ACP 34 Volume 2 Air Ll.Pmd
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Future Technology and International Cooperation a UK Perspective
MAY Future Technology and International Cooperation A UK perspective In 2011, NATO’s Integrated Air Defence (NATINAD) and the supporting NATO Integrated Air Defence System (NATINADS) marked 50 years of safeguarding NATO’s skies. In order to successfully reach future milestones NATO must continue (and in many cases improve) its air defence interoperability across the strategic, operational and tactical domains. In order for this to become reality a combination of exploiting synergies and acknowledging that the whole is greater than the sum of its parts1 is required at all levels. Recent improvements and a greater focus on future capability within the UK’s Joint Ground Based Air Defence (Jt GBAD) will enable the Formation to deploy its units and sub-units in order to operate the latest air defence weapon systems, within a multinational environment, against a near-peer adversary or asymmetric threat, and win. Major Charles W.I. May RA – 14 (Cole’s Kop) Battery Royal Artillery* the strategic direction of the British Armed ‘If I didn‘t have air supremacy, I wouldn‘t be here.’ Forces, and subsequently the operational level (SACEUR, Gen. Dwight D. Eisenhower, June 1944) construct. As the new direction is towards Joint Force 2025 (JF2025) it is pragmatic for this paper to focus on the next 10 years. The his article will highlight the UK military’s purpose is to identify and highlight the Tstrategic situation, perception and under- pertinent capability enhancements and future standing of the air threat before explaining the vision of the UK’s Ground Based Air Defence new military structure to which the Formation Formation and its developing role within the is adapting. -
Aerospace Engine Data
AEROSPACE ENGINE DATA Data for some concrete aerospace engines and their craft ................................................................................. 1 Data on rocket-engine types and comparison with large turbofans ................................................................... 1 Data on some large airliner engines ................................................................................................................... 2 Data on other aircraft engines and manufacturers .......................................................................................... 3 In this Appendix common to Aircraft propulsion and Space propulsion, data for thrust, weight, and specific fuel consumption, are presented for some different types of engines (Table 1), with some values of specific impulse and exit speed (Table 2), a plot of Mach number and specific impulse characteristic of different engine types (Fig. 1), and detailed characteristics of some modern turbofan engines, used in large airplanes (Table 3). DATA FOR SOME CONCRETE AEROSPACE ENGINES AND THEIR CRAFT Table 1. Thrust to weight ratio (F/W), for engines and their crafts, at take-off*, specific fuel consumption (TSFC), and initial and final mass of craft (intermediate values appear in [kN] when forces, and in tonnes [t] when masses). Engine Engine TSFC Whole craft Whole craft Whole craft mass, type thrust/weight (g/s)/kN type thrust/weight mini/mfin Trent 900 350/63=5.5 15.5 A380 4×350/5600=0.25 560/330=1.8 cruise 90/63=1.4 cruise 4×90/5000=0.1 CFM56-5A 110/23=4.8 16 -
Sir Frank Cooper on Air Force Policy in the 1950S & 1960S
