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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 -
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, 2014. By Aaron M. U. Church, Associate Editor I 2015 USAF Almanac BOMBER AIRCRAFT flight controls actuate trailing edge surfaces that combine aileron, elevator, and rudder functions. New EHF satcom and high-speed computer upgrade B-1 Lancer recently entered full production. Both are part of the Defensive Management Brief: A long-range bomber capable of penetrating enemy defenses and System-Modernization (DMS-M). Efforts are underway to develop a new VLF delivering the largest weapon load of any aircraft in the inventory. receiver for alternative comms. Weapons integration includes the improved COMMENTARY GBU-57 Massive Ordnance Penetrator and JASSM-ER and future weapons The B-1A was initially proposed as replacement for the B-52, and four pro- such as GBU-53 SDB II, GBU-56 Laser JDAM, JDAM-5000, and LRSO. Flex- totypes were developed and tested in 1970s before program cancellation in ible Strike Package mods will feed GPS data to the weapons bays to allow 1977. The program was revived in 1981 as B-1B. The vastly upgraded aircraft weapons to be guided before release, to thwart jamming. It also will move added 74,000 lb of usable payload, improved radar, and reduced radar cross stores management to a new integrated processor. Phase 2 will allow nuclear section, but cut maximum speed to Mach 1.2. The B-1B first saw combat in and conventional weapons to be carried simultaneously to increase flexibility. Iraq during Desert Fox in December 1998. -
Pdfcreator, Job 2
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. -
Annex III to Decision 2015/029/R
AMC/GM TO ANNEX III (PART-66) TO REGULATION (EU) No 1321/2014 APPENDICES TO AMC TO PART-66 APPENDICES TO AMC TO PART-66 APPENDIX I AIRCRAFT TYPE RATINGS FOR PART-66 AIRCRAFT MAINTENANCE LICENCES The following aircraft type ratings should be used to ensure a common standard throughout the Member States. The inclusion of an aircraft type in the licence does not indicate that the aircraft type has been granted a type certificate under the Regulation (EC) No 216/2008 and its Implementing Rules; this list is only intended for maintenance purposes. In order to keep this list current and the type ratings consistent, such information should be first passed on to the Agency using the Rulemaking Enquiry form (http://easa.europa.eu/webgate/rulemaking-enquiry/) in case a Member State needs to issue a type rating that is not included in this list. Notes on when the licences should be modified: When a modification is introduced by this Decision to an aircraft type rating or to an engine designation in the rating which affect licences already issued, the ratings on the Aircraft Maintenance Licences (AMLs) may be modified at the next renewal or when the licence is reissued, unless there is an urgent reason to modify the licence. Notes on aircraft modified by Supplemental Type Certificate (STC): — This Appendix I intends to include the type ratings of aircraft resulting from STCs for installation of another engine. These STCs are those approved by the Agency and those approved by the Member States before 2003 and grandfathered by the Agency. -
Military Vehicle Options Arising from the Barrel Type Piston Engine
Journal of Power Technologies 101 (1) (2021) 22–33 Military vehicle options arising from the barrel type piston engine Pawe l Mazuro1 and Cezary Chmielewski1,B 1Warsaw University of Technology B [email protected] Abstract in terms of efficiency, meaning that piston engines can deliver enhanced range and endurance. This is benefi- The article reviews knowledge about requirements for engines in cial in missions requiring a stopover for refueling and state-of-the-art unmanned aerial vehicles and tanks. Analysis of particularly useful for unmanned supply, observation design and operational parameters was carried out on selected and maritime missions. turboshaft and piston engines generating power in the range of 500 - 1500 kW (0.5 - 1.5 MW). The data was compared In contrast, land combat vehicles have significantly with the performance of innovative, barrel type piston engines, different drive unit requirements. High mobility en- which are likely to become an alternative drive solution in the ables the vehicle to rapidly change location after de- target vehicle groups. tection. To this end, the torque curve as a function of the rotational speed of the shaft is of decisive im- portance. Keywords: military UAV, tanks, turboshaft engines, piston engines, barrel type piston engines The complexity of tank engines adds an additional layer of requirements, impacting the reliability and durability of the power unit, and they come with re- 1 Introduction lated manufacturing and operating costs. In military land vehicles, the engine should be as small This article consolidates knowledge on options and as possible; the space saved can be used for other capabilities arising from use of the barrel type piston purposes. -
