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Future Battlefield Rotorcraft Capability (FBRC) – Anno 2035 and Beyond
November 2018 Future Battle eld Rotorcraft Capability Anno 2035 and Beyond Joint Air Power Competence Centre Cover picture © Airbus © This work is copyrighted. No part may be reproduced by any process without prior written permission. Inquiries should be made to: The Editor, Joint Air Power Competence Centre (JAPCC), [email protected] Disclaimer This document is a product of the Joint Air Power Competence Centre (JAPCC). It does not represent the opinions or policies of the North Atlantic Treaty Organization (NATO) and is designed to provide an independent overview, analysis and food for thought regarding possible ways ahead on this subject. Comments and queries on this document should be directed to the Air Operations Support Branch, JAPCC, von-Seydlitz-Kaserne, Römerstraße 140, D-47546 Kalkar. Please visit our website www.japcc.org for the latest information on JAPCC, or e-mail us at [email protected]. Author Cdr Maurizio Modesto (ITA Navy) Release This paper is releasable to the Public. Portions of the document may be quoted without permission, provided a standard source credit is included. Published and distributed by The Joint Air Power Competence Centre von-Seydlitz-Kaserne Römerstraße 140 47546 Kalkar Germany Telephone: +49 (0) 2824 90 2201 Facsimile: +49 (0) 2824 90 2208 E-Mail: [email protected] Website: www.japcc.org Denotes images digitally manipulated JAPCC |Future BattlefieldRotorcraft Capability and – AnnoBeyond 2035 | November 2018 Executive Director, JAPCC Director, Executive DEUAF General, Lieutenant Klaus Habersetzer port Branchviae-mail [email protected]. AirOperationsSup contact to theJAPCC’s free feel thisdocument.Please to withregard have you may comments welcome any We thisstudy. -
G410020002/A N/A Client Ref
Solicitation No. - N° de l'invitation Amd. No. - N° de la modif. Buyer ID - Id de l'acheteur G410020002/A N/A Client Ref. No. - N° de réf. du client File No. - N° du dossier CCC No./N° CCC - FMS No./N° VME G410020002 G410020002 RETURN BIDS TO: Title – Sujet: RETOURNER LES SOUMISSIONS À: PURCHASE OF AIR CARRIER FLIGHT MOVEMENT DATA AND AIR COMPANY PROFILE DATA Bids are to be submitted electronically Solicitation No. – N° de l’invitation Date by e-mail to the following addresses: G410020002 July 8, 2019 Client Reference No. – N° référence du client Attn : [email protected] GETS Reference No. – N° de reference de SEAG Bids will not be accepted by any File No. – N° de dossier CCC No. / N° CCC - FMS No. / N° VME other methods of delivery. G410020002 N/A Time Zone REQUEST FOR PROPOSAL Sollicitation Closes – L’invitation prend fin Fuseau horaire DEMANDE DE PROPOSITION at – à 02 :00 PM Eastern Standard on – le August 19, 2019 Time EST F.O.B. - F.A.B. Proposal To: Plant-Usine: Destination: Other-Autre: Canadian Transportation Agency Address Inquiries to : - Adresser toutes questions à: Email: We hereby offer to sell to Her Majesty the Queen in right [email protected] of Canada, in accordance with the terms and conditions set out herein, referred to herein or attached hereto, the Telephone No. –de téléphone : FAX No. – N° de FAX goods, services, and construction listed herein and on any Destination – of Goods, Services, and Construction: attached sheets at the price(s) set out thereof. -
National Rappel Operations Guide
National Rappel Operations Guide 2019 NATIONAL RAPPEL OPERATIONS GUIDE USDA FOREST SERVICE National Rappel Operations Guide i Page Intentionally Left Blank National Rappel Operations Guide ii Table of Contents Table of Contents ..........................................................................................................................ii USDA Forest Service - National Rappel Operations Guide Approval .............................................. iv USDA Forest Service - National Rappel Operations Guide Overview ............................................... vi USDA Forest Service Helicopter Rappel Mission Statement ........................................................ viii NROG Revision Summary ............................................................................................................... x Introduction ...................................................................................................... 