The opinions expressed in this publication are those of the authors concerned and are not necessarily those held by the Royal Air Force Historical Society Copyright © Royal Air Force Historical Society, 1993 All rights reserved. 1 Copyright © 1993 by Royal Air Force Historical Society First published in the UK in 1993 All rights reserved. No part of this book may be reproduced or transmitted in any form or by any means, electronic or mechanical including photocopying, recording or by any information storage and retrieval system, without permission from the Publisher in writing. Printed by Hastings Printing Company Limited Royal Air Force Historical Society 2 THE PROCEEDINGS OFTHE ROYAL AIR FORCE HISTORICAL SOCIETY Issue No 11 President: Marshal of the Royal Air Force Sir Michael Beetham GCB CBE DFC AFC Committee Chairman: Air Marshal Sir Frederick B Sowrey KCB CBE AFC General Secretary: Group Captain J C Ainsworth CEng MRAeS Membership Secretary: Commander P O Montgomery VRD RNR Treasurer: D Goch Esq FCCA Programme Air Vice-Marshal G P Black CB OBE AFC Sub-Committee: Air Vice-Marshal F D G Clark CBE BA Air Commodore J G Greenhill FBIM T C G James CMG MA *Group Captain I Madelin Air Commodore H A Probert MBE MA Group Captain A R Thompson MBE MPhil BA FBIM MIPM Members: A S Bennell Esq MA BLitt *Dr M A Fopp MA PhD FMA FBIM A E Richardson *Group Captain N E Taylor BSc D H Wood Comp RAeS * Ex-officio The General Secretary Regrettably our General Secretary of five years standing, Mr B R Jutsum, has found it necessary to resign from the post and the committee. -
Decision 2005/07/R
DECISION No 2005/07/R OF THE EXECUTIVE DIRECTOR OF THE AGENCY of 19-12-2005 amending Decision No 2003/19/RM of 28 November 2003 on acceptable means of compliance and guidance material to Commission Regulation (EC) No 2042/2003 on the continuing airworthiness of aircraft and aeronautical products, parts and appliances, and on the approval of organisations and personnel involved in these tasks THE EXECUTIVE DIRECTOR OF THE EUROPEAN AVIATION SAFETY AGENCY, Having regard to Regulation (EC) No 1592/2002 of 15 July 2002 on common rules in the field of civil aviation (hereinafter referred to as the Basic Regulation) and establishing a European Aviation Safety Agency1 (hereinafter referred to as the “Agency”), and in particular Articles 13 and 14 thereof. Having regard to the Commission Regulation (EC) No 2042/2003 of 28 November 2003 on the continuing airworthiness of aircraft and aeronautical products, parts and appliances, and on the approval of organisations and personnel involved in these tasks.2 Whereas: (1) Annex IV Acceptable Means of Compliance to Part- 66 Appendix 1 Aircraft type ratings for Part-66 aircraft maintenance licence (hereinafter referred to as Part-66 AMC Appendix I) is required to be up to date to serve as reference for the national aviation authorities. (2) To achieve this requirement the text of Part-66 AMC Appendix I should be amended regularly to add new aircraft type rating. (3) The regular amendment of Part-66 AMC Appendix I is considered as a permanent rulemaking task for the Agency. This decision represents the first update according to an accelerated procedure accepted by AGNA and SSCC. -
Security &Defence European
a sniper rifle 4/ 7.90 18 D 14974 E D European NO TIME? NO LAB? NO PROBLEM. & CZ TSR Security .308 WIN. EASILY IDENTIFY CHEMICAL HAZARDS WITH ES THE FLIR GRIFFIN™ G510 PORTABLE GC-MS. 2018 June/July · Defence & Security European WE KNOW THE SECRET OF ACCURATE & Defence 4/2018 LONG DISTANCE SHOOTING. The FLIR Griffin G510 is a completely self-contained GC-MS, including batteries, carrier gas, vacuum system, injector, touchscreen, and heated International Security and Defence Journal sample probe. It analyzes all phases of matter and confirms vapor-based threats in seconds, so that responders can take immediate action. ISSN 1617-7983 See FLIR in action at Eurosatory: Hall 5a Stand #A267 • OPTION TO FIT THE FOLDING HEIGHT MECHANISM ON ADJUSTABLE EITHER THE RIGHT CHEEKPIECE OR LEFT SIDE HEIGHT AND LENGTH www.euro-sd.com ADJUSTABLE • BUTTPLATE June/July 2018 HIGHLy RESISTANT TO CONTAMINATION DUE TO THE FLUTED BOLT 10-ROUND REMOVABLE METAL MAGAZINE FOR CARTRIDGES UP TO 73 MM TWO STAGE TRIGGER MECHANISM WITH THE OPTION TO SET THE TRIGGER PULL BOLT HANDLE ADAPTED FOR RELIABLE AND RAPID PISTOL GRIP WITH RELOADING WITH STORAGE SPACE AND A RIFLESCOPE ATTACHED INTERCHANGEABLE BACKSTRAPS MaxiMuM MiniMuM Barrel length Width of Weapon (MM) height of Weapon Weight Without With stoCk With stoCk With CheekpieCe With eMpty operating CaliBre Magazine CapaCity fraMe overall length (MM)* overal length (MM)** CoMpensator (MM) folded unfolded retraCted Magazine (g) teMperature range rate of tWist aCCuraCy .308 Win. 10 ALUMINIUM 1237 ± 5mm 920 ± 5mm 660 ± 1 95 ± 2 70± 2 192 ± 2 mm max. 6 300 from -50°C to + 50° 1:11“ Sub MOA FLIR Griffin™ G510 Portable GC-MS #CZGUNS www.FLIR.eu/G510 Chemical Identifier eurosatory2018 WWW.CZUB.CZ [email protected] FACEBOOK.COM/CESKAZBROJOVKA.CZ WWW.INSTAGRAM.COM/CZGUNS/ eurosatory2018 a sniper rifle 4/ 7.90 18 D 14974 E D European NO TIME? NO LAB? NO PROBLEM. -
