Australian Defence Capability Analysis Project LAND 4503 - ARH Replacement Program
Total Page:16
File Type:pdf, Size:1020Kb
Load more
Recommended publications
-
Tiger Helicopter Pureair System
Data Sheet AETIGERENPA Tiger Helicopter PUREair System The Ultimate in Engine Protection The Tiger attack helicopter is currently used by several European defense forces as well as the Australian Army. It has been deployed in desert operations and in 2009 the French Army Tiger helicopter received its operational certificate for use in Afghanistan. The PUREair system is the perfect solution for such challenging operations. It provides the highest level of engine protection which results in: • Reduced maintenance & operational costs © Airbus Helicopters • Increased operational availability & reduced downtime • Increased engine reliability PUREair system for the Tiger helicopter • Safer operation (protection against FOD, ice, snow and sand) • Protection against engine erosion For more information: WEB: FLTR.com.au PHONE: (+61) 1300 62 4020 EMAIL: [email protected] SKYPE: Purple.Engineering Product Details PUREair Vortex Tube Pall P/N: QB0677 (Left), QB0678 (Right) Principle of operation Scavenge air Scavenge System: Fan with contaminant Certified for inadvertent entry into icing conditions. No bypass door required. Clean air out Approval: Eurocopter approved Outlet tube Scavenge air with contaminant Dirty Vortex air in generator The PUREair system benefits: Self Cleaning System Increased Engine MTBUR No barrier filters to clean /replace Improved protection from engine erosion Constant Removal Efficiency Increased Flight Safety Non-bypass system. No degradation in Excellent protection against FOD filtration performance (Foreign Object Damage) No Filter Blockage All Weather Protection PUREair pressure drop does not increase Excellent protection in Ice, Snow, Heavy with use - no risk of in-flight filter blockage Rain, and Salt Spray Conditions. Certified for flight in “known icing conditions” Pall PUREair systems have been protecting helicopter engines since the 1960’s. -
Appendix B Characteristics and Analysis of Flares
APPENDIX B CHARACTERISTICS AND ANALYSIS OF FLARES 1.0 Introduction The F-15E and F-15C employ MJU-7 A/B and MJU-10/B self-protection flares in approved airspace over parts of Alaska. The F-22A uses MJU-10/B self-protection flares. Self-protection flares are magnesium pellets that, when ignited, burn for 3.5 to 5 seconds at 2,000 degrees Fahrenheit. The burn temperature is hotter than the exhaust of an aircraft, and therefore attracts and decoys heat-seeking weapons targeted on the aircraft. Flares are used in pilot training to develop the near instinctive reactions to a threat that are critical to combat survival. This appendix describes flare composition, ejection, risks, and associated regulations. 2.0 Flare Composition Self-protection flares are primarily mixtures of magnesium and Teflon (polytetrafluoroethylene) molded into rectangular shapes (United States Air Force [Air Force] 1997). Longitudinal grooves provide space for materials that aid in ignition such as: • First fire materials: potassium perchlorate, boron powder, magnesium powder, barium chromate, Viton A, or Fluorel binder. • Immediate fire materials: magnesium powder, Teflon, Viton A, or Fluorel • Dip coat: magnesium powder, Teflon, Viton A or Fluorel Typically, flares are wrapped with an aluminum-coated mylar or filament-reinforced tape (wrapping) and inserted into an aluminum (0.03 inches thick) case that is closed with a felt spacer and a small plastic end cap (Air Force 1997). The top of the case has a pyrotechnic impulse cartridge that is activated electrically to produce hot gases that push a piston, the flare material, and the end cap out of the aircraft into the airstream. -
MTR390 Turboshaft Engine
