IHS Jane's All the World's Aircraft

Total Page:16

File Type:pdf, Size:1020Kb

IHS Jane's All the World's Aircraft IHS Jane’s All the World’sAircraft Unmanned 2012-2013 Editor: Mark Daly ISBN -13 978 07106 3003 2 Copyright ©IHS Global Limited, .All rights reserved. Thirdparty details and websites No partofthis publication may be reproduced or transmitted, in any form or by any Any thirdparty details and websites aregiven for information and reference purposes means, electronic, mechanical, photocopying, recording or otherwise, or be stored in only and IHS Global Limited does not control, approve or endorse these thirdparties or any retrieval system of any nature, without prior written permission of IHS Global Limited. thirdparty websites. Further,IHS Global Limited does not control or guarantee the Applications for written permission should be directed to Christopher Bridge. accuracy, relevance, availability, timeliness or completeness of the information contained on any thirdparty website. Inclusion of any thirdparty details or websites is not Any views or opinions expressed by contributors and thirdparties arepersonal to them intended to reflect their importance, nor is it intended to endorse any views expressed, and do not represent the views or opinions of IHS Global Limited, its affiliates or staff. products or services offered, nor the companies or organisations in question. You access any thirdparty websites solely at your own risk. Disclaimer of liability Whilst everyefforthas been made to ensurethe quality and accuracy of the information Use of data contained in this publication at the time of going to press, IHS Global Limited, its affiliates, The company and personal data stated in any directoryordatabase may be used for the their officers, employees and agents assume no responsibility as to the accuracy or limited purpose of enquiring about the products and services of the companies listed completeness of and, to the extent permitted by law,shall not be liable for any errors or who have given permission for their data to be used for this purpose only.You may use omissions or any loss, damage or expense incurred by reliance on information or any the data only to the extent, and in such amanner,asisnecessaryfor the authorised statement contained in this publication. purpose. Youmust comply with the Data Protection Act 1998 and all other applicable data protection and privacy laws and regulations. In particular,you must not use the data Advertisement (i) for any unlawful, harmful or offensive purpose; (ii) as asource for any kind of marketing Advertisers aresolely responsible for the content of the advertising material which they or promotion activity; or (iii) for the purposes of compiling, confirming or amending your submit to us and for ensuring that the material complies with applicable laws. IHS Global Limited is not responsible for any error,omission or inaccuracy in any advertisement. IHS own database, directoryormailing list. Global Limited will not be liable for any damages arising from any use of products or services or any actions or omissions taken in reliance on information or any statement Trade Marks contained in advertising material. Inclusion of any advertisement is not intended to IHS Jane’sand All the World’sAircraft: Unmanned aretrade marks of IHS Global Limited. endorse any views expressed, nor products or services offered, nor the organisations sponsoring the advertisement. This book was produced using FSC® certified paper Printed and bound in the UK by Polestar Wheatons IHS Jane’s Div: JUAV_p01_TitlePage JOB: JUAVPage: 1Date: March 22, 2012 Time: 10:13:03 Operator: onc26353 Contents Alphabetical list of Advertisers .......................................................................................... [4] Executive Overview ............................................................................................................. [7] Users’ Charter ......................................................................................................................[12] Acknowledgements ............................................................................................................ [13] Glossary ................................................................................................................................. [14] How to use ...........................................................................................................................