Our Bureauhyderabad, August 17 Bharat Dynamics Ltd
Our BureauHyderabad, August 17 Bharat Dynamics Ltd (BDL) and MBDA of UK have signed up to establish a facility for the Final Assembly, Integration and Test facility for Advanced Short Range Air-to-Air Missile missiles in India. A licensing agreement was signed by NP Diwakar, Director (Technical), BDL, and George Kyriakides, International Industrial Cooperation Director, MBDA at a virtual ceremony today. MBDA will transfer the equipment and knowledge to BDL for establishing the facility. Work is due to start immediately on the unit which is expected to commence operations by 2022-23. In a statement, Commodore Siddharth Mishra (Retd), CMD, BDL said, “ASRAAM is one of the within-visual-range missiles available and BDL will be manufacturing these at its Bhanur Unit, Telangana, for the domestic and export market in future through MBDA.” “The new facility will provide India with the ability to carry out final assembly, integration and test of ASRAAM missiles. BDL has been endeavouring to enter into a tie-up with foreign Original Equipment Manufacturers in pursuit of its expansion programme,” he said. George Kyriakides of MBDA said: “MBDA has a long and highly successful history of working with BDL for over four decades, a partnership that has seen BDL manufacture a large number of MBDA- designed Milan missiles in India.” The agreement to establish the facility follows an earlier Memorandum of Understanding (MoU) between BDL and MBDA on ASRAAM FAIT signed during 2019. This facility can also be adapted to conduct final assembly, integration and test of the CAMM missile of MBDA used by the Sea Ceptor naval air defence system. -
Military Vehicle Options Arising from the Barrel Type Piston Engine
Journal of Power Technologies 101 (1) (2021) 22–33 Military vehicle options arising from the barrel type piston engine Pawe l Mazuro1 and Cezary Chmielewski1,B 1Warsaw University of Technology B [email protected] Abstract in terms of efficiency, meaning that piston engines can deliver enhanced range and endurance. This is benefi- The article reviews knowledge about requirements for engines in cial in missions requiring a stopover for refueling and state-of-the-art unmanned aerial vehicles and tanks. Analysis of particularly useful for unmanned supply, observation design and operational parameters was carried out on selected and maritime missions. turboshaft and piston engines generating power in the range of 500 - 1500 kW (0.5 - 1.5 MW). The data was compared In contrast, land combat vehicles have significantly with the performance of innovative, barrel type piston engines, different drive unit requirements. High mobility en- which are likely to become an alternative drive solution in the ables the vehicle to rapidly change location after de- target vehicle groups. tection. To this end, the torque curve as a function of the rotational speed of the shaft is of decisive im- portance. Keywords: military UAV, tanks, turboshaft engines, piston engines, barrel type piston engines The complexity of tank engines adds an additional layer of requirements, impacting the reliability and durability of the power unit, and they come with re- 1 Introduction lated manufacturing and operating costs. In military land vehicles, the engine should be as small This article consolidates knowledge on options and as possible; the space saved can be used for other capabilities arising from use of the barrel type piston purposes. -