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. -
Diesel, Spark-Ignition, and Turboprop Engines for Long-Duration Unmanned Air Flights
JOURNAL OF PROPULSION AND POWER Diesel, Spark-Ignition, and Turboprop Engines for Long-Duration Unmanned Air Flights Daniele Cirigliano,∗ Aaron M. Frisch,† Feng Liu,‡ and William A. Sirignano‡ University of California, Irvine, California 92697 DOI: 10.2514/1.B36547 Comparisons are made for propulsion systems for unmanned flights with several hundred kilowatts of propulsive power at moderate subsonic speeds up to 50 h in duration. Gas-turbine engines (turbofans and turboprops), two- and four-stroke reciprocating (diesel and spark-ignition) engines, and electric motors (with electric generation by a combustion engine) are analyzed. Thermal analyses of these engines are performed in the power range of interest. Consideration is given to two types of generic missions: 1) a mission dominated by a constant-power requirement, and 2) a mission with intermittent demand for high thrust and/or substantial auxiliary power. The weights of the propulsion system, required fuel, and total aircraft are considered. Nowadays, diesel engines for airplane applications are rarely a choice. However, this technology is shown to bea very serious competitor for long-durationunmanned air vehicle flights. The two strongest competitors are gas-turbine engines and turbocharged four-stroke diesel engines, each type driving propellers. It is shown that hybrid-electric schemes and configurations with several propellers driven by one power source are less efficient. At the 500 KW level, one gas-turbine engine driving a larger propeller is more efficient for durations up to 25 h, whereas several diesel engines driving several propellers become more efficient at longer durations. The decreasing efficiency of the gas-turbine engine with decreasing size and increasing compression ratio is a key factor. -
ATP® Libraries Catalog
2 ATP® Libraries Catalog Revision Date May 24 2016 ATP 101 South Hill Drive Brisbane, CA 94005 (+1) 415-330-9500 www.atp.com ATP® Policies and Legal www.atp.com/policy © Copyright 2016, ATP. All rights reserved. No part of this publication may be reproduced, stored in a retrieval system or transmitted in any form by any means, electronic, mechanical, photocopying, recording or otherwise, without prior written permission of ATP. The information in this catalog is subject to change without notice.ATP, ATP Knowledge, ATP Aviation Hub, HubConnect, NavigatorV, and their respective logos, are among the registered trademarks or trademarks of ATP. All third-party trademarks used herein are the property of their respective owners and ATP asserts no ownership rights to these items. iPad and iPhone are trademarks of Apple Inc., registered in the U.S. and other countries. App Store is a service mark of Apple Inc. All original authorship of ATP is protected under U.S. and foreign copyrights and is subject to written license agreements between ATP and its subscribers. Visit www.atp.com/policy for more information ATP Customer Support Please visit www.atp.com/support for customer support information ATP® Libraries Catalog – Revision Date: May 24 2016 3 CONTENTS CONTENTS ...................................................................................................................................................................... 3 REGULATORY LIBRARIES ............................................................................................................................................. -
How to Learn Trigonometry Intuitively | Betterexplained 9/26/15, 12:19 AM
