USAF's Ballistic Missiles --- 1954-1964 a Concise History by DR
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Footnotes for ATOMIC ADVENTURES
Footnotes for ATOMIC ADVENTURES Secret Islands, Forgotten N-Rays, and Isotopic Murder - A Journey into the Wild World of Nuclear Science By James Mahaffey While writing ATOMIC ADVENTURES, I tried to be careful not to venture off into subplots, however interesting they seemed to me, and keep the story flowing and progressing at the right tempo. Some subjects were too fascinating to leave alone, and there were bits of further information that I just could not abandon. The result is many footnotes at the bottom of pages, available to the reader to absorb at his or her discretion. To get the full load of information from this book, one needs to read the footnotes. Some may seem trivia, but some are clarifying and instructive. This scheme works adequately for a printed book, but not so well with an otherwise expertly read audio version. Some footnotes are short enough to be inserted into the audio stream, but some are a rambling half page of dense information. I was very pleased when Blackstone Audio agreed wholeheartedly that we needed to include all of my footnotes in this version of ATOMIC ADVENTURES, and we came up with this added feature: All 231 footnotes in this included text, plus all the photos and explanatory diagrams that were included in the text. I hope you enjoy reading some footnotes while listening to Keith Sellon-Wright tell the stories in ATOMIC ADVENTURES. James Mahaffey April 2017 2 Author’s Note Stories Told at Night around the Glow of the Reactor Always striving to beat the Atlanta Theater over on Edgewood Avenue, the Forsyth Theater was pleased to snag a one-week engagement of the world famous Harry Houdini, extraordinary magician and escape artist, starting April 19, 1915.1 It was issued an operating license, no. -
Materials for Liquid Propulsion Systems
https://ntrs.nasa.gov/search.jsp?R=20160008869 2019-08-29T17:47:59+00:00Z CHAPTER 12 Materials for Liquid Propulsion Systems John A. Halchak Consultant, Los Angeles, California James L. Cannon NASA Marshall Space Flight Center, Huntsville, Alabama Corey Brown Aerojet-Rocketdyne, West Palm Beach, Florida 12.1 Introduction Earth to orbit launch vehicles are propelled by rocket engines and motors, both liquid and solid. This chapter will discuss liquid engines. The heart of a launch vehicle is its engine. The remainder of the vehicle (with the notable exceptions of the payload and guidance system) is an aero structure to support the propellant tanks which provide the fuel and oxidizer to feed the engine or engines. The basic principle behind a rocket engine is straightforward. The engine is a means to convert potential thermochemical energy of one or more propellants into exhaust jet kinetic energy. Fuel and oxidizer are burned in a combustion chamber where they create hot gases under high pressure. These hot gases are allowed to expand through a nozzle. The molecules of hot gas are first constricted by the throat of the nozzle (de-Laval nozzle) which forces them to accelerate; then as the nozzle flares outwards, they expand and further accelerate. It is the mass of the combustion gases times their velocity, reacting against the walls of the combustion chamber and nozzle, which produce thrust according to Newton’s third law: for every action there is an equal and opposite reaction. [1] Solid rocket motors are cheaper to manufacture and offer good values for their cost. -
Small Satellite Launchers
