Canada's Fighter Capability

Total Page:16

File Type:pdf, Size:1020Kb

Canada's Fighter Capability CANADA’S FIGHTER CAPABILITY: THE F-35 JSF IS THE RIGHT CHOICE TO REPLACE THE CF-18 HORNET Lieutenant-Colonel A. Dobrei JCSP 37 PCEMI 37 Master of Defence Studies Maîtrise en études de la défense Disclaimer Avertissement Opinions expressed remain those of the author and do Les opinons exprimées n’engagent que leurs auteurs et not represent Department of National Defence or ne reflètent aucunement des politiques du Ministère de Canadian Forces policy. This paper may not be used la Défense nationale ou des Forces canadiennes. Ce without written permission. papier ne peut être reproduit sans autorisation écrite. © Her Majesty the Queen in Right of Canada, as represented by the © Sa Majesté la Reine du Chef du Canada, représentée par le Minister of National Defence, 2014, 2015. ministre de la Défense nationale, 2014, 2015. CANADIAN FORCES COLLEGE – COLLÈGE DES FORCES CANADIENNES JCSP 37 – PCEMI 37 MASTER OF DEFENCE STUDIES – MAÎTRISE EN ÉTUDES DE LA DÉFENSE CANADA’S FIGHTER CAPABILITY: THE F-35 JSF IS THE RIGHT CHOICE TO REPLACE THE CF-18 HORNET By Lieutenant-Colonel A. Dobrei 11 August 2014 “This paper was written by a student “La présente étude a été rédigée par attending the Canadian Forces College un stagiaire du Collège des Forces in fulfilment of one of the requirements canadiennes pour satisfaire à l'une des of the Course of Studies. The paper is exigences du cours. L'étude est un a scholastic document, and thus document qui se rapporte au cours et contains facts and opinions, which the contient donc des faits et des opinions author alone considered appropriate que seul l'auteur considère appropriés and correct for the subject. It does not et convenables au sujet. Elle ne reflète necessarily reflect the policy or the pas nécessairement la politique ou opinion of any agency, including the l'opinion d'un organisme quelconque, y Government of Canada and the compris le gouvernement du Canada et Canadian Department of National le ministère de la Défense nationale du Defence. This paper may not be Canada. Il est défendu de diffuser, de released, quoted or copied, except with citer ou de reproduire cette étude sans the express permission of the Canadian la permission expresse du ministère de Department of National Defence.” la Défense nationale.” Word Count: 15 844 Compte de mots : 15 844 i TABLE OF CONTENTS TABLE OF CONTENTS ..................................................................................................... i LIST OF FIGURES ............................................................................................................ ii LIST OF TABLES ............................................................................................................. iii ABSTRACT ....................................................................................................................... iv 1. INTRODUCTION ..................................................................................................... 1 2. FOUNDATIONS OF CANADIAN FOREIGN AND DEFENCE POLICY ............ 6 3. FORCE DEVELOPMENT, AEROSPACE DOCTRINE AND THE THREAT .... 22 4. THE JOINT STRIKE FIGHTER PROGRAM AND CANADA ............................ 38 5. OTHER POTENTIAL CF-18 REPLACEMENT OPTIONS .................................. 64 6. ANALYSIS SUMMARY ........................................................................................ 78 7. CONCLUSION ........................................................................................................ 87 APPENDIX 1 – SUMMARY OF JSF TECHNOLOGIES .............................................. 90 APPENDIX 2 – TECHNOLOGY AND RISK SUMMARY FOR NON-JSF CANDIDATES ...................................................................................................... 102 APPENDIX 3 – LIST OF ACRONYMS........................................................................ 134 BIBLIOGRAPHY ........................................................................................................... 139 ii LIST OF FIGURES Figure 1 – Developing CFDS ........................................................................................... 15 Figure 2 – Capability Based Planning Process ................................................................. 23 Figure 3 – The Three F-35 JSF Variants .......................................................................... 43 Figure 4 – JSF JORD Roadmap identifying key COPT assessment factors..................... 46 Figure 5 – Comparison of Classic F/A-18A-D Hornet with F/A-18E/F Super Hornet .... 