1—1 Administration .................................................................................................. 2—1 Rappel Position Standards ................................................................................. 2—6 Rappel and Cargo Letdown Equipment .............................................................. 4—1 Rappel and Cargo Letdown Operations .............................................................. 5—1 Rappel and Cargo Operations Emergency Procedures ........................................ 6—1 Documentation ................................................................................................ -
Hangar Fire Foam Systems: a Problem in the Aviation Industry, with One Event Occuring on Average Every Six Weeks
PUBLICATIONS Vol.49 | No.7 $9.00 JULY 2020 | ainonline.com USAIG Accidental hangar fire foam discharge is a growing Hangar fire foam systems: a problem in the aviation industry, with one event occuring on average every six weeks. The cleanup solution looking for a problem? costs from each can involve numerous insurance by Curt Epstein claims and in some cases lawsuits, pitting aircraft For FBOs, OEMs, and other hangar keepers, senior v-p of insurance provider Global Aero- could be worth more than 10 times the price owners and operators the inadvertent discharge of fire foam sys- space and the author of a white paper on the of the building. against hangar keepers tems is a persistent and growing problem. topic, stated that the average value of foam dis- As aircraft increased in size and fuel and fire system providers. Nearly everyone has seen photos taken in charge claims he has seen has been $1 million. capacity, fire authorities began to worry the aftermath of one of these events—a NATA estimates the overall clean up and air- that sprinklers would not be able to ade- hangar filled with a thick layer of foam that craft damage costs of those events at between quately reach and fight any fuel spill fires can reach 10 feet high, spilling out on to the $64 million and $235 million. that occurred under the ever-widening ramp in some cases. The National Fire Protection Association wings, which at the time had an unpleasant Electric Aircraft In a way, accidental foam discharge is like (NFPA), considered the world’s foremost tendency to leak fuel onto the hangar floor. -
Adventures in Low Disk Loading VTOL Design
NASA/TP—2018–219981 Adventures in Low Disk Loading VTOL Design Mike Scully Ames Research Center Moffett Field, California Click here: Press F1 key (Windows) or Help key (Mac) for help September 2018 This page is required and contains approved text that cannot be changed. NASA STI Program ... in Profile Since its founding, NASA has been dedicated • CONFERENCE PUBLICATION. to the advancement of aeronautics and space Collected papers from scientific and science. The NASA scientific and technical technical conferences, symposia, seminars, information (STI) program plays a key part in or other meetings sponsored or co- helping NASA maintain this important role. sponsored by NASA. The NASA STI program operates under the • SPECIAL PUBLICATION. Scientific, auspices of the Agency Chief Information technical, or historical information from Officer. It collects, organizes, provides for NASA programs, projects, and missions, archiving, and disseminates NASA’s STI. The often concerned with subjects having NASA STI program provides access to the NTRS substantial public interest. Registered and its public interface, the NASA Technical Reports Server, thus providing one of • TECHNICAL TRANSLATION. the largest collections of aeronautical and space English-language translations of foreign science STI in the world. Results are published in scientific and technical material pertinent to both non-NASA channels and by NASA in the NASA’s mission. NASA STI Report Series, which includes the following report types: Specialized services also include organizing and publishing research results, distributing • TECHNICAL PUBLICATION. Reports of specialized research announcements and feeds, completed research or a major significant providing information desk and personal search phase of research that present the results of support, and enabling data exchange services. -