SMALL SATELLITE LAUNCHERS NewSpace Index 2020/04/20 Current status and time from development start to the first successful or planned orbital launch NEWSPACE.IM Northrop Grumman Pegasus 1990 Scorpius Space Launch Demi-Sprite ? Makeyev OKB Shtil 1998 Interorbital Systems NEPTUNE N1 ? SpaceX Falcon 1e 2008 Interstellar Technologies Zero 2021 MT Aerospace MTA, WARR, Daneo ? Rocket Lab Electron 2017 Nammo North Star 2020 CTA VLM 2020 Acrux Montenegro ? Frontier Astronautics ? ? Earth to Sky ? 2021 Zero 2 Infinity Bloostar ? CASIC / ExPace Kuaizhou-1A (Fei Tian 1) 2017 SpaceLS Prometheus-1 ? MISHAAL Aerospace M-OV ? CONAE Tronador II 2020 TLON Space Aventura I ? Rocketcrafters Intrepid-1 2020 ARCA Space Haas 2CA ? Aerojet Rocketdyne SPARK / Super Strypi 2015 Generation Orbit GoLauncher 2 ? PLD Space Miura 5 (Arion 2) 2021 Swiss Space Systems SOAR 2018 Heliaq ALV-2 ? Gilmour Space Eris-S 2021 Roketsan UFS 2023 Independence-X DNLV 2021 Beyond Earth ? ? Bagaveev Corporation Bagaveev ? Open Space Orbital Neutrino I ? LIA Aerospace Procyon 2026 JAXA SS-520-4 2017 Swedish Space Corporation Rainbow 2021 SpinLaunch ? 2022 Pipeline2Space ? ? Perigee Blue Whale 2020 Link Space New Line 1 2021 Lin Industrial Taymyr-1A ? Leaf Space Primo ? Firefly 2020 Exos Aerospace Jaguar ? Cubecab Cab-3A 2022 Celestia Aerospace Space Arrow CM ? bluShift Aerospace Red Dwarf 2022 Black Arrow Black Arrow 2 ? Tranquility Aerospace Devon Two ? Masterra Space MINSAT-2000 2021 LEO Launcher & Logistics ? ? ISRO SSLV (PSLV Light) 2020 Wagner Industries Konshu ? VSAT ? ? VALT -
The Secret History of Extraterrestrials: Advanced Technology And
The Secret History of Extraterrestrials “With our present knowledge of the cosmos, there is now a real possibility of evolved and intelligent civilizations elsewhere in the vast cosmological space. And possible visitations and even encounters can no longer be ignored. Naturally we must tread with caution and not jump to conclusions too easily and too readily; but we must also keep an open mind and respect those bold investigators who apply rigorous research and common sense to this fascinating although very debated hypothesis. Len Kasten is such an investigator, and his book The Secret History of Extraterrestrials is a must for the libraries of all seekers of truth with unbiased minds.” ROBERT BAUVAL, AUTHOR OF THE ORION MYSTERY , MESSAGE OF THE SPHINX, AND BLACK GENESIS “Len Kasten has provided an up-to-date survey of the vast array of issues that are now emerging into the public consciousness regarding an extraterrestrial presence engaging the human race. For those who want to jump right into the pool and not just sit on the side and dangle their feet, take the plunge with The Secret History of Extraterrestrials.” STEPHEN BASSETT, EXECUTIVE DIRECTOR OF PARADIGM RESEARCH GROUP “You can always count on Len Kasten to take you on a spellbinding galactic adventure, for he never fails to seek out ideas and theories that challenge your assumptions of what is true while firing your imagination. Whether in this dimension or another, be it past or future, your travels with Len Kasten will open your mind and introduce you to realities and experiences, you may have mistakenly assumed can exist only as fiction.” PAUL DAVIDS, DIRECTOR/PRODUCER OF JESUS IN INDIA AND EXECUTIVE PRODUCER/COWRITER OF ROSWELL: THE UFO COVERUP “This comprehensive book covers some of the most intriguing UFO and alien-contact cases ever reported. -
NASA News National Aeronautics and Space Administration Washington