MTR390 turboshaft engine The innovative power MTR390 – The MTR390 engine was developed and is cur- Another 52 engines have been ordered by rently being produced by MTR GmbH, in an Australia. The Australian ARH Tigers powered technology features international consortium formed by MTU Aero by MTR390 engines started operational service Engines (Germany), Turbomeca (France) and at the end of 2004. Rolls-Royce (UK). It has been designed to sat- isfy the challenging requirements set for Euro- In late 2004, a four-year development program copter’s Tiger weapon platform for the German was launched with participation of the Spanish and French armies. company Industria de Turbo Propulsores (ITP) covering the 14-percent growth version of the The engine’s reliability has been proven in more MTR390 engine, called MTR390-E. ITP also than 120,000 flight hours in Eurocopter’s Tiger joined the new engine consortium MTRI as helicopters since 1991. The production in- fourth company. In late 2006 MTRI signed an vestment phase was launched in 1997, and agreement with OCCAR, the European organi- the production contract for a first batch of 342 zation for joint armament cooperation, con- engines was signed by the French-German cerning the delivery of 162 MTR390-E (En- launch customer in early 2000. Production hanced) engines. These engines will equip the engine deliveries commenced early in 2002. Tigers of the Spanish, French and German army’s light aircraft groups as of 2009. Part The service phase started in the first quarter of the agreement is also the full scale devel- of 2005. Maintenance, repair and overhaul opment of a new state-of-the-art Engine (MRO) capabilities have been set up at AIA Control and Monitoring Unit (ECMU) for the Bordeaux for the French customer and at MTU “Enhanced” engine version to meet future Aero Engines in Munich for the German cus- operational needs. -
Aircraft Philipp Group October 2017
Aircraft Philipp Group October 2017 www.aircraft-philipp.com Sites of the Aircraft Philipp Group Aircraft Philipp Karlsruhe GmbH & Co. KG ß Aircraft Philipp Group Gewerbestraße 12-14 83236 Übersee/Germany Aircraft Philipp Übersee GmbH & Co. KG Gewerbestraße 12-14 83236 Übersee/Germany ß Aircraft Philipp Group Company Presentation www.aircraft-philipp.com Capabilities • Machining • Sheet Metal • Additive Manufacturing • Best Cost Country Sourcing • Surface Treatments • NDT • Welding • Assembly Aircraft Philipp Group Company Presentation www.aircraft-philipp.com Aircraft Philipp Group Company Presentation www.aircraft-philipp.com Aircraft Philipp Group Company Presentation www.aircraft-philipp.com Aircraft Philipp Group Company Presentation www.aircraft-philipp.com Certifications Company certifications Customer approvals BAZ EN/AS 9100 GKN DIN EN ISO 14001 Boeing QSF-A, QSF-B Hamilton Sundstrand NADCAP Lockheed Martin Spirit Aerosystems Honeywell Customer approvals Aircraft Philipp Sikorsky Airbus Embraer Airbus UK Cyclone Airbus Germany Elbit Airbus Helicopters IAI Gulfstream Gulfstream Liebherr Aerospace Bombardier Nord Micro Goodrich Telair Triumph PFW Spirit Aerosystems Customer approvals SANSERA Airbus Defense & Space Airbus UK Embraer Goodrich MTU Aero Engines UTAS Rolls Royce Deutschland Magellan Pilatus Aircraft Meggit RUAG Aerostructures GKN Aircraft Philipp Group Company Presentation www.aircraft-philipp.com Programs (Direct & Indirect) Involvement Aircraft (Civil / Military) Lockheed F16 Aircraft Engines Lockheed C130 (Super PW1000 -
Sanctuary Lost: the Air War for ―Portuguese‖ Guinea, 1963-1974
Sanctuary Lost: The Air War for ―Portuguese‖ Guinea, 1963-1974 Dissertation Presented in Partial Fulfillment of the Requirements for the Degree Doctor of Philosophy in the Graduate School of The Ohio State University By Matthew Martin Hurley, MA Graduate Program in History The Ohio State University 2009 Dissertation Committee: Professor John F. Guilmartin, Jr., Advisor Professor Alan Beyerchen Professor Ousman Kobo Copyright by Matthew Martin Hurley 2009 i Abstract From 1963 to 1974, Portugal and the African Party for the Independence of Guinea and Cape Verde (Partido Africano da Independência da Guiné e Cabo Verde, or PAIGC) waged an increasingly intense war for the independence of ―Portuguese‖ Guinea, then a colony but today the Republic of Guinea-Bissau. For most of this conflict Portugal enjoyed virtually unchallenged air supremacy and increasingly based its strategy on this advantage. The Portuguese Air Force (Força Aérea Portuguesa, abbreviated FAP) consequently played a central role in the war for Guinea, at times threatening the PAIGC with military defeat. Portugal‘s reliance on air power compelled the insurgents to search for an effective counter-measure, and by 1973 they succeeded with their acquisition and employment of the Strela-2 shoulder-fired surface-to-air missile, altering the course of the war and the future of Portugal itself in the process. To date, however, no detailed study of this seminal episode in air power history has been conducted. In an international climate plagued by insurgency, terrorism, and the proliferation of sophisticated weapons, the hard lessons learned by Portugal offer enduring insight to historians and current air power practitioners alike. -