[30] UNMANNED AERIAL VEHICLES ........................................................................................... 1 AERIAL TARGETS ................................................................................................................. 281 POWER PLANTS .................................................................................................................... 359 CONTROL AND COMMUNICATIONS .............................................................................. 387 LAUNCH AND RECOVERY SYSTEMS ............................................................................... 415 Contractors ........................................................................................................................... 431 Alphabetical index ............................................................................................................... 441 Manufacturers’Index .......................................................................................................... 449 ©IHS Global Limited 2012 [3] IHS Jane’sAll the World’sAircraft: Unmanned 2012-2013 IHS Jane’s Div: JUAV_p03_Contents JOB: JUAVPage: 1Date: March 21, 2012 Time: 13:09:57 Operator: onc26353 214 Unmanned aerial vehicles >United States > Boeing Phantom Ray –Boeing ScanEagle Boeing Phantom Ray Phantom Ray Type:Technology demonstrator. Dimensions, External Development:The company‐funded Phantom Ray project was launched Overall, length..........................................................................10.97 m(36 ft 0in) by Boeing's Phantom Works in October 2008, although not announced Wings, wing span....................................................................15.24 m(50 ft 0in) publicly until 8May 2009. In essence, it resumes work performed on the Weights and Loadings X‐45C, the ultimate X‐45 variant developed by Boeing as its entrant in the Weight, Max T-O weight...................................................... 16,556 kg (36,499 lb) former joint‐service J‐UCAS programme. In October 2004, Boeing Performance received aUSD767 million DARPA contract for three X‐45C prototypes, Altitude, Operating altitude...................................................12,190 m(40,000 ft) the first of which should have had its public roll‐out on 2March 2006. Power plant........................................................................................ 1×turbofan However, this was pre‐empted by termination of the J‐UCAS programme. Status:Design development continued in 2009 and construction was The aircraft never flew and, along with the uncompleted second completed in 2010. Phantom Ray was shipped by NASA Boeing 747 prototype, was placed in storage. Shuttle Carrier Aircraft from St Louis to Edwards Air Force Base, California As announced, the X‐45C will now serve as the basis for the Phantom in December 2010. The Phantom Ray (the successor to the X‐45) took its Ray, as atestbed for advanced technologies. A10‐flight flying maiden flight on 27 April 2011 at NASA's Dryden Research Center at programme is envisaged over aperiod of about six months, supporting Edwards Air Force Base, Calif, US. missions that may include ISR, SEAD, hunter/killer and electronic attack. Contractor:The Boeing Company, Boeing Defense, Space and Security Also tested will be autonomous in‐flight refuelling —the X‐45C design St Louis, Missouri. included space provision in the rear fuselage for arefuelling receptacle, and this capability was to have been explored with the third X‐45C. Description: Airframe: Stealthy, ‘arrow‐head' flying wing design with about 55° leading‐edge sweepback and W‐planform trailing‐edge; blended fuselage, with internal bay(s); buried turbofan engine with serpentine dorsal intake; no vertical tail surfaces. Retractable tricycle Boeing ScanEagle landing gear. All‐composites construction. Type:Endurance mini‐UAV. Mission payloads: Specific to individual test flights; details not yet Development:ScanEagle is avariant of the Insitu SeaScan ,built under a announced. 