Perspectives on Early Spaceflight
Total Page:16
File Type:pdf, Size:1020Kb
Load more
Recommended publications
-
Orbital Debris: a Chronology
NASA/TP-1999-208856 January 1999 Orbital Debris: A Chronology David S. F. Portree Houston, Texas Joseph P. Loftus, Jr Lwldon B. Johnson Space Center Houston, Texas David S. F. Portree is a freelance writer working in Houston_ Texas Contents List of Figures ................................................................................................................ iv Preface ........................................................................................................................... v Acknowledgments ......................................................................................................... vii Acronyms and Abbreviations ........................................................................................ ix The Chronology ............................................................................................................. 1 1961 ......................................................................................................................... 4 1962 ......................................................................................................................... 5 963 ......................................................................................................................... 5 964 ......................................................................................................................... 6 965 ......................................................................................................................... 6 966 ........................................................................................................................ -
Les Puissances Spatiales Qui Montent
SOMMAIRE Les puissances spatiales qui montent Par Philippe VOLVERT 1 SOMMAIRE 2 SOMMAIRE Les puissances spatiales qui montent Par Philippe VOLVERT 3 SOMMAIRE SOMMAIRE SOMMAIRE ..................................................................................................................................................... 4 INTRODUCTION ............................................................................................................................................. 5 L’ESPACE AU PAYS DU SOLEIL LEVANT ..................................................................................................... 6 LES AMBITIONS CHINOISES ........................................................................................................................ 14 L’INDEPENDANCE SPATIALE INDIENNE ................................................................................................... 24 L’ESPACE ET LE RESTE DU MONDE ........................................................................................................... 29 LES GRANDES DATES DE L’ASTRONAUTIQUE JAPONAISE .................................................................... 36 LES GRANDES DATES DE L’ASTRONAUTIQUE CHINOISE ....................................................................... 39 LES GRANDES DATES DE L’ASTRONAUTIQUE INDIENNE........................................................................ 41 LES VOLS HABITES ...................................................................................................................................... -
A Low-Cost Launch Assistance System for Orbital Launch Vehicles
Hindawi Publishing Corporation International Journal of Aerospace Engineering Volume 2012, Article ID 830536, 10 pages doi:10.1155/2012/830536 Review Article A Low-Cost Launch Assistance System for Orbital Launch Vehicles Oleg Nizhnik ERATO Maenaka Human-Sensing Fusion Project, 8111, Shosha 2167, Hyogo-ken, Himeji-shi, Japan Correspondence should be addressed to Oleg Nizhnik, [email protected] Received 17 February 2012; Revised 6 April 2012; Accepted 16 April 2012 Academic Editor: Kenneth M. Sobel Copyright © 2012 Oleg Nizhnik. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited. The author reviews the state of art of nonrocket launch assistance systems (LASs) for spaceflight focusing on air launch options. The author proposes an alternative technologically feasible LAS based on a combination of approaches: air launch, high-altitude balloon, and tethered LAS. Proposed LAS can be implemented with the existing off-the-shelf hardware delivering 7 kg to low-earth orbit for the 5200 USD per kg. Proposed design can deliver larger reduction in price and larger orbital payloads with the future advances in the aerostats, ropes, electrical motors, and terrestrial power networks. 1. Introduction point to the progress in the orbital delivery systems for these additional payload classes. Spaceflight is the mature engineering discipline—54 years old as of 2012. But seemingly paradoxically, it still relies solely 2. Overview of Previously Proposed LAS on the hardware and methodology developed in the very beginning of the spaceflight era. Modernly, still heavily-used A lot of proposals have been made to implement nonrocket Soyuz launch vehicle systems (LVSs) are the evolutionary LASandarelistedinTable 1. -