MAPPING the DEVELOPMENT of AUTONOMY in WEAPON SYSTEMS Vincent Boulanin and Maaike Verbruggen
MAPPING THE DEVELOPMENT OF AUTONOMY IN WEAPON SYSTEMS vincent boulanin and maaike verbruggen MAPPING THE DEVELOPMENT OF AUTONOMY IN WEAPON SYSTEMS vincent boulanin and maaike verbruggen November 2017 STOCKHOLM INTERNATIONAL PEACE RESEARCH INSTITUTE SIPRI is an independent international institute dedicated to research into conflict, armaments, arms control and disarmament. Established in 1966, SIPRI provides data, analysis and recommendations, based on open sources, to policymakers, researchers, media and the interested public. The Governing Board is not responsible for the views expressed in the publications of the Institute. GOVERNING BOARD Ambassador Jan Eliasson, Chair (Sweden) Dr Dewi Fortuna Anwar (Indonesia) Dr Vladimir Baranovsky (Russia) Ambassador Lakhdar Brahimi (Algeria) Espen Barth Eide (Norway) Ambassador Wolfgang Ischinger (Germany) Dr Radha Kumar (India) The Director DIRECTOR Dan Smith (United Kingdom) Signalistgatan 9 SE-169 72 Solna, Sweden Telephone: +46 8 655 97 00 Email: [email protected] Internet: www.sipri.org © SIPRI 2017 Contents Acknowledgements v About the authors v Executive summary vii Abbreviations x 1. Introduction 1 I. Background and objective 1 II. Approach and methodology 1 III. Outline 2 Figure 1.1. A comprehensive approach to mapping the development of autonomy 2 in weapon systems 2. What are the technological foundations of autonomy? 5 I. Introduction 5 II. Searching for a definition: what is autonomy? 5 III. Unravelling the machinery 7 IV. Creating autonomy 12 V. Conclusions 18 Box 2.1. Existing definitions of autonomous weapon systems 8 Box 2.2. Machine-learning methods 16 Box 2.3. Deep learning 17 Figure 2.1. Anatomy of autonomy: reactive and deliberative systems 10 Figure 2.2. -
Az Airbus H145m Helikopter És a Túlélőképesség Bevezetés
Domán László AZ AIRBUS H145M HELIKOPTER ÉS A TÚLÉLŐKÉPESSÉG DOI: 10.32560/rk.2019.1.8 A cikkben a H145M típusú könnyű, többcélú helikoptert kívánom bemutatni. A fejlesztés, majd főbb harcászat-technikai jellemzők leírását követően, a helikopter túlélőképesség szempontjából történő elemzésével foglalkozom. Részletezve a szerkezeti felépítést, a különböző önvédelmi eszközöket, végezetül a jelenleg alkalmazott fedélzeti fegyvereket. Kulcsszavak: túlélőképesség, helikopter, önvédelmi eszközök, fegyverzet BEVEZETÉS A Magyarország a Zrínyi 2026 Honvédelmi és Haderőfejlesztési Program keretében 2018-ban megrendelt a HForce fegyverrendszerrel ellátott 20 db H145M helikoptert (1. ábra) az Airbus Helicopters vállalattól. A beszerzés célja többek között a szárazföldi csapatok támogatása ér- dekében a lassan üzemidejük és rendszerben tarthatóságuk végső határidejét elérő szovjet gyár- tású helikopterek kiválása miatt, a helikopterflotta megújítása [1]. A publikációban a szerző arra keresi a választ, hogy ennek a helikopter típusnak a túlélőképes- séget növelő technikai megoldásai, hogyan járulnak hozzá a Magyar Honvédség forgószárnyas képességének megújításához, mivel a helikopterek harctéri túlélésének biztosítása elsődleges fontosságú feladat a műveletek tervezésben és a végrehajtásában egyaránt. 1. ábra Az Airbus H145M helikopter [2] AZ AIRBUS H145M HELIKOPTER FEJLESZTÉSE ÉS VÁLTOZATAI Előzmények A német MBB1 és a japán Kawasaki által kifejlesztett BK117 kéthajtóműves könnyű helikopter prototípusának első repülése 1979-ben volt, ezt követően a -
America's Secret Migs
