Us - USSR Strategic Offensive Nuclear Forces 1946 - 1989
Total Page:16
File Type:pdf, Size:1020Kb
Load more
Recommended publications
-
Collezione Per Genova
1958-1978: 20 anni di sperimentazioni spaziali in Occidente La collezione copre il ventennio 1958-1978 che è stato particolarmente importante nella storia della esplorazio- ne spaziale, in quanto ha posto le basi delle conoscenze tecnico-scientifiche necessarie per andare nello spa- zio in sicurezza e per imparare ad utilizzare le grandi potenzialità offerte dallo spazio per varie esigenze civili e militari. Nel clima di guerra fredda, lo spazio è stato fin dai primi tempi, utilizzato dagli Americani per tenere sotto con- trollo l’avversario e le sue dotazioni militari, in risposta ad analoghe misure adottate dai Sovietici. Per preparare le missioni umane nello spazio, era indispensabile raccogliere dati e conoscenze sull’alta atmo- sfera e sulle radiazioni che si incontrano nello spazio che circonda la Terra. Dopo la sfida lanciata da Kennedy, gli Americani dovettero anche prepararsi allo sbarco dell’uomo sulla Luna ed intensificarono gli sforzi per conoscere l’ambiente lunare. Fin dai primi anni, le sonde automatiche fecero compiere progressi giganteschi alla conoscenza del sistema solare. Ben presto si imparò ad utilizzare i satelliti per la comunicazione intercontinentale e il supporto alla navigazio- ne, per le previsioni meteorologiche, per l’osservazione della Terra. La Collezione testimonia anche i primi tentativi delle nuove “potenze spaziali” che si avvicinano al nuovo mon- do dei satelliti, che inizialmente erano monopolio delle due Superpotenze URSS e USA. L’Italia, con San Mar- co, diventò il terzo Paese al mondo a lanciare un proprio satellite e allestì a Malindi la prima base equatoriale, che fu largamente utilizzata dalla NASA. Alla fine degli anni ’60 anche l’Europa entrò attivamente nell’arena spaziale, lanciando i propri satelliti scientifici e di telecomunicazione dalla propria base equatoriale di Kourou. -
Thierry Moreau
Compilation and Hardware Support for Approximate Acceleration Thierry Moreau, Adrian Sampson, Andre Baixo, Mark Wyse, Ben Ransford, Jacob Nelson, Hadi Esmaeilzadeh (Georgia Tech), Luis Ceze and Mark Oskin University of Washington [email protected] Theme: 2384.004 1 Thierry Moreau Approximate Computing Aims to exploit application resilience to trade-off quality for efficiency 2 Thierry Moreau Approximate Computing 3 Thierry Moreau Approximate Computing ✅ Accurate ✅ Approximate ❌ Expensive ✅ Cheap 4 Thierry Moreau 5 Thierry Moreau 6 Thierry Moreau 7 Thierry Moreau Neural Networks as Approximate Accelerators CPU Esmaeilzadeh et al. [MICRO 2012] 8 Thierry Moreau Neural Acceleration float foo (float a, float b) { AR F … NPUM P G return val; approximation acceleration } 9 Thierry Moreau Neural Acceleration compiler-support float foo (float a, float b) { AR F … NPUM P G return val; approximation acceleration } ACCEPT* *Sampson et. al [UW-TR] 10 Thierry Moreau Neural Acceleration compiler-support HW-support float foo (float a, float b) { AR F … NPUM P G return val; approximation acceleration } ACCEPT SNNAP* *Moreau et. al [HPCA2015] 11 Thierry Moreau Neural Acceleration compiler-support HW-support float foo (float a, float b) { AR F … NPUM P G return val; approximation acceleration } ACCEPT SNNAP 3.8x speedup and 2.8x efficiency - 10% error 12 Thierry Moreau Talk Outline Introduction Compiler Support with ACCEPT SNNAP Accelerator design Evaluation & Comparison with HLS 13 Thierry Moreau Compilation Overview code 1. Region detection annotation 14 Thierry Moreau Compilation Overview ACCEPT code region detection 1. Region detection & program annotation instrumentation 15 Thierry Moreau Compilation Overview ACCEPT code region detection 1. Region detection & program annotation instrumentation back prop. -
L'étrange Histoire Du Premier Moteur-Fusée À Liquides Par Jean-Jacques Serra, Membre De L’IFHE