66 Figure 6 – Eurofighter General Characteristics ................................................................ 68 Figure 7 – Dassault Rafale Technical Characteristics ...................................................... 69 Figure 8 – Gripen NG Technical Characteristics .............................................................. 71 Figure 9 – Potential sets of platform capabilities for UAS ............................................... 73 Figure 10 – Medium Class UAS Evolution ...................................................................... 74 Figure 11 – F-35 Advanced Fusion Avionics Suite .......................................................... 92 iii LIST OF TABLES Table 1 – Aerospace Functions, Roles and Missions for Fighter Aircraft ........................ 28 Table 2 – Potential Threat Exposure Matrix for RCAF Fighters by CFDS Role ............. 32 Table 3 – International Participation in the JSF CDP ....................................................... 41 Table 4 – JSF KPPs........................................................................................................... 47 Table 5 – Aircraft Cost Composition and Definitions ...................................................... 57 Table 6 – Full Canadian Program Cost Estimate for the F-35 JSF (2013) ....................... 59 Table 7 – Summary of non-JSF Contenders ..................................................................... 76 Table 8 – Comparison of CF-18 Hornet Replacement Options ........................................ 79 iv ABSTRACT The Harper Government’s planned sole-source procurement of the advanced fifth- generation F-35 Lightning II fighter currently in development, to replace Canada’s ageing CF-18 Hornets, has left it open to significant criticism from the opposition, media, subject matter experts and the interested public. More specifically, the belief is that a sole-source procurement of the F-35 would lead to higher procurement costs and expose Canada to the risk of buying an aircraft with capabilities driven by costly technologies that are not yet proven, and potentially not even needed. Yet, a detailed look at the facts surrounding Canada’s participation in the Joint Strike Fighter (JSF) program, the RCAF’s list of unclassified requirements, the future security environment, projected capabilities and costs, as well as an examination of the alternatives suggest otherwise. Canada remaining in the JSF partnership provides taxpayers with access to the best possible purchase price for the F-35 along with significant industrial opportunities. The technologies developed for this aircraft are all assessed as critical to Canadian aerospace operations both at home and abroad for the projected life of the aircraft in Canadian service. And finally, based on the current market and available contenders, the procurement of an existing, less capable design in lieu of the F-35 as Canada’s replacement fighter for the next thirty years will not likely generate any procurement savings to the Canadian taxpayer, and would expose the RCAF’s new fighter force to operational and sustainment risks in the longer term. 1 1. INTRODUCTION While there has been a growing consensus that Canada needs a CF-18 replacement aircraft, there has been more vigorous debate with respect to the wisdom of the Government’s selection of the F-35 as its candidate aircraft. Some of this debate has been balanced, but much has been based upon misconceptions and half-truths, and some commentators – including those who should know better – have willingly contributed to the confusion that exists about the F-35. - Lieutenant-General (Ret’d) Lloyd Campbell1 The Next Generation Fighter Capability (NGFC) procurement program to replace the Royal Canadian Air Force’s (RCAF’s) aging CF-18 Hornet fighters has garnered significant media attention since Prime Minister Harper’s Conservative government announced on 16 July 2010 that it would procure, without a competition, and at a cost of $9 billion, up to 65 Lockheed Martin F-35 Lightning II fighters.2 The F-35, also known as the Joint Strike Fighter (JSF), is a recognized fifth generation fighter3, one of only a few types currently flying today.4 Other currently known fifth generation designs include the United States Air Force’s (USAF’s) F-22 Raptor, the only operational type of its 1 Lloyd Campbell, “Replacing the Canadian Manned Fighter Capability,” Canadian Military Journal 11 No. 3 (Summer 2011), 60. 2 CBC News | Canada, “Canada to spend $9B on F-35 fighter jets,” http://www.cbc.ca/news/ canada/story/2010/07/16/canada-jets.html; Internet; accessed 04 May 2013. 3 The definition of jet fighter “generations” has long been subject to debate. According to John A. Tirpak, broadly speaking, Generation 4 fighter designs incorporate pulse-doppler radar; high manoeuvrability and look-down, shoot-down missiles (e.g. F-15, CF-18, Mirage, MiG-29). Generation 4+ fighters include high agility; sensor fusion; reduced signatures (e.g. Eurofighter Typhoon, Su-30, advanced versions
