DOCSLIB.ORG

The Market for Missile/Drone/UAV Engines

Total Page：16

File Type：pdf, Size：1020Kb

Download full-text PDF Read full-text
The Market for Missile/Drone/UAV Engines The Market for Missile/Drone/UAV Engines Product Code #F655 A Special Focused Market Segment Analysis by: Aviation Gas Turbine Forecast Analysis 5 The Market for Missile/Drone/UAV Engines 2010-2019 Table of Contents Executive Summary .................................................................................................................................................2 Introduction................................................................................................................................................................2 Methodology ..............................................................................................................................................................2 Trends..........................................................................................................................................................................3 The Competitive Environment...............................................................................................................................3 Market Statistics .......................................................................................................................................................4 Table 1 - The Market for Missile/Drone/UAV Engines Unit Production by Headquarters/Company/Program 2010 - 2019 ..................................................5 Table 2 - The Market for Missile/Drone/UAV Engines Value Statistics by Headquarters/Company/Program 2010 - 2019...................................................8 Figure 1 - The Market for Missile/Drone/UAV Engines Unit Production 2010 - 2019 (Bar Graph) ...............................................................................11 Figure 2 - The Market for Missile/Drone/UAV Engines Value of Production 2010 - 2019 (Bar Graph).........................................................................11 Table 3 - The Market for Missile/Drone/UAV Engines Unit Production % Market Share by Headquarters/Company 2010 - 2019 ....................................12 Table 4 - The Market for Missile/Drone/UAV Engines Value Statistics % Market Share by Headquarters/Company 2010 - 2019.....................................13 Figure 3 - The Market for Missile/Drone/UAV Engines Unit Production % Market Share 2010 - 2019 (Pie Chart) ......................................................14 Figure 4 - The Market for Missile/Drone/UAV Engines Value Statistics % Market Share 2010 -2019 (Pie Chart)........................................................14 Conclusion ...............................................................................................................................................................15 * * * ©2010 November 2010 Product Code F655 The Market for Missile/Drone/UAV Engines PROGRAMS The following reports are included in this section: (Note: a single report may cover several programs.) HAL PTAE-7 Hamilton Sundstrand TJ-50/TJ-120 (Includes only TJ-120) Microturbo TRI 40/TRI 60 Microturbo TRS 18 Mitsubishi TJM2/3/4 Teledyne J402 Turbomeca Arbizon Williams International F107/F122/F415 (F107 Out of Production) Williams International WR2/WR24 (Includes only WR24) ©2010 November 2010 Product Code F655 The Market for Missile/Drone/UAV Engines Introduction Small turbine engine technology is generally leveraged militaries, and will guarantee their continuing from turbofan development programs. Advances in development and production. metallurgy allow higher operating temperatures and The small turbine engine industry's major players are lower fuel consumption as well as greater durability. Williams International, Microturbo, Teledyne, and The combination of these advances in technology Hamilton Sundstrand. All of these manufacturers provides for changes in the tactics by the military, the produce turbofan or turbojet engines in the low thrust largest user of UAVs. range for missile and UAV programs. Turbofan and turboprop-powered UAVs can loiter at In this analysis, Forecast International reviews the world altitudes that keep them out of enemy engagement range market for missile, drone, and UAV turbine engines. All while giving battlefield commanders real-time known engine programs in production were reviewed in