Radiation—Risks, Dose Assessment, and Shielding
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Photographs Written Historical and Descriptive
CAPE CANAVERAL AIR FORCE STATION, MISSILE ASSEMBLY HAER FL-8-B BUILDING AE HAER FL-8-B (John F. Kennedy Space Center, Hanger AE) Cape Canaveral Brevard County Florida PHOTOGRAPHS WRITTEN HISTORICAL AND DESCRIPTIVE DATA HISTORIC AMERICAN ENGINEERING RECORD SOUTHEAST REGIONAL OFFICE National Park Service U.S. Department of the Interior 100 Alabama St. NW Atlanta, GA 30303 HISTORIC AMERICAN ENGINEERING RECORD CAPE CANAVERAL AIR FORCE STATION, MISSILE ASSEMBLY BUILDING AE (Hangar AE) HAER NO. FL-8-B Location: Hangar Road, Cape Canaveral Air Force Station (CCAFS), Industrial Area, Brevard County, Florida. USGS Cape Canaveral, Florida, Quadrangle. Universal Transverse Mercator Coordinates: E 540610 N 3151547, Zone 17, NAD 1983. Date of Construction: 1959 Present Owner: National Aeronautics and Space Administration (NASA) Present Use: Home to NASA’s Launch Services Program (LSP) and the Launch Vehicle Data Center (LVDC). The LVDC allows engineers to monitor telemetry data during unmanned rocket launches. Significance: Missile Assembly Building AE, commonly called Hangar AE, is nationally significant as the telemetry station for NASA KSC’s unmanned Expendable Launch Vehicle (ELV) program. Since 1961, the building has been the principal facility for monitoring telemetry communications data during ELV launches and until 1995 it processed scientifically significant ELV satellite payloads. Still in operation, Hangar AE is essential to the continuing mission and success of NASA’s unmanned rocket launch program at KSC. It is eligible for listing on the National Register of Historic Places (NRHP) under Criterion A in the area of Space Exploration as Kennedy Space Center’s (KSC) original Mission Control Center for its program of unmanned launch missions and under Criterion C as a contributing resource in the CCAFS Industrial Area Historic District. -
Fusion Space Propulsion-A Shorter Time Frame Than You Think
FusionFusion SpaceSpace Propulsion--Propulsion-- AA ShorterShorter TimeTime FrameFrame thanthan YouYou ThinkThink JohnJohn F.F. SantariusSantarius FusionFusion TechnologyTechnology InstituteInstitute UniversityUniversity ofof WisconsinWisconsin JANNAFJANNAF Monterey,Monterey, 5-85-8 DecemberDecember 20052005 D-3He and Pulsed-Power Fusion Approaches Would Shorten Development Times $$$ Fusion D-3HeD-3He FRC,FRC, dipole,dipole, Rocket spheromak,spheromak, ST;ST; Pulsed-powerPulsed-power MTF,MTF, PHD,PHD, fast-ignitorfast-ignitor JFS 2005 Fusion Technology Institute 2 D-3He Fusion Will Provide Capabilities Not Available from Other Propulsion Options 107 Fusion ) s 6 / 10 10 kW/kg m ( y 1 kW/kg t i c o l 5 0.1 kW/kg e 10 v t Nuclear us (fission) Ga s-core fission ha electric x 4 E 10 Nuclear thermal Chemical 103 10-5 10-4 10-3 10-2 10-1 1 10 Thrust-to-weight ratio JFS 2005 Fusion Technology Institute 3 Predicted Specific Power of D-3He Magnetic Fusion Rockets Is Attractive (>1 kW/kg) • Predictions based on reasonably detailed magnetic fusion rocket studies. Specific Power First Author Year Configuration (kW/kg) Borowski 1987 Spheromak 10.5 Borowski 1987 Spherical torus 5.8 Santarius 1988 Tandem mirror 1.2 Bussard 1990 Riggatron 3.9 Teller 1991 Dipole 1.0 Nakashima 1994 Field-reversed configuration 1.0 Emrich 2000 Gasdynamic mirror 130 Thio 2002 Magnetized-target fusion 50 Williams 2003 Spherical torus 8.7 Cheung 2004 Colliding-beam FRC 1.5 JFS 2005 Fusion Technology Institute 4 Fusion Propulsion Would Enable Fast and Efficient Solar-System Travel • Fusion propulsion would dramatically reduce trip times (shown below) or increase payload fractions. -
DIRECT FUSION DRIVE for Interstellar Exploration S.A