Recommended publications
  • Project No.: R. 089145.001
    Project No.: R. 089145.001 Section 01 01 50 Mission Minimum Institution GENERAL INSTRUCTIONS 33737 Dewdney Trunk Road, Mission, BC Page 1 of 18 EXPANSION OF HEALTH CARE 1 SUMMARY OF WORK .1 Work covered by Contract Documents: .1 Work under this Contract comprises construction of a health care building expansion and renovation work as indicated, located at Mission Minimum Institution, Mission, B.C. .2 Contractor’s Use of Premises: .1 Contractor has controlled use of site within the construction area for Work, storage, and access as directed by the Departmental Representative. .2 Use of areas inside Mission Institution, for access to the construction site is controlled, by the Departmental Representative. .3 Obtain and pay for use of additional storage or work areas needed for operations under this Contract. .4 The new building will be constructed inside the security fence. The institution will be fully operational during work of this Contract. Provide temporary construction fence around site until new security fencing is installed. .3 Conform to National Building Code 2015 or British Columbia Building Code 2012 as applicable. .4 Contractor to apply for Building Permit before construction and Occupancy Permit upon Substantial completion. .1 Departmental Representative will supply the required drawings and Letters of Assurance for such applications. .2 Contractor to pay for all required fees for Building Permit and Occupancy Permit. .3 Before issuing the Substantial Completion certificate, Contractor must provide fire alarm verification report and Occupancy Permit from local authority having jurisdiction. 2 WORK RESTRICTIONS .1 Notify, Departmental Representative of intended interruption of disconnected services and provide schedule for review.
    [Show full text]
  • US Export Controls
    U.S. Export Controls A Commerce Department Perspective EAR BOOT CAMP ECCN, EAR99 and the 600 Series Chicago, IL Oct 9, 2013 Gene Christiansen 202 482 2894 [email protected] Factors to be considered in determining if item is “subject to the EAR” • Jurisdiction – Characteristics of Item: • Nuclear---Energy, NRC, Commerce • Military---USML, Commerce • Destination Country – For Cuba, Iran, N Korea, N Sudan and Syria---OFAC • Public Domain technology and software What is covered under the Commerce Control List (CCL) • Everything not under the jurisdiction of another Agency or technical data that is not in the public domain. See part 734.3 – All items in the United States – All U.S. origin items wherever they are – Foreign made items that include in excess of de minimis value of controlled U.S. origin content. – Foreign made items that are the direct product of certain U.S. origin technical data or software. – Certain commodities produced by any plant located outside the U.S. that is the direct product of certain U.S. origin technical data or software Navigating the Commerce Control List (CCL) • The Commerce Control List – 10 categories • 0 Nuclear and miscellaneous • 1 Materials, chemicals, microorganisms, toxins • 2 Materials processing • 3 Electronics computers • 4 Computers • 5 Telecommunications and encryption • 6 Sensors • 7 Navigation and avionics • 8 Marine • 9 Propulsion systems and space vehicles Navigating the Commerce Control List • The Commerce Control List – 5 groups • A--- Equipment—end items • B--- Test and production
    [Show full text]
  • Eurofighter World Editorial 2016 • Eurofighter World 3