#19 - janvier 2017 LES LANCEMENTS DE 1967 15 ANS D’ANDROMEDE 50 ANS D’APOLLO-1 50 ANS DE SOYOUZ-1 ESPACE & TEMPS Le mot du président IFHE Institut Français d’Histoire de l’Espace adresse de correspondance : 2, place Maurice Quentin Chers amis, 75039 Paris Cedex 01 e-mail : [email protected] Je vous souhaite à tous une très bonne année 2017. L’année Tél : 01 40 39 04 77 écoulée a vu la sortie des deux livres qui ont nécessité cinq ans de travail : 50 ans de coopération spatiale France-URSS/Russie et L’institut Français d’Histoire de l’Espace (IFHE) est une L’Observation spatiale de la Terre optique et radar - La france et association selon la Loi de 1901 créée le 22 mars 1999 l’Europe pionnières. qui s’est fixée pour obiectifs de valoriser l’histoire de Nous avons organisé des présentations lors des conférences l’espace et de participer à la sauvegarde et à la préserva- du 20 janvier et du 7 avril à Paris. Par ailleurs, ils ont été présentés tion du patrimoine documentaire. Il est administré par à Toulouse le 20 février (Observation de la Terre), le 13 juin et le 5 un Conseil, et il s’est doté d’un Conseil Scientifique. décembre (50 ans de coopération spatiale). Au 31 octobre 2016, l’éditeur a établi un compte d’exploi- Conseil d’administration tation provisoire : l’Observation de la Terre avait été vendu à 828 Président d’honneur.......Michel Bignier exemplaires et le 50 ans de coopération spatiale à 625 exemplaires. -
Heater Element Specifications Bulletin Number 592
Technical Data Heater Element Specifications Bulletin Number 592 Topic Page Description 2 Heater Element Selection Procedure 2 Index to Heater Element Selection Tables 5 Heater Element Selection Tables 6 Additional Resources These documents contain additional information concerning related products from Rockwell Automation. Resource Description Industrial Automation Wiring and Grounding Guidelines, publication 1770-4.1 Provides general guidelines for installing a Rockwell Automation industrial system. Product Certifications website, http://www.ab.com Provides declarations of conformity, certificates, and other certification details. You can view or download publications at http://www.rockwellautomation.com/literature/. To order paper copies of technical documentation, contact your local Allen-Bradley distributor or Rockwell Automation sales representative. For Application on Bulletin 100/500/609/1200 Line Starters Heater Element Specifications Eutectic Alloy Overload Relay Heater Elements Type J — CLASS 10 Type P — CLASS 20 (Bul. 600 ONLY) Type W — CLASS 20 Type WL — CLASS 30 Note: Heater Element Type W/WL does not currently meet the material Type W Heater Elements restrictions related to EU ROHS Description The following is for motors rated for Continuous Duty: For motors with marked service factor of not less than 1.15, or Overload Relay Class Designation motors with a marked temperature rise not over +40 °C United States Industry Standards (NEMA ICS 2 Part 4) designate an (+104 °F), apply application rules 1 through 3. Apply application overload relay by a class number indicating the maximum time in rules 2 and 3 when the temperature difference does not exceed seconds at which it will trip when carrying a current equal to 600 +10 °C (+18 °F). -
K-12 Individual No. Name Team Gr Rate Pts Tbrk1 Tbrk2 Tbrk3 Tbrk4
K-12 Individual No. Name Team Gr Rate Pts TBrk1 TBrk2 TBrk3 TBrk4 Rnd1 Rnd2 Rnd3 Rnd4 Rnd5 Rnd6 1 Chakraborty, Dipro 11 2299 5.5 21 24 43 20.5 W27 W12 W5 W32 W8 D3 State Champion, AZ Denker Representative 2 Yim, Tony Sung BASISS 8 2135 5 20.5 23.5 38.5 17.5 W24 W10 D3 D16 W11 W9 3 Aletheia-Zomlefer, Soren CHANPR 11 1961 5 20 23 35.5 18.5 W25 W26 D2 W40 W15 D1 4 Desmarais, Nicholas Eduard NOTRED 10 1917 5 18 20 33 18 W39 W23 W18 L15 W10 W8 5 Wong, Kinsleigh Phillip CFHS 10 1992 4.5 20 20 24.5 15 -X- W17 L1 W26 D7 W15 6 Todd, Bryce BASISC 10 1923 4.5 17 19 26.5 14.5 W38 D18 L9 W23 W21 W16 7 Chaliki, Kalyan DSMTHS 9 1726 4.5 17 18.5 26 15 W46 L16 W28 W22 D5 W17 8 Li, Bohan UHS 9 2048 4 22 25 29 18 W30 W11 W45 W9 L1 L4 9 Mittal, Rohan CFHS 9 1916 4 19.5 20.5 23 17 W47 W22 W6 L8 W20 L2 10 Pennock, Joshua CFHS 10 1682 4 19 22 24 14 W31 L2 W25 W21 L4 W29 11 Aradhyula, Sumhith CFHS 9 1631 4 18 20 22 14 W41 L8 W38 W13 L2 W19 12 Johnston, Nicolas Godfrey CFHS 9 1803 4 18 19.5 21 13 W43 L1 W29 L17 W24 W20 13 Martis, Tyler BRHS 12 1787 4 17 18 21 13 W42 L15 W24 L11 W18 W22 14 Plumb, Justin Rodney GCLACA 10 1700 4 16 17 20 13 W51 L32 W19 L20 W28 W27 15 Martinez, Isaac GLPREP 10 2159 3.5 21.5 24.5 27.5 16 W28 W13 D16 W4 L3 L5 16 Chen, Derek H CFHS 10 1965 3.5 21 23.5 26 15.5 W35 W7 D15 D2 D17 L6 17 Woodson, Tyler GILBHS 1640 3.5 19 19 17.5 14 W50 L5 W30 W12 D16 L7 18 Cancio, Aiya CFHS 9 1469 3.5 18.5 20 17.5 12.5 W36 D6 L4 W46 L13 W25 AZ Girls' Invitational Representative 19 Folden, Kurt CHANPR 10 1207 3 14 18 12 10 L32 W50 L14 W31 W23 L11 20 Thornton, -
