designing advanced fighter aircraft · aircraft design is a compromise • it is the task of the...
TRANSCRIPT
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DESIGNING ADVANCED FIGHTER AIRCRAFT
Burt Dicht
Director,
University Programs
IEEE
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• Fighter Aircraft Requirements
• The Evolution of Stealth Technology
• The Advanced Tactical Fighter
• The Design Process
• The Future of Aerospace Design
• Opportunities for engineers in Aerospace
• Job Search Strategies
TODAY’S AGENDA
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MY BACKGROUND
NASA Intern
Facilities Design
Kennedy Space Center
Member of Technical Staff
Payload Integration
Rockwell STSD – Space Shuttle
Finance Director
Member of Congress
Lead Engineer
Configuration/Systems Integration
Northrop Grumman
Technical/Business Writer
Words & Ideas
Managing Director
Knowledge & Community
ASME
Director
University Programs
IEEE
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AIR SUPERIORITY FIGHTER REQUIREMENTS
All Aspect Stealth
Maneuverability
Aerodynamics
Range
Engine
Avionics Systems
Armament
Reliability & Maintainability
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THE EVOLUTION OF STEALTH AIRCRAFT
Romulan “Bird of Prey”
• Equipped with “Cloaking Device.”
• Made the craft invisible to
Federation sensors.
• From the earliest days,
deception and stealth have
been used to gain the
advantage over an enemy
in combat.
• The advent of RADAR in
the late 1930’s and during
WWII enabled the early
detection of aircraft in
flight.
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THE EVOLUTION OF STEALTH (cont)
NORTHROP YB-49 BOMBER
• Designed by Jack Northrop
in the late 1940’s.
• Role was as a strategic
bomber.
• Its unique wing shape
produced a low radar cross
section, although the goal
was improved performance.
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THE EVOLUTION OF STEALTH (cont)
DESIGN IN THE 50’S AND 60’S
• Little effort in the 50’s and 60’s.
Integrating low observable
aspects meant compromising
performance – so designers
concentrated on speed,
maneuverability, and weapons.
• A-12/SR-71 has rounded lines,
wing/body blending, conical
center bodies, fuselage chine
and canted twin fins to reduce
radar reflectivity.
Lockheed SR-71 Blackbird
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STEALTH CHARACTERISTICS
• Stealth does not mean “invisible,”
it means “low observable” and can
include:
•Aircraft shape
•Radar Absorbent Material (RAM)
•Minimized engine noise
•Reduced infrared signature
•Electronic countermeasures
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THE FIRST STEALTH AIRCRAFT
F-117A Nighthawk
• USAF and DARPA studies
initiated in 1973 – project
Have Blue
•Air Force invites proposals
to develop technology
prototype
•Lockheed and Northrop were
finalists and each built a
prototype for a “fly-off”
•Lockheed wins production
contract in 1976
Mission – covert reconnaissance
and covert surgical strikes
Subsonic – limited performance
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STEALTH MATURES
• 1980 report concluded that B-1 bomber would be
unable to penetrate Soviet air space beyond 1990
• Positive results from Have Blue (F-117) justified
launch of a full-scale low-observable bomber
program (Advanced Technology Bomber – ATB)
• Lockheed/Rockwell team and a Northrop/Boeing
team responded to requests for proposals
• Northrop relied on experience studying stealth
technology and its extensive experience with
flying wing designs and was awarded the contract
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STEALTH MATURES (cont)
NORTHROP – GRUMMAN
B-2 SPIRIT
• Length – 69ft
• Height – 17ft
• Wingspan – 172 ft
• Max Speed – Mach .85
• Range 6300 nm
• Armament – 40,000 lbs in
internal weapons bays
•Powerplant – four GE F-118-
GE-100 turbofans – 17,300 lbs
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DEVELOPING A TRULY STEALTH FIGHTER
WHY THE NEED?
