aviation week A New Approach To VTOL Page 36 Secure Collaboration On The Internet THE FIGHT OVER F-22 & SPACE TECHNOLOGY Page 53 Page 44

Similar documents
AT-10 Electric/HF Hybrid VTOL UAS

Electric VTOL Aircraft

Designing evtol for the Mission NDARC NASA Design and Analysis of Rotorcraft. Wayne Johnson From VTOL to evtol Workshop May 24, 2018

UNCLASSIFIED: Distribution Statement A. Approved for public release.

Versatile Affordable Advanced Turbine Engines Provide Game Changing Capability with Superior Fuel Efficiency

Skycar Flight Control System Overview By Bruce Calkins August 14, 2012

Electric Flight Potential and Limitations

UNCLASSIFIED FY 2017 OCO. FY 2017 Base

Predator B: The Multi-Role UAV

Predator ACTD. Presentation To NDIA IOT&E

UNCLASSIFIED. FY 2016 Base FY 2016 OCO

Electric Penguin s philosophy:

neuron An efficient European cooperation scheme

The quest continues for ways to make unmanned systems

High aspect ratio for high endurance. Mechanical simplicity. Low empty weight. STOVL or STOL capability. And for the propulsion system:

for Unmanned Aircraft

AIAA Foundation Undergraduate Team Aircraft Design Competition. RFP: Cruise Missile Carrier

Innovating the future of disaster relief

Innovative Airship Solutions from Guardian Flight Systems

German Aerospace Center Flight Operations

Reducing Landing Distance

Ejemplos de aeronaves existentes similares a las propuestas en los RFP 2007

Design and Development of Hover bike

NASA centers team up to tackle sonic boom 18 March 2014, by Frank Jennings, Jr.

BAYLOR UNIVERSITY DEPARTMENT OF ENGINEERING. EGR 4347 Analysis and Design of Propulsion Systems Fall 2002 ASSIGNMENT GUIDELINES

Jay Gundlach AIAA EDUCATION SERIES. Manassas, Virginia. Joseph A. Schetz, Editor-in-Chief. Blacksburg, Virginia. Aurora Flight Sciences

UNCLASSIFIED FY 2016 OCO. FY 2016 Base

Analysts/Fund Managers Visit 19 April Autonomous Systems and Future Capability Mark Kane

RDT&E BUDGET ITEM JUSTIFICATION SHEET (R-2 Exhibit) June 2001

ELECTRIC POWER TRAINS THE KEY ENABLER FOR CONTRA ROTATING PROPELLERS IN GENERAL AVIATION (& VICE VERSA)

Air Platforms Community of Interest Update

Backgrounder. The Boeing ecodemonstrator Program

UNCLASSIFIED. R-1 Program Element (Number/Name) PE F / Aerospace Propulsion and Power Technology

International Journal of Scientific & Engineering Research, Volume 4, Issue 7, July ISSN BY B.MADHAN KUMAR

North American F-86F Sabre USER MANUAL. Virtavia F-86F Sabre DTG Steam Edition Manual Version 1

Micro Craft Ducted Air Vehicle. Larry Lipera istar Program Manager Micro Craft Inc., San Diego, CA

Mike Gibbons Paul Summers John Murnane

MAV and UAV Research at Rochester Institute of Technology. Rochester Institute of Technology

Sciences for Maneuver Campaign

UNCLASSIFIED FY 2017 OCO. FY 2017 Base

Airships: A New Horizon for Science April 30 May 3, Worldwide Aeros Corp. Montebello, California. Presented by:

WHY TWO SPOOLS ARE BETTER THAN ONE: EQUIPPING OUR MILITARY WITH THE BEST TECHNOLOGY FOR EXISTING AND EMERGING THREATS

AN ADVANCED COUNTER-ROTATING DISK WING AIRCRAFT CONCEPT Program Update. Presented to NIAC By Carl Grant November 9th, 1999

31 st Annual American Helicopter Society Student Design Competition: Graduate Submission

PROLIFERATION LANDMINES DEFENSE ADVICE. Airships

Air Buzz. 32nd Annual AHS International Student Design Competition

The following slideshow and talk were presented at the Uber Elevate Summit on April 25 th, The text included here is an approximate transcript

