Stealth Technology and Its Effect on Aerial Warfare
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The Luftwaffe Wasn't Alone
PIONEER JETS OF WORLD WAR II THE LUFTWAFFE WASN’T ALONE BY BARRETT TILLMAN he history of technology is replete with Heinkel, which absorbed some Junkers engineers. Each fac tory a concept called “multiple independent opted for axial compressors. Ohain and Whittle, however, discovery.” Examples are the incandes- independently pursued centrifugal designs, and both encoun- cent lightbulb by the American inventor tered problems, even though both were ultimately successful. Thomas Edison and the British inventor Ohain's design powered the Heinkel He 178, the world's first Joseph Swan in 1879, and the computer by jet airplane, flown in August 1939. Whittle, less successful in Briton Alan Turing and Polish-American finding industrial support, did not fly his own engine until Emil Post in 1936. May 1941, when it powered Britain's first jet airplane: the TDuring the 1930s, on opposite sides of the English Chan- Gloster E.28/39. Even so, he could not manufacture his sub- nel, two gifted aviation designers worked toward the same sequent designs, which the Air Ministry handed off to Rover, goal. Royal Air Force (RAF) Pilot Officer Frank Whittle, a a car company, and subsequently to another auto and piston 23-year-old prodigy, envisioned a gas-turbine engine that aero-engine manufacturer: Rolls-Royce. might surpass the most powerful piston designs, and patented Ohain’s work detoured in 1942 with a dead-end diagonal his idea in 1930. centrifugal compressor. As Dr. Hallion notes, however, “Whit- Slightly later, after flying gliders and tle’s designs greatly influenced American savoring their smooth, vibration-free “Axial-flow engines turbojet development—a General Electric– flight, German physicist Hans von Ohain— were more difficult built derivative of a Whittle design powered who had earned a doctorate in 1935— to perfect but America's first jet airplane, the Bell XP-59A became intrigued with a propeller-less gas- produced more Airacomet, in October 1942. -
The Foundations of US Air Doctrine
DISCLAIMER This study represents the views of the author and does not necessarily reflect the official opinion of the Air University Center for Aerospace Doctrine, Research, and Education (CADRE) or the Department of the Air Force. This manuscript has been reviewed and cleared for public release by security and policy review authorities. iii Library of Congress Cataloging-in-Publication Data Watts, Barry D. The Foundations ofUS Air Doctrine . "December 1984 ." Bibliography : p. Includes index. 1. United States. Air Force. 2. Aeronautics, Military-United States. 3. Air warfare . I. Title. 11. Title: Foundations of US air doctrine . III. Title: Friction in war. UG633.W34 1984 358.4'00973 84-72550 355' .0215-dc 19 ISBN 1-58566-007-8 First Printing December 1984 Second Printing September 1991 ThirdPrinting July 1993 Fourth Printing May 1996 Fifth Printing January 1997 Sixth Printing June 1998 Seventh Printing July 2000 Eighth Printing June 2001 Ninth Printing September 2001 iv THE AUTHOR s Lieutenant Colonel Barry D. Watts (MA philosophy, University of Pittsburgh; BA mathematics, US Air Force Academy) has been teaching and writing about military theory since he joined the Air Force Academy faculty in 1974 . During the Vietnam War he saw combat with the 8th Tactical Fighter Wing at Ubon, Thailand, completing 100 missions over North Vietnam in June 1968. Subsequently, Lieutenant Colonel Watts flew F-4s from Yokota AB, Japan, and Kadena AB, Okinawa. More recently, he has served as a military assistant to the Director of Net Assessment, Office of the Secretary of Defense, and with the Air Staff's Project CHECKMATE. -
China's Aircraft Carrier Ambitions