• Late 1970’s – Soviets building far more fighters than US
• Massive Soviet surface to air missile threat
• USAF looking to technology to counter Soviet numerical
advantage
• In 1981 USAF issued a Request for Information (RFI) for the
Advanced Tactical Fighter (ATF)
• Supercruise (the ability to achieve supersonic flight without
afterburner) and stealth were considered essential components,
although stealth was still considered an exotic technology
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DEVELOPING A TRULY STEALTH FIGHTER
(cont) THE ADVANCED TACTICAL FIGHTER (ATF) PROGRAM
• Air Force opts to build a truly air-to-air fighter to follow the F-15
Eagle air superiority fighter - designed to enter service in mid 90’s
• In 1983 USAF issues Request for Proposals (RFP) for ATF and the
Joint Advanced Fighter Engine (JAFE) – GE and P & W
•Lockheed, Rockwell, Grumman, McDonnell Douglas, General
Dynamics, Boeing and Northrop vie for aircraft contract
• McDonnell Douglas and General Dynamics were thought to have
the inside track because of F-15 and F-16
• But stealth proved to be the deciding factor. Both Northrop and
Lockheed fell back on their stealth experience and proposed
stealthy fighters that could perform as well as non-stealthy fighters
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Most aerospace analysts thought General Dynamics and McDonnell Douglas
had the inside track to win the ATF contract because of the F-16 and F-15.
They were wrong! The designs they proposed were not innovative.
McDonnell Douglas
F-15 Eagle
General Dynamics F-16
Fighting Falcon
Lockheed F-117
Nighthawk
Northrop B-2 Spirit
Lockheed YF-22A Northrop YF-23A
Note: Company
names in 1986.
DEVELOPING A TRULY STEALTH FIGHTER (cont)
INNOVATION WAS THE KEY
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DEVELOPING A TRULY STEALTH FIGHTER
(cont)
THE ADVANCED TACTICAL FIGHTER (ATF) PROGRAM
• In October 1986 the USAF awards the contracts to
build prototype aircraft to Northrop and Lockheed
• Northrop teamed with McDonnell Douglas to build the
YF-23A
• Lockheed - Boeing - General Dynamics comprised the
other team to build the YF-22A.
• Aircraft first flights in the Fall of 1990.
• Lockheed Martin awarded contract in April 1991. More
than 180 F-22s are now in operation.
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JET FIGHTER GENERATIONS
Gen 1 – Earliest jet fighters: Germany’s Me 262, Britain’s Meteor, US F-80.
Hallmark was advance in speed over piston engine aircraft
Gen 2 – Korean War era: USAF F-86 and Soviet MiG-15. Designers maximized
performance by tailoring airframe to jet engine. (Use of swept wings is an
example)
Gen 3 – late 50s early 60s: USAF Century Series F-100, F-101, F-102,
F-104, F-105, F-106 and Soviet MiG-17 and MiG-21. Featured advanced missiles,
supersonic speed and sophisticated engines. F-4 Phantom was late Gen 3 fighter.
Gen 4 – mid 1970s: USAF F-15 and F-16 and Russian Su-27 and MiG-29. Highly
maneuverable, sophisticated weapons, engines and avionics.
Gen 5 – today: all aspect stealth, internal weapons, plug and play electronics and
super-cruise. USAF F-22 operational and F-35 in flight test. Chinese Chengdu J-
20 and Russian Su-T50 in development.
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YF-23A BLACK WIDOW II
• Two Prototypes were built
• PAV 1 - two Pratt & Whitney YF119 engines
• PAV 2 - two GE YF120 engines
•Wing Span 43.6 ft
•Length 67.4 ft
•Height 13.9 ft
•Wing area 900 sq. ft.