    PROGRAMME NEWS & FEATURES DECEMBER 2016 GROSSETO EXCLUSIVE BALTIC AIR POLICING A CHANGING AIR FORCE FIT FOR THE FUTURE 2 2016 • EUROFIGHTER WORLD EDITORIAL 2016 • EUROFIGHTER WORLD 3 CONTENTS EUROFIGHTER WORLD PROGRAMME NEWS & FEATURES DECEMBER 2016 05 Editorial 24 Baltic policing role 42 Dardo 03 Welcome from Volker Paltzo, Germany took over NATO’s Journalist David Cenciotti was lucky enough to CEO of Eurofighter Jagdflugzeug GmbH. Baltic Air Policing (BAP) mis - get a back seat ride during an Italian Air Force sion in September with five training mission. Read his eye-opening first hand Eurofighters from the Tactical account of what life onboard the Eurofighter Title: Eurofighter Typoon with 06 At the heart of the mix Air Wing 74 in Neuburg, Typhoon is really like. P3E weapons fit. With the UK RAF evolving to meet new demands we speak to Bavaria deployed to Estonia. Typhoon Force Commander Air Commodore Ian Duguid about the Picture: Jamie Hunter changing shape of the Air Force and what it means for Typhoon. 26 Meet Sina Hinteregger By day Austrian Sina Hinteregger is an aircraft mechanic working on Typhoon, outside work she is one of the country’s best Eurofighter World is published by triathletes. We spoke to her Eurofighter Jagdflugzeug GmbH about her twin passions. 46 Power base PR & Communications Am Söldnermoos 17, 85399 Hallbergmoos Find out how Eurofighter Typhoon wowed the Tel: +49 (0) 811-80 1587 crowds at AIRPOWER16, Austria’s biggest Air [email protected] 12 Master of QRA Show. Editorial Team Discover why Eurofighter Typhoon’s outstanding performance and 28 Flying visit: GROSSETO Theodor Benien ability make it the perfect aircraft for Quick Reaction Alert.
    [Show full text]
  • Why China Has Not Caught Up
    Why China Has Not Caught Up Yet Why China Has Not Andrea Gilli and Caught Up Yet Mauro Gilli Military-Technological Superiority and the Limits of Imitation, Reverse Engineering, and Cyber Espionage Can adversaries of the United States easily imitate its most advanced weapon systems and thus erode its military-technological superiority? Do reverse engineering, industrial espi- onage, and, in particular, cyber espionage facilitate and accelerate this process? China’s decades-long economic boom, military modernization program, mas- sive reliance on cyber espionage, and assertive foreign policy have made these questions increasingly salient. Yet, almost everything known about this topic draws from the past. As we explain in this article, the conclusions that the ex- isting literature has reached by studying prior eras have no applicability to the current day. Scholarship in international relations theory generally assumes that ris- ing states beneªt from the “advantage of backwardness,” as described by Andrea Gilli is a senior researcher at the NATO (North Atlantic Treaty Organization) Defense College in Rome, Italy. Mauro Gilli is a senior researcher at the Center for Security Studies at the Swiss Federal Insti- tute of Technology in Zurich, Switzerland. The authors are listed in alphabetical order to reºect their equal contributions to this article. The views expressed in the article are those of the authors and do not represent the views of NATO, the NATO Defense College, or any other institution with which the authors are or have been
    [Show full text]
  • Air Defence in Northern Europe
    FINNISH DEFENCE STUDIES AIR DEFENCE IN NORTHERN EUROPE Heikki Nikunen National Defence College Helsinki 1997 Finnish Defence Studies is published under the auspices of the National Defence College, and the contributions reflect the fields of research and teaching of the College. Finnish Defence Studies will occasionally feature documentation on Finnish Security Policy. Views expressed are those of the authors and do not necessarily imply endorsement by the National Defence College. Editor: Kalevi Ruhala Editorial Assistant: Matti Hongisto Editorial Board: Chairman Prof. Pekka Sivonen, National Defence College Dr. Pauli Järvenpää, Ministry of Defence Col. Erkki Nordberg, Defence Staff Dr., Lt.Col. (ret.) Pekka Visuri, Finnish Institute of International Affairs Dr. Matti Vuorio, Scientific Committee for National Defence Published by NATIONAL DEFENCE COLLEGE P.O. Box 266 FIN - 00171 Helsinki FINLAND FINNISH DEFENCE STUDIES 10 AIR DEFENCE IN NORTHERN EUROPE Heikki Nikunen National Defence College Helsinki 1997 ISBN 951-25-0873-7 ISSN 0788-5571 © Copyright 1997: National Defence College All rights reserved Oy Edita Ab Pasilan pikapaino Helsinki 1997 INTRODUCTION The historical progress of air power has shown a continuous rising trend. Military applications emerged fairly early in the infancy of aviation, in the form of first trials to establish the superiority of the third dimension over the battlefield. Well- known examples include the balloon reconnaissance efforts made in France even before the birth of the aircraft, and it was not long before the first generation of flimsy, underpowered aircraft were being tested in a military environment. The Italians used aircraft for reconnaissance missions at Tripoli in 1910-1912, and the Americans made their first attempts at taking air power to sea as early as 1910-1911.