surveillance information. This intelligence capability preparing this analysis, and an overview of the has made unmanned aircraft irreplaceable in the world's marketplace is provided. * * * ©2010 Aviation Gas Turbine Forecast Microturbo TRI 40/TRI 60 Outlook Unit Production Forecast 2010-2019 SCALP missile series popular in Europe 350 300 TRI 40 replaces solid fuel engine on Exocet 250 200 150 100 50 0 2010 2011 2012 2013 2014 2015 2016 2017 2018 2019 Units 302 315 307 321 329 272 271 214 207 163 Units Orientation Description. Small, single-shaft, axial-flow turbojet Power Class. Current series of powerplants: 750- to series in the 750- to 1,250-lbst class. 1,250-lbst class (3.36 to 5.56 kN). Sponsor. The Microturbo TRI 60 engine series was Status. In production for Exocet, RBS15M Mk 2, developed under contract by the Direction des Storm Shadow/SCALP missiles, and BQM-167A Recherches et Moyens d'Essais, with funding directly Skeeter. from the government of France. Total Produced. As of August 2010, an estimated Licensees. Microturbo Ltd (formerly Ames Industrial 6,197 TRI 40/TRI 60 engines of all variants were built. Ltd), Fort Walling, Fareham, Hants, United Kingdom, and Microturbo Inc (formerly Microturbo North America), Grand Prairie, Texas, USA. Application. Missiles, cruise missiles, drones, remotely piloted vehicles (RPVs), and other unmanned air vehicles (UAVs). Current or proposed applications include the following (all power ratings are at ISA sea-level conditions): Engine Power or Engines per Variant Thrust Rating Application Airframe TRI 40 560-750 lbst (2.5-3.3 kN) Kongsberg/MBDA NSM 1 TRI 60 800-1,200 lbst (3.5-5.3 kN) Saab TGA (potentially) 1 TRI 60-1 787 lbst (3.5 kN) Meteor Mirach 300 RPV/Target 1 Meteor Mirach 600 MAV 2 TRI 60-1 067 787 lbst (3.5 kN) BAE Sea Eagle (P.3T) Anti-ship Missile 1 TRI 60-2 071 832 lbst (3.7 kN) Aerospatiale C.22 RPV/Drone 1 TRI 60-2 074 832 lbst (3.7 kN) Beech MQM-107B Streaker Missile Target 1 TRI 60-2 077 832 lbst (3.7 kN) Saab RBS15M Anti-ship Missile 1 TRI 60-2 080 832 lbst (3.7 kN) HAL PTA Drone (early models) 1 TRI 60-2 088 832 lbst (3.7 kN) Northrop NV-144/NV-151 drone (flight test units only) 1 TRI 60-2 089 832 lbst (3.7 kN) Saab RBS15F/ASM15 Missile (air-launched) 1 ©2010 October 2010 Page 2 Aviation Gas Turbine Forecast Microturbo TRI 40/TRI 60 Engine Power or Engines per Variant Thrust Rating Application Airframe TRI 60-3 097 900 lbst (4.0 kN) Beech BQM-126 drone 1 TRI 60-30 1,200 lbst (5.3 kN) SCALP-EG (APACHE) 1 Matra SCALP Navale 1 MBDA Storm Shadow 1 Price Range. TRI 60 variants estimated at $52,000 to Competition. The TRI 40/60 faces competition from $83,000. TRI 40 estimated at $100,000 (in 2010 U.S. the 600- to 750-lbst (2.6- to 3.3-kN) Williams dollars). F107/112, the 800-lbst (3.5-kN) Turbomeca Arbizon, and the 640- to 1,100-lbst (2.8- to 4.8-kN) Teledyne CAE J402. Contractors Prime Microturbo SA http://www.microturbo/fr, 8, Chemin du Pont de Rupé, B.P. 2089, Toulouse, 31019 France, Tel: + 33 5 61 37 55 00, Fax: + 33 5 61 70 74 45, Prime Subcontractor Pacific Scientific - ATG http://www.pacsci.com, 4301 Kishwaukee St, PO Box 106, Rockford, IL 61105 United States, Tel: + 1 (815) 226-3100, Fax: + 1 (815) 226-3122, Email: [email protected] (Alternator) Comprehensive information on Contractors can be found in Forecast International’s “International Contractors” series. For a detailed description, go to www.forecastinternational.com (see Products & Samples/Governments & Industries) or call + 1 (203) 426-0800. Contractors are invited to submit updated information to Editor, International Contractors, Forecast International, 22 Commerce Road, Newtown, CT 06470, USA; [email protected] Technical Data Design Features. The Microturbo TRI 40/60 has the by a peripheral manifold. Mid-frame is fabricated from following design features: an investment casting and forging. Intake. Annular intake with bullet dome. Turbine. Single axial-flow unit of IN718 drives the compressor through direct shaft coupling. Turbine inlet Compressor. A three-stage axial-flow compressor temperature (TIT) is approximately 1,850°F (1,010°C). (four stages in TRI 60-20/30) gives a pressure ratio of Exhaust gases are exited via a convergent exhaust 3.83:1 to 5.58:1. Light alloy aluminum wheels and nozzle. Rear housing is cast and carries the rear main stators are machined from drop-forged blanks. bearing, fuel manifold, injectors, and