Sikorsky S70i CAL FIRE HAWK Fact Sheet
SIKORSKY S70i CAL FIRE HAWK CALIFORNIA DEPARTMENT OF FORESTRY & FIRE PROTECTION AVIATION PROGRAM MANUFACTURER CREW Sikorsky Aircraft, Stratford, Connecticut (Built in Mielec, Poland) One pilot, two Helitack Captains, an operations supervisor, and up to AIRCRAFT FIRE BUILD-UP nine personnel. United Rotorcraft, Englewood, Colorado PAYLOAD ORIGINAL OWNER Fixed tank - 1000 gallons of water/foam with pilot controlled drop volumes. CAL FIRE, 2019 ACQUIRED BY CAL FIRE SPECIFICATIONS Gross Weight: Internal 22,000 lbs./ In 2018 CAL FIRE received approval from the Governor’s Office to purchase External 23,500 lbs. up to 12 new Sikorsky S70i firefighting helicopters from United Rotorcraft. Cruise Speed: 160 mph These new generation helicopters will replace CAL FIRE’s aging fleet of Night Vision Capable 12 Super Huey Helicopters. The new generation of S70i CAL FIRE HAWK Range: 250 miles helicopters will bring enhanced capabilities including flight safety, higher Endurance: 2.5 hours payloads, increased power margins, and night flying capabilities. Rotor Diameter: 53 feet and 8 inches Engines: Twin turbine engine, T700-GE701D MISSION The CAL FIRE HAWK’s primary mission is responding to initial attack wildfires and rescue missions. When responding to wildfires, the helicopter can quickly deliver up to a 9-person Helitack Crew for ground firefighting operations and quickly transition into water/foam dropping missions. The helicopters are also used for firing operations using either a Helitorch or a Chemical Ignition Device System (CIDS) on wildland fires or prescribed burns, transporting internal cargo loads, mapping, medical evacuations and numerous non-fire emergency missions. The CAL FIRE HAWK is also equipped with an external hoist for rescue missions. -
4.2.2 Wildlife 4.2.2.1 Caribou Labrador's Caribou (Rangifer Tarandus) Can Be Classified Into Two Main Groups, the Migratory An
REVISED ENVIRONMENTAL IMPACT STATEMENT 4.2.2 Wildlife 4.2.2.1 Caribou Labrador’s caribou (Rangifer tarandus) can be classified into two main groups, the migratory and sedentary (also known as woodland) ecotypes, which are distinguished by their use of calving grounds or fidelity to specific calving sites. Migratory caribou travel large distances, occupy large home ranges, and aggregate during calving periods. Conversely, sedentary caribou display limited movements, occupy smaller home ranges, and tend to disperse during the calving period (Schaefer et al. 2000; Bergerud et al. 2008). The Project occupies a portion of Western Labrador which overlaps with the range of the George River (GR) Herd. Straddling the Québec-Labrador peninsula, the GR Herd is one of the world’s largest Rangifer populations, with population estimates peaking at almost 800,000 individuals in the 1980’s (Couturier et al. 1996; Russell et al. 1996, Rivest et al. 1998). This area of western Labrador overlaps the GR Herd as a portion of their winter range (Jacobs 1996). In addition to the GR Herd, there is another migratory ecotype that is recognized on the Ungava Peninsula and known as the Rivière-aux-Feuilles (‘Leaf River’) (RAF) Herd. Existing and recognized sedentary populations include the Lac Joseph (LJ) Herd located south of the Assessment Area, and the Red Wine Mountains (RWM), the Joir River (JR), and the Mealy Mountains (MM) Herds all much further to the east. The Mealy Mountains act as a geographic barrier separating this herd from the other herds of Labrador, but the lack of a geographic barrier between the other three sedentary herds results in an overlap of herd ranges (Schmelzer et al. -
2017 Top Markets Report Rotorcraft Sector Snapshot