THE UNITED STATES AIR FORCE SECRET COLD WAR TRAINING PROGRAM RED EAGLES America’s Secret MiGs STEVE DAVIES FOREWORD BY GENERAL J. JUMPER © Osprey Publishing • www.ospreypublishing.com RED EAGLES America’s Secret MiGs OSPREY PUBLISHING © Osprey Publishing • www.ospreypublishing.com CONTENTS DEDICATION 6 ACKNOWLEDGMENTS 7 FOREWORD 10 INTRODUCTION 12 PART 1 ACQUIRING “THE ASSETS” 15 Chapter 1: HAVE MiGs, 1968–69 16 Chapter 2: A Genesis for the Red Eagles, 1972–77 21 PART 2 LAYING THE GROUND WORK 49 Chapter 3: CONSTANT PEG and Tonopah, 1977–79 50 Chapter 4: The Red Eagles’ First Days and the Early MiGs 78 Chapter 5: The “Flogger” Arrives, 1980 126 Chapter 6: Gold Wings, 1981 138 PART 3 EXPANDED EXPOSURES AND RED FLAG, 1982–85 155 Chapter 7: The Fatalists, 1982 156 Chapter 8: Postai’s Crash 176 Chapter 9: Exposing the TAF, 1983 193 Chapter 10: “The Air Force is Coming,” 1984 221 Chapter 11: From Black to Gray, 1985 256 PART 4 THE FINAL YEARS, 1986–88 275 Chapter 12: Increasing Blue Air Exposures, 1986 276 Chapter 13: “Red Country,” 1987 293 Chapter 14: Arrival Shows, 1988 318 POSTSCRIPT 327 ENDNOTES 330 APPENDICES 334 GLOSSARY 342 INDEX 346 © Osprey Publishing • www.ospreypublishing.com DEDICATION In memory of LtCdr Hugh “Bandit” Brown and Capt Mark “Toast” Postai — 6 — © Osprey Publishing • www.ospreypublishing.com ACKNOWLEDGMENTS This is a story about the Red Eagles: a group of men, and a handful of women, who provided America’s fighter pilots with a level of training that was the stuff of dreams. It was codenamed CONSTANT PEG. -
Australian ARH Decision
Platforms, Concepts of Operations and Defense Decisions: The Australian ARH Decision By Robbin Laird November 10, 2020 PLATFORMS AND STRATEGIC OPTIONS 3 THE TIGER OPTION 4 AN UPGRADED TIGER 5 THE APACHE OPTION 8 WHAT IS THE ROLE OF THE AUSTRALIAN ARMY IN AUSTRALIA’S NEW STRATEGY? 12 WHAT IS THE ROLE OF AMPHIBIOSITY IN AUSTRALIAN DEFENCE STRATEGY? 16 PUTTING THE VIPER OPTION INTO STRATEGIC CONTEXT 19 DIGITAL INTEROPERABILITY AND KILL WEB PERSPECTIVE FOR PLATFORM MODERNIZATION: THE CASE OF THE VIPER ATTACK HELICOPTER 20 THE VIPER OPTION 24 THE UNMANNED OPTION 25 CONCLUSIONS 27 THE TIGER OPTION 28 THE APACHE OPTION 28 THE VIPER OPTION 29 THE UNMANNED OPTION 29 2 Platforms and Strategic Options As the Australian Defence Force shapes its future, one focused significantly on its neighborhood, and expeditionary operations, a key decision will be about its next armed reconnaissance helicopter. The Department of Defence has indicated in a number of reports over the past few years, that they would like to replace the current Tiger helicopter and have generated an RFI last year to examine options for so doing. The choices being discussion are the Tiger replacing itself; or the American options, either the US Army’s Apache or the USMC’s Viper attack helicopters. And there have been suggestions as well by some analysts, that the Australian Army should forgo replacing its current ARH and add an unmanned capability and to prepare for the coming of the US Army’s next generation attack helicopter which is at least a decade or more away. But as is often the case, a platform choice is not simply about side by side comparisons as if picking different styles of bananas but are choices that have tactical and strategic consequences. -
Military Helicopter Modernization: Background and Issues for Congress
Order Code RL32447 CRS Report for Congress Received through the CRS Web Military Helicopter Modernization: Background and Issues for Congress June 24, 2004 Christian F. M. Liles Research Associate Foreign Affairs, Defense and Trade Division Christopher Bolkcom Specialist in National Defense Foreign Affairs, Defense and Trade Division Congressional Research Service ˜ The Library of Congress Military Helicopter Modernization: Background and Issues for Congress Summary Recent military operations, particularly those in Afghanistan and Iraq, have brought to the fore a number of outstanding questions concerning helicopters in the U.S. armed forces, including deployability, safety, survivability, affordability, and operational effectiveness. These concerns are especially relevant, and made more complicated, in an age of “military transformation,” the “global war on terrorism,” and increasing pressure to rein in funding for the military, all of which provide contradictory pressures with regard to DOD’s large, and often complicated, military helicopter modernization efforts. Despite these questions, the military use of helicopters is likely to hold even, if not grow. This report includes a discussion of the evolving role of helicopters in military transformation. The Department of Defense (DOD) fields 10 different types of helicopters, which are largely of 1960s and 1970s design. This inventory numbers approximately 5,500 rotary-wing aircraft, not including an additional 144 belonging to the Coast Guard, and ranges from simple “utility” platforms such as the ubiquitous UH-1 “Huey” to highly-advanced, “multi-mission” platforms such as the Air Force’s MH- 53J “Pave Low” special operations helicopter and the still-developmental MV-22B “Osprey” tilt-rotor aircraft. Three general approaches can be taken to modernize DOD’s helicopter forces: upgrading current platforms, rebuilding current helicopter models (often called recapitalization), or procuring new models. -
