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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. -
Abstract Effect of Interactional
ABSTRACT Title of thesis: EFFECT OF INTERACTIONAL AERODYNAMICS ON COMPUTATIONAL AEROACOUSTICS OF SIKORSKY'S NOTIONAL X2 PLATFORM Ian Kevin Bahr Master of Science in Aerospace Engineering, 2020 Thesis directed by: Professor James Baeder A. James Clark School of Engineering Department of Aerospace Engineering An in-house acoustics code, ACUM, was used in conjunction with full vehicle CFD/CSD coupling to create a computational aeroacoustic framework to investigate the effect of aerodynamic interactions on the acoustic prediction of a compound coaxial helicopter. The full vehicle CFD/CSD was accomplished by using a high- fidelity computational fluid dynamics framework, HPCMP CREATETM-AV Helios, combined with an in-house computational structural dynamics solver to simulate the helicopter in steady forward flight. A notional X2TD helicopter consisting of a coaxial rotor, airframe and pusher propeller was used and split into three simulation cases: isolated coaxial and propeller, airframe and full helicopter configuration to investigate each component's affect on the others noise as well as the total noise. The primary impact on the acoustic prediction was the inclusion of the airframe in the CFD simulation as it affected both coaxial rotors as well as the propeller. It was found that the propeller and coaxial rotors had negligible impact on each other. EFFECT OF INTERACTIONAL AERODYNAMICS ON COMPUTATIONAL AEROACOUSTICS OF SIKORSKY'S NOTIONAL X2 PLATFORM by Ian Kevin Bahr Thesis submitted to the Faculty of the Graduate School of the University of Maryland, College Park in partial fulfillment of the requirements for the degree of Master of Science 2020 Advisory Committee: Dr. James Baeder, Chair/Advisor Dr. -
AHS -- Future of Vertical Flight
The Future of Vertical Flight www.tinyurl.com/VFS-Heli-Expo-2020 Mike Hirschberg, Executive Director The Vertical Flight Society www.vtol.org • [email protected] © Vertical Flight Society: CC-BY-SA 4.0 www.vtol.org ▪ The international professional society for those working to advance vertical flight – Founded in 1943 as the American Helicopter Society (AHS) – Everything from VTOL MAVs/UAS to helicopters, eVTOL, etc. ▪ Expands knowledge about vertical flight technology and promotes its application around the world CFD of Joby S4, Aug 2015 ▪ Advances safety and acceptability ▪ Advocates for vertical flight R&D funding ▪ Helps educate and support today’s and tomorrow’s vertical flight engineers and leaders ▪ Brings together the community — industry, academia and government agencies — to tackle the toughest challenges Join us today: www.vtol.org VFF Scholarship Winners at Forum 71, May 2015 © Vertical Flight Society: CC-BY-SA 4.0 2 www.vtol.org ▪ VFS has a long history of advocacy and leadership – Helped establish NASA-Army Joint Office, Nat’l Rotorcraft Technology Center (NRTC), Centers of Excellence, RITA/VLC – Worked with NASA and DoD to save the NFAC wind tunnel ▪ Provided major support to transformative initiatives NFAC 40 ft x 80 ft wind tunnel Courtesy of NASA – Joint Strike Fighter/F-35B STOVL Lightning II – V-22 Osprey tiltrotor ▪ Providing major foundational support to new transformative initiatives – Future Vertical Lift (FVL)/Joint Multi-Role (JMR) – Electric and hybrid-electric VTOL (eVTOL) Future Vertical Lift (FVL) VFS Works -
Design and Performance of Lift-Offset Rotorcraft for Short-Haul Missions
Design and Performance of Lift-Offset Rotorcraft for Short-Haul Missions Wayne Johnson Aeromechanics Branch National Aeronautics and Space Administration Ames Research Center, Moffett Field, California [email protected] Alex M. Moodie and Hyeonsoo Yeo Aeroflightdynamics Directorate (AMRDEC) U.S. Army Research, Development, and Engineering Command Ames Research Center, Moffett Field, California [email protected], [email protected] ABSTRACT The design and performance of compound helicopters utilizing lift-offset rotors are examined, in the context of short-haul, medium-size civil and military missions. The analysis tools used are the comprehensive analysis CAMRAD II and the sizing code NDARC. Following correlation of the comprehensive analysis with existing lift-offset aircraft flight test