Journal of the British Interplanetary Society VOLUME 72 NO.2 FEBRUARY 2019 General interstellar issue DIRECT FUSION DRIVE for Interstellar Exploration S.A. Cohen et al. INTERMEDIATE BEAMERS FOR STARSHOT: Probes to the Sun’s Inner Gravity Focus James Benford & Gregory Matloff REALITY, THE BREAKTHROUGH INITIATIVES and Prospects for Colonization of Space Edd Wheeler A GRAVITATIONAL WAVE TRANSMITTER A.A. Jackson and Gregory Benford CORRESPONDENCE www.bis-space.com ISSN 0007-084X PUBLICATION DATE: 29 APRIL 2019 Submitting papers International Advisory Board to JBIS JBIS welcomes the submission of technical Rachel Armstrong, Newcastle University, UK papers for publication dealing with technical Peter Bainum, Howard University, USA reviews, research, technology and engineering in astronautics and related fields. Stephen Baxter, Science & Science Fiction Writer, UK James Benford, Microwave Sciences, California, USA Text should be: James Biggs, The University of Strathclyde, UK ■ As concise as the content allows – typically 5,000 to 6,000 words. Shorter papers (Technical Notes) Anu Bowman, Foundation for Enterprise Development, California, USA will also be considered; longer papers will only Gerald Cleaver, Baylor University, USA be considered in exceptional circumstances – for Charles Cockell, University of Edinburgh, UK example, in the case of a major subject review. Ian A. Crawford, Birkbeck College London, UK ■ Source references should be inserted in the text in square brackets – [1] – and then listed at the Adam Crowl, Icarus Interstellar, Australia end of the paper. Eric W. Davis, Institute for Advanced Studies at Austin, USA ■ Illustration references should be cited in Kathryn Denning, York University, Toronto, Canada numerical order in the text; those not cited in the Martyn Fogg, Probability Research Group, UK text risk omission. -
<> CRONOLOGIA DE LOS SATÉLITES ARTIFICIALES DE LA
1 SATELITES ARTIFICIALES. Capítulo 5º Subcap. 10 <> CRONOLOGIA DE LOS SATÉLITES ARTIFICIALES DE LA TIERRA. Esta es una relación cronológica de todos los lanzamientos de satélites artificiales de nuestro planeta, con independencia de su éxito o fracaso, tanto en el disparo como en órbita. Significa pues que muchos de ellos no han alcanzado el espacio y fueron destruidos. Se señala en primer lugar (a la izquierda) su nombre, seguido de la fecha del lanzamiento, el país al que pertenece el satélite (que puede ser otro distinto al que lo lanza) y el tipo de satélite; este último aspecto podría no corresponderse en exactitud dado que algunos son de finalidad múltiple. En los lanzamientos múltiples, cada satélite figura separado (salvo en los casos de fracaso, en que no llegan a separarse) pero naturalmente en la misma fecha y juntos. NO ESTÁN incluidos los llevados en vuelos tripulados, si bien se citan en el programa de satélites correspondiente y en el capítulo de “Cronología general de lanzamientos”. .SATÉLITE Fecha País Tipo SPUTNIK F1 15.05.1957 URSS Experimental o tecnológico SPUTNIK F2 21.08.1957 URSS Experimental o tecnológico SPUTNIK 01 04.10.1957 URSS Experimental o tecnológico SPUTNIK 02 03.11.1957 URSS Científico VANGUARD-1A 06.12.1957 USA Experimental o tecnológico EXPLORER 01 31.01.1958 USA Científico VANGUARD-1B 05.02.1958 USA Experimental o tecnológico EXPLORER 02 05.03.1958 USA Científico VANGUARD-1 17.03.1958 USA Experimental o tecnológico EXPLORER 03 26.03.1958 USA Científico SPUTNIK D1 27.04.1958 URSS Geodésico VANGUARD-2A -
The Technologies That Could Prevent More Mysteries Like That of Missing Malaysia Airlines Flight 370 Page 20
July-August 2014 The technologies that could prevent more mysteries like that of missing Malaysia Airlines Flight 370 Page 20 Hypersonics after WaveRider p.10 40 tons on a dime at Mars p. 36 A PUBLICATION OF THE AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS AIAA Progress in Astronautics and Aeronautics AIAA’s popular book series Progress in Astronautics and Aeronautics features books that present a particular, well- defi ned subject refl ecting advances in the fi elds of aerospace science, engineering, and/or technology. POPULAR TITLES Tactical and Strategic Missile Guidance, Sixth Edition Paul Zarchan 1026 pages This best-selling title provides an in-depth look at tactical and strategic missile guidance using common language, notation, and perspective. The sixth edition includes six new chapters on topics related to improving missile guidance system performance and