U.S. Department of Commerce International Trade Administration 2017 Top Markets Report Rotorcraft Sector Snapshot Rotorcraft Helicopters, also known as rotorcraft, offer a versatility not Grouping MTOW afforded by automobiles and fixed-wing airplanes. Able to access the inaccessible with significant speed and comfort, a Light single engine <4,000 lbs. rotorcraft is the optimal choice for many enforcement, Intermediate single >4,000 lbs. emergency, and executive endeavors. The industry also engine includes maintenance, repair, and overhaul (MRO) of rotorcraft. Light twin engine <9,000 lbs. Medium twin engine between 9000- The helicopter industry is segmented into six groups, which 15,000 lbs. are dependent on the number of engines and maximum Super-medium twin between 15,000- take-off weight (MTOW), as described in Figure 1 to the right. engine 20,000 lbs. Heavy twin engine >20,000 lbs. The helicopter industry can also be segmented into the Figure 1 following usage categories: • General Aviation (Business/Private/VIP) • Law Enforcement • Emergency Medical Services (EMS)/ Search & Rescue (SAR) • Utility • Oil & Gas/Offshore • Defense Global Industry Landscape The major rotorcraft design and production companies are either North American (U.S. and Canada) or European (France, Italy, and Russia). While the major companies are headquartered in these countries, many production and parts-production facilities are in operation throughout Asia and Latin America. Similarly, the major markets for civil and defense rotorcraft are nations in North America and Europe, which constitute approximately 55 percent of the global market. 2017 ITA Rotorcraft Top M arkets Report 1 This snapshot is part of a larger Top Markets Report. -
Aviation Photography
The Journal of the Canadian Owners and Pilots Association JULY 2020 FlightMore than Aviation Photography 80 JP Bonin marks Classified Ads (p.46) 20 years ‘shooting’ aircraft UNDERWING CAMPING TIPS FROM EXPERIENCED CAMPERS CHRISTINE GERVAIS INTRODUCING COPA’s new CEO HANDHELD TRANSCEIVERS WE HIGHLIGHT 3 DIFFERENT PM#42583014 MANUFACTURERS & CAPTURE THE FEELING OF FLIGHT. L’ESSENTIEL, C’EST LE CIEL! In Canada, the freedom to fly provides pilots Au Canada, cette vérité offre aux pilotes and aviation enthusiasts endless ways of et aux passionnés d’aviation plein de moyens expressing our love for flight. pour exprimer leur amour de voler. Recognizing this, COPA and Red Canoe C’est pourquoi COPA et Red Canoe came together to create a high quality s’associent pour pour créer une collection collection meant to capture d’excellente qualité, destinée à rendre and celebrate just a few of those ways. hommage à quelques-uns de ces moyens. Shop for yours today: Trouvez le vôtre aujourd’hui: www.copanational.org/en/store www.copanational.org/fr/boutique his hers Pour lui Pour elle CopaFlight-ApparelPrintAd-Feb.Final.indd 1 2019-01-13 3:25 PM coNTENTS DEpaRTMENTS 4 PRESident’S CORNER JC AUDET DEFINES WHat COPA IS 6 MAILBOX INSPIRatIONAL StoRIES 7 ALL FOR FLIGHT RISE AND Soar — STUDENT PIlot SHows GREat INITIatIVE 8 NEWSLINE INTRODUCING COPA’S NEW PRESIDENT AND CEO 16 AVIATION ACCEssORIES COPA FLIGHT REVIEws HANDHELD 26 TRanscEIVERS 18 YOUNGER VOICES FEatURE YOUNG PIlots PROFILED 20 AVIATION SAFETY A PAssIONATE SHUTTERBUG THE WALK AROUND The quality of aviation photographer and COPA Flight contributor Jean-Pierre Bonin’s work is such that it’s hard to comprehend that he does not do it for a living. -
MD540F Pilot Report
January 2013 Serving the Worldwide Helicopter Industry rotorandwing.com 2013 Annual Reports Executive Outlook VXX Presidential Helo MD540F Pilot Report Customize Your EDITORIAL Andrew Parker Editor-in-Chief, [email protected] Ernie Stephens Editor-at-Large, [email protected] Reprints! Andrew Drwiega Military Editor, [email protected] Claudio Agostini Latin America Bureau Chief Contributing Writers: Chris Baur; Lee Benson; Shannon Bower; Igor Bozinovski; Keith Brown; Tony Capozzi; Keith Cianfrani; Steve Colby; Frank Colucci; Dan Deutermann; Ian Frain; Pat Gray; REPRINTS Emma Kelly; Frank Lombardi; Elena Malova; Vicki McConnell; Robert Moorman; Douglas Nelms; Mark Robins; Dale Smith; Terry Terrell; Todd Vorenkamp; Richard Whittle. EPRINTS ADVERTISING/BUSINESS Jennifer Schwartz Senior Vice President and Group Publisher, [email protected] PLAQUES Randy Jones Publisher, 1-972-713-9612, [email protected] Eastern United States & Canada Carol Mata, 1-512-607-6361, [email protected] POSTERS International Sales, Europe/Pac Rim/Asia James McAuley +34 952 118 018, [email protected] DESIGN/PRODUCTION Gretchen Saval Graphic Designer Create a powerful statement for your product, service Tony Campana Production Manager, 1-301-354-1689 [email protected] or company through p rofessionally designed marketing David Hurwitz Web/E-letter Production Manager, 1-301-354-1459 [email protected] materials utilizing editorial content from Rotor & Wing. AUDIENCE DEVELOPMENT Contact Wright’s Media to d iscuss how we can George Severine Fulfillment Manager, [email protected] Customer Service/Back Issues 1-847-559-7314 [email protected] customize these materials to enhance your current marketing campaign. LIST SALES Statlistics Jen Felling ,1-203-778-8700, [email protected] U.S. -
