutia) 5 Overview of the Republic of Sakha (Yakutia) 6 Interesting facts about the Republic of Sakha (Yakutia) 7 Strategic priorities of the Republic of Sakha (Yakutia) investment policy 8 Seven reasons to start a business in the Republic of Sakha (Yakutia) 10 1. Rich reserves of natural resources 10 2. Significant business development potential for the extraction and processing of mineral and fossil resources 12 3. Unique geographical location 15 4. Stable credit rating 16 5. Convenient conditions for investment activity 18 6. Developed infrastructure for the support of small and medium-sized enterprises 19 7. High level of social and economic development 20 Investment infrastructure 22 Interaction with large businesses 24 Interaction with small and medium-sized enterprises 25 Other organisations and institutions 26 Practical information on doing business in the Republic of Sakha (Yakutia) 27 Public-Private Partnership 29 Information for small and medium-sized enterprises 31 Appendix 1. -
2015 October
TTSIQ #13 page 1 OCTOBER 2015 www.nasa.gov/press-release/nasa-confirms-evidence-that-liquid-water-flows-on-today-s-mars Flash! Sept. 28, 2015: www.space.com/30674-flowing-water-on-mars-discovery-pictures.html www.space.com/30673-water-flows-on-mars-discovery.html - “boosting odds for life!” These dark, narrow, 100 meter~yards long streaks called “recurring slope lineae” flowing downhill on Mars are inferred to have been formed by contemporary flowing water www.space.com/30683-mars-liquid-water-astronaut-exploration.html INDEX 2 Co-sponsoring Organizations NEWS SECTION pp. 3-56 3-13 Earth Orbit and Mission to Planet Earth 13-14 Space Tourism 15-20 Cislunar Space and the Moon 20-28 Mars 29-33 Asteroids & Comets 34-47 Other Planets & their moons 48-56 Starbound ARTICLES & ESSAY SECTION pp 56-84 56 Replace "Pluto the Dwarf Planet" with "Pluto-Charon Binary Planet" 61 Kepler Shipyards: an Innovative force that could reshape the future 64 Moon Fans + Mars Fans => Collaboration on Joint Project Areas 65 Editor’s List of Needed Science Missions 66 Skyfields 68 Alan Bean: from “Moonwalker” to Artist 69 Economic Assessment and Systems Analysis of an Evolvable Lunar Architecture that Leverages Commercial Space Capabilities and Public-Private-Partnerships 71 An Evolved Commercialized International Space Station 74 Remembrance of Dr. APJ Abdul Kalam 75 The Problem of Rational Investment of Capital in Sustainable Futures on Earth and in Space 75 Recommendations to Overcome Non-Technical Challenges to Cleaning Up Orbital Debris STUDENTS & TEACHERS pp 85-96 Past TTSIQ issues are online at: www.moonsociety.org/international/ttsiq/ and at: www.nss.org/tothestarsOO TTSIQ #13 page 2 OCTOBER 2015 TTSIQ Sponsor Organizations 1. -
The SUNSAT Micro Satellite Program
The SUNSAT Micro Satellite Program: Technical performance and limits of imaging micro satellites Sias Mostert, Thys Cronje and Francois du Plessis Department of Electrical and Electronic Engineering Stellenbosch University. Private Bag X1, MATIELAND, 7602. South Africa. Fax: +27 21 808 4981. Internet: [email protected]. http:\\sunsat.ee.sun.ac.za ABSTRACT - This paper examines the technical performance of the SUNSAT micro satellite bus, which is supporting the high resolution imager (HRI) payload on the micro satellite which is scheduled for launch in December 1998. A number of existing remote sensing satellites are investigated to determine some key parameters by which a micro satellite remote sensing mission should be evaluated. The SUNSAT 1 HRI instrument is then evaluated in this context and future possible missions suggested which is suitable for micro satellite missions. 1. INTRODUCTION SUNSAT, a professional micro satellite developed by a team of graduate students and engineers at Stellenbosch University in South Africa, is scheduled for launch from Vandenberg Airforce Base on a Delta II rocket, currently manifested for December 1998. The Flight Model hardware is complete and the pre-flight testing is drawing to a close. This paper examines the technical performance and capabilities of SUNSAT 1 micro satellite supporting the high resolution imager (HRI). Laboratory measured performance data are provided for the 15 m resolution 3 color CCD imager of SUNSAT, developed jointly by Stellenbosch University, the Council for Scientific Industrial Research (CSIR) in South Africa and the Korean Advanced Institute of Science and Technology (KAIST). The performance of the Attitude Determination and Control System (ADCS), which is required to support the imager, is described. -