BU97530KVT MAX 445 Segment(89Segx5com)
Datasheet LCD Segment Drivers Multi-function LCD Segment Drivers BU97530KVT MAX 445 Segment(89SEGx5COM) General Description Key Specifications The BU97530KVT is 1/5, 1/4, 1/3 duty or Static ■ Supply Voltage Range: +2.7V to +6.0V General-purpose LCD driver. The BU97530KVT can ■ Operating Temperature Range: -40°C to +85°C drive up to 445 LCD Segments directly. The ■ Max Segments: 445 Segments BU97530KVT can also control up to 9 General-purpose ■ Display Duty Static, 1/3, 1/4, 1/5 Selectable output pins / 9 PWM output pins. ■ Bias: 1/2, 1/3 Selectable These products also incorporate a key scan circuit that ■ Interface: 3wire Serial Interface accepts input from up to 30 keys to reduce printed circuit board wring. Features Package W (Typ) x D (Typ) x H (Max) Key Input Function for up to 30 Keys (A key scan is performed only when a key is pressed.) Either 1/5, 1/4, 1/3 Duty or Static Can be Selected with the Serial Control Data. 1/5 Duty Drive: Up to 445 Segments can be Driven 1/4 Duty Drive: Up to 360 Segments can be Driven 1/3 Duty Drive: Up to 270 Segments can be Driven Static Drive: Up to 90 Segments can be Driven Selectable Display Frame Frequency for Common and Segment Output Waveforms. Configurable Output Pin to Segment Output / PWM Output / General-purpose Output.(Max 9 Pins) Built-in OSC Circuit TQFP100V Integrated Voltage Detection Type Reset Circuit 16.00mm x 16.00mm x 1.20mm (VDET) No External Component Low Power Consumption Design Supports Line and Frame Inversion Applications Car Audio, Home Electrical Appliance, Meter Equipment etc. -
JASON D. FIEGE, B.Sc.H, M-Sc
FILAMENTARY MOLECULAR CLOUDS AND THEIR PROLATE CORES BY JASON D. FIEGE, B.Sc.H, M-Sc. A Thesis Submitted to the School of Graduate Studies in Partial Fulfilment of the Requirements for the Degree Doctor of Philosophy McMaster University @ Copyright by Jason D. Fiege, 1999 National Library Bibliothèque nationale 1*1 of Canada du Canada Acquisitions and Acquisitions et Bibliographie Services services bibliographiques 395 WeUington Street 395, rue Wellington OttawON KIAON4 OttawaON KlAûN4 Canada Canada The author has granted a non- L'auteur a accordé une licence non exclusive licence allowing the exclusive permettant à la National Lhrary of Canada to Bibliothèque nationale du Cana& de reproduce, loan, distribute or sell reproduire, prêter, distribuer ou copies of this thesis in rnicrofom, vendre des copies de cette thèse sous paper or electronic formats. la forme de microfiche/nlm, de reproduction sur papier ou sur format électronique. The author retains ownership of the L'auteur conserve la propriété du copyright in this thesis. Neither the droit d'auteur qui protège cette thèse. thesis nor substantial extracts fiom it Ni la thèse ni des extraits substantiels may be printed or othewise de celle-ci ne doivent être imprimés reproduced without the author's ou autrement reproduits sans son permission. autorisation. FILAMENTARY MOLECULAR CLOUDS AND THEIR PROLATE CORES DOCTOR OF PHILOSOPHY McMaster University (Physics and Astronomy) Hamilton, Ontario TITLE: Filamentary Molecular Clouds and Their Prolate Cores AUTHOR: Jason D. Fiege, B.Sc., M.Sc. (Queen's University) SUPERVISOR: Dr. Mph E. Pudritz NUMBER OF PAGES: xiv, 252. Abstract We develop a mode1 of self-gravitating, pressure truncated, filarnentary molecdar clouds wi t h a rather general helical magnetic field topology. -
Bob Farquhar