•Top Speed Mach 2+
•Range 800 Nm
•Altitude 65,000 ft
•Air Superiority
•Low Observable
•Super-cruise - mach
1+ without afterburner
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Northrop Chief Test Pilot Paul Metz comments on the YF-23A – YouTube Video:
http://youtu.be/nA718zigtzE
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NORTHROP GRUMMAN AN AIRFRAME
MANUFACTURER
• Responsible for the design,
manufacture and integration of aircraft
and aircraft sub-assemblies
Boeing (McDonnell Douglas/Northrop)
F/A-18F Super Hornet
F/A-18 Carrier
Takeoff
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AIRCRAFT DESIGN PROCESS
Customer Requirements
Mission • Range • Weapons • Weight • Fuel
• Lifecycle Cost
Conceptual Design Phase
General size and configuration of the
aircraft • aerodynamic studies • thrust loading •
wing loading • wing sweep • general body, wing and
tail configurations
Preliminary Design Phase
Best conceptual design is chosen for testing • inlet/engine/airframe
integration • major loads and stresses • weight • stability and control • internal arrangement
Detailed Design Phase
Configuration frozen • Detailed structural design • Detailed system design and installation • avionics, flight control and weapons
integration • Production drawings
Development Phase
Manufacturing, assembly and test
1 – 2
years
1 – 3
years
2 – 3
years
2 – 4
years
2 – 4+
years
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AIRCRAFT ENGINEERING
GROUPS
• Aerodynamics
• Advanced Design
• Armament
• Avionics (airborne electronics)
• Crew Station (cockpit)
• ECS (environmental control system)
• Electrical
• Flight Test
• Fuel Systems
• Hydraulic Systems
• Propulsion Integration (engines)
• Reliability and Maintainability
• Safety
• Structures
• Vehicle Management (flight control)
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CONFIGURATION/ SYSTEMS
INTEGRATION
• Responsible for overall internal and external systems arrangement
• Work with every design group and coordinate and integrate their designs into a single aircraft design
• Final Product:
Inboard Profile Drawing • Aperture Arrangement • Three Views • Zone Drawings
F-20A Tigershark
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AIRCRAFT DESIGN IS A COMPROMISE
• It is the task of the aircraft design engineer
to balance the customer requirements with
the physical constraints, cost and time-
scale, in order to produce the most
effective aircraft possible.
• Aircraft Design Requires Teamwork
• No “one” design group is more important
than the others.
• Note: All Engineering involves
Compromises!
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ENGINEERING FUNCTION
DESCRIPTIONS • Design - From Concept to Production
o Good understanding of engineering principles
o See things in 3-D (Geometry, Graphics, Kinematics)
o Like to solve problems, come up with better ways of doing things
• Analysis - Verify engineering designs (Stress, Thermal, Aerodynamics, Dynamics) o Engineering Theory and Mathematics
o Problem solving
• Test - Verify functionality of design o Basic understanding of engineering theory and design principles
o Lab work and strict guidelines and procedures
• Operations- Maintaining and operating final product o Basic understanding of engineering design and systems
o Understand how and why things work
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AN AEROSPACE CAREER
STS 26 Landing
Edwards Air Force Base (EAFB)
October 3, 1988
Northrop – Lockheed Open House - EAFB
November 1990
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LOCKHEED
MARTIN F-22A
RAPTOR
•Wing Span 44.5 ft
•Length 62 ft 1 in
•Wing area 830 sq. ft.
•Top Speed Mach 2+
•Range 800 Nm
•Altitude 65,000 ft
•Air Superiority
•Low Observable
•Two Pratt & Whitney
F119-PW-100 Turbofans
@ 35,000 lbs
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Northrop Grumman X-47B Pegasus Unmanned Combat Air System Demonstrator (UCAS-D).
THE FUTURE: REMOTELY PILOTED VEHICLES
Future Concepts: Hypersonic
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Lockheed Martin SR-72
THE FUTURE: HYPERSONIC
DARPA Hypersonic Technology Vehicle (HTV)
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Lockheed Martin
Orion
Boeing CST-100
Spacecraft
Space X Dragon
The Boeing CST and the Dragon will be used to ferry astronauts to low Earth orbit (LEO). The Orion is designed for deep-space, including missions to the moon, Mars and asteroids. All are designed to be reusable.