Navy Space and Astronautics Orientation. INSTITUTION Bureau of Naval Personnel, Washington, D
DOCUMENT RESUME ED 070 566 SE 013 889 AUTHOR Herron, R. G. TITLE Navy Space and Astronautics Orientation. INSTITUTION Bureau of Naval Personnel, Washington, D. C.; Naval Personnel Program Support Activity, Washington, D. C. REPORT NO NAVPERS- 10488 PUB DATE 67 NOTE 235p. '2 EDRS PRICE MF-$0.65 HC-$9.87 DESCRIPTORS Aerospace Education; AerospaceTechnology; *Instructional Materials; Military Science; *Military Training; Navigatioti; *Post Secondary Education; *Space Sciences; *Supplementary Textbooks; Textbooks ABSTRACT Fundamental concepts of the spatial environment, technologies, and applications are presented in this manual prepared for senior officers and key civilian employees. Following basic information on the atmosphere, solar system, and intergalactic space, a detailed review is included of astrodynamics, rocket propulsion, bioastronautics, auxiliary spacecraft survival systems, and atmospheric entry.Subsequentlythere is an analysis of naval space facilities, and satellite applications, especially those of naval interests, are discussed with a background of launch techniques, spatial data gathering, communications programs ,of)servation techniques, measurements by geodetic and navigation systems. Included is a description of space defense and future developments of both national and international space programs. Moreover, commercial systems are mentioned, such as the 85-pound Early Bird (Intelsat I) Intelsat II series, global Intelsat III series, and Soviet-made elMolnlyan satellites. The total of 29 men and one woman orbiting the earth In-1961-67 are tabulated in terms of their names, flight series, launching dates, orbit designations, or biting periods,. stand-up periods, and extra vehicular activity records. Besides numerous illustrations, a list ofsignificantspace launches and a glossary of special terms are included in the manual appendices along with two tables of frequencybanddesignation. -
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. -
The Annual Compendium of Commercial Space Transportation: 2017
Federal Aviation Administration The Annual Compendium of Commercial Space Transportation: 2017 January 2017 Annual Compendium of Commercial Space Transportation: 2017 i Contents 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 (2017) Publication produced for FAA AST by The Tauri Group under contract. 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. ii Annual Compendium of Commercial Space Transportation: 2017 GENERAL CONTENTS Executive Summary 1 Introduction 5 Launch Vehicles 9 Launch and Reentry Sites 21 Payloads 35 2016 Launch Events 39 2017 Annual Commercial Space Transportation Forecast 45 Space Transportation Law and Policy 83 Appendices 89 Orbital Launch Vehicle Fact Sheets 100 iii Contents DETAILED CONTENTS EXECUTIVE SUMMARY . -
Seniors and Juniors 29 July – 04 August (Opening Ceremony to the Closing Ceremony) WLOCLAWEK, POLAND FINAL SCORE LISTS SENIORS
2018 FAI S WORLD CHAMPIONSHIPS for SPACE MODELS Seniors and Juniors 29 July – 04 August (Opening Ceremony to the Closing Ceremony) WLOCLAWEK, POLAND FINAL SCORE LISTS SENIORS 1 FAI JURY: Jury president Mr. Narve JENSEN Norway Jury member Mr. Vladimir SVEC Slovakia Jury member Mr. Tadeusz KASPRZYCKI Poland FAI JUDGES OF S5 AND S7: Judge chief Mr. Zoran PELAGIC Slovakia Judge Mr. Valery HRABOUSKI Belarus Judge Mr. Arnis BACA Latvia Judge Mr. Michał FILAS Poland Judge Mr. Ion GUZU Romania DIMENSION MEASURING OF S5 AND S7: Team chief Mr. Wojciech WOJDYŁO Poland Assistant Mr. Maciej ŁUKASZEWSKI Poland Assistant Mr. Andrzej PIKOSZ Poland RANGE SAFETY OFICERS: For Seniors Mr. Denis PRIDANNIKOW Ukraine Assistant Mr. Marcin POKRZYWA Poland For Juniors Mrs. Janka KAJANOWA Slovakia Assistant Mr. Jarosław ZASUŃ Poland Director of the Championships: Mr. Marek KOŹIŃSKI Poland Sports director: Mrs. Ewa DUDZIAK-PRZYBYTEK Poland Assistant sports director: Mr. Mateusz NIEBIELSKI Poland IT service manager: Mr. Krzysztof TURMIŃSKI Poland Secretary of the Championship: Mr. Mateusz DYBA Poland 2 2018 FAI S WORLD CHAMPIONSHIPS for SPACE MODELS 31’st July 2018 Seniors and Juniors Air temperaturę: 