15‐month original agreement announced on 11 February 2002 and being Guidance and control: Fully autonomous, including taxi, take‐off and developed separately by Boeing's Phantom Works in collaboration with landing phases. Insitu. Boeing equipped the prototype air vehicle using its own systems Launch: Conventional and autonomous wheeled take‐off. integration, communications and payload technologies. It made its first, Recovery: Conventional and autonomous wheeled landing. remotely controlled, flight in April that year and its first autonomous flight Power plant: Aand B: One approx 51.2 kN (11,500 lb st) General on 19 June 2002, following apneumatic catapult launch. Made at Electric F404‐GE‐102D non‐afterburning turbofan. Boeing's Boardman, Oregon, facility, the latter flight lasted 45 minutes, (A: X‐45C, B: Phantom Ray) flying apreprogrammed course at amaximum altitude of 457 m(1,500 ft). Anumber of test waypoints were completed using DGPS, as well as the ability to make real‐time updates to the flight plan from the GCS. The UAV was retrieved using the patented Insitu Skyhook technique. In late January 2003, the ScanEagle made five flights, totalling more than 20 hours, as acommunications
Recommended publications
  • Paper Number
    Impact of mission requirements on the design of low observable UCAV configurations E. Sepulveda, H. Smith SATM, Cranfield University, Cranfield, UK. Purpose – The purpose of this paper is to characterise the effects of mission and performance parameters on the design space of low observable subsonic unmanned combat aerial vehicles operating in typical Hi-Lo-Hi ground strike missions. Design/methodology/approach – Conceptual design methodologies appropriate to low observable, tailless UCAVs have been integrated into a multidisciplinary aircraft design environment, GENUS, developed at Cranfield University’s Aircraft Design Group. A basic Hi-Lo-Hi mission is designed and a baseline configuration is established through the GENUS framework. Subsequently, an evolutionary optimiser and a robust gradient-based optimiser are employed to obtain convergent design solutions for various leading edge sweep angles, mission ranges, cruise Mach numbers, and other operational constraints. Findings – The results indicate that performance constraints, specifically in the form of specific excess power, have a large influence on the overall sizing of subsonic tailless UCAVs. This requirement drives the engine sizing which represents a considerable proportion of the empty and gross mass of the vehicle. Cruise Mach number studies show that no significant advantages exist for operating at low speeds while maintaining performance requirements consistent with combat missions. There is a drastic increase in the vehicle’s mass and thrust requirements for flight speeds above Mach 0.8, with low sweep configurations showing a more pronounced effect. Increases in range are not overly dependent on the leading edge sweep angle. Top-level radar cross section results also favour configurations with higher leading edge sweep angles, especially from the nose-on aspect.
    [Show full text]
  • Up from Kitty Hawk Chronology
    airforcemag.com Up From Kitty Hawk Chronology AIR FORCE Magazine's Aerospace Chronology Up From Kitty Hawk PART ONE PART TWO 1903-1979 1980-present 1 airforcemag.com Up From Kitty Hawk Chronology Up From Kitty Hawk 1980-1989 F-117 Nighthawk stealth fighters, first flight June 1981. Articles noted throughout the chronology are hyperlinked to the online archive for Air Force Magazine and the Daily Report. 1980 March 12-14, 1980. Two B-52 crews fly nonstop around the world in 43.5 hours, covering 21,256 statute miles, averaging 488 mph, and carrying out sea surveillance/reconnaissance missions. April 24, 1980. In the middle of an attempt to rescue US citizens held hostage in Iran, mechanical difficulties force several Navy RH-53 helicopter crews to turn back. Later, one of the RH-53s collides with an Air Force HC-130 in a sandstorm at the Desert One refueling site. Eight US servicemen are killed. Desert One May 18-June 5, 1980. Following the eruption of Mount Saint Helens in northwest Washington State, the Aerospace Rescue and Recovery Service, Military Airlift Command, and the 9th Strategic Reconnaissance Wing conduct humanitarian-relief efforts: Helicopter crews lift 61 people to safety, while SR–71 airplanes conduct aerial photographic reconnaissance. May 28, 1980. The Air Force Academy graduates its first female cadets. Ninety-seven women are commissioned as second lieutenants. Lt. Kathleen Conly graduates eighth in her class. Aug. 22, 1980. The Department of Defense reveals existence of stealth technology that “enables the United States to build manned and unmanned aircraft that cannot be successfully intercepted with existing air defense systems.” Sept.