How To Learn Trigonometry Intuitively | BetterExplained 9/26/15, 12:19 AM (/) How To Learn Trigonometry Intuitively by Kalid Azad · 101 comments Tweet 73 Trig mnemonics like SOH-CAH-TOA (http://mathworld.wolfram.com/SOHCAHTOA.html) focus on computations, not concepts: TOA explains the tangent about as well as x2 + y2 = r2 describes a circle. Sure, if you’re a math robot, an equation is enough. The rest of us, with organic brains half- dedicated to vision processing, seem to enjoy imagery. And “TOA” evokes the stunning beauty of an abstract ratio. I think you deserve better, and here’s what made trig click for me. Visualize a dome, a wall, and a ceiling Trig functions are percentages to the three shapes http://betterexplained.com/articles/intuitive-trigonometry/ Page 1 of 48 How To Learn Trigonometry Intuitively | BetterExplained 9/26/15, 12:19 AM Motivation: Trig Is Anatomy Imagine Bob The Alien visits Earth to study our species. Without new words, humans are hard to describe: “There’s a sphere at the top, which gets scratched occasionally” or “Two elongated cylinders appear to provide locomotion”. After creating specific terms for anatomy, Bob might jot down typical body proportions (http://en.wikipedia.org/wiki/Body_proportions): The armspan (fingertip to fingertip) is approximately the height A head is 5 eye-widths wide Adults are 8 head-heights tall http://betterexplained.com/articles/intuitive-trigonometry/ Page 2 of 48 How To Learn Trigonometry Intuitively | BetterExplained 9/26/15, 12:19 AM (http://en.wikipedia.org/wiki/Vitruvian_Man) How is this helpful? Well, when Bob finds a jacket, he can pick it up, stretch out the arms, and estimate the owner’s height. -
Mathematics Tables
MATHEMATICS TABLES Department of Applied Mathematics Naval Postgraduate School TABLE OF CONTENTS Derivatives and Differentials.............................................. 1 Integrals of Elementary Forms............................................ 2 Integrals Involving au + b ................................................ 3 Integrals Involving u2 a2 ............................................... 4 Integrals Involving √u±2 a2, a> 0 ....................................... 4 Integrals Involving √a2 ± u2, a> 0 ....................................... 5 Integrals Involving Trigonometric− Functions .............................. 6 Integrals Involving Exponential Functions ................................ 7 Miscellaneous Integrals ................................................... 7 Wallis’ Formulas ................................................... ...... 8 Gamma Function ................................................... ..... 8 Laplace Transforms ................................................... 9 Probability and Statistics ............................................... 11 Discrete Probability Functions .......................................... 12 Standard Normal CDF and Table ....................................... 12 Continuous Probability Functions ....................................... 13 Fourier Series ................................................... ........ 13 Separation of Variables .................................................. 15 Bessel Functions ................................................... ..... 16 Legendre -
Structural Certification of the F-16 Block 52+ Aircraft 29 November 2005 2005 USAF Aircraft Structural Integrity Program Conference
Structural Certification of the F-16 Block 52+ Aircraft 29 November 2005 2005 USAF Aircraft Structural Integrity Program Conference Robert J. Burt Director and Deputy F-35 Structural Development and Integrity Lockheed Martin Aeronautics Company Fort Worth © 2005 LOCKHEED MARTIN CORPORATION Lockheed Martin Aeronautics Company Structural Certification of the F-16 Block 52+ Aircraft Abstract This presentation will describe in some detail the process followed by Lockheed Martin Aeronautics – Fort Worth for the structural certification of the new production F-16 Block 52+ aircraft for foreign military sales (FMS). The F-16 Block 52+ aircraft are structurally upgraded from the USAF Block 50/52 aircraft due to carriage of the fuselage shoulder mounted conformal fuel tanks and due to the addition of numerous advanced systems. The structural requirements and their methods of verification are set forth in the program contract and subsequent program documents such as the weapon system specification and air vehicle specification. Every USAF and FMS F-16 has an Aircraft Structural Integrity Program (ASIP) based upon program contractual requirement and tailored to MIL-STD-1530B Aircraft Structural Integrity Program. An ASIP Master Plan has been written for the Block 52+ aircraft which has been coordinated with and approved by the USAF F-16 System Group. This ASIP Master Plan states in specific terms how all the tasking outlined in the “five pillars” is accomplished. An overall design process will be discussed in depth pointing out how all historical structural analysis, structural test and field information has been used in the structural design of the Block 52+ aircraft.