Air Platforms Community of Interest Update

Stagger Around #3: AGM-129 Advanced Cruise Missile, Abridged Edition

Statement of Jim Schoppenhorst, Director, DD(X) BAE Systems / Armament Systems Division. Before the

F/A-18A/B/C/D Flight Control Computer Software Upgrade

Mike Hirschberg, Executive Director AHS International The Vertical Flight Technical Society

Aeronautical Systems Center

PENGUIN B UAV PLATFORM

Versatile Affordable Advance Turbine Engine (VAATE)

Appenidix E: Freewing MAE UAV analysis

20 February 2018 The Airlander Hybrid Air Vehicle Andy Barton, CEng, FRAeS Civil Business Development Director

Republic of Korea Airworthiness Certification of Unmanned Aerial System

Mobilus. Creating A New Transport Airship Capability in the US Aerospace Industry

Focus Areas Power and Energy Operational Environments

수직이착륙형고속비행무인기로임무효율성및운용편의성증대 자동수직이착륙으로높은운용성 ( 고정익대비 ) 고도 / 속도 / 체공성능우월로임무효율성제고 ( 회전익대비 ) EO/IR, LRF 탑재및임무장비교체가능한다목적용무인기

UNCLASSIFIED R-1 ITEM NOMENCLATURE. FY 2014 FY 2014 OCO ## Total FY 2015 FY 2016 FY 2017 FY 2018

THE KARANTANIA UNMANNED AERIAL SYSTEM

Preface. Acknowledgments. List of Tables. Nomenclature: organizations. Nomenclature: acronyms. Nomenclature: main symbols. Nomenclature: Greek symbols

External Aerodynamics: Lift of airship created only by buoyancy which doesn t need lift generating surface like an airfoil or a wing

The Future of Engine Technology

'Prototype' Commission Regulation on Unmanned Aircraft Operations. FAI proposal for model flying activities

Key Drivers for evtol Design Christopher Silva From VTOL to evtol Workshop May 24, 2018

Powertrain Design for Hand- Launchable Long Endurance Unmanned Aerial Vehicles

(VTOL) Propulsion Systems Design

Flight Stability and Control of Tailless Lambda Unmanned Aircraft

UAV Drones. Team RamRod: Tyler Barry James Bohn Daniel Ramirez Hari Shrestha Arlo Swanson Garret Wilbanks

FLASHCARDS AIRCRAFT. Courtesy of the Air Safety Institute, a Division of the AOPA Foundation, and made possible by AOPA Services Corporation.

WHEN BORDER SECURITY MATTERS

A FLYING EJECTION SEAT. By R. H. Hollrock* and J. J. Barzda* ABSTRACT

Program Summary Model 281 Proteus

Better Performance Starts with Better Technology THE BLR ADVANTAGE

INNOVATION POWERING SAFRAN

V-280 Valor Joint Multi-Role Technology Demonstrator

MS1-A Military Spaceplane System and Space Maneuver Vehicle. Lt Col Ken Verderame Air Force Research Laboratory 27 October 1999

Performance means how fast will it go? How fast will it climb? How quickly it will take-off and land? How far it will go?

Compared Air Combat Performances analysis Mig-21 versus F-5E

A short Company & Technology Overview

Hybrid-Electric Propulsion System Conceptual Design Challenges

SILENT SUPERSONIC TECHNOLOGY DEMONSTRATION PROGRAM

UNCLASSIFIED. R-1 ITEM NOMENCLATURE PE F: Aerospace Propulsion and Power Technology FY 2012 OCO

Bild : Bernhard Mühr German Aerospace Center Flight Operations

Hybrid VTOL: Increased Energy Density for Increased Payload and Endurance

UNCLASSIFIED R-1 ITEM NOMENCLATURE. FY 2014 FY 2014 OCO ## Total FY 2015 FY 2016 FY 2017 FY 2018

A SOLAR POWERED UAV. 1 Introduction. 2 Requirements specification

AF Hypersonic Vision

MA THOR SolarLight UAS

Friday, 27 June Realizing a small UAV for medical transport in developing countries Master thesis: Ferdinand Peters. Dr.One

UNCLASSIFIED R-1 ITEM NOMENCLATURE

Opportunities For Innovative Collaboration. Propulsion Directorate Propulsion & Power for the 21st Century Warfighter

Small UAV A French MoD perspective and planning

MINI-REIS A FAMILY OF MULTIFUNCTIONAL UNMANNED LIGHT JET AIRCRAFTS

VAST AUAV (Variable AirSpeed Telescoping Additive Unmanned Air Vehicle)

CarterCopters. Cleaner Greener. Safer. Your affordable environmentally-friendly VTOL technology Carter Aviation Technologies, LLC

The winner team will have the opportunity to perform a wind tunnel test campaign in the transonic/supersonic Wind tunnel at the VKI.

