Helicopter Flying Handbook (FAA-H-8083-21B) Chapter 13
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United Nations Peacekeeping Missions Military Aviation Unit Manual Second Edition April 2021
UN Military Aviation Unit Manual United Nations Peacekeeping Missions Military Aviation Unit Manual Second Edition April 2021 Second Edition 2019 DEPARTMENT OF PEACE OPERATIONS DEPARTMENT OF OPERATIONAL SUPPORT UN Military Aviation Unit Manual Produced by: Office of Military Affairs, Department of Peace Operations UN Secretariat One UN Plaza, New York, NY 10017 Tel. 917-367-2487 Approved by: Jean-Pierre Lacroix, Under-Secretary-General for Peace Operations Department of Peace Operations (DPO). Atul Khare Under-Secretary-General for Operational Support Department of Operational Support (DOS) April 2021. Contact: PDT/OMA/DPO Review date: 30/ 04 / 2026 Reference number: 2021.04 Printed at the UN, New York © UN 2021. This publication enjoys copyright under Protocol 2 of the Universal Copyright Convention. Nevertheless, governmental authorities or Member States may freely photocopy any part of this publication for exclusive use within their training institutes. However, no portion of this publication may be reproduced for sale or mass publication without the express consent, in writing, of the Office of Military Affairs, UN Department of Peace Operations. ii UN Military Aviation Unit Manual Foreword We are delighted to introduce the United Nations Peacekeeping Missions Military Aviation Unit Manual, an essential guide for commanders and staff deployed in peacekeeping operations, and an important reference for Member States and the staff at United Nations Headquarters. For several decades, United Nations peacekeeping has evolved significantly in its complexity. The spectrum of multi-dimensional UN peacekeeping operations includes challenging tasks such as restoring state authority, protecting civilians and disarming, demobilizing and reintegrating ex-combatants. In today’s context, peacekeeping missions are deploying into environments where they can expect to confront asymmetric threats and contend with armed groups over large swaths of territory. -
Aircraft Collection
A, AIR & SPA ID SE CE MU REP SEU INT M AIRCRAFT COLLECTION From the Avenger torpedo bomber, a stalwart from Intrepid’s World War II service, to the A-12, the spy plane from the Cold War, this collection reflects some of the GREATEST ACHIEVEMENTS IN MILITARY AVIATION. Photo: Liam Marshall TABLE OF CONTENTS Bombers / Attack Fighters Multirole Helicopters Reconnaissance / Surveillance Trainers OV-101 Enterprise Concorde Aircraft Restoration Hangar Photo: Liam Marshall BOMBERS/ATTACK The basic mission of the aircraft carrier is to project the U.S. Navy’s military strength far beyond our shores. These warships are primarily deployed to deter aggression and protect American strategic interests. Should deterrence fail, the carrier’s bombers and attack aircraft engage in vital operations to support other forces. The collection includes the 1940-designed Grumman TBM Avenger of World War II. Also on display is the Douglas A-1 Skyraider, a true workhorse of the 1950s and ‘60s, as well as the Douglas A-4 Skyhawk and Grumman A-6 Intruder, stalwarts of the Vietnam War. Photo: Collection of the Intrepid Sea, Air & Space Museum GRUMMAN / EASTERNGRUMMAN AIRCRAFT AVENGER TBM-3E GRUMMAN/EASTERN AIRCRAFT TBM-3E AVENGER TORPEDO BOMBER First flown in 1941 and introduced operationally in June 1942, the Avenger became the U.S. Navy’s standard torpedo bomber throughout World War II, with more than 9,836 constructed. Originally built as the TBF by Grumman Aircraft Engineering Corporation, they were affectionately nicknamed “Turkeys” for their somewhat ungainly appearance. Bomber Torpedo In 1943 Grumman was tasked to build the F6F Hellcat fighter for the Navy. -
Rotor Spring 2018