understanding key design concepts and tradeoffs. ISBN: 978-1-60086-894-8 List Price: $134.95 “AIAA Best Seller” AIAA Member Price: $104.95 Morphing Aerospace Vehicles and Structures John Valasek 286 pages Morphing Aerospace Vehicles and Structures is a synthesis of the relevant disciplines and applications involved in the morphing of fi xed wing fl ight vehicles. The book is organized into three major sections: Bio-Inspiration; Control and Dynamics; and Smart Materials and Structures. Most chapters are both tutorial and research-oriented in nature, covering elementary concepts through advanced – and in many cases novel – methodologies. ISBN: 978-1-60086-903-7 “Features the -
Fusion Propulsion
Fusion Propulsion Opening the Solar System Frontier John F Santarius Lecture 28 Resources from Space NEEP 533/ Geology 533 / Astronomy 533 / EMA 601 University of Wisconsin March 31, 2004 Key Points • D-3He appears to be the fusion fuel of choice for space applications. • D-3He fusion will provide capabilities not available from other propulsion options. • Several configurations appear promising for space propulsion, particularly the field-reversed configuration (FRC), magnetized-target fusion (MTF), spheromak, and spherical torus. • Successful development of D-3He fusion would provide attractive propulsion, power, and materials processing capabilities. JFS 2004 Fusion Technology Institute 2 A Prophecy Whose Time Will Come “The short-lived Uranium Age will see the dawn of space flight; the succeeding era of fusion power will witness its fulfillment.” From the essay “The Planets Are Not Enough” (1961). JFS 2004 Fusion Technology Institute 3 D-3He Fusion Will Provide Capabilities Not Available from Other Propulsion Options 107 Fusion ) s 6 / 10 10 kW/kg m ( y 1 kW/kg t i c o l 5 0.1 kW/kg e 10 v t Nuclear us (fission) Ga s-core fission ha electric x 4 E 10 Nuclear thermal Chemical 103 10-5 10-4 10-3 10-2 10-1 1 10 Thrust-to-weight ratio JFS 2004 Fusion Technology Institute 4 At the Predicted Specific Power, α=1-10 kW/kg, Fusion Propulsion Would Enable Attractive Solar-System Travel • Comparison of trip times and payload fractions for chemical and fusion rockets: Fast human transport Efficient cargo transport 1000 1 900 0.9 ) s 800 0.8 on -
RSA Envision Event Explorer 4.0.3 Installation Guide
RSA enVision Event Explorer 4.1 Installation Guide Revision 1 Contact Information Go to the RSA corporate web site for regional Customer Support telephone and fax numbers: www.rsa.com Trademarks RSA, the RSA Logo, RSA enVision Event Explorer, and EMC are either registered trademarks or trademarks of EMC Corporation in the United States and/or other countries. All other trademarks used herein are the property of their respective owners. For a list of EMC trademarks, go to www.rsa.com/legal/trademarks_list.pdf. License agreement This software and the associated documentation are proprietary and confidential to EMC, are furnished under license, and may be used and copied only in accordance with the terms of such license and with the inclusion of the copyright notice below. This software and the documentation, and any copies thereof, may not be provided or otherwise made available to any other person. No title to or ownership of the software or documentation or any intellectual property rights thereto is hereby transferred. Any unauthorized use or reproduction of this software and the documentation may be subject to civil and/or criminal liability. This software is subject to change without notice and should not be construed as a commitment by EMC. Third-party licenses This product may include software developed by parties other than RSA. The text of the license agreements applicable to third-party software in this product may be viewed in the thirdpartylicenses.pdf file. Note on encryption technologies This product may contain encryption technology. Many countries prohibit or restrict the use, import, or export of encryption technologies, and current use, import, and export regulations should be followed when using, importing or exporting this product. -
CYBERSECURITY When Will You Be Hacked?