Transcription:

THE FIGHT OVER F-22 aviation $6.00 JULY 20, 2009 week & SPACE TECHNOLOGY A New Approach To VTOL Page 36 Secure Collaboration On The Internet Page 44 Page 53 AviationWeek.com/awst

Page 1 of 1 Print This Page On The Cover On the Cover Aviation Week & Space Technology Jul 20, 2009, p. 01 Aurora Flight Sciences Excalibur experimental vertical-takeoff-and-landing unmanned combat aircraft rises to a hover on its June 24 first flight at Aberdeen Proving Grounds, Md. The 13-ft.-long subscale proof-of-concept aircraft is the testbed for a hybrid turbine-electric propulsion system comprising a tilting jet engine and battery-driven lift fans (see p. 36). Using exclusive first-flight photographs by John Tylko of Aurora Flight Sciences, the AW&ST Art Dept. created a time-lapse image of the aircraft lifting off. Find this article at: http://www.aviationweek.com:80/publication/awst/loggedin/avnowstorydisplay.do? fromchannel=awst&pubkey=awst&channel=awst&issuedate=2009-07- 20&story=xml/awst_xml/2009/07/20/AW_07_20_2009_p04-154173-01.xml&headline=On+the+Cover Copyright 2009, AVIATION WEEK, a division of The McGraw-Hill Companies All rights reserved Terms of Use Privacy Notice Contact Us

Page 1 of 5 Print This Page Unmanned Aircraft Aurora Flies Hybrid VTOL UCAV Demonstrator Aviation Week & Space Technology Jul 20, 2009, p. 36 Graham Warwick Washington Aurora flies turbine-electric UAV designed to combine high speed and vertical flight Printed headline: Hovering Hybrid One hundred feet above the U.S. Army s Aberdeen Proving Grounds in Maryland, executing pre-programmed hover maneuvers, the experimental Excalibur could be providing a glimpse of future unmanned combat aircraft. And not just because of its unusual configuration. Excalibur hovers on jet engine and electric lift-fan power during its June 24 first flight, which lasted just under 2 min. Takeoff, hover and landing were autonomous.credit: AURORA FLIGHT SCIENCES CORPORATION/JOHN TYLKO Flown for the first time on June 24, the aircraft is a testbed for a hybrid turbine-electric propulsion system that developer Aurora Flight Sciences believes can efficiently combine high speed and vertical takeoff and landing (VTOL) capability. Beyond that, the Virginia-based unmanned aircraft specialist sees hybrid propulsion as fundamentally