CHINA’S AIRCRAFT CARRIER AMBITIONS An Update Nan Li and Christopher Weuve his article will address two major analytical questions. First, what are the T necessary and suffi cient conditions for China to acquire aircraft carriers? Second, what are the major implications if China does acquire aircraft carriers? Existing analyses on China’s aircraft carrier ambitions are quite insightful but also somewhat inadequate and must therefore be updated. Some, for instance, argue that with the advent of the Taiwan issue as China’s top threat priority by late 1996 and the retirement of Liu Huaqing as vice chair of China’s Central Military Commission (CMC) in 1997, aircraft carriers are no longer considered vital.1 In that view, China does not require aircraft carriers to capture sea and air superiority in a war over Taiwan, and China’s most powerful carrier proponent (Liu) can no longer infl uence relevant decision making. Other scholars suggest that China may well acquire small-deck aviation platforms, such as helicopter carriers, to fulfi ll secondary security missions. These missions include naval di- plomacy, humanitarian assistance, disaster relief, and antisubmarine warfare.2 The present authors conclude, however, that China’s aircraft carrier ambitions may be larger than the current literature has predicted. Moreover, the major implications of China’s acquiring aircraft carriers may need to be explored more carefully in order to inform appropriate reactions on the part of the United States and other Asia-Pacifi c naval powers. This article updates major changes in the four major conditions that are necessary and would be largely suffi cient for China to acquire aircraft carriers: leadership endorsement, fi nancial affordability, a relatively concise naval strat- egy that defi nes the missions of carrier operations, and availability of requisite 14 NAVAL WAR COLLEGE REVIEW technologies. -
A Clipped Wing: an Assessment of the Effectiveness of the B-21
University of Denver Digital Commons @ DU Electronic Theses and Dissertations Graduate Studies 1-1-2016 A Clipped Wing: An Assessment of the Effectiveness of the B-21 Aidan Thomas Hughes University of Denver Follow this and additional works at: https://digitalcommons.du.edu/etd Part of the International Relations Commons Recommended Citation Hughes, Aidan Thomas, "A Clipped Wing: An Assessment of the Effectiveness of the B-21" (2016). Electronic Theses and Dissertations. 1124. https://digitalcommons.du.edu/etd/1124 This Thesis is brought to you for free and open access by the Graduate Studies at Digital Commons @ DU. It has been accepted for inclusion in Electronic Theses and Dissertations by an authorized administrator of Digital Commons @ DU. For more information, please contact [email protected],[email protected]. A Clipped Wing: An Assessment of the Effectiveness of the B-21 _________________________ A Thesis Presented to the Faculty of the Josef Korbel School of International Studies University of Denver _________________________ In Partial Fulfilment of the Requirements for the Degree Master of Arts _________________________ by Aidan Thomas Hughes June 2016 Advisor: Professor T. Farer Author: Aidan Thomas Hughes Title: A Clipped Wing: An Assessment of the Effectiveness of the B-21 Advisor: Professor T. Farer Degree Date: June 2016 Abstract This thesis examines the effectiveness of the Northrop Grumman B-21 long range strike bomber in advancing the ability of U.S. policy makers to achieve national security objectives. The operational value of the B-21 is assessed through analysing its probable role in four hypothetical combat scenarios, and the relative effectiveness of the B-21 is measured alongside the potential performance of alternative systems. -
A Brief Review on Electromagnetic Aircraft Launch System
International Journal of Mechanical And Production Engineering, ISSN: 2320-2092, Volume- 5, Issue-6, Jun.-2017 http://iraj.in A BRIEF REVIEW ON ELECTROMAGNETIC AIRCRAFT LAUNCH SYSTEM 1AZEEM SINGH KAHLON, 2TAAVISHE GUPTA, 3POOJA DAHIYA, 4SUDHIR KUMAR CHATURVEDI Department of Aerospace Engineering, University of Petroleum and Energy Studies, Dehradun, India E-mail: [email protected] Abstract - This paper describes the basic design, advantages and disadvantages of an Electromagnetic Aircraft Launch System (EMALS) for aircraft carriers of the future along with a brief comparison with traditional launch mechanisms. The purpose of the paper is to analyze the feasibility of EMALS for the next generation indigenous aircraft carrier INS Vishal. I. INTRODUCTION maneuvering. Depending on the thrust produced by the engines and weight of aircraft the length of the India has a central and strategic location in the Indian runway varies widely for different aircraft. Normal Ocean. It shares the longest coastline of 7500 runways are designed so as to accommodate the kilometers amongst