    [Show full text]
  • Boeing History Chronology Boeing Red Barn
    Boeing History Chronology Boeing Red Barn PRE-1910 1910 1920 1930 1940 1950 1960 1970 1980 1990 2000 2010 Boeing History Chronology PRE-1910 1910 1920 1930 1940 1950 1960 1970 1980 1990 2000 2010 PRE -1910 1910 Los Angeles International Air Meet Museum of Flight Collection HOME PRE-1910 1910 1920 1930 1940 1950 1960 1970 1980 1990 2000 2010 1881 Oct. 1 William Edward Boeing is born in Detroit, Michigan. 1892 April 6 Donald Wills Douglas is born in Brooklyn, New York. 1895 May 8 James Howard “Dutch” Kindelberger is born in Wheeling, West Virginia. 1898 Oct. 26 Lloyd Carlton Stearman is born in Wellsford, Kansas. 1899 April 9 James Smith McDonnell is born in Denver, Colorado. 1903 Dec. 17 Wilbur and Orville Wright make the first successful powered, manned flight in Kitty Hawk, North Carolina. 1905 Dec. 24 Howard Robard Hughes Jr. is born in Houston, Texas. 1907 Jan. 28 Elrey Borge Jeppesen is born in Lake Charles, Louisiana. HOME PRE-1910 1910 1920 1930 1940 1950 1960 1970 1980 1990 2000 2010 1910 s Boeing Model 1 B & W seaplane HOME PRE-1910 1910 1920 1930 1940 1950 1960 1970 1980 1990 2000 2010 1910 January Timber baron William E. Boeing attends the first Los Angeles International Air Meet and develops a passion for aviation. March 10 William Boeing buys yacht customer Edward Heath’s shipyard on the Duwamish River in Seattle. The facility will later become his first airplane factory. 1914 May Donald W. Douglas obtains his Bachelor of Science degree from the Massachusetts Institute of Technology (MIT), finishing the four-year course in only two years.
    [Show full text]
  • YEAR in REVIEW 2011 a PUBLICATION of the AMERICAN INSTITUTE of AERONAUTICS and ASTRONAUTICS Change Your Perception of MESHING
    cover-fin12-2011_AA Template 11/18/11 11:37 AM Page 1 11 AMERICA AEROSPACE December 2011 DECEMBER 2011 YEAR IN REVIEW 2011 A PUBLICATION OF THE AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS change your perception of MESHING VISIT US AT THE AIAA AEROSPACE SCIENCES MEETING 9-12 JANUARY 2012 > THIS IS NOT THE FUNNEST PART OF THE PROJECT. You’re not generating a computational grid for pleasure. It’s simply a necessary step in the process of completing your analysis, so you can improve the performance of your design. With its intuitive interface, high-level automation, and sophisticated grid generation algorithms, Pointwise helps ease you through the process. Try it for free, and see how Pointwise can reduce your meshing pain. POINTWISE. Reliable People, Reliable Tools, Reliable CFD Meshing. Toll Free (800) 4PTWISE www.pointwise.com toc.DEC2011a_AA Template 11/17/11 10:46 AM Page 1 December 2011 EDITORIAL 3 OUT OF THE PAST 76 2011 SUBJECT AND AUTHOR INDEX 78 CAREER OPPORTUNITIES 84 THE YEAR IN REVIEW Adaptive structures 4 Intelligent systems 39 Aeroacoustics 12 Legal aspects 32 Aerodynamic decelerators 25 Life sciences 56 Aerodynamic measurement Lighter-than-air systems 30 technology 13 Liquid propulsion 51 Aerospace power systems 44 Materials 6 Aerospace traffic management 68 Meshing, visualization and Air-breathing propulsion systems computational environments 21 integration 45 Nondeterministic approaches 7 Aircraft design 26 Nuclear and future flight Air transportation 24 propulsion 52 Applied aerodynamics 14 Plasmadynamics and lasers
    [Show full text]
  • Phantom Ray Unmanned Aircraft Makes Its Debut 12 May 2010
    Phantom Ray unmanned aircraft makes its debut 12 May 2010 “We’re really excited about this because Phantom Works is back as a rapid prototyping house, operation and organization,” said Craig Brown, Boeing Phantom Ray program manager. “This is the first of what I expect to be many exciting prototypes, and they’re all with exciting technology.” Financed entirely by Boeing, Phantom Ray is a testament to the company and its Phantom Works division’s commitment to becoming the leader in the global unmanned systems market. “Phantom Ray represents a series of significant After only two years of development, the Phantom changes we’re making within Boeing Defense, Ray unmanned airborne system (UAS) was Space & Security,” said Darryl Davis, president of unveiled at a ceremony in St. Louis on May 10. Phantom Works. “For the first time in a long time, Built by Boeing in St. Louis, the sleek, fighter-sized we are spending our own money on designing, UAS combines survivability with a powerful arsenal building and flying near-operational prototypes. of new capabilities. We’re spending that money to leverage the decades of experience we have in unmanned “Phantom Ray offers a host of options for our systems that span the gamut from sea to space.” customers as a test bed for advanced technologies, including intelligence, surveillance This aircraft is on-schedule to take its first taxi tests and reconnaissance; suppression of enemy air later this summer and soar through its initial flight defenses; electronic attack and autonomous aerial profiles as early as December, continuously gaining refueling - the possibilities are nearly endless,” ground toward becoming an unmanned system that said Dennis Muilenburg, president and CEO of could one day penetrate enemy forces and provide Boeing Defense, Space & Security.