Page 2 of 5 enabling for a wide range of missions. Electric propulsion has an enormous place in next-generation aircraft, says Aurora President John Langford. Excalibur is the first flight article in a very rich vein with a lot of applications. Also for NASA, the company conceived a series of unmanned aircraft designed to fly in the rarefied Martian atmosphere, culminating in 2002 in a high-altitude deployment in which a half-scale MarsFlyer demonstrator was released from a helium balloon above 100,000 ft. to unfold and descend autonomously. The experimental unmanned combat aircraft is checked out before its first flight at Aberdeen Proving Grounds. Thrust-vectoring vanes under lift fans are used for yaw control.credit: AURORA FLIGHT SCIENCES CORP./JOHN LANGFORD The experimental unmanned combat aircraft is checked out before its first flight at Aberdeen Proving Grounds. Thrust-vectoring vanes under lift fans are used for yaw control.credit: AURORA FLIGHT SCIENCES CORP./JOHN LANGFORD Since it was founded 20 years ago, the company has made its name developing one-off unmanned aircraft for NASA and the U.S. military. Aurora built the Perseus and Theseus remotely piloted vehicles for NASA to test high-altitude propulsion systems; the Perseus B exceeded 60,000 ft. in 1998 on a triple-turbocharged piston engine. Aurora has continued to focus on high altitude, designing the Orion long-loiter UAV around a liquid hydrogen-fueled propulsion system using an automotive engine modified to operate above 65,000 ft. Construction of the 132-ft.-span aircraft is under way at Aurora s Columbus, Miss., plant, but the Army-supported technology demonstration may be changing direction, with the possibility that the Orion might fly in mid-2010 with a conventional piston engine to demonstrate five-day endurance at medium altitudes of around 20,000 ft. The company is also working under the U.S. Defense Research Projects Agency s (Darpa s) Vulture program to demonstrate technology for a solar-electric unmanned aircraft capable of staying aloft in the stratosphere for up to five years. Aurora s Odysseus concept involves three UAVs that would be launched independently to join up in flight to form a unique Z-wing vehicle designed to maximize solar energy collection by day and minimize drag by night. Aurora was not selected to proceed into Phase 2 of the Vulture program, but it filed a protest that has forced a recompetition. Meanwhile, in May the company flew a large solar-powered unmanned aircraft, the SunLight Eagle, produced by modifying an airframe originally built as a prototype for the Daedalus human-powered aircraft. The company plans to fly the 114-ft.-span UAV to progressively longer durations and higher altitudes.

Page 3 of 5 Despite its association with high altitude and long endurance, Aurora has ventured into tactical UAVs. In the late 1990s, the company built a subscale version of Raytheon s proposed unmanned combat air vehicle demonstrator. A quarter-scale tailless delta flying-wing vehicle was flown, but Raytheon did not win the contract. Aurora then began to focus on VTOL, flying the GoldenEye ducted-fan UAV in July 2003. The autonomous aircraft was designed to take off vertically, then transition to forward flight on swiveling wings. Developed with Army funding as a clandestine UAV for deploying ground sensor packages, the initial GoldenEye 100 was a 150-lb. vehicle with 22- lb. payload, 4-hr. endurance and 160-kt. maximum speed. The company also built several smaller GoldenEye 50s, an 18-lb. version with 2-lb. payload and 1-hr. endurance, for flight-testing and potential homeland security missions. But a 2004 contract from Darpa led to development of a third version, the GoldenEye 80, first flown in 2006. Three 12-kw. battery-powered lift fans and a 700-lb.-thrust-class Williams F415 turbofan developed to power the Tactical Tomahawk cruise missile provide thrust for vertical flight.credit: AURORA FLIGHT SCIENCES CORP./PATTI WOODSIDE Originally intended to produce an organic UAV for the Army s Future Combat Systems program, the Darpa project was eventually terminated, but Aurora continued work and in April completed company-funded development of the Block 1 vehicle. This is Aurora s first UAV product, although the company has yet to secure a customer. The GoldenEye 80 is a 150-lb. vehicle with 18-lb. payload. Endurance ranges from a couple of hours for the Block 1 vehicle to 8 hr. for the eventual wing-equipped Block 3. When work began on the Excalibur in 2005, there were no examples of hybrid electric aircraft. The initial problem was how to merge VTOL with high-speed flight, says Tom Clancy, chief technology officer. The fundamental challenge with VTOL is that the high power required for vertical flight means the engines are oversized for cruise, he says. To avoid carrying around too much engine, Aurora surveyed technologies and settled on a hybrid turbine-electric approach to matching the thrust requirements for vertical and forward flight. The Excalibur uses a tilting jet engine for primary propulsion and electric lift fans for supplemental thrust and attitude control in vertical flight. A significant portion of vertical thrust is provided by lift fans, so we can size the engine optimally for the cruise, says Clancy. For VTOL mode, the turbine engine tilts vertically and provides about 70% of the thrust. This allows use of an off-the-shelf turbine engine, reducing costs. Battery-powered lift fans in the nose and wingtips provide the balance of vertical thrust. Pitch and roll control is achieved by differentially varying the speeds of the fixed-pitch fans, while yaw control is via vanes that vector the fan thrust. Using the lift fans simplifies attitude control compared with more complex systems that have to extract engine power and get it some way from the center of gravity, he says. For forward flight, the main engine tilts to the horizontal, the lift fans retract into the wingtips, doors cover the nose fan, and the aircraft rolls over so the wing is on the bottom. Subwings would carry weapons, principally four Hellfire missiles.

