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US Export Controls
U.S. Export Controls A Commerce Department Perspective EAR BOOT CAMP ECCN, EAR99 and the 600 Series Chicago, IL Oct 9, 2013 Gene Christiansen 202 482 2894 [email protected] Factors to be considered in determining if item is “subject to the EAR” • Jurisdiction – Characteristics of Item: • Nuclear---Energy, NRC, Commerce • Military---USML, Commerce • Destination Country – For Cuba, Iran, N Korea, N Sudan and Syria---OFAC • Public Domain technology and software What is covered under the Commerce Control List (CCL) • Everything not under the jurisdiction of another Agency or technical data that is not in the public domain. See part 734.3 – All items in the United States – All U.S. origin items wherever they are – Foreign made items that include in excess of de minimis value of controlled U.S. origin content. – Foreign made items that are the direct product of certain U.S. origin technical data or software. – Certain commodities produced by any plant located outside the U.S. that is the direct product of certain U.S. origin technical data or software Navigating the Commerce Control List (CCL) • The Commerce Control List – 10 categories • 0 Nuclear and miscellaneous • 1 Materials, chemicals, microorganisms, toxins • 2 Materials processing • 3 Electronics computers • 4 Computers • 5 Telecommunications and encryption • 6 Sensors • 7 Navigation and avionics • 8 Marine • 9 Propulsion systems and space vehicles Navigating the Commerce Control List • The Commerce Control List – 5 groups • A--- Equipment—end items • B--- Test and production -
2018 Annual Report Our Leadership Team (From Left to Right): Frank A
FINANCIAL HIGHLIGHTS In millions, except per share data 2018 2017 2016 Net Sales $53,762 $49,960 $47,290 Segment Operating Profit 5,877 5,092 4,982 Consolidated Operating Profit 7,334 6,744 5,888 Net Earnings From Continuing Operations 5,046 1,890 3,661 Net Earnings 5,046 1,963 5,173 Diluted Earnings Per Common Share Continuing Operations 17.59 6.50 12.08 Net Earnings 17.59 6.75 17.07 Cash Dividends Per Common Share 8.20 7.46 6.77 Average Diluted Common Shares Outstanding 287 291 303 Cash and Cash Equivalents $772$ 2,861 $ 1,837 Total Assets 44,876 46,620 47,560 Total Debt, net 14,104 14,263 14,282 Total Equity (Deficit) 1,449 (776) 1,477 Common Shares Outstanding at Year-End 281 284 289 Net Cash Provided by Operating Activities $3,138 $ 6,476 $ 5,189 NOTE: For additional information regarding the amounts presented above, see the Form 10-K portion of this Annual Report. A reconciliation of Segment Operating Profit to Consolidated Operating Profit is included on the page preceding the back cover of this Annual Report. On the Cover: F-35B Lightning II On September 29, 2018, the first F-35B Lightning II stealth fighters landed on the flight deck of HMS Queen Elizabeth, as Britain’s newest Royal Navy aircraft carrier conducted trials off the Eastern Seaboard of the United States. These developmental trials included more than 500 take-offs and landings from the warship over an 11-week period. The F-35B is one of three variants of the world’s most advanced supersonic fifth-generation fighter jet. -
Aerospace-Facts-And-Figures-1988
Facts and Figures 8 8 8 9 Key Technologies Legacy for the 21st Century Aerospace Industries Association of America, Inc. $16.95 Compiled by Economic Data Service Aerospace Research Center Aerospace Industries Association of America, Inc. 1250 Eye Street, N.W., Washington , D.C. 20005 (202) 371 -8400 Director , Research Center: Virginia C. Lopez Manager, Economic Data Servi ce: Carl M. P ~ s ale Ed itorial onsultant: Jam s 1. Hagg rty De~ign : wen Hoelscher and Associates Published by Aviation Week 1221 Avenue of the Americas New York, N.Y. 10020 1-800-433-0880 Copyright © 19tl!l by Aerospace Industries A ss ociution u f i\mericu. Inc . Library o f Congre ss utalog N<> . 46-25 007 Ackno-wledgments Air Transport Association of America Battelle Memorial Institute Council of Economic Advisers Export-Import Bank of the United States Exxon International Company General Aviation Manufacturers Association Helicopter Association International International Air Transport Association International Civil Aviation Organization McGraw-Hill Publications Company National Aeronautics and Space Administration National Science Foundation Office of Management and Budget Price Waterhouse U.S. Departments of Commerce (Bureau of the Census, Bureau of Economic Analysis, International Trade Administration) Defense (Comptroller; Directorate for Information, Operations and Reports: Army, Navy, Air Force) Labor (Bureau of Labor Statistics) Transportation (Federal Aviation Administration) Focused development of key "enabling" technologies will determine the U.S. aerosp~ce. industry's technological and market leadership mto the next century. These technologies will help ensure U.S. defense superiority and will also provide endless possibilities for a range of products to revolutionize the way we live-from fully-automated factories to crash-resistant, ultra safe automobiles to greatly improved medical diagnostic equipment. -
Lockheed Martin F-35 Lightning II Incorporates Many Significant Technological Enhancements Derived from Predecessor Development Programs