Propulsione Aeronautica 2020/2021 Francesco Barato
PROPULSIONE AERONAUTICA 2020/2021 FRANCESCO BARATO MATERIALE DI SUPPORTO FONDAMENTI DI PROPULSIONE AERONAUTICA Thrust 푇 = (푚̇ 푎 + 푚̇ 푓)푉푒 − 푚̇ 푎푉0 + (푝푒 − 푝푎)퐴푒 푇 ≈ 푚̇ 푎(푉푒 − 푉0) + (푝푒 − 푝푎)퐴푒 1 PROPULSIONE AERONAUTICA 2020/2021 FRANCESCO BARATO Ramjet P-270 Moskit (left), BrahMos (right) Turboramjet Pratt & Whitney J-58 turbo(ram)jet 2 PROPULSIONE AERONAUTICA 2020/2021 FRANCESCO BARATO Scramjet 3 PROPULSIONE AERONAUTICA 2020/2021 FRANCESCO BARATO Specific impulse 푇 푉푒 푇 푚̇ 푝 푉푒 − 푉0 퐼푠푝 = = [푠] 푟표푐푘푒푡푠 퐼푠푝 = = [푠] 푎푟 푏푟푒푎푡ℎ푛푔 푚̇ 푝푔0 푔0 푚̇ 푓푔0 푚̇ 푓 푔0 4 PROPULSIONE AERONAUTICA 2020/2021 FRANCESCO BARATO Propulsive efficiency Overall efficiency Overall efficiency with Mach number 5 PROPULSIONE AERONAUTICA 2020/2021 FRANCESCO BARATO Engine bypass ratios Bypass Engine Name Major applications ratio turbojet early jet aircraft, Concorde 0.0 SNECMA M88 Rafale 0.30 GE F404 F/A-18, T-50, F-117 0.34 PW F100 F-16, F-15 0.36 Eurojet EJ200 Typhoon 0.4 Klimov RD-33 MiG-29, Il-102 0.49 Saturn AL-31 Su-27, Su-30, J-10 0.59 Kuznetsov NK-144A Tu-144 0.6 PW JT8D DC-9, MD-80, 727, 737 Original 0.96 Soloviev D-20P Tu-124 1.0 Kuznetsov NK-321 Tu-160 1.4 GE Honda HF120 HondaJet 2.9 RR Tay Gulfstream IV, F70, F100 3.1 GE CF6-50 A300, DC-10-30,Lockheed C-5M Super Galaxy 4.26 PowerJet SaM146 SSJ 100 4.43 RR RB211-22B TriStar 4.8 PW PW4000-94 A300, A310, Boeing 767, Boeing 747-400 4.85 Progress D-436 Yak-42, Be-200, An-148 4.91 GE CF6-80C2 A300-600, Boeing 747-400, MD-11, A310 4.97-5.31 RR Trent 700 A330 5.0 PW JT9D Boeing 747, Boeing 767, A310, DC-10 5.0 6 PROPULSIONE -
The Raf Harrier Story
THE RAF HARRIER STORY ROYAL AIR FORCE HISTORICAL SOCIETY 2 The opinions expressed in this publication are those of the contributors concerned and are not necessarily those held by the Royal Air Force Historical Society. Copyright 2006: Royal Air Force Historical Society First published in the UK in 2006 by the Royal Air Force Historical Society All rights reserved. No part of this book may be reproduced or transmitted in any form or by any means, electronic or mechanical including photocopying, recording or by any information storage and retrieval system, without permission from the Publisher in writing. ISBN 0-9530345-2-6 Printed by Advance Book Printing Unit 9 Northmoor Park Church Road Northmoor OX29 5UH 3 ROYAL AIR FORCE HISTORICAL SOCIETY President Marshal of the Royal Air Force Sir Michael Beetham GCB CBE DFC AFC Vice-President Air Marshal Sir Frederick Sowrey KCB CBE AFC Committee Chairman Air Vice-Marshal N B Baldwin CB CBE FRAeS Vice-Chairman Group Captain J D Heron OBE Secretary Group Captain K J Dearman Membership Secretary Dr Jack Dunham PhD CPsychol AMRAeS Treasurer J Boyes TD CA Members Air Commodore H A Probert MBE MA *J S Cox Esq BA MA *Dr M A Fopp MA FMA FIMgt *Group Captain N Parton BSc (Hons) MA MDA MPhil CEng FRAeS RAF *Wing Commander D Robertson RAF Wing Commander C Cummings Editor & Publications Wing Commander C G Jefford MBE BA Manager *Ex Officio 4 CONTENTS EARLY HISTORICAL PERSPECTIVES AND EMERGING 8 STAFF TARGETS by Air Chf Mshl Sir Patrick Hine JET LIFT by Prof John F Coplin 14 EVOLUTION OF THE PEGASUS VECTORED -
SP's Aviation August 2010
SP’s AN SP GUIDE PUBLICATION A-BASED BUYER ONLY) BUYER A-BASED I News Flies. We Gather Intelligence. Every Month. From India. RS. 75.00 (IND RS. Aviationwww.spsaviation.net AUGUST • 2010 IAF to get more AWACS Military Aero Engines Interviews with Lockheed Martin’s Ralph Heath & Boeing’s Chris Chadwick FARNBOROUGH AIRSHOW 2010 Iconic RNI NUMBER: DELENG/2008/24199 PAGE 24 SHOW Answering the call with confidence. It’s in our power.