Departments Features Index of Advertisers Spring 2018 rotor.org Serving the International BY THE INDUSTRY Helicopter Community FOR THE INDUSTRY Grand Canyon Helitack The Best Job in Aviation? What’s In Your Jet Fuel? p 58 Vietnam Pilots and Crew Members Honored p 28 Make the Connection March 4–7, 2019 • Atlanta Georgia World Congress Center Exhibits Open March 5–7 Apply for exhibit space at heliexpo.rotor.org LOTTERY 1* Open to HAI HELI-EXPO 2018 Exhibitors APPLY BY June 22, 2018 WITH PAYMENT LOTTERY 2 Open to All Companies APPLY BY Aug. 10, 2018 WITH PAYMENT heliexpo.rotor.org * For information on how to upgrade within Lottery 1, contact [email protected]. EXHIBIT NOW FALCON CREST AVIATION PROUDLY SUPPLIES & MAINTAINS AVIATION’S BEST SEALED LEAD ACID BATTERY RG-380E/44 RG-355 RG-214 RG-222 RG-390E RG-427 RG-407 RG-206 Bell Long Ranger Bell 212, 412, 412EP Bell 407 RG-222 (17 Ah) or RG-224 (24 Ah) RG-380E/44 (42 Ah) RG-407A1 (27 Ah) Falcon Crest STC No. SR09069RC Falcon Crest STC No. SR09053RC Falcon Crest STC No. SR09359RC Airbus Helicopters Bell 222U Airbus Helicopters AS355 E, F, F1, F2, N RG-380E/44 (42 Ah) BK 117, A-1, A-3, A-4, B-1, B-2, C-1 RG-355 (17 Ah) Falcon Crest STC No. SR09142RC RG-390E (28 Ah) Falcon Crest STC No. SR09186RC Falcon Crest STC No. SR09034RC Sikorsky S-76 A, C, C+ Airbus Helicopters RG-380E/44 (42 Ah) Airbus Helicopters AS350B, B1, B2, BA, C, D, D1 Falcon Crest STC No. -
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. -
Replace with Your Title
Advancing Vertical Flight: A Historical Perspective on AHS International and its Times M.E. Rhett Flater L. Kim Smith AHS Executive Director (1991-2011) AHS Deputy Director (1993-2011) M. E. Rhett Flater & Associates M.E. Rhett Flater & Associates Pine Knoll Shores, NC Pine Knoll Shores, NC ABSTRACT1 This paper describes AHS’s vital role in the development of the rotorcraft industry, with particular emphasis on events since 1990. It includes first-hand accounts of the formation of the Society, how it matured and evolved, and the particular influences that compelled change. It describes key events which occurred during various stages of the Society’s growth, including the formation of its technical committees, the evolution of the AHS Annual Forum and technical specialists’ meetings, and the creation and evolution of the Society’s publications. Featured prominently are accounts of AHS’s role in pursuing a combined government, industry and academia approach to rotorcraft science and technology. Also featured is the creation in 1965 of the Army-NASA Agreement for Joint Participation in Aeronautics Technology, the establishment of the U.S. Army Rotorcraft Centers of Excellence, the National Rotorcraft Technology Center (NRTC), the inauguration of the Congressional Rotorcraft Caucus and its support for the U.S. defense industrial base for rotorcraft, the battle for the survival of NASA aeronautics and critical NASA subsonic ground test facilities, and the launching of the International Helicopter Safety Team (IHST). First Annual AHS Banquet, October 7, 1944. 1Presented at the AHS 72nd Annual Forum, West Palm Beach, Florida, USA, May 17-19, 2016. Copyright © 2016 by the American Helicopter Society International, Inc. -
Sikorsky Uh-60M Helicopter
SIKORSKY UH-60M BLACK HAWK HELICOPTER This Page Does Not Contain Export Controlled Technical Data BEST-IN-CLASS MULTI-MISSION PERFORMER THE WORLD’S BEST COMBAT ASSAULT/UTILITY HELICOPTER GETS BETTER. Sikorsky has been responding to the needs of the United States Army for nearly a century. The Multi-mission UH-60M is the latest in the BLACK HAWK helicopter product family, more capable, more survivable, more maintainable, more powerful and more effective than its predecessors. The BLACK HAWK helicopter has proven itself both in combat and peace time missions. The UH-60M builds upon its robust predecessors and incorporates design improvements that extends this platform well into the future as the premier combat utility helicopter of choice for the United States as well as 27 other nations. Sikorsky sets the standard for rotorcraft safety and performance, continually developing improvements that make the entire industry safer. The UH-60M BLACK HAWK helicopter is no exception to this and is a safe, cost-effective, top performing helicopter ready to perform your missions. READY FOR BATTLE, TODAY AND TOMORROW. The Sikorsky BLACK HAWK is the primary medium lift helicopter for the U.S. Army performing a wide range of missions that encompass Air Assault, MEDEVAC, CSAR, Command and Control, and VIP transport. The newest version of the Army’s premier combat utility helicopter, the UH-60M, ensures compatibility with the U.S. Army’s Future Force. It will bring new life to the existing fleet, improve their effectiveness, reduce their vulnerability, and allow for future growth while lowering operating and support costs. -
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. -
The Pennsylvania State University