    [Show full text]
  • Know the Past ...Shape the Future
    FALL 2018 - Volume 65, Number 3 WWW.AFHISTORY.ORG know the past .....Shape the Future The Air Force Historical Foundation Founded on May 27, 1953 by Gen Carl A. “Tooey” Spaatz MEMBERSHIP BENEFITS and other air power pioneers, the Air Force Historical All members receive our exciting and informative Foundation (AFHF) is a nonprofi t tax exempt organization. Air Power History Journal, either electronically or It is dedicated to the preservation, perpetuation and on paper, covering: all aspects of aerospace history appropriate publication of the history and traditions of American aviation, with emphasis on the U.S. Air Force, its • Chronicles the great campaigns and predecessor organizations, and the men and women whose the great leaders lives and dreams were devoted to fl ight. The Foundation • Eyewitness accounts and historical articles serves all components of the United States Air Force— Active, Reserve and Air National Guard. • In depth resources to museums and activities, to keep members connected to the latest and AFHF strives to make available to the public and greatest events. today’s government planners and decision makers information that is relevant and informative about Preserve the legacy, stay connected: all aspects of air and space power. By doing so, the • Membership helps preserve the legacy of current Foundation hopes to assure the nation profi ts from past and future US air force personnel. experiences as it helps keep the U.S. Air Force the most modern and effective military force in the world. • Provides reliable and accurate accounts of historical events. The Foundation’s four primary activities include a quarterly journal Air Power History, a book program, a • Establish connections between generations.
    [Show full text]
  • Aviation Machinist's Mate 3 & 2
    NONRESIDENT TRAINING COURSE Aviation Machinist’s Mate 3 & 2 NAVEDTRA 14008 DISTRIBUTION STATEMENT A: Approved for public release; distribution is unlimited. PREFACE About this course: This is a self-study course. By studying this course, you can improve your professional/military knowledge, as well as prepare for the Navywide advancement-in-rate examination. It contains subject matter about day- to-day occupational knowledge and skill requirements and includes text, tables, and illustrations to help you understand the information. An additional important feature of this course is its reference to useful information in other publications. The well-prepared Sailor will take the time to look up the additional information. History of the course: • Sep 1991: Original edition released. Prepared by ADCS(AW) Terence A. Post. • Jan 2004: Administrative update released. Technical content was not reviewed or revised. Published by NAVAL EDUCATION AND TRAINING PROFESSIONAL DEVELOPMENT AND TECHNOLOGY CENTER TABLE OF CONTENTS CHAPTER PAGE 1. Jet Engine Theory and Design ............................................................................... 1-1 2. Tools and Hardware ............................................................................................... 2-1 3. Aviation Support Equipment.................................................................................. 3-1 4. Jet Aircraft Fuel and Fuel Systems ........................................................................ 4-1 5. Jet Aircraft Engine Lubrication Systems ..............................................................