AIAA AVIATION Forum 10.2514/6.2018-3368 June 25-29, 2018, Atlanta, Georgia 2018 Aviation Technology, Integration, and Operations Conference F-35 Air Vehicle Technology Overview Chris Wiegand,1 Bruce A. Bullick,2 Jeffrey A. Catt,3 Jeffrey W. Hamstra,4 Greg P. Walker,5 and Steve Wurth6 Lockheed Martin Aeronautics Company, Fort Worth, TX, 76109, United States of America The Lockheed Martin F-35 Lightning II incorporates many significant technological enhancements derived from predecessor development programs. The X-35 concept demonstrator program incorporated some that were deemed critical to establish the technical credibility and readiness to enter the System Development and Demonstration (SDD) program. Key among them were the elements of the F-35B short takeoff and vertical landing propulsion system using the revolutionary shaft-driven LiftFan® system. However, due to X- 35 schedule constraints and technical risks, the incorporation of some technologies was deferred to the SDD program. This paper provides insight into several of the key air vehicle and propulsion systems technologies selected for incorporation into the F-35. It describes the transition from several highly successful technology development projects to their incorporation into the production aircraft. I. Introduction HE F-35 Lightning II is a true 5th Generation trivariant, multiservice air system. It provides outstanding fighter T class aerodynamic performance, supersonic speed, all-aspect stealth with weapons, and highly integrated and networked avionics. The F-35 aircraft -
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F-100 for AMT Pegasus jet engine or Jet CAT P-120 / P-160 Assembly Manual NcVNaV\[-QrÅvt{ ZI le chenet, 91490 Milly La Foret, FRANCE Tel : 33 1 64 98 93 93 Fax : 33 1 64 98 93 88 E-mail : [email protected] www.adjets.com Version 01/10/2006 1 INTRODUCTION The F-100 from NcVNaV\[-QR`VT[ is designed for high thrust jet engines. It is a scale kit, with all the panel lines engraved in the fuselage and a lot of scale details (gears, hinges, cockpit...). It is fully molded in fiberglass, carbon and epoxy. The flight characteristics are excellent with low and high speed capability. The model has plug in wings, stabs and fin. F-100 is avaialable : - in ’’C’’ version with small fin and small fixed flaps - in ’’D’’ version with larger fin and large movable flaps F-100 model includes - High quality epoxy-glass fuselage painted. - All plywood and wood parts premounted. - Epoxy-glass inlet - Exhaust nozzle. - Fully molded wings, stabs and fin painted - Access hatch requiring no additional framework. - ABS cockpit interior. - Clear formed canopy. - All hardware (ball links, bearings, screws ...) - Instructions in English. To complete the kit : The following items are not included in the kit. They are available from NcVNaV\[-QR`VT[. Jet Engine : 1 Complete AMT Pegasus jet engine or 1 Jet Cat P120 or P160 Cockpit detail kit : ref : ADJ 465 This kit include : 1/7 full body jet pilot, 1/7 ejector seat & instrument panel. 2 Landing gear : ref : ADJ 467 NÑvnÇv|{-QrÅvt{ retractable landing gear is specially designed for the F-100. -
Gallery of USAF Weapons Note: Inventory Numbers Are Total Active Inventory Figures As of Sept
Gallery of USAF Weapons Note: Inventory numbers are total active inventory figures as of Sept. 30, 2011. ■ 2012 USAF Almanac Bombers B-1 Lancer Brief: A long-range, air refuelable multirole bomber capable of flying intercontinental missions and penetrating enemy defenses with the largest payload of guided and unguided weapons in the Air Force inventory. Function: Long-range conventional bomber. Operator: ACC, AFMC. First Flight: Dec. 23, 1974 (B-1A); Oct. 18, 1984 (B-1B). Delivered: June 1985-May 1988. IOC: Oct. 1, 1986, Dyess AFB, Tex. (B-1B). Production: 104. Inventory: 66. Aircraft Location: Dyess AFB, Tex.; Edwards AFB, Calif.; Eglin AFB, Fla.; Ellsworth AFB, S.D. Contractor: Boeing, AIL Systems, General Electric. Power Plant: four General Electric F101-GE-102 turbofans, each 30,780 lb thrust. Accommodation: pilot, copilot, and two WSOs (offensive and defensive), on zero/zero ACES II ejection seats. Dimensions: span 137 ft (spread forward) to 79 ft (swept aft), length 146 ft, height 34 ft. B-1B Lancer (SSgt. Brian Ferguson) Weight: max T-O 477,000 lb. Ceiling: more than 30,000 ft. carriage, improved onboard computers, improved B-2 Spirit Performance: speed 900+ mph at S-L, range communications. Sniper targeting pod added in Brief: Stealthy, long-range multirole bomber that intercontinental. mid-2008. Receiving Fully Integrated Data Link can deliver nuclear and conventional munitions Armament: three internal weapons bays capable of (FIDL) upgrade to include Link 16 and Joint Range anywhere on the globe. accommodating a wide range of weapons incl up to Extension data link, enabling permanent LOS and Function: Long-range heavy bomber. -
COMPUTATIONAL AEROELASTICITY in HIGH PERFORMANCE AIRCRAFT FLIGHT LOADS* Mike Love, Tony De La Garza, Eric Charlton, Dan Egle Lockheed Martin Aeronautics Company