1 2 Created by Bob Farquhar For and dedicated to my grandchildren, their children, and all humanity. This is Copyright material 3 Table of Contents Preface 4 Conclusions 6 Gadget 8 Making Bombs Tick 15 ‘Little Boy’ 25 ‘Fat Man’ 40 Effectiveness 49 Death By Radiation 52 Crossroads 55 Atomic Bomb Targets 66 Acheson–Lilienthal Report & Baruch Plan 68 The Tests 71 Guinea Pigs 92 Atomic Animals 96 Downwinders 100 The H-Bomb 109 Nukes in Space 119 Going Underground 124 Leaks and Vents 132 Turning Swords Into Plowshares 135 Nuclear Detonations by Other Countries 147 Cessation of Testing 159 Building Bombs 161 Delivering Bombs 178 Strategic Bombers 181 Nuclear Capable Tactical Aircraft 188 Missiles and MIRV’s 193 Naval Delivery 211 Stand-Off & Cruise Missiles 219 U.S. Nuclear Arsenal 229 Enduring Stockpile 246 Nuclear Treaties 251 Duck and Cover 255 Let’s Nuke Des Moines! 265 Conclusion 270 Lest We Forget 274 The Beginning or The End? 280 Update: 7/1/12 Copyright © 2012 rbf 4 Preface 5 Hey there, I’m Ralph. That’s my dog Spot over there. Welcome to the not-so-wonderful world of nuclear weaponry. This book is a journey from 1945 when the first atomic bomb was detonated in the New Mexico desert to where we are today. It’s an interesting and sometimes bizarre journey. It can also be horribly frightening. Today, there are enough nuclear weapons to destroy the civilized world several times over. Over 23,000. “Enough to make the rubble bounce,” Winston Churchill said. The United States alone has over 10,000 warheads in what’s called the ‘enduring stockpile.’ In my time, we took care of things Mano-a-Mano. -
BU91530KVT-M : Display Drivers
Datasheet LCD Segment Drivers Multi-function LCD Segment Drivers BU91530KVT-M MAX 445 Segment(89SEGx5COM) General Description Key Specifications The BU91530KVT-M is 1/5, 1/4, 1/3 or 1/1 duty ■ Supply Voltage Range: +2.7V to +6.0V general-purpose LCD driver that can be used for ■ Operating Temperature Range: -40°C to +85°C frequency display in electronic tuners under the control of ■ Max Segments: 445 Segments a microcontroller. The BU91530KVT-M can drive up to ■ Display Duty 1/1, 1/3, 1/4, 1/5 Selectable 445 LCD Segments directly. The BU91530KVT-M can ■ Bias: 1/2, 1/3 Selectable also control up to 9 general-purpose output ports. ■ Interface: 3wire Serial Interface These products also incorporate a key scan circuit that accepts input from up to 30 keys to reduce printed circuit board wring. Package W (Typ.) x D (Typ.) x H (Max.) Features AEC-Q100 Qualified (Note1) Key input function for up to 30 keys (A key scan is performed only when a key is pressed.) Either 1/5, 1/4, 1/3 or 1/1 duty (static) can be selected with the serial control data. 1/5 duty drive: Up to 445 segments can be driven 1/4 duty drive: Up to 360 segments can be driven 1/3 duty drive: Up to 270 segments can be driven 1/1 duty drive: Up to 90 segments can be driven Serial Data Control of frame frequency for common and segment output waveforms. Serial data control of switching between the segment TQFP100V output port , PWM output port and general-purpose 16.00mm x 16.00mm x 1.20mm output port functions.(Max 9 ports) Built-in OSC circuit Integrated Power-on Reset Circuit No external component Low power consumption design Supports Line and Frame Inversion (Note1) Grade 3 Applications Car Audio, Home Electrical Appliance, Meter Equipment etc. -
INTRODUCTION This Study of Reentry Vehicle (RV)
INTRODUCTION This study of Reentry Vehicle (RV) systems and their associated operations was conducted for the Department of Transportation/Office of Commercial Space Transportation. The purpose of the study was to investigate and present an overview of reentry vehicle systems and to identify differences in mission requirements and operations. This includes reentry vehicle system background, system design considerations, description of past/present/future reentry systems, and hazards associated with reentry vehicles that attain orbit, reenter, and are recovered. A general literature search that included the OCST data base, NASA, Air Force, and other technical libraries and personal contact with various government or private industry organizations knowledgeable in reentry system vehicles was performed. A reference page is provided at the end of this report. A history of early manned reentry vehicle launches is shown in Appendix I. A listing of some of the agencies and companies found to be most knowledgeable in the reentry