data, the rotor performance model for the sizing code was developed, and an initial estimate was made of the rotor size and key hover and cruise flight conditions. The rotor planform and twist were optimized for those conditions, and the sizing code rotor performance model updated. Two models for estimating the blade and hub weight of lift-offset rotors are discussed. The civil and military missions are described, along with the aircraft design assumptions. The aircraft are sized for 30 passengers or 6600 lb payload, with a range of 300 nm. Civil and military aircraft designs are described for each of the rotor weight models. Disk loading and blade loading were varied to optimize the designs, based on gross weight and fuel burn. The influence of technology is shown, in terms of rotor hub drag and rotor weight. and the rotor efficiency and lift capability steadily INTRODUCTION. -
Over Thirty Years After the Wright Brothers
ver thirty years after the Wright Brothers absolutely right in terms of a so-called “pure” helicop- attained powered, heavier-than-air, fixed-wing ter. However, the quest for speed in rotary-wing flight Oflight in the United States, Germany astounded drove designers to consider another option: the com- the world in 1936 with demonstrations of the vertical pound helicopter. flight capabilities of the side-by-side rotor Focke Fw 61, The definition of a “compound helicopter” is open to which eclipsed all previous attempts at controlled verti- debate (see sidebar). Although many contend that aug- cal flight. However, even its overall performance was mented forward propulsion is all that is necessary to modest, particularly with regards to forward speed. Even place a helicopter in the “compound” category, others after Igor Sikorsky perfected the now-classic configura- insist that it need only possess some form of augment- tion of a large single main rotor and a smaller anti- ed lift, or that it must have both. Focusing on what torque tail rotor a few years later, speed was still limited could be called “propulsive compounds,” the following in comparison to that of the helicopter’s fixed-wing pages provide a broad overview of the different helicop- brethren. Although Sikorsky’s basic design withstood ters that have been flown over the years with some sort the test of time and became the dominant helicopter of auxiliary propulsion unit: one or more propellers or configuration worldwide (approximately 95% today), jet engines. This survey also gives a brief look at the all helicopters currently in service suffer from one pri- ways in which different manufacturers have chosen to mary limitation: the inability to achieve forward speeds approach the problem of increased forward speed while much greater than 200 kt (230 mph). -
HELP from ABOVE Air Force Close Air
HELP FROM ABOVE Air Force Close Air Support of the Army 1946–1973 John Schlight AIR FORCE HISTORY AND MUSEUMS PROGRAM Washington, D. C. 2003 i Library of Congress Cataloging-in-Publication Data Schlight, John. Help from above : Air Force close air support of the Army 1946-1973 / John Schlight. p. cm. Includes bibliographical references and index. 1. Close air support--History--20th century. 2. United States. Air Force--History--20th century. 3. United States. Army--Aviation--History--20th century. I. Title. UG703.S35 2003 358.4'142--dc22 2003020365 ii Foreword The issue of close air support by the United States Air Force in sup- port of, primarily, the United States Army has been fractious for years. Air commanders have clashed continually with ground leaders over the proper use of aircraft in the support of ground operations. This is perhaps not surprising given the very different outlooks of the two services on what constitutes prop- er air support. Often this has turned into a competition between the two serv- ices for resources to execute and control close air support operations. Although such differences extend well back to the initial use of the airplane as a military weapon, in this book the author looks at the period 1946- 1973, a period in which technological advances in the form of jet aircraft, weapons, communications, and other electronic equipment played significant roles. Doctrine, too, evolved and this very important subject is discussed in detail. Close air support remains a critical mission today and the lessons of yesterday should not be ignored. This book makes a notable contribution in seeing that it is not ignored. -