The Pennsylvania State University The Graduate School Department of Aerospace Engineering REAL-TIME PATH PLANNING AND AUTONOMOUS CONTROL FOR HELICOPTER AUTOROTATION A Dissertation in Aerospace Engineering by Thanan Yomchinda 2013 Thanan Yomchinda Submitted in Partial Fulfillment of the Requirements for the Degree of Doctor of Philosophy May 2013 The dissertation of Thanan Yomchinda was reviewed and approved* by the following: Joseph F. Horn Associate Professor of Aerospace Engineering Dissertation Co-Advisor Co-Chair of Committee Jacob W. Langelaan Associate Professor of Aerospace Engineering Dissertation Co-Advisor Co-Chair of Committee Edward C. Smith Professor of Aerospace Engineering Christopher D. Rahn Professor of Mechanical Engineering George A. Lesieutre Professor of Aerospace Engineering Head of the Department of Aerospace Engineering *Signatures are on file in the Graduate School iii ABSTRACT Autorotation is a descending maneuver that can be used to recover helicopters in the event of total loss of engine power; however it is an extremely difficult and complex maneuver. The objective of this work is to develop a real-time system which provides full autonomous control for autorotation landing of helicopters. The work includes the development of an autorotation path planning method and integration of the path planner with a primary flight control system. The trajectory is divided into three parts: entry, descent and flare. Three different optimization algorithms are used to generate trajectories for each of these segments. The primary flight control is designed using a linear dynamic inversion control scheme, and a path following control law is developed to track the autorotation trajectories. Details of the path planning algorithm, trajectory following control law, and autonomous autorotation system implementation are presented. -
A Qualitative Introduction to the Vortex-Ring-State, Autorotation, and Optimal Autorotation
UNCLASSIFIED Nationaal Lucht- en Ruimtevaartlaboratorium National Aerospace Laboratory NLR Executive summary A Qualitative Introduction to the Vortex-Ring-State, Autorotation, and Optimal Autorotation Problem area survey relative to single-engine The main objective of this paper is helicopter optimal autorotation, and Report no. to provide the reader with some its associated problem formulation NLR-TP-2010-282 qualitative insight into the areas of as a nonlinear, constrained, optimal Vortex-Ring-State (VRS), control problem. Author(s) autorotation, and optimal S. Taamallah autorotation. Results and conclusions Presenting a complete survey of a Report classification Description of work field as diverse as helicopter VRS, UNCLASSIFIED First this paper summarizes the autorotation, and optimal Date results of a brief VRS literature trajectories in autorotation is a May 2011 survey, where the emphasis has daunting task. Hence the review been placed on a qualitative is from a common qualitative Knowledge area(s) description of the following items: approach, with emphasis on Helikoptertechnologie conditions leading to VRS flight, concepts rather than on details. the VRS region, avoiding the VRS, Descriptor(s) the early symptoms, recovery from Applicability Vortex-Ring-State (VRS) VRS, experimental investigations, This survey was essentially tailored Autorotation and VRS modeling. The focus of for researchers interested in Height-Velocity diagram the paper is subsequently moved designing control systems, for Optimal control towards the autorotation helicopter flight in the VRS and Optimal autorotation phenomenon, where a review of the autorotation, such as automatic following items is given: the VRS avoidance, automatic recovery maneuver, the height-velocity from VRS flight, and automatic zones, and factors affecting autorotation. -
V-22 Osprey Tilt-Rotor Aircraft
Order Code RL31384 V-22 Osprey Tilt-Rotor Aircraft Updated March 13, 2007 Christopher Bolkcom Specialist in National Defense Foreign Affairs, Defense, and Trade Division V-22 Osprey Tilt-Rotor Aircraft Summary The V-22 Osprey is a tilt-rotor aircraft, capable of vertical or short take off and landing, with forward flight like a conventional fixed-wing aircraft. The MV-22 is the Marine Corps’ top aviation priority. Marine Corps leaders believe that the Osprey will provide them an unprecedented capability to quickly and decisively project power from well over the horizon. The Air Force’s CV-22 version will be used for special operations. Army officials have testified that the service has no requirement for the V-22, but the Navy has expressed interest in purchasing MV-22s for a variety of missions. The V-22 program has been under development