other nations sharing the Indian launch for such deviation in takeoff lengths, but the Ocean. India's 80% trade is via sea routes passing scenario is different when it comes to aircraft carriers. through the Indian Ocean and 85% of its oil and gas Launch of an aircraft from a mobile platform always are imported through sea routes. Indian Ocean also requires additional systems and methods to assist the serves as the locus of important international Sea launch because the runway has to be scaled down, Lines Of Communication (SLOCs) . Development of which is only about 300 feet as compared to 5,000- India’s political structure, industrial and commercial 6,000 feet required for normal aircraft to takeoff from growth has no meaning until its shores are protected. -
Aircraft, Defense & Space Domain Business Plan
Aircraft, Defense & Space Domain Business Plan Keisuke Hisakazu Naohiko HIROSE MIZUTANI ABE Senior Vice President, President, Senior Vice President, Head of Commercial Aviation Mitsubishi Aircraft Corporation Head of Integrated Defense Systems & Space Systems June 12, 2017 © 2017 MITSUBISHI HEAVY INDUSTRIES, LTD. All Rights Reserved. Contents 1. Business Overview 2. Commercial Aviation Systems Segment 2-1. Overview 2-2. FY2016 Summary & FY2017 Outlook 2-3. FY2017 Business Strategy 3. MRJ Business 3-1. Overview 3-2. Development Activities 3-3. Implementation of Development Schedule 4. Integrated Defense & Space Systems Segment 4-1. Overview 4-2. FY2016 Summary & FY2017 Outlook 4-3. FY2017 Business Strategy © 2017 MITSUBISHI HEAVY INDUSTRIES, LTD. All Rights Reserved. 1 1-1. Overview (Domain Reorganization) The Aircraft, Defense & Space domain was created as a result of MHI’s domain reorganization, carried out 2017年4月の全社ドメイン再編・事業再配置により、航空・防衛・宇宙ドメインを発足。 in April 2017.直轄による育成基盤の早期形成と収益安定を図る。 Under the CEO’s direct oversight, the new domain is pursuing prompt formation of a strong developmentCEO foundation and stable earnings. [Until March 2017] [From April 2017] Energy & Environment Power Systems Business Group company Mitsubishi Aircraft MRJ Thermal Power Nuclear Power Thermal Power Compressors Corporation Renewable Energy Chemical Plants Aero Engines Nuclear Power Commercial Aviation & Renewable Energy Transportation Systems Commercial / Cruise Land Transportation Ships Systems Industry & Infrastructure Material Handling Commercial Aircraft -
Read Book # World War II Jet Aircraft of Germany: V-1
IZGMSHR0AW2L eBook // World War II jet aircraft of Germany: V-1, Messerschmitt Me 262, Heinkel... W orld W ar II jet aircraft of Germany: V -1, Messersch mitt Me 262, Heinkel He 162, Horten Ho 229, A rado A r 234, Focke-W ulf Ta 183, Heinkel He 280 Filesize: 8.19 MB Reviews This ebook is great. I really could comprehended every thing using this composed e ebook. Its been designed in an exceedingly simple way and it is only following i finished reading this publication where basically modified me, modify the way in my opinion. (Herminia Blanda) DISCLAIMER | DMCA BN6TSLX9Q92P / eBook \ World War II jet aircraft of Germany: V-1, Messerschmitt Me 262, Heinkel... WORLD WAR II JET AIRCRAFT OF GERMANY: V-1, MESSERSCHMITT ME 262, HEINKEL HE 162, HORTEN HO 229, ARADO AR 234, FOCKE-WULF TA 183, HEINKEL HE 280 To download World War II jet aircra of Germany: V-1, Messerschmitt Me 262, Heinkel He 162, Horten Ho 229, Arado Ar 234, Focke-Wulf Ta 183, Heinkel He 280 PDF, please follow the hyperlink below and download the document or get access to other information that are highly relevant to WORLD WAR II JET AIRCRAFT OF GERMANY: V-1, MESSERSCHMITT ME 262, HEINKEL HE 162, HORTEN HO 229, ARADO AR 234, FOCKE-WULF TA 183, HEINKEL HE 280 book. Books LLC, Wiki Series, 2016. Paperback. Book Condition: New. PRINT ON DEMAND Book; New; Publication Year 2016; Not Signed; Fast Shipping from the UK. No. book. Read World War II jet aircraft of Germany: V-1, Messerschmitt Me 262, Heinkel He 162, Horten Ho 229, Arado Ar 234, Focke-Wulf Ta 183, Heinkel He 280 Online Download PDF World War II jet aircraft of Germany: V-1, Messerschmitt Me 262, Heinkel He 162, Horten Ho 229, Arado Ar 234, Focke-Wulf Ta 183, Heinkel He 280 Download ePUB World War II jet aircraft of Germany: V-1, Messerschmitt Me 262, Heinkel He 162, Horten Ho 229, Arado Ar 234, Focke-Wulf Ta 183, Heinkel He 280 ZZ9D0KF7ISAA // Kindle # World War II jet aircraft of Germany: V-1, Messerschmitt Me 262, Heinkel.. -