Enforcer Close Air Support Aircraft” of the John Marsh Files at the Gerald R
The original documents are located in Box 11, folder “Defense - Enforcer Close Air Support Aircraft” of the John Marsh Files at the Gerald R. Ford Presidential Library. Copyright Notice The copyright law of the United States (Title 17, United States Code) governs the making of photocopies or other reproductions of copyrighted material. Gerald R. Ford donated to the United States of America his copyrights in all of his unpublished writings in National Archives collections. Works prepared by U.S. Government employees as part of their official duties are in the public domain. The copyrights to materials written by other individuals or organizations are presumed to remain with them. If you think any of the information displayed in the PDF is subject to a valid copyright claim, please contact the Gerald R. Ford Presidential Library. - Digitized from Box 11 of The John Marsh Files at the Gerald R. Ford Presidential Library JOHN L MCCLELLAN, AnK., Cf~I\IRM.t.'-11 VJAr.. !"H G. MM:;NIJ~';.CJN• WASH. MILTC'If.l R Y~UN<;, N. I"I'.K. J() 1'11 C, ~Tt"riNI$ 0 MISS. ROMAN L. fHl\I~KI\, NF.PR• .ll"t.r.. "t., rA!'.1C.'H-=:, R.I. NORRIS C0TION0 h.H. 1\l 1\N l!ll'LI?. NI:V.. CL rrnr~o P. C'A~f". N.l. f~O<Ji:::f r C. BVHC", W. VA, HIRI\M L, FONG, ttl\ WAll GJ\LE W. MCGI:E, WYO. £OW/\RO W, CROOK£', MASS. floU,.;.E MIINSF'•Ct...O. Mt\NT. Ml\llK 0, UI\TFIEl..C\1 OREG. -
New Rotary Wing Technologies Dr Carlo Kopp
New rotary wing technologies Dr Carlo Kopp Rotary wing technology like most aerospace technologies has evolved slowly since the end of the Cold War. Without the imperative of a well identified threat there has been little political or bureaucratic interest in maintaining the technological advantage the West held over all nations in 1991. heli & uv pacific 2010 At the end of the Cold War, the United States held a commanding advantage in most conventional rotary wing areas, with the Europeans lagging but closely behind, and the Soviets behind in all areas other than heavy lift helicopters. At that time the US had two new programs in development, the V-22 Osprey, which was to herald a generation of new tiltrotor technology designs, and the RAH-66 Comanche Scout helicopter which was to have been the vehicle for new rotor technologies, and a very low signature or ‘stealth’ design. Two decades later the Comanche is ‘dead’ and the V-22, after a very painful and protracted development cycle, is only now achieving credible operational maturity. Most of the military helicopter types remaining in production in the US are derivatives or variants of Cold War era designs. Europe is faring better, as it has a generation of new rotary wing designs now in production, using composite structural materials extensively, but these vehicles are in aerodynamic and propulsion Sikorsky X2. terms just as conventional as their trans-atlantic siblings. Much the same can be said of the latest The principal impediment to faster helicopters has designs in Asia. been the retreating blade stall effect, inherent in In terms of mainstream production helicopter single rotor designs, and often the reason why designs it would be fair to describe the area as fast helicopters are also equipped with short span largely stagnant. -
Rotor Diameter
Scaling Up Success The SB>1 Defiant Joint Multi-Role Technology Demonstrator challenges Sikorsky and Boeing to grow the integrated X2 technologies By Frank Colucci peed and range improvements The SB>1 Defiant JMR Technology Demonstrator scales up Sikorsky X2 rigid coaxial rotor sought by US Army Aviation drove compound helicopter technologies to achieve speed, range and agility far better than SSikorsky, Boeing and their Defiant conventional helicopters. (Sikorsky graphic) team to scale up technologies flown on the 6,000 lb (3 t) X2 and 11,400 lb The MPS summary of FVL-M teams, Sikorsky Innovations vice (5.2 t) S-97 to the 30,000 lb (14 t) class performance includes cruising president Chris Van Buiten previously SB>1 Joint Multi-Role Technology speeds greater than 230 kt (426 stated, “Raider is risk-reduction for JMR.” Demonstrator (JMR-TD). A Systems km/h), vertical