NASA News National Aeronautics and Space Administration Washington. D C 20546 AC 202 755-8370 For Release IMMEDIATE Press Kit Project Intelsat V-D RELEASE NO: 82-30 Contents GENERAL RELEASE 1 ATLAS CENTAUR, LAUNCH VEHICLE STATISTICS 3 LAUNCH OPERATIONS 4 LAUNCH SEQUENCE FOR INTELSAT V-D 5 THE NASA INTELSAT TEAM 6 CONTRACTORS 7 /lNASA-News-Belease-82^TOl INTELSAT N82-22295 "\ (SATELLITE SCHEDULED FOR LAUNCH (National (Aeronautics and Space Administration) 8 p I CSCL 22A Unclas I 00/15 18771 February 26, 1982 NASA News National Aeronautics and Space Administration Washington. D C 20546 AC 202 755-8370 For Release Dick McCormack Headquarters, Washington, D.C. IMMEDIATE (Phone: 202/755-8104) RELEASE NO: 82-30 INTELSAT SATELLITE SCHEDULED FOR LAUNCH Intelsat V-D, the fourth of a new series of nine inter- national telecommunications satellites owned and operated by the 105-nation International Telecommunications Satellite Organiza- tion (Intelsat), is scheduled to be launched by the NASA Kennedy Space Center on board an Atlas Centaur launch vehicle no earlier than March 4, 1982, from Cape Canaveral, Fla. The three Intelsat Vs were successfully launched by NASA in December 1980, May 1981 and December 1981. Intelsat V-D weighs 1,928 kilograms (4,251 pounds) at launch and has almost double the communications capability of early satellites in the Intelsat series — 12,000 voice circuits and two color television channels. It will be positioned in geosyn- chronous orbit over the Indian Ocean as the prime Intelsat satel- lite to provide communications services between Europe, the Middle East and the Far East. -
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 Pedagogy of Diminishing Returns: Scientific Involution Across Three Generations of Nuclear Weapons Science
3 A Pedagogy of Diminishing Returns: Scientific Involution across Three Generations of Nuclear Weapons Science Hugh Gusterson In science studies we hear a lot about the construction of facts, the building of net- works, and the growth of disciplines, but much less about the withering, decay, or arte- riosclerosis of fields of knowledge (brought on either through natural exhaustion of a particular approach or through external constraints). We have a disciplinary bias toward scientific evolution and revolution rather than what I am here calling involu- tion.1 A generation of historians, sociologists, and anthropologists of science has learned from actor-network theory and the sociology of scientific knowledge (SSK) to focus on the building of scientific institutions and facts, and from Thomas Kuhn to expect a certain historical rhythm in the evolution of scientific fields of knowledge: first, a dynamic burst of creativity (the “revolution”) as the foundational ideas of the new field are laid down; second, a period of “normal science” in which gaps are filled in as the new knowledge is institutionalized; and, finally, as puzzles emerge that can- not be fully explained by the established paradigm, a new burst of creativity as another generation redefines the fundamental precepts of the field.2 In this essay, looking at three generations of nuclear weapons designers, I follow and then depart from the Kuhnian script. Although the first two generations of nuclear weapons scientists con- formed perfectly to the Kuhnian storyline, the final story -
Desind Finding
NATIONAL AIR AND SPACE ARCHIVES Herbert Stephen Desind Collection Accession No. 1997-0014 NASM 9A00657 National Air and Space Museum Smithsonian Institution Washington, DC Brian D. Nicklas © Smithsonian Institution, 2003 NASM Archives Desind Collection 1997-0014 Herbert Stephen Desind Collection 109 Cubic Feet, 305 Boxes Biographical Note Herbert Stephen Desind was a Washington, DC area native born on January 15, 1945, raised in Silver Spring, Maryland and educated at the University of Maryland. He obtained his BA degree in Communications at Maryland in 1967, and began working in the local public schools as a science teacher. At the time of his death, in October 1992, he was a high school teacher and a freelance writer/lecturer on spaceflight. Desind also was an avid model rocketeer, specializing in using the Estes Cineroc, a model rocket with an 8mm movie camera