for over 25 years. Safety and maintenance concerns have arisen during this period (due in large part to three fatal accidents). The commander of the V-22 maintenance squadron admitted to falsifying maintenance records to make the aircraft appear more maintainable than it was, and three Marines were found guilty of misconduct. The program has maintained support from many in Congress despite these deficiencies. The program has undergone restructuring to accommodate congressional direction, budget constraints, and recommendations from outside experts, and DOD managers. After a 17 month hiatus, the Osprey embarked on its second set of flight tests in May of 2002. Tests were completed in June 2005 to the satisfaction of Navy testers, who believe that the V-22 has resolved all technical and engineering problems identified in internal and external reviews. -
Motivations and Preliminary Design for Mid-Air Deployment of a Science Rotorcraft on Mars
Motivations and Preliminary Design for Mid-Air Deployment of a Science Rotorcraft on Mars Jeff Delaune∗ Jacob Izraelevitz† Evgeniy Sklyanskiy‡ Aaron Schutte§ Abigail Fraeman¶ Valerie Scott‖ Carl Leake∗∗ Erik Ballesteros†† Kim Aaron‡‡ Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA, 91109 Larry A. Young§§ Wayne Johnson¶¶ Shannah Withrow-Maser∗∗∗ Haley Cummings††† Raghav Bhagwat‡‡‡ NASA Ames Research Center, Moffett Field, CA, 94035 Marcel Veismann§§§ Skylar Wei¶¶¶ Regina Lee17 Luis Pabon Madrid18 Morteza Gharib19 Joel Burdick20 Center for Autonomous Systems and Technologies (CAST), California Institute of Technology, Pasadena, CA, 91125 William Rapin21 CNRS, Toulouse, 31400, France Mid-Air Deployment (MAD) of a rotorcraft during Entry, Descent and Landing (EDL) on Mars eliminates the need to carry a propulsion or airbag landing system. This reduces the total mass inside the aeroshell by more than 100 kg and simplifies the aeroshell architecture. MAD’s lighter and simpler design is likely to bring the risk and cost associated with the mission down. Moreover, the lighter entry mass enables landing in the Martian highlands, at elevations inaccessible to current EDL technologies. This paper proposes a novel MAD concept for a Mars helicopter. We suggest a minimum science payload package to perform relevant science in the highlands. A variant of the Ingenuity helicopter is proposed to provide increased deceleration during MAD, and enough lift to fly the science payload in the highlands. We show in simulation that the lighter aeroshell results in a lower terminal velocity (30 m/s) at the end of the parachute phase of the EDL, and at higher altitudes than other approaches. -
Flight Dynamics Investigation of Compound Helicopter Configurations
Ferguson, Kevin, and Thomson, Douglas (2014) Flight dynamics investigation of compound helicopter configurations. Journal of Aircraft. ISSN 1533-3868 Copyright © 2014 American Institute of Aeronautics and Astronautics, Inc. A copy can be downloaded for personal non-commercial research or study, without prior permission or charge Content must not be changed in any way or reproduced in any format or medium without the formal permission of the copyright holder(s) When referring to this work, full bibliographic details must be given http://eprints.gla.ac.uk/92870 Deposited on: 29 May 2014 Enlighten – Research publications by members of the University of Glasgow http://eprints.gla.ac.uk Flight Dynamics Investigation of Compound Helicopter Configurations Kevin M. Ferguson∗, Douglas G. Thomsony, University of Glasgow, Glasgow, United Kingdom, G12 8QQ Compounding has often been proposed as a method to increase the maximum speed of the helicopter. There are two common types of compounding known as wing and thrust compounding. Wing compounding offloads the rotor at high speeds delaying the onset of retreating blade stall, hence increasing the maximum achievable speed, whereas with thrust compounding, axial thrust provides additional propulsive force. There has been a resurgence of interest in the configuration due to the emergence of new requirements for speeds greater than those of con- ventional helicopters. The aim of this paper is to investigate the dynamic stability characteristics of compound helicopters and compare the results with a conventional helicopter. The paper discusses the modeling of two com- pound helicopters, which are named the coaxial compound and hybrid compound helicopters. Their respective trim results are contrasted with a conventional helicopter model.