takeoff at 6,000 ft/95˚F Sikorsky and Boeing teamed Integration Laboratory (SIL) for Defiant (1,800 m/35˚C) density altitude and up on the SB>1 Defiant in January came on line in December and a a combat radius of 229 nm (424 km) 2013. Boeing program co-director Transmission System Test Bed will run with four crew and 12 troops. The 250 Pat Donnelly said, “When we put in 2016. The JMR-TD due to fly in 2017 is kt (463 km/h) Defiant answers the this together, we were certainly very based on a 2013 Mission Performance specification with rigid coaxial rotors, sensitive to the scaling issues of the Specification (MPS) for a medium-size an integrated tail propeller, optimized X2 technology. -
New Design Approach of Compound Helicopter
Prasetyo Edi, Nukman Yusoff, Aznijar Ahmad Yazid, Catur Setyawan K., WSEAS TRANSACTIONS on APPLIED and THEORETICAL MECHANICS Nurkas W., Suyono W. A. New Design Approach of Compound Helicopter PRASETYO EDI, NUKMAN YUSOFF and AZNIJAR AHMAD YAZID Department of Engineering Design & Manufacture, Faculty of Engineering, University of Malaya, 50603 Kuala Lumpur, MALAYSIA [email protected] http://design-manufacturer.eng.um.edu.my/ CATUR SETYAWAN K., NURKAS W., and SUYONO W. A. Directorate of Technology Indonesian Aerospace (IAe) Jl. Pajajaran 154, Bandung Indonesia [email protected] http://www.indonesian-aerospace.com/index.php Abstract: - Current trends in the design of helicopter have shown that in order to be economically viable and competitive it is necessary to investigate new design concept which may give an improvement in performance and operational flexibility goal and expanding the flight envelope of rotorcraft, but must be shown to be cost- effective. The helicopter has carved a niche for itself as an efficient vertical take-off and landing aircraft, but have limitation on its cruising speed due to restrictions of retreating blade stall and advancing blade compressibility on the rotor in edgewise flight. This is a challenging task, which might be solved by the use of new design approach. It is believed that the application of a compound helicopter design concept would assist in achieving such a task. This paper describes an investigation aimed to examine the suitability of a compound helicopter design concept, allowing for the use of a combined conventional fix-wing aircraft with single propeller in the nose and conventional helicopter to satisfy the above objectives. -
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. -
Sikorsky S-97 Raider Exceeds 200 Knots As Company Prepares Proposal for U.S. Army's Future Attack Reconnaissance Aircraft
Sikorsky S-97 Raider Exceeds 200 Knots as Company Prepares Proposal for U.S. Army's Future Attack Reconnaissance Aircraft October 4, 2018 Sikorsky's self-funded X2 Technology is backbone of company's next generation helicopters WEST PALM BEACH, Fla., Oct. 4, 2018 /PRNewswire/ -- The Sikorsky S-97 Raider light tactical prototype helicopter is advancing rapidly through its flight test schedule, recently exceeding 200 knots at the Sikorsky Development Flight Center. Raider, developed by Sikorsky, a Lockheed Martin (NYSE: LMT) company, is based on the company's proven X2 Technology, enabling speeds twice that of conventional helicopters. View the latest Sikorsky S-97 Raider video. "The Sikorsky S-97 Raider flight test program is exceeding expectations, demonstrating Raider's revolutionary speed, maneuverability and agility," said Tim Malia, Sikorsky director, Future Vertical Lift Light. "X2 Technology represents a suite of technologies needed for the future fight, enabling the warfighter to engage in high-intensity conflict anytime, anywhere as a member of a complex, multi-domain team." Sikorsky continues to demonstrate the application of its X2 Technology as the company prepares its proposal for the U.S. Army's Future Attack Reconnaissance Aircraft (FARA) competition, driving forward the Army's efforts to revolutionize its aircraft fleet as part of what is known as Future Vertical Lift. Raider incorporates the latest advances in fly-by-wire flight controls, vehicle management systems and systems integration. The suite of X2 Technologies enables the aircraft to operate at high speeds while maintaining the low-speed handling qualities and maneuverability of conventional single main rotor helicopters.