mounted in the nose. To many members of the National Association of Rocketry (NAR), he was known as “Mr. Cineroc.” His extensive requests worldwide for information and photographs of rocketry programs even led to a visit from FBI agents who asked him about the nature of his activities. Mr. Desind used the collection to support his writings in NAR publications, and his building scale model rockets for NAR competitions. Desind also used the material in the classroom, and in promoting model rocket clubs to foster an interest in spaceflight among his students. Desind entered the NASA Teacher in Space program in 1985, but it is not clear how far along his submission rose in the selection process. He was not a semi-finalist, although he had a strong application. -
Eisenhower and the Gaither Report: the Influence of a Committee of Experts on National Security Policy in the Late 19501
Eisenhower and the Gaither Report: The Influence of a Committee of Experts on National Security Policy in the Late 19501 David Lindsey Snead Richmond, Virginia B.A., Virginia Polytechnic Institute and State Univenity, 1990 M.A., Virginia Polytechnic Institute and State Uuivenity, 1991 A Dissertation presented to the Graduate Faculty of the Univenity of Virginia in Candidacy for the Degree of Doctor of Philosophy Department of History Univenity of Virginia January 1997 ii (c) Copyright by David Lindsey Snead All Rights Reserved January 1997 iii Eisenhower and the Gaither Report: The Influence of a Committee of Experts on National Security Policy in the Late 19505 by David Lindsey Snead Melvyn P. Leffler, Chairman (ABSTRACT) As the United States reeled from the Soviet Union's launch of Sputnik in late 1957, President Dwight D. Eisenhower received a top secret report prepared by a committee of leading scientific, business, and military experts. The panel, called the Gaither committee in recognition of its first chairman, H. Rowan Gaither, Jr., emphasized both the inadequacy of U.S. defense measures designed to protect the civil population and the vulnerability of the country's strategic nuclear forces in the event of a Soviet attack. The Gaither committee viewed these defense measures--ranging from a missile system to defend the continental United States to the construction of shelters to protect the population from radioactive fallout-and the maintenance of sufficient strategic forces to launch military strikes against Soviet targets as essential for the preservation of U.S. security. It concluded that in the case of a surprise Soviet nuclear attack the United States would be unable to defend itselfwith any degree of success. -
Adjutant-General*
AN N U AL REPORT** S7*Tf Oh- THE WAR 171959 GOVEfi/VjvjEN'f DOCUMENTS ADJUTANT-GENERAL* OF THE STATE OF NEW YORK. FOR THE YEAR 1901. Registers of the Sixty-ninth, Seventieth, Seventy-first, Seventy-second, Seventy-third and Seventy- fourth Regiments of Infantry. TRANSMITTED TO THE LEGISLATURE JANUARY 7, 1902. SERIAL No. 28. ALBANY J. B. LYON COMPANY, STATE PRINTERS 1902 NEW YORK STATE LIBRARY ALBANY SIXTY-NINTH REGIMENT. ABBEBTON, JOHN.— Age, 21 years. Enlisted at New York city, to serve tliree years, and mustered in as private, Co. 0, October 9, 1861; deserted, November 15, 1861, at New York city. ABBITT, THOMAS.—• Age, 28 years. Enlisted at New York city, to serve tbree years, and mustered in as private, Co. A, Marcb 1, 1864; deserted, Marcb 29,1864, at Stevensburg, Ya.; also borne as Abbott. ABBOTT, JAMES H.— Age, 19 years. Enlisted at Plattsburgb, to serve one year, and mustered in as private, Co. H, August 25, 1864; captured in action, October 30, 1864, near Petersburg, Ya.; no furtber record; also borne as James Abott and Abbatt. ABEAMS, see Abrams. ABEAMS, "WILLIAM.— Age, 27 years. Enlisted at Jamaica, to serve one year, and mustered in as private, Co. O, October 5,1864; wounded in action, Marcb 25, 1865, before Petersburg, Ya.; promoted corporal, June 21, 1865; mustered out witb com• pany, June 30, 1865, near Alexandria, Ya.; also borne as Abeams. ACKEBMANN, SAMUEL.— Age, 34 years. Enlisted, August 27, 1864, at Poughkeepsie, to serve tbree years; mustered in as private, Co. E, September 3, 1864; wounded on picket and died of his wounds, October 28, 1864, at City Point Hospital, Ya.; also borne as Ackerman. -