THE FUTURE: SPACECRAFT CONCEPTS
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The SPACE LAUNCH SYSTEM (SLS)
Initial Lift Capability - 150,000 lbs
More than Double any Operational Vehicle
Today
Propulsion
Two Solid Rocket Boosters, 1 J-2X engine for
the upper stage and 4 RS-25 engines (SSME)
on the core booster
Evolved Lift Capability - 280,000 lbs
More than Any Past, Present, or Future
Vehicle
Propulsion
Two Advanced Solid Rocket Boosters, 2 J-
2X engines for the upper stage and 4 RS-
25 engines (SSME) on the core booster
THE FUTURE: SPACE LAUNCH SYSTEM (SLS)
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Biconic Space Vehicle - Blue
Origin (Designed to
take astronauts to LEO)
Sierra Nevada Dream Chaser (Designed to
carry 7 astronauts to
LEO)
Virgin Galactic – Spaceship
Two (Designed for space
tourism on sub-orbital flights)
The Future of Space Technology:
Commercial Space Projects in
Development
XCOR Lynx Spaceship Two (Designed for space tourism on sub-orbital
flights)
THE FUTURE: COMMERCIAL SPACE PROJECTS
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BUREAU OF LABOR STATISTICS - JOB OUTLOOK
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Employment Change 2010 – 2020
• Aerospace engineers held about 81,000 jobs in 2010. • Aerospace engineers are expected to have 5 percent growth in employment over the projections decade, slower than average for all occupations.
• Mechanical engineers held about 243,200 jobs in 2010.
• Mechanical engineers are projected to have 9 percent employment growth over
the projections decade, slower than the average for all occupations.
• Electrical and electronics engineers held about 294,000 jobs in 2010.
• Electrical and electronics engineers are expected to have employment growth of
6 percent over the projections decade, slower than the average for all occupations.
• Computer hardware engineers held about 70,000 jobs in 2010.
• Computer hardware engineers are expected to have employment growth of 9%
over the projections decade, slower than the average for all occupations.
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STARTING SALARIES
• Average starting salary for Bachelor’s degree candidates
in aerospace engineering is $64,000 a year. (2013)
• Average starting salary for Bachelor’s degree candidates
in mechanical engineering is $62,800 a year. (2013)
• Average starting salary for Bachelor’s degree candidates
in electrical engineering is $62,200 a year (2013)
• Average starting salary for all entry level engineers is
$60,291per year (2013)
• Note: Salaries will vary depending on industry and
location
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REQUIRED COMPETENCIES FOR TODAY’S ENGINEERS
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Technical excellence
Communication skills
Creativity
Innovation
Critical thinking
Skill in interpersonal interactions
Multiple languages
Ability to define a vision
Attitude of seizing opportunities
A positive thinker and a decision maker
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JOB SEARCH STRATEGIES
• Know Yourself: What do you like to do? What kind of work do you
want to do? Where do you want to work?
• You need to STAND OUT in the crowd: What are your special
skills and talents? What are your significant achievements? How can
your skills help the company?
• Develop Your Brand: Develop your two-minute pitch. Use Targeted
Resumes and Cover Letters. Use social networking like LinkedIn,
Facebook, etc.
• Target Your Search: Conduct research on industries and
companies that interest you.
• Finding the Opportunities: Use multiple methods . . . Campus
Career Services, On-Campus Recruiting, Career Fairs, Online Job-
Boards, Company Websites, Professional Associations, Social
Networks and your Network
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Aerospace Web Sites
• Bureau of Labor Statistics
http://www.bls.gov/
http://www.bls.gov/ooh/home.htm
Occupational Outlook Handbook, 2012-13 Edition
• Aircraft Design Sites
http://www.aircraftdesign.com/other.html
• Aerospace Industries Association – sign up for AIA Update http://www.aia-aerospace.org/
• Aerospace Mall - A directory of many aerospace/aviation related
companies (From airframe to suppliers, from military to general
aviation)
http://www.aerospacemall.com/
• Internships
http://www.Tech-Interns.com
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Reading List
• Car Guys versus Bean Counters – by Bob Lutz
• 747: Creating the World’s First Jumbo Jet and Other
Adventures from My Life in Aviation – by Joe Sutter
• Flight: My Life in Mission Control – by Christopher Kraft
• Steve Jobs - by Walter Issacson
• A Fiery Peace in a Cold War: Bernard Schriever and the
Ultimate Weapon - by Neil Sheehan
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For More Information
Burt Dicht, Director
University Programs, IEEE
445 Hoes Lane
Piscataway, NJ 08854
732-981-3419
www.ieee.org/education