    [Show full text]
  • Phantom Ray - Wikipedia, the Free Encyclopedia
    Boeing Phantom Ray - Wikipedia, the free encyclopedia http://en.wikipedia.org/wiki/Boeing_Phantom_Ray From Wikipedia, the free encyclopedia The Boeing Phantom Ray is a stealth unmanned combat air vehicle being developed by Boeing using company funds. Phantom Ray The Phantom Ray is a demonstrator aircraft, about the size of a fighter that will conduct a program of test flights involving surveillance, ground attack and autonomous aerial refueling missions.[2][3] Role Unmanned Combat Air Vehicle 1 Design and development Manufacturer Boeing Integrated Defense 2 Specifications Systems 3 See also [1] 4 References First flight 27 April 2011 Status Under development Number built 1 Developed from Boeing X-45C The Phantom Ray project, called "Project Reblue" internally at Boeing, was first conceived in mid-2007, and started in earnest in June 2008. The project was secret, even within the company, except for a handful of executives and engineers, until May 2009.[4] Developed by the Boeing Phantom Works, the Phantom Ray is based on the X-45C prototype aircraft[5] that Boeing originally developed for the Defense Advanced Research Projects Agency (DARPA), the U.S. Air Force, and the U.S. Navy Joint-Unmanned Combat Air System (J-UCAS) program. However, Phantom Ray was not aimed at any particular program or competition.[6] The Phantom Ray was unveiled on May 10, 2010 in St. Louis, Missouri.[3][7] In late November 2010 low-speed taxi tests were carried out in St. Louis.[8][9] The demonstrator aircraft is to perform 10 test flights over six months, supporting
    [Show full text]
  • Space Transportation System, N905NA and N911NA)
    HISTORIC AMERICAN ENGINEERING RECORD SPACE TRANSPORTATION SYSTEM, SHUTTLE CARRIER AIRCRAFT (Space Transportation System, N905NA and N911NA) HAER No. TX-116-L Location: Lyndon B. Johnson Space Center 2101 NASA Parkway Houston Harris County Texas When not in active use, Shuttle Carrier Aircraft (SCA) N905NA and N911NA (hereinafter NASA 905 and NASA 911, respectively) were maintained at the National Aeronautics and Space Administration’s (NASA) Dryden Flight Research Center (DFRC) at Edwards Air Force Base (AFB) in Edwards, California, located at latitude 34.949167, longitude: -117.885000. These coordinates represent Area A of DFRC, the location where the aircraft were parked; they were obtained on November 25, 2012 through Google Earth™. The coordinates’ datum are North American Datum 1983. Dates of Construction: NASA 905 was originally constructed in 1970; it was modified into a SCA in 1976. NASA 911 was originally built in 1973; it was modified into a SCA in 1988. Builder: NASA 905 and NASA 911 were built by The Boeing Company (Boeing) as 747-123 and 747-SR-46, respectively. Each was subsequently modified by Boeing for use as a SCA. Original Owner and Use: Before its purchase by NASA in July 1974, NASA 905 was owned and operated by American Airlines as a commercial jetliner. Prior to its purchase by NASA in April 1988, NASA 911 was owned and operated by Japan Air Lines as a commercial jetliner. Present Owner: Both NASA 905 and NASA 911 are owned by NASA’s Lyndon B. Johnson Space Center (JSC) in Houston, Texas. Significance: NASA’s Shuttle Carrier Aircraft, N905NA and N911NA, are significant in the context of the U.S.