turbine casing. The TRI 40 has a four-stage axial compressor. Accessories. Starting can be accomplished by air Combustor. Annular smokeless combustor with 12 motor, windmilling, or pyrotechnic cartridge, depending nozzles and a single spark or pyro-flare igniter, housed on the application. Electronic controls ensure speed in a stainless-steel turbine case. Spray burners are fed governing and automatic sequencing when starting. Dimensions. The approximate dimensions of the Microturbo TRI 60-2/-20/-30 and TRI 40 are as follows: Metric Units English Units TRI 60-2/-20/-30 Length 749/851/851 mm 29.5/33.5/33.5 in Diameter, maximum 330/348/348 mm 13.0/13.7/13.7 in Weight 49/64.4/61.2 kg 108/142/135 lb October 2010 Aviation Gas Turbine Forecast Page 3 Microturbo TRI 40/TRI 60 Metric Units English Units TRI 40 Length 680 mm 26.77 in Diameter, maximum 280 mm 11.02 in Weight
Load more

Recommended publications
  • 3-VIEWS - TABLE of CONTENTS to Search: Hold "Ctrl" Key Then Press "F" Key
    3-VIEWS - TABLE of CONTENTS To search: Hold "Ctrl" key then press "F" key. Enter manufacturer or model number in search box. Click your back key to return to the search page. It is highly recommended to read Order Instructions and Information pages prior to selection. Aircraft MFGs beginning with letter A ................................................................. 3 B ................................................................. 6 C.................................................................10 D.................................................................14 E ................................................................. 17 F ................................................................. 18 G ................................................................21 H................................................................. 23 I .................................................................. 26 J ................................................................. 26 K ................................................................. 27 L ................................................................. 28 M ................................................................30 N................................................................. 35 O ................................................................37 P ................................................................. 38 Q ................................................................40 R................................................................
    [Show full text]
  • CRUISE MISSILE THREAT Volume 2: Emerging Cruise Missile Threat
    By Systems Assessment Group NDIA Strike, Land Attack and Air Defense Committee August 1999 FEASIBILITY OF THIRD WORLD ADVANCED BALLISTIC AND CRUISE MISSILE THREAT Volume 2: Emerging Cruise Missile Threat The Systems Assessment Group of the National Defense Industrial Association ( NDIA) Strike, Land Attack and Air Defense Committee performed this study as a continuing examination of feasible Third World missile threats. Volume 1 provided an assessment of the feasibility of the long range ballistic missile threats (released by NDIA in October 1998). Volume 2 uses aerospace industry judgments and experience to assess Third World cruise missile acquisition and development that is “emerging” as a real capability now. The analyses performed by industry under the broad title of “Feasibility of Third World Advanced Ballistic & Cruise Missile Threat” incorporate information only from unclassified sources. Commercial GPS navigation instruments, compact avionics, flight programming software, and powerful, light-weight jet propulsion systems provide the tools needed for a Third World country to upgrade short-range anti-ship cruise missiles or to produce new land-attack cruise missiles (LACMs) today. This study focuses on the question of feasibility of likely production methods rather than relying on traditional intelligence based primarily upon observed data. Published evidence of technology and weapons exports bears witness to the failure of international agreements to curtail cruise missile proliferation. The study recognizes the role LACMs developed by Third World countries will play in conjunction with other new weapons, for regional force projection. LACMs are an “emerging” threat with immediate and dire implications for U.S. freedom of action in many regions .