SUFFOLK ACADEMY OF LAW The Educational Arm of the Suffolk County Bar Association 560 Wheeler Road, Hauppauge, NY 11788 (631) 234-5588 CYBERSECURITY When Will You Be Hacked? FACULTY Victor John Yannacone, Jr., Esq. April 26, 2017 Suffolk County Bar Center, NY Cybersecurity Part I 12 May 2017 COURSE MATERIALS 1. A cybersecurity primer 3 – 1.1. Cybersecurity practices for law firms 5 – 1.2. Cybersecurity and the future of law firms 11 – 2. Information Security 14 – 2.1. An information security policy 33 – 2.2. Data Privacy & Cloud Computing 39 – 2.3. Encryption 47 – 3. Computer security 51 – 3.1. NIST Cybersecurity Framework 77 – 4. Cybersecurity chain of trust; third party vendors 113 – 5. Ransomware 117 – 5.1. Exploit kits 132 – 6. Botnets 137 – 7. BIOS 139 – 7.1. Universal Extensible Firmware Interface (UEFI) 154– 8. Operating Systems 172 – 8.1. Microsoft Windows 197 – 8.2. macOS 236– 8.3. Open source operating system comparison 263 – 9. Firmware 273 – 10. Endpoint Security Buyers Guide 278 – 11. Glossaries & Acronym Dictionaries 11.1. Common Computer Abbreviations 282 – 11.2. BABEL 285 – 11.3. Information Technology Acronymns 291 – 11.4. Glossary of Operating System Terms 372 – 2 Cyber Security Primer Network outages, hacking, computer viruses, and similar incidents affect our lives in ways that range from inconvenient to life-threatening. As the number of mobile users, digital applications, and data networks increase, so do the opportunities for exploitation. Cyber security, also referred to as information technology security, focuses on protecting computers, networks, programs, and data from unintended or unauthorized access, change, or destruction. -
Our First Quarter Century of Achievement ... Just the Beginning I
NASA Press Kit National Aeronautics and 251hAnniversary October 1983 Space Administration 1958-1983 >\ Our First Quarter Century of Achievement ... Just the Beginning i RELEASE ND: 83-132 September 1983 NOTE TO EDITORS : NASA is observing its 25th anniversary. The space agency opened for business on Oct. 1, 1958. The information attached sumnarizes what has been achieved in these 25 years. It was prepared as an aid to broadcasters, writers and editors who need historical, statistical and chronological material. Those needing further information may call or write: NASA Headquarters, Code LFD-10, News and Information Branch, Washington, D. C. 20546; 202/755-8370. Photographs to illustrate any of this material may be obtained by calling or writing: NASA Headquarters, Code LFD-10, Photo and Motion Pictures, Washington, D. C. 20546; 202/755-8366. bQy#qt&*&Mary G. itzpatrick Acting Chief, News and Information Branch Public Affairs Division Cover Art Top row, left to right: ffComnandDestruct Center," 1967, Artist Paul Calle, left; ?'View from Mimas," 1981, features on a Saturnian satellite, by Artist Ron Miller, center; ftP1umes,*tSTS- 4 launch, Artist Chet Jezierski,right; aeronautical research mural, Artist Bob McCall, 1977, on display at the Visitors Center at Dryden Flight Research Facility, Edwards, Calif. iii OUR FIRST QUARTER CENTER OF ACHIEVEMENT A-1 -3 SPACE FLIGHT B-1 - 19 SPACE SCIENCE c-1 - 20 SPACE APPLICATIQNS D-1 - 12 AERONAUTICS E-1 - 10 TRACKING AND DATA ACQUISITION F-1 - 5 INTERNATIONAL PROGRAMS G-1 - 5 TECHNOLOGY UTILIZATION H-1 - 5 NASA INSTALLATIONS 1-1 - 9 NASA LAUNCH RECORD J-1 - 49 ASTRONAUTS K-1 - 13 FINE ARTS PRQGRAM L-1 - 7 S IGN I F ICANT QUOTAT IONS frl-1 - 4 NASA ADvIINISTRATORS N-1 - 7 SELECTED NASA PHOTOGRAPHS 0-1 - 12 National Aeronautics and Space Administration Washington, D.C. -
Open Dissertation.Pdf
The Pennsylvania State University The Graduate School TRANSHUMANISM: EVOLUTIONARY LOGIC, RHETORIC, AND THE FUTURE A Dissertation in English by Andrew Pilsch c 2011 Andrew Pilsch Submitted in Partial Fulfillment of the Requirements for the Degree of Doctor of Philosophy May 2011 The dissertation of Andrew Pilsch was reviewed and approved∗ by the following: Richard Doyle Professor of English Dissertation Advisor, Chair of Committee Jeffrey Nealon Liberal Arts Research Professor of English Mark Morrisson Professor of English and Science, Technology, and Society Robert Yarber Distinguished Professor of Art Mark Morrisson Graduate Program Director Professor of English ∗Signatures are on file in the Graduate School. Abstract This project traces the discursive formation called “transhumanism” through vari- ous incarnations in twentieth century science, philosophy, and science fiction. While subject to no single, clear definition, I follow most of the major thinkers in the