vehicle area is provided in Appendix II. The following sections provide more detailed information on reentry system vehicles. A. Background - The development of reentry vehicles began in the late 1950's due to the need for Department of Defense and Central Intelligence Agency photo reconnaissance of Soviet ICBM sites. NASA has also been involved in the use of reentry vehicles since the early 1960's, including manned space programs Mercury, Gemini and Apollo. The following sections describe the evolution of reentry system development in the United States and foreign countries: 1. Discoverer1 - The Discoverer program was of major importance because it provided a vehicle for testing orbital maneuvering capability and reentry techniques and it played a large role in enabling the first United States manned space flights to be conducted in Project Mercury. -
NEMA Motor Control
Bulletin Eutectic Alloy Overload Relays Heater Elements Selection For Application on Bulletin 100/500/609/1200 Line Starters Eutectic Alloy Overload Relay Heater Elements Heater Element Selection Type J — CLASS 10 Table of Contents 0 Type P — CLASS 20 (Bul. 600 ONLY) Type W — CLASS 20 Overload Relay Type WL — CLASS 30 Class Designation...... this page Heater Element Selection ....................... this page 1 Type W Heater Elements Ambient Temperature Correction..................... this page Time — Current Characteristics............ 1-169 2 Index to Heater Element Selection Tables ............................. 1-170 3 Description The following is for motors rated for Continuous Duty: For motors with marked service factor of not less than 1.15, or Overload Relay Class Designation motors with a marked temperature rise not over +40 °C United States Industry Standards (NEMA ICS 2 Part 4) designate an (+104 °F), apply application rules 1 through 3. Apply application 4 overload relay by a class number indicating the maximum time in rules 2 and 3 when the temperature difference does not exceed seconds at which it will trip when carrying a current equal to 600 +10 °C (+18 °F). When the temperature difference is greater, see percent of its current rating. below. A Class 10 overload relay will trip in 10 seconds or less at a current 1. The Same Temperature at the Controller and the Motor — equal to 600 percent of its rating. Select the “Heater Type Number” with the listed “Full Load 5 Amperes” nearest the full load value shown on the motor A Class 20 overload relay will trip in 20 seconds or less at a current nameplate. -
Delta Natural Gas Company, Inc. Case No. 2010-001 16
DELTA NATURAL GAS COMPANY, INC. CASE NO. 2010-001 16 ATTORNEY GENERAL'S ]INITIAL REQUEST F R INFORMATION DATED MAY 24,2010 1. Please provide copies of June year-to-date financial, operating and/or statistical reports for 2006,2007,2008 and 2009 (when available). Response: See PSC-1 Item 41 for financial statements subsequent to the test year. See our application, tab 37 for a copy of the January, 2009 through December, 2009. The financial reports for 2006 through 2008 are on file with the Public Service Commission. Sponsoring Witness: Matthew D. Wesalosky DEL,TA NATURAL GAS COMPANY, INC. CASE NO. 2010-001 16 ATTORNEY GENERAL'S INITIAL,REQUEST FOR INFORMATION DATED MAY 24,2010 2. Please provide a copy of the Board of Directors minutes for 2007, 2008, 2009 and 2010 to date. Response: The Board minutes have been filed under seal with motion for confidential treatment. Sponsoring Witness: John B. Brown DELTA NATURAL GAS COMPANY, INC. CASE NO. 201 0-001 16 ATTORNEY GENERAL'S INITIAL REQUEST FOR INFORMATION DATED MAY 24,2010 3. Please explain in detail any major changes in accounting treatment for O&M expenses, retirements, replacements and removal costs instituted by the Company since 2003. Response: The most significant change resulted from changing our capitalization threshold from $500 to $2,000 in 2004. For SEC reporting purposes, the Company reclassified cost of removal out of accumulated depreciation into regulatory liabilities, adopted SFAS 143 and adopted FIN 47. None of these changes have any impact on this rate case, as Delta has excluded all of these balances in the pro forma numbers.