ICAS 2000 CONGRESS COMPUTATIONAL AEROELASTICITY IN HIGH PERFORMANCE AIRCRAFT FLIGHT LOADS* Mike Love, Tony De La Garza, Eric Charlton, Dan Egle Lockheed Martin Aeronautics Company Keywords: computational aeorelasticity, CFD, flight loads Abstract A computational aeroelasticity method has been developed that combines a compu- tational fluid dynamics (CFD) code based on a finite volume, Cartesian / prismatic grid scheme with automated unstructured grid creation and adaption with established structural finite element methods. This analysis is motivated by the need to develop an analysis capability for fighter-aircraft critical flight loads. Flight conditions for such often reside in transonic flow regimes and comprise nonlinear aerodynamics due to shocks, flow-separation onset, and complex geometry. The Multidisciplinary Computa- tional Environment, MDICE [1], is provid- Figure 1: Pressures and streamlines obtained from a ing for timely integration of Lockheed computational aeroelastic maneuver simulation Martin’s CFD software, SPLITFLOW [2] in in maneuver simulations. The Loads engi- a maintenance friendly, loosely coupled neer’s time is mostly consumed in the nonlinear analysis method. Analysis corre- assembly of accurate data for the maneuver lation with static aeroelastic wind tunnel simulation. Adequate characterization of data demonstrates potential. Analysis set-up vehicle aerodynamics is critical. Recent tool and results for a fighter aircraft with multi- and technology developments are facilitating ple control surfaces are demonstrated. the aerodynamic characterization task of integrating data from CFD methods, wind 1 Introduction tunnel testing and other aerodynamic meth- ods to assemble an aerodynamic pressure Computational aeroelasticity, or computa- database [3, 4]. This database is augmented tional fluid dynamics (CFD) based aeroelas- by static aeroelastic analyses to account for ticity, is an emerging technology with high flexibility effects of the structure and inertial potential for the development of critical effects of the flight vehicle. -
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SIX DECADES OF GUIDED MUNITIONS AND BATTLE NETWORKS: PROGRESS AND PROSPECTS Barry D. Watts Thinking Center for Strategic Smarter and Budgetary Assessments About Defense www.csbaonline.org Six Decades of Guided Munitions and Battle Networks: Progress and Prospects by Barry D. Watts Center for Strategic and Budgetary Assessments March 2007 ABOUT THE CENTER FOR STRATEGIC AND BUDGETARY ASSESSMENTS The Center for Strategic and Budgetary Assessments (CSBA) is an independent, nonprofit, public policy research institute established to make clear the inextricable link between near-term and long- range military planning and defense investment strategies. CSBA is directed by Dr. Andrew F. Krepinevich and funded by foundations, corporations, government, and individual grants and contributions. This report is one in a series of CSBA analyses on the emerging military revolution. Previous reports in this series include The Military-Technical Revolution: A Preliminary Assessment (2002), Meeting the Anti-Access and Area-Denial Challenge (2003), and The Revolution in War (2004). The first of these, on the military-technical revolution, reproduces the 1992 Pentagon assessment that precipitated the 1990s debate in the United States and abroad over revolutions in military affairs. Many friends and professional colleagues, both within CSBA and outside the Center, have contributed to this report. Those who made the most substantial improvements to the final manuscript are acknowledged below. However, the analysis and findings are solely the responsibility of the author and CSBA. 1667 K Street, NW, Suite 900 Washington, DC 20036 (202) 331-7990 CONTENTS ACKNOWLEGEMENTS .................................................. v SUMMARY ............................................................... ix GLOSSARY ………………………………………………………xix I. INTRODUCTION ..................................................... 1 Guided Munitions: Origins in the 1940s............. 3 Cold War Developments and Prospects ............ -
Table of Contents
Table of Contents March 2021 User’s Guide User’s Guide Index Index (System Type) ................................................................................................................................March 2021 Market Overviews Airborne AESA Fighter Radars: Northrop Grumman (#1) ............................................................... November 2020 Airborne AESA Fighter Radars: Raytheon (#2) ......................................................................................... July 2020 Airborne DIRCM Systems & Missile Warning Systems (MWS) ............................................................... May 2020 Airborne Large SAR/GMTI Radar Market ........................................................................................... August 2021 Airborne SOF TF/TA Radars ............................................................................................................ November 2020 Air Defense/BMD Radars: Fixed/Transportable Ground Systems ........................................................ August 2020 Ballistic Missile Defense (BMD): Mobile Ground Systems ............................................................. November 2020 F-16 Electronic Warfare (EW) Systems ..................................................................................................... July 2020 Naval Electronic Warfare (EW) Systems ............................................................................................. October 2020 USAF Legacy Bomber Electronics Programs ............................................................................................ -