    [Show full text]
  • Cranfield University
    CRANFIELD UNIVERSITY LEIGH MOODY SENSORS, SENSOR MEASUREMENT FUSION AND MISSILE TRAJECTORY OPTIMISATION COLLEGE OF DEFENCE TECHNOLOGY PhD THESIS CRANFIELD UNIVERSITY COLLEGE OF DEFENCE TECHNOLOGY DEPARTMENT OF AEROSPACE, POWER AND SENSORS PhD THESIS Academic Year 2002 - 2003 Leigh Moody Sensors, Measurement Fusion and Missile Trajectory Optimisation Supervisor: Professor B.A. White July 2003 Leigh Moody asserts his right to be identified as the author. © Cranfield University 2003 All rights reserved. No part of this publication may be reproduced without the written permission of Cranfield University and without acknowledging that it may contain copyright material owned by MBDA UK Limited. i ii ABSTRACT When considering advances in “smart” weapons it is clear that air-launched systems have adopted an integrated approach to meet rigorous requirements, whereas air-defence systems have not. The demands on sensors, state observation, missile guidance, and simulation for air-defence is the subject of this research. Historical reviews for each topic, justification of favoured techniques and algorithms are provided, using a nomenclature developed to unify these disciplines. Sensors selected for their enduring impact on future systems are described and simulation models provided. Complex internal systems are reduced to simpler models capable of replicating dominant features, particularly those that adversely effect state observers. Of the state observer architectures considered, a distributed system comprising ground based target and own-missile tracking, data up-link, and on-board missile measurement and track fusion is the natural choice for air-defence. An IMM is used to process radar measurements, combining the estimates from filters with different target dynamics. The remote missile state observer combines up-linked target tracks and missile plots with IMU and seeker data to provide optimal guidance information.
    [Show full text]
  • Aeronautical Engineering
    NASA/S P--1999-7037/S U P PL410 December 1999 AERONAUTICAL ENGINEERING A CONTINUING BIBLIOGRAPHY WITH INDEXES National Aeronautics and Space Administration Langley Research Center Scientific and Technical Information Program Office The NASA STI Program Office... in Profile Since its founding, NASA has been dedicated CONFERENCE PUBLICATION. Collected to the advancement of aeronautics and space papers from scientific and technical science. The NASA Scientific and Technical conferences, symposia, seminars, or other Information (STI) Program Office plays a key meetings sponsored or cosponsored by NASA. part in helping NASA maintain this important role. SPECIAL PUBLICATION. Scientific, technical, or historical information from The NASA STI Program Office is operated by NASA programs, projects, and missions, Langley Research Center, the lead center for often concerned with subjects having NASA's scientific and technical information. substantial public interest. The NASA STI Program Office provides access to the NASA STI Database, the largest collection TECHNICAL TRANSLATION. of aeronautical and space science STI in the English-language translations of foreign world. The Program Office is also NASA's scientific and technical material pertinent to institutional mechanism for disseminating the NASA's mission. results of its research and development activities. These results are published by NASA in the Specialized services that complement the STI NASA STI Report Series, which includes the Program Office's diverse offerings include following report types: creating custom thesauri, building customized databases, organizing and publishing research TECHNICAL PUBLICATION. Reports of results.., even providing videos. completed research or a major significant phase of research that present the results of For more information about the NASA STI NASA programs and include extensive data or Program Office, see the following: theoretical analysis.