Development of a Helicopter Vortex Ring State Warning System Through a Moving Map Display Computer
Calhoun: The NPS Institutional Archive Theses and Dissertations Thesis Collection 1999-09 Development of a helicopter vortex ring state warning system through a moving map display computer Varnes, David J. Monterey, California. Naval Postgraduate School http://hdl.handle.net/10945/26475 DUDLEY KNOX LIBRARY NAVAL POSTGRADUATE SCHOOL MONTEREY CA 93943-5101 NAVAL POSTGRADUATE SCHOOL Monterey, California THESIS DEVELOPMENT OF A HELICOPTER VORTEX RING STATE WARNING SYSTEM THROUGH A MOVING MAP DISPLAY COMPUTER by David J. Varnes September 1999 Thesis Advisor: Russell W. Duren Approved for public release; distribution is unlimited. Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instruction, searching existing data sources, gathering and maintaining the data needed, and completing and reviewing the collection of information. Send comments regarding this burden estimate or any other aspect of this collection of information, including suggestions for reducing this burden, to Washington headquarters Services, Directorate for Information Operations and Reports, 1215 Jefferson Davis Highway, Suite 1204, Arlington. VA 22202-4302, and to the Office of Management and Budget. Paperwork Reduction Project (0704-0188) Washington DC 20503. REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 2. REPORT DATE 3. REPORT TYPE AND DATES COVERED 1. agency use only (Leave blank) September 1999 Master's Thesis 4. TITLE AND SUBTITLE 5. FUNDING NUMBERS DEVELOPMENT OF A HELICOPTER VORTEX RING STATE WARNING SYSTEM THROUGH A MOVING MAP DISPLAY COMPUTER 6. AUTHOR(S) Varnes, David, J. 7. PERFORMING ORGANIZATION NAME(S) AND ADDRESS(ES) PERFORMING ORGANIZATION Naval Postgraduate School REPORT NUMBER Monterey, CA 93943-5000 10. -
A Qualitative Introduction to the Vortex-Ring-State, Autorotation, and Optimal Autorotation
36th European Rotorcraft Forum, Paris, France, September 7-9, 2010 Paper Identification Number 089 A Qualitative Introduction to the Vortex-Ring-State, Autorotation, and Optimal Autorotation Skander Taamallah ∗† ∗ Avionics Systems Department, National Aerospace Laboratory (NLR) 1059 CM Amsterdam, The Netherlands ([email protected]). † Delft Center for Systems and Control (DCSC) Faculty of Mechanical, Maritime and Materials Engineering Delft University of Technology, 2628 CD Delft, The Netherlands. Keywords: Vortex-Ring-State (VRS); autorotation; Height-Velocity diagram; optimal control; optimal autorotation Abstract: The main objective of this pa- 1 Introduction per is to provide the reader with some qualita- tive insight into the areas of Vortex-Ring-State This paper summarizes the results of a brief (VRS), autorotation, and optimal autorota- literature survey, of relevant work in the open tion. First this paper summarizes the results literature, covering the areas of the VRS, of a brief VRS literature survey, where the em- autorotation, and optimal autorotation. Due phasis has been placed on a qualitative descrip- to time and space constraints, only published tion of the following items: conditions leading accounts relative to standard helicopter to VRS flight, the VRS region, avoiding the configurations will be covered, omitting thus VRS, the early symptoms, recovery from VRS, other types such as tilt-rotor, side-by-side, experimental investigations, and VRS model- tandem, and co-axial. Presenting a complete ing. The focus of the paper is subsequently survey of a field as diverse as helicopter VRS, moved towards the autorotation phenomenon, autorotation, and optimal trajectories in where a review of the following items is given: autorotation is a daunting task.