    [Show full text]
  • Bell 429 Product Specifications
    BELL 429 SPECIFICATIONS BELL 429 SPECIFICATIONS Publisher’s Notice The information herein is general in nature and may vary with conditions. Individuals using this information must exercise their independent judgment in evaluating product selection and determining product appropriateness for their particular purpose and requirements. For performance data and operating limitations for any specific mission, reference must be made to the approved flight manual. Bell Helicopter Textron Inc. makes no representations or warranties, either expressed or implied, including without limitation any warranties of merchantability or fitness for a particular purpose with respect to the information set forth herein or the product(s) and service(s) to which the information refers. Accordingly, Bell Helicopter Textron Inc. will not be responsible for damages (of any kind or nature, including incidental, direct, indirect, or consequential damages) resulting from the use of or reliance on this information. Bell Helicopter Textron Inc. reserves the right to change product designs and specifications without notice. © 2019 Bell Helicopter Textron Inc. All registered trademarks are the property of their respective owners. FEBRUARY 2019 © 2019 Bell Helicopter Textron Inc. Specifications subject to change without notice. i BELL 429 SPECIFICATIONS Table of Contents Bell 429 ..................................................................................................................................1 Bell 429 Specification Summary (U.S. Units) ........................................................................4
    [Show full text]
  • Thrush Aircraft, Inc
    THRUSH AIRCRAFT, INC. P.O. Box 3149 Albany, GA 31706-3149 Phone (229) 883-1440 Fax (229) 439-9790 CUSTOM KIT CUSTOM KIT No. CK-AG-40 Rev. A Date: 12/8/06 WING SPAR UPGRADE The wing spars of most early Thrush models are the subject of FAA Airworthiness Directives (most recently FAA AD 2006-07-15) which require periodic inspection of the lower wing spar caps at the splice block attach holes for fatigue cracks. This Custom Kit is an acceptable way to replace the lower spar caps, but it does more than this for the aircraft owner. It brings the spars up to the best fatigue capability that is compatible with the existing wings. This upgrade includes not only the lower spar caps that have the first two splice holes cold expanded, but it also includes new inboard webs and doublers as well as the “big butterfly” and lower splice plate. When a set of wings is rebuilt according to this Custom Kit, it will gain the initial inspection interval of a “Group 4” airplane while retaining the spar fatigue life of its current group. The inspection intervals between initial inspection and spar fatigue life limit will be the larger inspection intervals currently used for Group 4 and 5 airplanes. The upgraded wing will be as strong as or, in many cases, stronger than the original. Note that this upgrade is for both wings. If the airplane has one relatively young spar cap and it is not replaced, the inspection intervals will be based on that spar, not the new one.
    [Show full text]
  • 19730021074.Pdf
    NASA TECHNICAL NOTE NASA TN D-7328 CO LE CORY STEADY-STATE AND DYNAMIC PRESSURE PHENOMENA IN THE PROPULSION SYSTEM OF AN F-111A AIRPLANE by Frank W. Burcbam, Jr., Donald L. Hughes, and Jon K. Holzman Flight Research Center Edwards, Calif. 93523 NATIONAL AERONAUTICS AND SPACE ADMINISTRATION • WASHINGTON, D. C. • JULY 1973 1. Report No. 2. Government Accession No. 3. Recipient's Catalog No. NASA TN D-7328 4. Title and Subtitle 5. Report Date STEADY-STATE AND DYNAMIC PRESSURE PHENOMENA IN THE July 1973 PROPULSION SYSTEM OF AN F-111A AIRPLANE 6. Performing Organization Code 7. Author(s) 8. Performing Organization Report No. Frank W. Burcham, Jr., Donald L. Hughes, and Jon K. Holzman H-741 10. Work Unit No. 9. Performing Organization Name and Address 136-13-08-00-24 NASA Flight Research Center P. O. Box 273 11. Contract or Grant No. Edwards, California 93523 13. Type of Report and Period Covered 12. Sponsoring Agency Name and Address Technical Note National Aeronautics and Space Administration 14. Sponsoring Agency Code Washington, D. C. 20546 15. Supplementary Notes 16. Abstract Flight tests were conducted with two F-111A airplanes to study the effects of steady-state and dynamic pressure phenomena on the propulsion system. Analysis of over 100 engine compressor stalls revealed that the stalls were caused by high levels of instantaneous distortion. In 73 per- cent of these stalls, the instantaneous circumferential distortion parameter, Kg, exhibited a peak just prior to stall higher than any previous peak. The Kg parameter was a better indicator of stall than the distortion factor, K_, and the maximum-minus-minimum distortion parameter, D, was a poor indicator of stall.