    [Show full text]
  • Jacques Tiziou Space Collection
    Jacques Tiziou Space Collection Isaac Middleton and Melissa A. N. Keiser 2019 National Air and Space Museum Archives 14390 Air & Space Museum Parkway Chantilly, VA 20151 [email protected] https://airandspace.si.edu/archives Table of Contents Collection Overview ........................................................................................................ 1 Administrative Information .............................................................................................. 1 Biographical / Historical.................................................................................................... 1 Scope and Contents........................................................................................................ 2 Arrangement..................................................................................................................... 2 Names and Subjects ...................................................................................................... 2 Container Listing ............................................................................................................. 4 Series : Files, (bulk 1960-2011)............................................................................... 4 Series : Photography, (bulk 1960-2011)................................................................. 25 Jacques Tiziou Space Collection NASM.2018.0078 Collection Overview Repository: National Air and Space Museum Archives Title: Jacques Tiziou Space Collection Identifier: NASM.2018.0078 Date: (bulk 1960s through
    [Show full text]
  • Operation in Iraq, Our Diplomatic Efforts Were Concentrated in the UN Process
    OPERATIONS IN IRAQ First Reflections IRAQ PUBLISHED JULY 2003 Produced by Director General Corporate Communication Design by Directorate of Corporate Communications DCCS (Media) London IRAQ FIRST REFLECTIONS REPORT Contents Foreword 2 Chapter 1 - Policy Background to the Operation 3 Chapter 2 - Planning and Preparation 4 Chapter 3 - The Campaign 10 Chapter 4 - Equipment Capability & Logistics 22 Chapter 5 - People 28 Chapter 6 - Processes 32 Chapter 7 - After the Conflict 34 Annex A - Military Campaign Objectives 39 Annex B - Chronology 41 Annex C - Deployed Forces and Statistics 43 1 Foreword by the Secretary of State for Defence On 20 March 2003 a US-led coalition, with a substantial contribution from UK forces, began military operations against the Saddam Hussein regime in Iraq. Just 4 weeks later, the regime was removed and most of Iraq was under coalition control. The success of the military campaign owed much to the determination and professionalism of the coalition’s Armed Forces and the civilians who supported them. I regret that, during the course of combat operations and subsequently, a number of Service personnel lost their lives. Their sacrifice will not be forgotten. The UK is playing a full part in the re-building of Iraq through the establishment of conditions for a stable and law-abiding Iraqi government. This process will not be easy after years of repression and neglect by a brutal regime. Our Armed Forces are performing a vital and dangerous role by contributing to the creation of a secure environment so that normal life can be resumed, and by working in support of humanitarian organisations to help the Iraqi people.
    [Show full text]
  • US Navy Program Guide 2012
    U.S. NAVY PROGRAM GUIDE 2012 U.S. NAVY PROGRAM GUIDE 2012 FOREWORD The U.S. Navy is the world’s preeminent cal change continues in the Arab world. Nations like Iran maritime force. Our fleet operates forward every day, and North Korea continue to pursue nuclear capabilities, providing America offshore options to deter conflict and while rising powers are rapidly modernizing their militar- advance our national interests in an era of uncertainty. ies and investing in capabilities to deny freedom of action As it has for more than 200 years, our Navy remains ready on the sea, in the air and in cyberspace. To ensure we are for today’s challenges. Our fleet continues to deliver cred- prepared to meet our missions, I will continue to focus on ible capability for deterrence, sea control, and power pro- my three main priorities: 1) Remain ready to meet current jection to prevent and contain conflict and to fight and challenges, today; 2) Build a relevant and capable future win our nation’s wars. We protect the interconnected sys- force; and 3) Enable and support our Sailors, Navy Civil- tems of trade, information, and security that enable our ians, and their Families. Most importantly, we will ensure nation’s economic prosperity while ensuring operational we do not create a “hollow force” unable to do the mission access for the Joint force to the maritime domain and the due to shortfalls in maintenance, personnel, or training. littorals. These are fiscally challenging times. We will pursue these Our Navy is integral to combat, counter-terrorism, and priorities effectively and efficiently, innovating to maxi- crisis response.