™ Pratt & Whitney builds and supports the most advanced military engines in the world, including the F117 engine for the C-17 Globemaster III airlifter. In fact, 27 armed services across the globe employ 11,000 of our engines to deliver when it really counts. Learn more at www.pw.utc.com. Military Engines SP’s AN SP GUIDE PUBLICATION TABLE of CONTENTS News Flies. We Gather Intelligence. Every Month. From India. AviationIssue 8 • 2010 CEOSPEAK 28 Ralph Heath ‘We are the only provider of the fifth generation aircraft to the world’ OEM 30 Interview ‘We focus on the market through the eyes of our customers’ INTERVIEW 32 OEM ‘Reliability and maintainability: A400M, manufactured by Airbus Military, during an impressive two outstanding benefits’ flying display at the Farnborough Airshow 2010. T he aircraft 24 was rechristened – Grizzly HALL OF famE 34 Lawrence Hargrave FIRST Lead Story REGULAR DEpaRTMENTS 8 Transformer 5 A Word from Editor ICONIC SHOW TECH WATCH Farnborough, the biggest air 6 NewsWithViews show of the year, witnessed 9 – Phantom Eye several new aircraft, new - Laser System to track – At an Advantage players and new orders. -
The Market for Aviation Turbofan Engines
The Market for Aviation Turbofan Engines Product Code #F640 A Special Focused Market Segment Analysis by: Aviation Gas Turbine Forecast Analysis 1 The Market for Aviation Turbofan Engines 2010-2019 Table of Contents Executive Summary .................................................................................................................................................2 Introduction................................................................................................................................................................2 Trends..........................................................................................................................................................................3 Market Focus .............................................................................................................................................................3 Competitive Environment.......................................................................................................................................4 Figure 1 - The Market for Aviation Turbofan Engines Unit Production 2010 - 2019 (Bar Graph) .................................................................................6 Figure 2 - The Market for Aviation Turbofan Engines Value of Production 2010 - 2019 (Bar Graph)...........................................................................6 Manufacturers Review.............................................................................................................................................7 -
Testing Down to the Last Detail
1/2010 Testing down to the last detail MTU Aero Engines Holding AG Customers + PartnersTechnology + Science MTU Global Dachauer Straße 665 80995 Munich • Germany Tel. +49 89 1489-0 Fax +49 89 1489-5500 Power for the Jumbo Jet Hardfaced tips for top MTU support for the [email protected] www.mtu.de and the Dreamliner efficiency “flying gas station” Contents Editorial Cover Story Dear Readers: Testing down to the last detail 4 – 7 Finally, yes finally, the bird is on the wing. However, the program highlights something Late last year, the new A400M military trans- else too—something we have witnessed re- Customers + Partners port aircraft successfully completed its long- peatedly in the past. Almost all the major Power for the Jumbo Jet and 8 – 11 awaited, eagerly anticipated maiden flight commercial and military aircraft programs the Dreamliner above the Spanish city of Seville. The relief that have ever been initiated in Europe and A boost for the MRJ 12 – 15 Testing down to the last detail was palpable throughout the industry; delays the United States have been subject to to the project had been creating too much delays, some of them massive. In this respect, Four TP400-D6 engines lift Europe’s new military transport, the A400M, up into turbulence all round. Now, the ongoing flight the A400M is no exception. As things stand the air—now almost an everyday occurrence at Seville airport. Since the maiden Technology + Science test program is demonstrating the superior at present, in pure economic terms, MTU flight in December 2009, flight testing has been in full swing.