Emulation of Recoil in Pyrotechnic Countermeasure Dispenser System
DEGREE PROJECT IN MATHEMATICS, SECOND CYCLE, 30 CREDITS STOCKHOLM, SWEDEN 2020 Emulation of Recoil in Pyrotechnic Countermeasure Dispenser System EBBA LINDGREN KTH ROYAL INSTITUTE OF TECHNOLOGY SCHOOL OF ENGINEERING SCIENCES Emulation of Recoil in Pyrotechnic Countermeasure Dispenser System EBBA LINDGREN Degree Projects in Systems Engineering (30 ECTS credits) Master’s Programme in Aerospace Engineering (120 credits) KTH Royal Institute of Technology year 2020 Supervisors at Saab AB: Knut-Oloj Jönsson, Marcus Birksjö Supervisor at KTH: Per Enqvist Examiner at KTH: Per Enqvist TRITA-SCI-GRU 2020:234 MAT-E 2020:064 Royal Institute of Technology School of Engineering Sciences KTH SCI SE-100 44 Stockholm, Sweden URL: www.kth.se/sci Abstract Developing countermeasures dispenser systems requires many and careful tests. When it comes to testing products with pyrotechnics, testing can often be very complicated and expensive. This might lead to no testing at all due to time or resource shortages. Products to be used in the military requires further testing and even more thorough reviews to meet the strict demands placed on the products. In order to enable more tests of pyrotechnic flares in the countermeasures industry, this degree project aims to increase theability to perform tests without the need for pyrotechnic means. This was done by designing, constructing and optimizing a recoil emulator, an apparatus that imitates the force-time curve obtained by pyrotechnic flares without the need of pyrotechnic means. The construction of the recoil emulator was conducted at a department that develops countermeasure systems at Saab Surveillance in Järfälla. The apparatus aims to be used in the future for testing and verification of product series of countermeasures dispenser systems. -
Composite Chronicles: a Study of the Lessons Learned in the Development, Production, and Service of Composite Structures
NASA Contractor Report 4620 Composite Chronicles: A Study of the Lessons Learned in the Development, Production, and Service of Composite Structures Louis F. Vosteen Analytical Services & Materials, Inc. • Hampton, Virginia Richard N. Hadcock RNH Associates • Huntington, New York National Aeronautics and Space Administration Prepared for Langley Research Center Langley Research Center • Hampton, Virginia 23681-0001 under Contract NAS1-19317 November 1994 This publication is available from the following sources: NASA Center for AeroSpace Information National Technical Information Service (NTIS) 800 Elkridge Landing Road 5285 Port Royal Road Linthicum Heights, MD 21090-2934 Springfield, VA 22161-2171 (301) 621-0390 (703) 487-4650 TABLE OF CONTEN_I'S Section Title Page Section Title Page Introduction Quality Control 23 General 23 Organizational Issues 2 Nondestructive Inspection 23 Organizational Barriers 2 Effects of Defects 23 Organizational Needs 2 Lessons Learned 23 Technology Transfer 3 Lessons Learned 4 Supportability 24 General 24 Structural Design, Analysis, and Test 5 In-Service Damage & Repair 24 Design and Certification Requirements 5 Lessons Learned 25 Structural Design 7 Structural Analysis 11 Conclusions and Recommendations 25 Structural Test 11 Cost Considerations in Design 12 Appendix 27 Design R&D Needs 13 Lessons Learned 14 Military Aircraft 27 Commercial Transport Aircraft 35 Materials & Processes 15 General Aviation 40 Materials 15 Remotely Piloted Research Vehicles and Processes 16 Drones 43 Joints and Attachments 17 Helicopter Applications 44 Lessons Learned 17 Observations and Conclusions 48 Manufacturing and Tooling 18 References 51 Manufacturing 18 Tooling 20 Acknowledgments 54 Lessons Learned 22 LIST OF FIGURES Figure Number Title Page 1. Organization of structures Design Build Team.