    [Show full text]
  • Desind Finding
    NATIONAL AIR AND SPACE ARCHIVES Herbert Stephen Desind Collection Accession No. 1997-0014 NASM 9A00657 National Air and Space Museum Smithsonian Institution Washington, DC Brian D. Nicklas © Smithsonian Institution, 2003 NASM Archives Desind Collection 1997-0014 Herbert Stephen Desind Collection 109 Cubic Feet, 305 Boxes Biographical Note Herbert Stephen Desind was a Washington, DC area native born on January 15, 1945, raised in Silver Spring, Maryland and educated at the University of Maryland. He obtained his BA degree in Communications at Maryland in 1967, and began working in the local public schools as a science teacher. At the time of his death, in October 1992, he was a high school teacher and a freelance writer/lecturer on spaceflight. Desind also was an avid model rocketeer, specializing in using the Estes Cineroc, a model rocket with an 8mm movie camera mounted in the nose. To many members of the National Association of Rocketry (NAR), he was known as “Mr. Cineroc.” His extensive requests worldwide for information and photographs of rocketry programs even led to a visit from FBI agents who asked him about the nature of his activities. Mr. Desind used the collection to support his writings in NAR publications, and his building scale model rockets for NAR competitions. Desind also used the material in the classroom, and in promoting model rocket clubs to foster an interest in spaceflight among his students. Desind entered the NASA Teacher in Space program in 1985, but it is not clear how far along his submission rose in the selection process. He was not a semi-finalist, although he had a strong application.
    [Show full text]
  • China Missile Chronology
    China Missile Chronology Last update: June 2012 2012 18 May 2012 The Department of Defense releases the 2012 “Military and Security Developments Involving the People’s Republic of China” report. The report highlights that the PLA Air force is modernizing its ground‐based air defense forces with conventional medium‐range ballistic missiles, which can “conduct precision strikes against land targets and naval ships, including aircraft carriers, operating far from China’s shores beyond the first island chain.” According to the Department of Defense’s report, China will acquire DF‐31A intercontinental ballistic missiles (ICBMs) and enhanced, silo‐based DF‐5 (CSS‐4) ICMBs by 2015. To date, China is the third country that has developed a stealth combat aircraft, after the U.S. and Russia. J‐20 is expected conduct military missions by 2018. It will be equipped with “air‐to‐air missiles, air‐to‐surface missiles, anti‐radiation missiles, laser‐guided bombs and drop bombs.”J‐20 stealth fighter is a distinguished example of Chinese military modernization. – Office of Secretary of Defense, “Annual Report to Congress: Military and Security Developments Involving the People’s Republic of China 2012,” distributed by U.S. Department of Defense, May 2012, www.defense.gov; Office of the Assistant Secretary of Defense, David Helvey, “Press Briefing on 2012 DOD Report to Congress on ‘Military and Security Developments Involving the People’s Republic of China,’” distributed by U.S. Department of Defense, 18 May 2012, www.defense.gov; “Chengdu J‐20 Multirole Stealth Fighter Aircraft, China,” Airforce‐Technology, www.airforce‐technology.com. 15 April 2012 North Korea shows off a potential new ICBM in a military parade.
    [Show full text]
  • HMS Southampton
    HMS Southampton HMS SoutHaMpton The replacement for the destroyers of the County-class, were much more compact and austere than their fore bearers. The primary on role of the Type 42s was to provide area air I defence for the ships they had to escort. With their long-range sensor fit they also could act as radar pickets, sailing ahead of a Task Group to act as its eyes and ears. The loss of HMS Sheffield and Coventry dem- Introduct onstrated, this latter role denied the ships supporting fire from accompanying warships and highlighted their vulnerability. 2 Warship 09 developMent In the 1960s the Royal Navy was still one On 14 February 1966, after a day long an all-gas turbine (COGOG) propul- of the premier carrier fleets in the world, meeting, the Cabinet decided to cancel sion system, using Rolls-Royce Olympus second only to the US Navy which was the plans for the construction of the new turbines for main drive and Tynes for in the process of building 80,000 tons carrier. The Labour government calculated cruising. aircraft carriers of the Kitty Hawk-class. that maintaining a carrier air group East of Although lacking Ikara, the ASW capabil- The increasing weight and size of modern Suez would be 60% more expensive than ity was greatly improved over previous jet fighters meant that a larger deck area as a land based airforce. Along with the ships by providing a hangared Lynx light was required for take offs and landings. cancellation went the proposed Type 82 helicopter (armed with torpedoes and Although the Royal Navy had come up destroyers designed to escort them.