33 - 38˚C Wind speed: 1-3 m/s Kruszyn Airfield S1B SENIORS - TEAMS No. Team name 1 Competitor 2 Competitor 3 Competitor Sum Place 1 CHN 708,4 702,1 800,8 2 211,3 I 2 SLO 708,3 628,3 700,2 2 036,8 II 3 USA 618,2 656,2 706,1 1 980,5 III 4 SVK 682,6 633,0 646,1 1 961,7 4 5 RUS 657,7 665,0 591,3 1 914,0 5 6 UKR 770,0 215,2 642,4 1 627,6 6 7 SRB 534,7 569,2 490,9 1 594,8 7 8 POL 569,6 767,0 193,1 1 529,7 8 9 CZE 492,4 466,1 516,8 1 475,3 9 10 ROU 494,3 483,3 493,2 1 470,8 10 11 GBR 530,9 0,0 588,4 1 119,3 11 12 ESP 482,4 0,0 575,5 1 057,9 12 13 BUL 515,0 526,8 0,0 1 041,8 13 14 ITA 654,1 654,1 14 15 LTU 121,0 0,0 0,0 121,0 15 16 JPN 0,0 0,0 16 Jury President ________________________ Sport Director ________________________ Mr. -
The Egyptian, September 28, 1966
Southern Illinois University Carbondale OpenSIUC September 1966 Daily Egyptian 1966 9-28-1966 The gE yptian, September 28, 1966 Daily Egyptian Staff Follow this and additional works at: http://opensiuc.lib.siu.edu/de_September1966 Volume 48, Issue 6 Recommended Citation , . "The gE yptian, September 28, 1966." (Sep 1966). This Article is brought to you for free and open access by the Daily Egyptian 1966 at OpenSIUC. It has been accepted for inclusion in September 1966 by an authorized administrator of OpenSIUC. For more information, please contact [email protected]. I ' q.- Protest Meeting Sends Derogates To sm -Officiah A representation from a said, "I didil't believe a stu protest meeting on student dent should be forced into a bouslng will attempt to conler dorm owne\l by out of town With SIU officials today. If people, I don't believe the they are successful, others University should help tbe hlg from the protest meeting plan business force out the little to gather on campus in a show man.. It of suppon for the negotiations. Lannin said Sfudents are N Committee bf two students being forced to bteak p,e con and tWo Iandldrds to flleet with tracts they m;tde. · for un offiCials was ;to be IIPpointed approved housill~, . He S3ld after' ~e 'meeting' at City Hall a number of Jati!U~da are mt [f~sday night. The committee going to releaslh,\,e ~tudents ropes to meet with president from these contracts if the Delyte W,' Morris,' . -- University forces them to live Carbondale anor0I'Y and in approved housing. -
Profile 2007
Profile 2007 Japan Nissan Motor Co., Ltd. Global Communications and CSR Division Nissan: Enriching People’s Lives Communication and CSR Department 17-1, Ginza 6-chome, Chuo-ku, Tokyo 104-8023, Japan Phone: +81(0)3-5565-2141 Fax: +81(0)3-3546-2669 North America Nissan North America, Inc. Corporate Communications 333 Commerce Street, Nashville, TN 37201-3300, U.S.A. Phone: +1(615)725-1000 Fax: +1(615)725-3343 Europe Nissan Europe S.A.S. Communications Department Parc de Pissaloup 13 Avenue Jean d’Alembert B.P. 123, 78194 Trappes Cedex, France Phone: +33(0)1 30 13 66 00 Fax: +33(0)1 30 13 68 70 Corporate Information Website www.nissan-global.com/EN/ 2007-06 OUTLINE OFNISSAN MESSAGE FROM THE PRESIDENT AND CEO The global automotive industry has entered a new era – one that can be expected Today, with a much healthier balance sheet, our R&D budget is more than double to change almost every facet of the car in the years ahead. the level of 1999. The impact is much more than double, however, because over the same period we have significantly increased the efficiency of our R&D activities. This is an exciting time. In pursuit of environmentally sustainable mobility, we are now engaged in a great race – one of the greatest engineering competitions in This allows us to intensively pursue a broad range of technologies under “Nissan history. The outcome will deliver significant benefit to humanity. And within our Green Program 2010,” our environmental blueprint. And thanks to our alliance with industry it will distinguish the winners from the rest. -
Vysoké Učení Technické V Brně Vývoj Raketových
VYSOKÉ UČENÍ TECHNICKÉ V BRNĚ BRNO UNIVERSITY OF TECHNOLOGY FAKULTA STROJNÍHO INŽENÝRSTVÍ LETECKÝ ÚSTAV FACULTY OF MECHANICAL ENGINEERING INSTITUTE OF AEROSPACE ENGINEERING VÝVOJ RAKETOVÝCH MOTORŮ DEVELOPMENT OF ROCKET ENGINES BAKALÁŘSKÁ PRÁCE BACHELOR'S THESIS AUTOR PRÁCE PETER MARCINKO AUTHOR VEDOUCÍ PRÁCE Ing. ROSTISLAV KOŠTIAL SUPERVISOR BRNO 2014 Vysoké učení technické v Brně, Fakulta strojního inženýrství Letecký ústav Akademický rok: 2013/2014 ZADÁNÍ BAKALÁŘSKÉ PRÁCE student(ka): Peter Marcinko který/která studuje v bakalářském studijním programu obor: Strojní inženýrství (2301R016) Ředitel ústavu Vám v souladu se zákonem č.111/1998 o vysokých školách a se Studijním a zkušebním řádem VUT v Brně určuje následující téma bakalářské práce: Vývoj raketových