topic by defining transhumanism as a discourse surrounding the view of human beings as subject to ongoing evolutionary processes. Humanism, from Descartes forward, has histori- cally viewed the human as stable; transhumanism, instead, views humans as constantly evolving and changing, whether through technological or cultural means. The degree of change, the direction of said change, and the shape the species will take in the distant future, however, are all topics upon which there is little consensus in transhuman circles. In tracing this discourse, I accomplish a number of things. First, previously dis- parate zones of academic inquiry–poststructural philosophy, science studies, literary modernism and postmodernism, etc.–are shown to be united by a common vocabulary when viewed from the perspective of the “evolutionary futurism” suggested by tran- shuman thinkers. -
NASA Is Not Archiving All Potentially Valuable Data
‘“L, United States General Acchunting Office \ Report to the Chairman, Committee on Science, Space and Technology, House of Representatives November 1990 SPACE OPERATIONS NASA Is Not Archiving All Potentially Valuable Data GAO/IMTEC-91-3 Information Management and Technology Division B-240427 November 2,199O The Honorable Robert A. Roe Chairman, Committee on Science, Space, and Technology House of Representatives Dear Mr. Chairman: On March 2, 1990, we reported on how well the National Aeronautics and Space Administration (NASA) managed, stored, and archived space science data from past missions. This present report, as agreed with your office, discusses other data management issues, including (1) whether NASA is archiving its most valuable data, and (2) the extent to which a mechanism exists for obtaining input from the scientific community on what types of space science data should be archived. As arranged with your office, unless you publicly announce the contents of this report earlier, we plan no further distribution until 30 days from the date of this letter. We will then give copies to appropriate congressional committees, the Administrator of NASA, and other interested parties upon request. This work was performed under the direction of Samuel W. Howlin, Director for Defense and Security Information Systems, who can be reached at (202) 275-4649. Other major contributors are listed in appendix IX. Sincerely yours, Ralph V. Carlone Assistant Comptroller General Executive Summary The National Aeronautics and Space Administration (NASA) is respon- Purpose sible for space exploration and for managing, archiving, and dissemi- nating space science data. Since 1958, NASA has spent billions on its space science programs and successfully launched over 260 scientific missions. -
Mass Beam Propulsion, an Overview
See discussions, stats, and author profiles for this publication at: https://www.researchgate.net/publication/303682465 Mass beam propulsion, an overview Article · January 2015 CITATIONS READS 0 260 2 authors, including: Adam Crowl Icarus Interstellar 22 PUBLICATIONS 22 CITATIONS SEE PROFILE Some of the authors of this publication are also working on these related projects: Galactic Surveys View project BFR to Titan View project All content following this page was uploaded by Adam Crowl on 21 August 2018. The user has requested enhancement of the downloaded file. Mass BeamJBIS, Propulsion, Vol. 68, Anpp.?-?, Overview 2015 MASS BEAM PROPULSION, AN OVERVIEW GERALD D. NORDLEY1 AND ADAM JAMES CROWL2 1. 1238 Prescott Avenue, Sunnyvale, CA 94089, USA. 2. 4 Ulmarra Crescent, Strathpine 4500, Queensland, Australia Email: [email protected] An alternative to rockets is to push spacecraft with a reflected beam. The advantage is that it leaves most of the propulsion system mass at rest. Use of mass beams, as opposed to photons, allows great efficiency by adjusting the beam velocity so the reflected mass is left near zero velocity relative to the source. There is no intrinsic limit to the proper frame map velocity that can be achieved. To make a propulsion system, subsystems need to be developed to acquire propulsive energy, accelerate the mass into a collimated beam, insure that the mass reaches the spacecraft and reflect the mass. A number of approaches to these requirements have been proposed and are summarized here. Generally no new scientific discoveries or breakthroughs are needed. These concepts are supported by ongoing progress in robotics, in nanometre scale technologies and in those technologies needed to use of space resources for the automated manufacture of space-based solar power facilities.