    [Show full text]
  • Streamlined Adaptive System Works
    National Aeronautics and Space Administration Volume 53 Number 1 January 7, 2011 Simplify, simplify Streamlined adaptive system works; capabilities verified By Jay Levine X-Press Editor A Dryden F/A-18 proved a simplified adaptive controller can compensate for simulated failures of flight control surfaces and keep the aircraft flyable until landing safely. The Model Reference Adaptive Control, or MRAC, project also showed the range of the aircraft’s research capabilities during a December flight. Mark Dickerson, deputy project manager for Dryden’s aviation safety program, and Jim Lee, project chief engineer for the MRAC and F/A- 18 No. 853, recently talked about the success of the MRAC and the aircraft. It has been demonstrated through flight that the aircraft can be used to validate a number of new ED10 0372-24 NASA Photo by Carla Thomas technologies that could lead to safer NASA’s F/A-18 No. 853 validated through flight in December that a streamlined adaptive system could help an aircraft and a smoother ride and aircraft that has sustained damage to its flight control surfaces remain flyable. It also proved the aircraft’s capabilities enable the aircraft to communicate for a number of potential flight research projects. when it needs maintenance. The MRAC work takes what was “We pulled out what wasn’t strain gages remain on the flight to vehicles that control the shape started on the F-15 No. 837 prior absolutely needed,” he added. control surfaces from the Active of a fuselage while an aircraft is to that test bed’s retirement and However, the aircraft has Aeroelastic Wing research program, traveling supersonically.
    [Show full text]
  • Stealth Unmanned Combat Vehicle Makes First Flight 4 May 2011, by Nancy Atkinson
    Stealth unmanned combat vehicle makes first flight 4 May 2011, By Nancy Atkinson follow-on tests will expand Phantom Ray's flight envelope, they also will help Boeing expand its presence in the unmanned systems market." The flight demonstrated Phantom Ray's basic airworthiness, and Boeing engineers are planning additional flights in the next few weeks. Other potential uses for the vehicle include intelligence, surveillance and reconnaissance, and suppression of enemy air defenses. "The first flight moves us farther into the next phase of unmanned aircraft," said Craig Brown, Phantom Ray program manager for Boeing. "Autonomous, fighter-sized unmanned aircraft are real, and the The Boeing Phantom Ray unmanned airborne system UAS bar has been raised. Now I'm eager to see (UAS) on its first flight. Credit: Boeing. how high that bar will go." Source: Universe Today Looking like something straight from a 1950's science fiction magazine, the stealthy Phantom Ray unmanned airborne system (UAS) successfully completed its first flight on April 27, 2011 at NASA's Dryden Flight Research Center at Edwards Air Force Base in California. The 17-minute flight took place following a series of high-speed taxi tests in March that validated ground guidance, navigation and control and verified mission planning, pilot interface and operational procedures. The Phantom Ray is a demonstrator aircraft, about the size of a fighter jet, developed to test operations such as air surveillance, ground attack and autonomous aerial refueling missions. During the test flight, the Phantom Ray flew to 2,290 meters (7,500 feet) and reached a speed of 178 knots.