Horten Ho 229 V3 All Wood Short Kit
Horten Ho 229 V3 All Wood Short Kit a Radio Controlled Model in 1/8 Scale Design by Gary Hethcoat Copyright 2007 Aviation Research P.O. Box 9192, San Jose, CA 95157 http://www.wingsontheweb.com Email: [email protected] Phone: 408-660-0943 Table of Contents 1 General Building Notes ......................................................................................................................... 4 1.1 Getting Help .................................................................................................................................. 4 1.2 Laser Cut Parts .............................................................................................................................. 4 1.3 Electronics ..................................................................................................................................... 4 1.4 Building Options ........................................................................................................................... 4 1.4.1 Removable Outer Wing Panels .............................................................................................. 4 1.4.2 Drag Rudders ......................................................................................................................... 4 1.4.3 Retracts .................................................................................................................................. 5 1.4.4 Frise Style Elevons ............................................................................................................... -
Precision Weapons in Aerial Warfare
IDSA Issue Brief IDSIDSAA ISSUEISSUE BRIEFBRIEF1 Precision Weapons in Aerial Warfare Vivek Kapur Gp. Capt. Vivek Kapur is Research Fellow at the Institute for Defence Studies & Analyses (IDSA), New Delhi May 08, 2012 Summary Precision weapon delivery has come into the general public's mind space especially in the past two decades. While technology did not permit the achievement of great precision in earlier years, today technology has delivered the ability to place weapons at desired locations with great accuracy, currently measured in a few metres. Precision in aerial warfare, which initially lay in the individual skills of combatants, has shifted to machines through the incorporation of advanced technology. Today precision is more widespread on the battlefield that at any time in history. Indications are that in the coming years, the development of Directed Energy Weapons (DEW) will give greater magnitudes of precision than are available today. Disclaimer: Views expressed in IDSA’s publications and on its website are those of the authors and do not necessarily reflect the views of the IDSA or the Government of India. Precision Weapons in Aerial Warfare 2 Precision in warfare has been a much sought after capability that was realised when modern technology matured adequately. Precision has changed the very nature of aerial warfare in particular. Today modern air forces have the ability to put a bomb through a chosen window with confidence. However, trends indicate that in future precision weaponry could migrate towards directed energy weapons that have the potential to deliver a degree ofe precision that lies in the realm of science fiction today. -
Effects-Based Operations and the Law of Aerial Warfare
Washington University Global Studies Law Review Volume 5 Issue 2 January 2006 Effects-based Operations and the Law of Aerial Warfare Michael N. Schmitt George C. Marshall European Center for Security Studies Follow this and additional works at: https://openscholarship.wustl.edu/law_globalstudies Part of the Military, War, and Peace Commons Recommended Citation Michael N. Schmitt, Effects-based Operations and the Law of Aerial Warfare, 5 WASH. U. GLOBAL STUD. L. REV. 265 (2006), https://openscholarship.wustl.edu/law_globalstudies/vol5/iss2/2 This Article is brought to you for free and open access by the Law School at Washington University Open Scholarship. It has been accepted for inclusion in Washington University Global Studies Law Review by an authorized administrator of Washington University Open Scholarship. For more information, please contact [email protected]. Washington University Global Studies Law Review VOLUME 