motorů v anglickém jazyce: Development of rocket engines Stručná charakteristika problematiky úkolu: Zdůvodnění zavedení a rozvoje raketových motorů. Přehled dosud vyvinutých, vyvíjených a využívaných významných raketových nosičů, pro kosmické účely, jejich stručný technický popis a technicko-taktická data. Perspektivy dalšího rozvoje a nově vyvíjené projekty nosných raket pro kosmické účely. Cíle bakalářské práce: Zpracovat historicko-technický vývoj raketových motorů používaných pro kosmické účely. Seznam odborné literatury: [1]Časopis Letectví a kosmonautika [2]Internetové zdroje [3]Rakety a Kosmodromy Vedoucí bakalářské práce: Ing. Rostislav Koštial Termín odevzdání bakalářské práce je stanoven časovým plánem akademického roku 2013/2014. V Brně, dne L.S. _______________________________ _______________________________ doc. Ing. Jaroslav Juračka, Ph.D. doc. Ing. Jaroslav Katolický, Ph.D. Ředitel ústavu Děkan fakulty Abstrakt Táto práca popisuje vývoj raketových motorov od prvých rakiet až po súčasnosť. Práca je rozdelená na tri základné časti. Prvá časť popisuje základné fyzikálne princípy, ktorými sa musí raketa počas letu riadiť. -
A Low-Cost Launch Assistance System for Orbital Launch Vehicles
Hindawi Publishing Corporation International Journal of Aerospace Engineering Volume 2012, Article ID 830536, 10 pages doi:10.1155/2012/830536 Review Article A Low-Cost Launch Assistance System for Orbital Launch Vehicles Oleg Nizhnik ERATO Maenaka Human-Sensing Fusion Project, 8111, Shosha 2167, Hyogo-ken, Himeji-shi, Japan Correspondence should be addressed to Oleg Nizhnik, [email protected] Received 17 February 2012; Revised 6 April 2012; Accepted 16 April 2012 Academic Editor: Kenneth M. Sobel Copyright © 2012 Oleg Nizhnik. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited. The author reviews the state of art of nonrocket launch assistance systems (LASs) for spaceflight focusing on air launch options. The author proposes an alternative technologically feasible LAS based on a combination of approaches: air launch, high-altitude balloon, and tethered LAS. Proposed LAS can be implemented with the existing off-the-shelf hardware delivering 7 kg to low-earth orbit for the 5200 USD per kg. Proposed design can deliver larger reduction in price and larger orbital payloads with the future advances in the aerostats, ropes, electrical motors, and terrestrial power networks. 1. Introduction point to the progress in the orbital delivery systems for these additional payload classes. Spaceflight is the mature engineering discipline—54 years old as of 2012. But seemingly paradoxically, it still relies solely 2. Overview of Previously Proposed LAS on the hardware and methodology developed in the very beginning of the spaceflight era. Modernly, still heavily-used A lot of proposals have been made to implement nonrocket Soyuz launch vehicle systems (LVSs) are the evolutionary LASandarelistedinTable 1. -
Medium-Earth Orbit Begins 300 Miles 0.95
0.05 g 60,000 miles Geosynchronous orbit 22,300 miles - — Hard vacuum 1,000 miles -- Medium-Earth orbit begins 300 miles 0.95 g 100 miles — Low-Earth orbit begins 60 miles Astronaut wings awarded 50 miles —. for ramjet engines 28 miles — Limit for turbojet engines 20 miles, --- Stratosphere begins 10 miles • On the following pages appears a Center History Office; and Air Force variety of information and statistical Space Command Public Affairs Office. Col. Gilbert Siegert, USAF, provided material about space—particularly. • military activity in space. This technical advice. almanac was compiled by the staff of 6,4tr Force Magazine,tith assistance and information from Dr. R. W. • Stuidevant, Air Force Space Command History Office; Tina Figures that appear in this section Thompson, editor of TRW Space Log: will not always agree because of . Phillip S. Clark, Molniya Space different cutoff dates, rounding,. or Consultancy, Whitton, UK; Theresa different methods of reporting. The Foley; Dr. Harry N. Waldron Ill, Air information is intended to illustrate Force Space and Missile Systems trends in space activity. • Compiled by Tamar A. Mehuron, Associate Editor Space Terms Ferret. A satellite whose Remote imaging. Images of primary function is to gather Earth generated from space- electronic intelligence, such craft that provide data for Aerospace. A physical region as microwave, radar, radio, Magnetosphere. A region mapping, construction, made up of Earth's atmo- and voice emissions. dominated by Earth's magneti agriculture, oil and gas sphere and the space beyond. field, which traps charged exploration, news media Geostationary Earth orbit. A particles, including those in services, and the like.