Usafalmanac ■ Gallery of USAF Weapons
USAFAlmanac ■ Gallery of USAF Weapons By Susan H.H. Young The B-1B’s conventional capability is being significantly enhanced by the ongoing Conventional Mission Upgrade Program (CMUP). This gives the B-1B greater lethality and survivability through the integration of precision and standoff weapons and a robust ECM suite. CMUP will include GPS receivers, a MIL-STD-1760 weapon interface, secure radios, and improved computers to support precision weapons, initially the JDAM, followed by the Joint Standoff Weapon (JSOW) and the Joint Air to Surface Standoff Missile (JASSM). The Defensive System Upgrade Program will improve aircrew situational awareness and jamming capability. B-2 Spirit Brief: Stealthy, long-range, multirole bomber that can deliver conventional and nuclear munitions anywhere on the globe by flying through previously impenetrable defenses. Function: Long-range heavy bomber. Operator: ACC. First Flight: July 17, 1989. Delivered: Dec. 17, 1993–present. B-1B Lancer (Ted Carlson) IOC: April 1997, Whiteman AFB, Mo. Production: 21 planned. Inventory: 21. Unit Location: Whiteman AFB, Mo. Contractor: Northrop Grumman, with Boeing, LTV, and General Electric as principal subcontractors. Bombers Power Plant: four General Electric F118-GE-100 turbo fans, each 17,300 lb thrust. B-1 Lancer Accommodation: two, mission commander and pilot, Brief: A long-range multirole bomber capable of flying on zero/zero ejection seats. missions over intercontinental range without refueling, Dimensions: span 172 ft, length 69 ft, height 17 ft. then penetrating enemy defenses with a heavy load Weight: empty 150,000–160,000 lb, gross 350,000 lb. of ordnance. Ceiling: 50,000 ft. Function: Long-range conventional bomber. -
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INTRODUCTION................................................................................................................. 4 1. AERODYNAMIC SECTION........................................................................................... 8 1.1 Introduction ............................................................................................................................................................ 8 1.2 The Pitch limiters ................................................................................................................................................. 10 1.2 The Lift and Drag ( Cl / Cd )............................................................................................................................... 12 1.3 The Rudder ( CY )................................................................................................................................................ 19 1.4 The Drag Index (DI)............................................................................................................................................. 20 2 ENGINES SECTION................................................................................................ 22 2.1 The Pratt & Whitney engines ............................................................................................................................. 22 2.2 The General Electric Engines ............................................................................................................................. 28 3 A BIT OF HISTORY............................................................................................. -
The Market for Aviation Turbofan Engines
The Market for Aviation Turbofan Engines Product Code #F640 A Special Focused Market Segment Analysis by: Aviation Gas Turbine Forecast Analysis 1 The Market for Aviation Turbofan Engines 2010-2019 Table of Contents Executive Summary .................................................................................................................................................2 Introduction................................................................................................................................................................2 Trends..........................................................................................................................................................................3 Market Focus .............................................................................................................................................................3 Competitive Environment.......................................................................................................................................4 Figure 1 - The Market for Aviation Turbofan Engines Unit Production 2010 - 2019 (Bar Graph) .................................................................................6 Figure 2 - The Market for Aviation Turbofan Engines Value of Production 2010 - 2019 (Bar Graph)...........................................................................6 Manufacturers Review.............................................................................................................................................7