    [Show full text]
  • Archie to SAM a Short Operational History of Ground-Based Air Defense
    Archie to SAM A Short Operational History of Ground-Based Air Defense Second Edition KENNETH P. WERRELL Air University Press Maxwell Air Force Base, Alabama August 2005 Air University Library Cataloging Data Werrell, Kenneth P. Archie to SAM : a short operational history of ground-based air defense / Kenneth P. Werrell.—2nd ed. —p. ; cm. Rev. ed. of: Archie, flak, AAA, and SAM : a short operational history of ground- based air defense, 1988. With a new preface. Includes bibliographical references and index. ISBN 1-58566-136-8 1. Air defenses—History. 2. Anti-aircraft guns—History. 3. Anti-aircraft missiles— History. I. Title. 358.4/145—dc22 Disclaimer Opinions, conclusions, and recommendations expressed or implied within are solely those of the author and do not necessarily represent the views of Air University, the United States Air Force, the Department of Defense, or any other US government agency. Cleared for public re- lease: distribution unlimited. Air University Press 131 West Shumacher Avenue Maxwell AFB AL 36112-6615 http://aupress.maxwell.af.mil ii In memory of Michael Lewis Hyde Born 14 May 1938 Graduated USAF Academy 8 June 1960 Killed in action 8 December 1966 A Patriot, A Classmate, A Friend THIS PAGE INTENTIONALLY LEFT BLANK Contents Chapter Page DISCLAIMER . ii DEDICATION . iii FOREWORD . xiii ABOUT THE AUTHOR . xv PREFACE TO THE SECOND EDITION . xvii PREFACE TO THE FIRST EDITION . xix ACKNOWLEDGMENTS . xxi 1 ANTIAIRCRAFT DEFENSE THROUGH WORLD WAR II . 1 British Antiaircraft Artillery . 4 The V-1 Campaign . 13 American Antiaircraft Artillery . 22 German Flak . 24 Allied Countermeasures . 42 Fratricide . 46 The US Navy in the Pacific .
    [Show full text]
  • 1 Introduction 1
    Notes 1 Introduction 1. A debate exists whether a ‘Second Cold War’ did in fact break out or whether this merely a changing phase of the ongoing Cold War. This changing situation in East-West relations from the late 1970s onwards will henceforth, be referred to as the Second Cold War. See, for example, Fred Halliday, The Making of the Second Cold War (London: Verso Editions and NLB, second edition, 1986). 2. Private discussions. In 1979 only 2 per cent of the electorate thought defence was a major issue in the election. By 1983 this had risen to 38 per cent. Michael Heseltine, ‘The United Kingdom’s Strategic Interests and Priorities’, RUSI Journal, vol. 128, no. 4, December 1983, pp. 3–5, p. 3. The 1983 election campaign was noteworthy for the action of the previous Labour Prime Minister, James Callaghan, who took the unprecedented step of repudiating his own party’s defence policy; Ian Aitken, ‘Callaghan Wrecks Polaris Repairs’, Guardian, 26 May 1983; Peter M. Jones, ‘British Defence Policy: the Breakdown of the Inter-party Consensus’, Review of International Studies, vol. 13, no. 2, April 1987, pp. 111–31; Bruce George and Curt Pawlisch, ‘Defence and 1983 Election’, ADIU Report, vol. 5, no. 4, July/August 1983, p. 2; Michael Heseltine, Life in the Jungle: My Autobiography (London: Hodder and Stoughton, 2000), p. 250. 3. Peter Calvocoressi, ‘Deterrence, the Costs, the Issues, the Choices’, Sunday Times, 6 April 1980. 4. Nicholas J. Wheeler, ‘Perceptions of the Soviet Threat’, in British Security Policy: the Thatcher Years and the End of the Cold War, edited by Stuart Croft (London: HarperCollins Academic, 1991), p.
    [Show full text]