Barrow Hanley Presentation
PORTFOLIO REVIEW MUNICIPAL EMPLOYEES’ RETIREMENT SYSTEM OF LOUISIANA JOHN P. HARLOE, CFA COLEMAN HUBBARD, CFA APRIL 18, 2019 BARROW, HANLEY, MEWHINNEY & STRAUSS, LLC 2200 Ross Avenue | 31st Floor | Dallas, TX 75201-2761 Telephone: 214.665.1900 | [email protected] FIRM OVERVIEW BARROW, HANLEY, MEWHINNEY & STRAUSS, LLC 1 BARROW HANLEY: A LEGACY OF STABILITY STABILITY OF THE FIRM ❑ 40-Year-Old Firm, Founded in 1979 in Dallas, Texas, USA – $76 Billion AUM (3/31/19) ❑ Four-Decade History of Unique Organizational Stability ❑ Institutional Focus – Boutique Culture ❑ 99 Employees, Including 57 Investment Professionals ❑ Significant Employee Equity Ownership STABILITY OF THE PROCESS ❑ For the Past 40 Years, the BHMS Value-Oriented Approach to Stock Selection has Always Emphasized the Importance of Dividends and the Protection of Assets ❑ Our Firm’s Size and Stature Provides Direct Access to the Senior Management of Publicly-Traded Companies Worldwide Benefiting our Research ❑ BHMS has a 40-Year Record of Consistently Producing Alpha in the Large, Mid, and Small Cap Sectors of the Market with a Proven Ability to Protect Assets in Down Markets through Risk Control and Yield STABILITY OF OUR PARTNERSHIPS ❑ Uniquely Stable Client Base – 45 Clients for More than 20 Years ❑ Experienced in Management of Large Portfolios – 25+ Larger than $500 Million ❑ Serving Clients Globally: North America, Europe, Asia, Australia, Africa BARROW, HANLEY, MEWHINNEY & STRAUSS, LLC 2 BRIEF HISTORY OF BHMS Global Value Dividend 2019 Bank Loans 2018 ESG Strategies -
Analysis of a Heavy Lift Launch Vehicle Design Using Small Liquid
Analysis of a Heavy Lift Launch Vehicle Design Using Small Liquid Rocket Engines by DAVID PHILLIP RUSS S.B., Massachusetts Institute of Technology 1987 SUBMITTED IN PARTIAL FULFILLMENT OF THE REQUIREMENTS FOR THE DEGREE OF MASTER OF SCIENCE IN AERONAUTICS AND ASTRONAUTICS at the MASSACHUSETTS INSTITUTE OF TECHNOLOGY May 1988 ® David P. Russ 1988 The author hereby grants M.I.T. and Hughes Aircraft Company permission to reproduce and to distribute copies of this thesis document in whole or in part. Signature of Author Department of Aeronautics and Astronautics December 18, 1987 Reviewed by C. P. Rubin Hughes Aircraft Company Certified by Professor Walter M. Hollister Thesis Supervjsor, Departmer of Aeronautics and Astronautics .. Accepted by , .AU Professor Harold Y. Wachman Chairman, Depart'rmental Graduate Committee Department of Aeronautics and Astronautics MAY i od ;WITHDRAWfIN i M.I.1W.i..: P. I LBRARt S UBAer 7:Ir_ Aero Analysis of a Heavy Lift Launch Vehicle Design Using Small Liquid Rocket Engines by David P. Russ Submitted to the Department of Aeronautics and Astronautics in partial fulfillment of the requirements for the degree of Master of Science in Aeronautics and Astronautics May, 1988 Abstract The trend in launch vehicle design has been to increase performance by using en- gines of greater and greater complexity, which has a negative effect on cost and reliability. However, a design making use of over 300 small, simple rocket engines can deliver over 340,000 lbs to low Earth orbit. This design, derived by using the rocket equations to size the major components, features a 42 ft.