Page 4 of 5 Aurora plans to complete low-speed testing waking the box in hover mode using the lift fans for attitude and speed control on company funding.credit: AURORA FLIGHT SCIENCES CORP./JOHN TYLKO Recharging the batteries from the engine in the cruise is expected to take 15-20 min. The proof-of-principle vehicle lacks the ability to recharge in flight and starts with each of the 12-kw. lithium-polymer battery packs fully charged, providing about 6 min. of power, enough for two takeoffs and landings. This is a VTOL vehicle and is not designed to hover, says Langford. A takeoff and landing cycle is well under 3 min., so we should get two full cycles without recharging. The original design mission was to deliver 400 lb. of weapons in a survivable aircraft with high speed and low signature and the ability to operate from small ships and unprepared fields. The objective design has a 4,000-lb. VTOL gross weight, a 30-ft. span reducing to 21 ft. with the lift fans retracted, and a 300-kt. maximum speed at sea level increasing to 460 kt. at 30,000 ft. Ceiling is 40,000 ft. and loiter speed 90 kt. Aurora wanted to demonstrate the concept at a relevant scale that was large enough to use the same type of technologies as the full-size aircraft. The resulting proof-of-principle (POP) vehicle is half-scale: 13 ft. long with a VTOL gross weight of 720 lb., 10-ft. span with lift fans retracted and a 280-kt. sea-level speed capability. In this phase, we are not initially focused on leap-ahead technology in any area, such as energy storage or motor performance, says Clancy. The question is, what can current technologies enable? Our goal is to bring through flight test a high-speed VTOL vehicle at significant scale to demonstrate a point in the broad space of hybrid technologies. The batteries come from the personal electronics industry, and are packaged with power control electronics and brushless direct-drive motors to produce a reliable aerospace power system. It s pretty mature technology with relatively high specific energy and power. We got the performance we were aiming for to get a realistic impression of what the technology can do, Clancy says. The program was begun with support from the Army s Aviation Applied Technology Directorate and the Office of Naval Research. Funding has paced development, with $20 million spent to date. Recent work, including the first flight, has been funded internally by Aurora, which is looking for additional support for the next phases. The company plans to test the Excalibur in three flight regimes: low speed to 20 kt., medium speed to 40 kt. and high speed to 300 kt. indicated/400 kt. true airspeed. Up to 20 kt. is the hover regime, where the engine remains at a fixed angle and attitude and velocity are controlled by the lift fans. As speed is pushed to 40 kt., control becomes a blend of aerodynamic surfaces and lift fans. Beyond 40 kt. the aircraft goes through a configuration change, retracting and covering the lift fans, retracting the gear, lowering the engine and moving to all-aerodynamic lift and control. As built, the POP aircraft is only capable of low-speed flight and will require minor modifications to get to medium

Page 5 of 5 speed. These include making the control surfaces active. Because more significant modifications, such as retracting gear, would be needed for high-speed flight, there are plans to build a second demonstrator. While it looks for funding sources, Aurora plans to complete low-speed testing on company money. Hybrid technology is evolving rapidly, but Aurora believes the original design concept is still valid. We have a calibrated design point in a broad trade space. We can look at trades between jetborne and lift-fan power, electrical and fuel energy storage, etc., for a number of different roles, capabilities and concepts of operation, says Clancy. But for the mission the Excalibur was designed for rapid response and survivable weapons delivery it is quite appropriate. The original intent was to focus on high-speed VTOL, but Aurora sees a broad range of missions. Overall, we see high-speed VTOL as an enabling capability for commercial and military markets. Meanwhile, specific power continues to increase, which can only improve the effectiveness of the turbine electric hybrid configuration, says Clancy. We are on the leading edge of a trend toward electric propulsion. It s a real trend, and not a flash in the pan. Find this article at: http://www.aviationweek.com/search/printarticles.do? parameter=printpublicarticles&&pubkey=awst&issuedate=2009-07-20& story=xml/awst_xml/2009/07/20/aw_07_20_2009_p36-154810.xml& headline=aurora Flies Hybrid VTOL UCAV Demonstrator Copyright 2009, AVIATION WEEK, a division of The McGraw-Hill Companies All rights reserved Terms of Use Privacy Notice Contact Us