Quarterly Launch Report
Commercial Space Transportation QUARTERLY LAUNCH REPORT Featuring the launch results from the previous quarter and forecasts for the next two quarters 4th Quarter 1997 U n i t e d S t a t e s D e p a r t m e n t o f T r a n s p o r t a t i o n • F e d e r a l A v i a t i o n A d m i n i s t r a t i o n A s s o c i a t e A d m i n i s t r a t o r f o r C o m m e r c i a l S p a c e T r a n s p o r t a t i o n QUARTERLY LAUNCH REPORT 1 4TH QUARTER 1997 REPORT Objectives This report summarizes recent and scheduled worldwide commercial, civil, and military orbital space launch events. Scheduled launches listed in this report are vehicle/payload combinations that have been identified in open sources, including industry references, company manifests, periodicals, and government documents. Note that such dates are subject to change. This report highlights commercial launch activities, classifying commercial launches as one or more of the following: • Internationally competed launch events (i.e., launch opportunities considered available in principle to competitors in the international launch services market), • Any launches licensed by the Office of the Associate Administrator for Commercial Space Transportation of the Federal Aviation Administration under U.S. -
Lunar Prospector Collection
Guide to the Lunar Prospector Project Records, 1995-1998 AFS8000.5-LP NASA Ames History Office NASA Ames Research Center Contact Information: NASA Ames Research Center NASA Ames History Office Mail-Stop 207-1 Moffett Field, CA 94035-1000 Phone: (650) 604-1032 Email: [email protected] URL: http://history.arc.nasa.gov/ Collection processed by: April Gage, June 2011 Table of Contents Descriptive Summary .......................................................................................................... 1 Administrative Information ................................................................................................ 2 Administrative History ........................................................................................................ 2 Scope and Content .............................................................................................................. 4 System of Arrangement ...................................................................................................... 4 Series Descriptions .............................................................................................................. 5 Indexing Terms ................................................................................................................... 7 Container List ...................................................................................................................... 8 NASA Ames History Office Descriptive Summary Title: Lunar Prospector Project Records, 1995-1998 Collection Number: AFS8000.5-LP -
Commercial Spacecraft Mission Model Update
Commercial Space Transportation Advisory Committee (COMSTAC) Report of the COMSTAC Technology & Innovation Working Group Commercial Spacecraft Mission Model Update May 1998 Associate Administrator for Commercial Space Transportation Federal Aviation Administration U.S. Department of Transportation M5528/98ml Printed for DOT/FAA/AST by Rocketdyne Propulsion & Power, Boeing North American, Inc. Report of the COMSTAC Technology & Innovation Working Group COMMERCIAL SPACECRAFT MISSION MODEL UPDATE May 1998 Paul Fuller, Chairman Technology & Innovation Working Group Commercial Space Transportation Advisory Committee (COMSTAC) Associative Administrator for Commercial Space Transportation Federal Aviation Administration U.S. Department of Transportation TABLE OF CONTENTS COMMERCIAL MISSION MODEL UPDATE........................................................................ 1 1. Introduction................................................................................................................ 1 2. 1998 Mission Model Update Methodology.................................................................. 1 3. Conclusions ................................................................................................................ 2 4. Recommendations....................................................................................................... 3 5. References .................................................................................................................. 3 APPENDIX A – 1998 DISCUSSION AND RESULTS........................................................