    [Show full text]
  • 2011 State of the VITA Technology Industry
    2011 State of the VITA Technology Industry March 2011 P.O. Box 19658 Fountain Hills, AZ 85269 480.837.7486 [email protected] www.vita.com State of the VITA Technology Industry March 2011 by: Ray Alderman, Executive Director, VITA This report provides the reader with updates on the state of the VME Technology industry in particular and of the board industry in general, from the perspective of Ray Alderman, the executive director of VITA. VITA is the trade association dedicated to fostering American National Standards Institute (ANSI) accredited, open system architectures in critical embedded system applications. The entire series of reports can be found at www.vita.com. Business Conditions The world macro-economic situation improved in many ways in late 2010. The US economy stabilized with 3.2% GDP growth in the third quarter and 2.9% growth for the Contents year.1 The EU responded to the financial crises in Ireland and Portugal with bail-out funds, growing their GDP 0.4% in the 4th quarter.2 China grew greater than 10% in Q-3 Business Conditions. 1 and even Japan was up 1.1%. Markets. 3 The November mid-term election results in the US brought a different attitude to the MIL/Aero . 3 previous congressional policy of spending our way out of this recession. Gridlock in the Telecom . 7 US Congress for the next two years is the new reality and is viewed as more stable than Industrial. 7 what we have experienced in the previous two years. The looming economic concerns Healthcare/Medical. 8 in the US are the severe budget deficits of many states and whether they will default on their municipal bonds.3 Ex Ante Update .
    [Show full text]
  • Study of Blended Wing Body Design Concept Thesis Submitted in Partial Fulfillment of the Requirements for the Degree of Bachelor of Science
    بسم اهلل الرحمن الرحيم Sudan University of Science and Technology Faculty of Engineering Aeronautical Engineering Department Study of blended wing body design concept Thesis Submitted in Partial Fulfillment of the Requirements for the Degree of Bachelor of Science. (BSc Honor) By: 1. REEM MOHAMMED ABDELGAFFER ABDALLAH 2. SAMAR MOHAMMED EBAID HASSAB-ELSEED 3. SHOWG IDRIS JAFER TAHA Supervised By: October 2016 اﻵيــــة قال تعالى: بسم اهلل الرحمن الرحيم }وَابْتَغِ فِيمَا آتَاكَ اللَّهُ الدَّارَ الْآخِرَةَ * وَلَا تَنْسَ وَصِيبَلَ مِهَ الدُّوْيَا * وَأَحْسِهْ مَمَا أَحْسَهَ اللَّهُ إِلَيْلَ ۖ* وَلَا تَبْغِ الْفَسَادَ فِي الْؤَرْضِ * إِنَّ اللَّهَ لَا يُحِبُّ الْمُفْسِدِيهَ{ صدق اهلل العظيم سورة القصص اﻵيت }77{ I Abstract This thesis represents a simple study of the design concept of a new generation of civilian aircrafts called "BLENDED WING BODY" aircraft , which are meant to replace the current cylindrical figure aircrafts in the sooner future . The search and study began with the conceptual design phase , taking both AIRBUS 380 & BOEING 747 & BOEING 777 as design references as they are all of the same weight and passenger capacity (500) . The design process started by setting the requirements based on historical data mostly, following all the conceptual design stages till the 3D-VIEWS was obtained. Going through airfoil selection , mission , weight estimation to the performance analysis of the aircraft which is mentioned in details . To conclude this study, this type of aircrafts has less fuel consumption and a better performance when compared to conventional aircrafts. However , the only problem that had to be dealt with was the airfoil selection which was solved at the drawing phase . with a better solutions proposed for any future work.
    [Show full text]
  • Autonomous Unmanned Aerial Vehicles a Technology Warning Assessment
    THE GEORGE WASHINGTON UNIVERISTY Autonomous Unmanned Aerial Vehicles A Technology Warning Assessment Syed Azeem 2/29/2012 This report presents a technology warning assessment based on National Academies’ methodology. The particular technology area analyzed relates to fully autonomous unmanned aerial vehicles (AUAVs) from the perspective of the United States government with the objective to assess AUAV technology with the goal of strongly enabling, promoting and increasing economic growth. Table of Contents Focus ............................................................................................................................................... 4 Introduction ............................................................................................................................. 4 History..................................................................................................................................... 5 UAVs Come to the Lime Light in Contemporary Times ....................................................... 5 Civilian Use of UAVs is Gaining Momentum ........................................................................ 6 The Road to Autonomy ............................................................................................................. 10 State of the Art ...................................................................................................................... 10 Alternative Energy and Extreme Endurance ........................................................................
    [Show full text]