    [Show full text]
  • SP2016-3124855 a Generic Thermodynamic Assessment Of
    SP2016-3124855 A Generic Thermodynamic Assessment of Reusable High-Speed Vehicles V. Fernandez Villace, J. Steelant ESA-ESTEC, Section of Aerothermodynamics and Propulsion Analysis Keplerlaan 1, 2200 AG Noordwijk, The Netherlands Email: [email protected], [email protected] ABSTRACT Lifting based vehicles for either space transportation or sustained hypersonic cruise are exposed to high thermal loads during the atmospheric trajectory. The thermal protection system has therefore to efficiently manage the thermal load that penetrates the aeroshell in order to guarantee a satisfactory mission performance. In the present study, the thermal endurance of a LH2-fuelled Mach 8 hypersonic cruiser is assured by soaking the thermal load across the aeroshell into the on-board tank system. The so-produced boil-off acts as a coolant for other aircraft subsystems, like the cabin environmental control system. Further, in order to avoid over-board dumping of the vaporized fuel, a boil-off compression system is proposed to inject the fuel into the propulsion plant. The numerical approach comprised a detailed model of the airframe, where the heat transfer across the interfacing areas between the different subsystems, namely tanks, cabin, propulsion plant and the aeroshell, was resolved based on one-dimensional engineering models. This methodology allowed the evaluation of the complete mission cycle, from the apron, through taxiing and airborne phases and back to apron. 1. INTRODUCTION 2. PRELIMINARY EVALUATION The thermal management of cruising high-speed One of the purposes of the present study was to aircraft plays a very important role. These vehicles design a thermodynamic cycle able to balance the are submitted to high heat loads originating from the airframe thermal and mechanical loads.
    [Show full text]
  • Remote ID NPRM Maps out UAS Airspace Integration Plans by Charles Alcock
    PUBLICATIONS Vol.49 | No.2 $9.00 FEBRUARY 2020 | ainonline.com « Joby Aviation’s S4 eVTOL aircraft took a leap forward in the race to launch commercial service with a January 15 announcement of $590 million in new investment from a group led by Japanese car maker Toyota. Joby says it will have the piloted S4 flying as part of the Uber Air air taxi network in early adopter cities before the end of 2023, but it will surely take far longer to get clearance for autonomous eVTOL operations. (Full story on page 8) People HAI’s new president takes the reins page 14 Safety 2019 was a bad year for Part 91 page 12 Part 135 FAA has stern words for BlackBird page 22 Remote ID NPRM maps out UAS airspace integration plans by Charles Alcock Stakeholders have until March 2 to com- in planned urban air mobility applications. Read Our SPECIAL REPORT ment on proposed rules intended to provide The final rule resulting from NPRM FAA- a framework for integrating unmanned air- 2019-100 is expected to require remote craft systems (UAS) into the U.S. National identification for the majority of UAS, with Airspace System. On New Year’s Eve, the exceptions to be made for some amateur- EFB Hardware Federal Aviation Administration (FAA) pub- built UAS, aircraft operated by the U.S. gov- When it comes to electronic flight lished its long-awaited notice of proposed ernment, and UAS weighing less than 0.55 bags, (EFBs), most attention focuses on rulemaking (NPRM) for remote identifica- pounds.
    [Show full text]