5 NUMBER 2 2006 EFFECTS-BASED OPERATIONS AND THE LAW OF AERIAL WARFARE MICHAEL N. SCHMITT* Law responds almost instinctively to tectonic shifts in warfare.1 For instance, the Fourth Geneva Convention of 1949 constituted a dramatic reaction to the suffering of civilian populations during World War II.2 Similarly, the 1977 Protocols Additional3 updated and expanded the law of armed conflict (LOAC) in response both to the growing prevalence of non-international armed conflicts and wars of national liberation and to the recognized need to codify the norms governing the conduct of hostilities.4 In light of this symbiotic relationship, it is essential that LOAC experts carefully monitor developments in military affairs, because such developments may well either strain or strengthen aspects of that body of law.5 As an example, the widespread use in Iraq of civilian contractors and * Professor of International Law and Director, Program in Advanced Security Studies, George C. -
The Third Battle
NAVAL WAR COLLEGE NEWPORT PAPERS 16 The Third Battle Innovation in the U.S. Navy's Silent Cold War Struggle with Soviet Submarines N ES AV T A A L T W S A D R E C T I O N L L U E E G H E T R I VI IBU OR A S CT MARI VI Owen R. Cote, Jr. Associate Director, MIT Security Studies Program The Third Battle Innovation in the U.S. Navy’s Silent Cold War Struggle with Soviet Submarines Owen R. Cote, Jr. Associate Director, MIT Security Studies Program NAVAL WAR COLLEGE Newport, Rhode Island Naval War College The Newport Papers are extended research projects that the Newport, Rhode Island Editor, the Dean of Naval Warfare Studies, and the Center for Naval Warfare Studies President of the Naval War College consider of particular Newport Paper Number Sixteen interest to policy makers, scholars, and analysts. Candidates 2003 for publication are considered by an editorial board under the auspices of the Dean of Naval Warfare Studies. President, Naval War College Rear Admiral Rodney P. Rempt, U.S. Navy Published papers are those approved by the Editor of the Press, the Dean of Naval Warfare Studies, and the President Provost, Naval War College Professor James F. Giblin of the Naval War College. Dean of Naval Warfare Studies The views expressed in The Newport Papers are those of the Professor Alberto R. Coll authors and do not necessarily reflect the opinions of the Naval War College or the Department of the Navy. Naval War College Press Editor: Professor Catherine McArdle Kelleher Correspondence concerning The Newport Papers may be Managing Editor: Pelham G. -
P-38 Lightning
P-38 Lightning P-38 Lightning Type Heavy fighter Manufacturer Lockheed Designed by Kelly Johnson Maiden flight 27 January 1939 Introduction 1941 Retired 1949 Primary user United States Army Air Force Produced 1941–45 Number built 10,037[1] Unit cost US$134,284 when new[2] Variants Lockheed XP-49 XP-58 Chain Lightning The Lockheed P-38 Lightning was a World War II American fighter aircraft. Developed to a United States Army Air Corps requirement, the P-38 had distinctive twin booms with forward-mounted engines and a single, central nacelle containing the pilot and armament. The aircraft was used in a number of different roles, including dive bombing, level bombing, ground strafing, photo reconnaissance missions,[3] and extensively as a long-range escort fighter when equipped with droppable fuel tanks under its wings. The P-38 was used most extensively and successfully in the Pacific Theater of Operations and the China-Burma-India Theater of Operations, where it was flown by the American pilots with the highest number of aerial victories to this date. The Lightning called "Marge" was flown by the ace of aces Richard Bong who earned 40 victories. Second with 38 was Thomas McGuire in his aircraft called "Pudgy". In the South West Pacific theater, it was a primary fighter of United States Army Air Forces until the appearance of large numbers of P-51D Mustangs toward the end of the war. [4][5] 1 Design and development Lockheed YP-38 (1943) Lockheed designed the P-38 in response to a 1937 United States Army Air Corps request for a high- altitude interceptor aircraft, capable of 360 miles per hour at an altitude of 20,000 feet, (580 km/h at 6100 m).[6] The Bell P-39 Airacobra and the Curtiss P-40 Warhawk were also designed to meet the same requirements.