26
Eurofighter GmbH Am Soeldnermoos 17 D - 85399 Hallbergmoos Germany Telephone +49 811 80 0 Fax +49 811 80 1557 E-mail [email protected] www.eurofighter.com
Eurofighter GmbH
Am Soeldnermoos 17
D - 85399 Hallbergmoos
Germany
Telephone +49 811 80 0
Fax +49 811 80 1557
E-mail [email protected]
www.eurofighter.com
0100
Eurofighter Typhoon is a highly agile Air Superiority and
Air-to-Surface, multi-role/swing-role weapon system.
Entering service in 2002 with the four partner nations –
Germany, Italy, Spain and the United Kingdom, it is the
most capable front line fighter available.
The collective military requirements of the four partner
nations are the foundation of the Eurofighter Typhoon
Weapon System. This provides a comprehensive and
flexible capability that will meet the demands of many
nations over the next half century. Each aspect of
the Eurofighter Typhoon is designed to provide a
balanced contribution to the overall effectiveness of
the Weapon System:
◆ Passive sensors, low radar signature, andsupercruise capability for low detectability
◆ Integrated sensors and data fusion, for pilotsituation awareness and low cockpit workload
◆ High supersonic performance for superior Beyond Visual Range (BVR) combat capability
◆ Carefree agility, Advanced Short-Range Air-to-AirMissile, Helmet Mounted Display (HMD), for excellentWithin Visual Range (WVR) combat capability
◆ Extensive weapons/stores inventory which includes effective long and short-range weapons for successful Air-to-Surface operations
◆ Automated and mission-tailored defensive aids for high survivability
◆ Designed for growth
Introduction 01
General Characteristics 05
Operational Capabilities 11
Avionics and Sensors 25
Main Aircraft Systems 33
Integrated Logistics Support 39
Data 43
Organisation and Structure 45
Glossary 47
Introduction
Pilot FriendlyThe cockpit and Human Machine Interface (HMI) have been
defined and fully tested to provide low pilot workload even
in the most adverse mission and threat scenarios predicted.
The cockpit is spacious, and the displays show the pilot:
What is needed, when it is needed, simply and clearly.
Other features such as Direct Voice Input/Output associated
with Hands On Throttle And Stick control functionality
have been implemented on the Eurofighter Typhoon to
drastically reduce the pilot’s workload. VTAS enables
single-seat operations even in the most demanding Air-to-Air,
Air-to-Surface, and swing-role missions.
Voice Throttle And Stick (VTAS) system= Low pilot workload
Total PerformanceReliability, Maintainability and Testability have been given
equal priority to flight safety, effectiveness and performance.
This reduces cost of ownership throughout the life cycle,
delivering a highly affordable solution.
Continuous Growth ProgrammeEurofighter Typhoon at the beginning of its life as a next
generation fighter offers exceptional capability at entry
into service. Through capability enhancement and a proven
technology insertion plan, Eurofighter is designed to
meet future operational requirements that will maintain
its operational dominance well into the 21st century.
0302
All of these characteristics contribute to a balanced weapon
system for maximum effectiveness in a dense and complex
threat scenario. The multi-role/swing-role Eurofighter Typhoon
allows a single-tier air force structure with dramatic reductions
in costs and with the opportunity for commonality and
interoperability on a worldwide scale.
AgilityDue to its foreplane/delta low drag configuration and high
thrust-to-weight ratio, Eurofighter Typhoon exhibits
exceptional acceleration, instantaneous and sustained turn
rate performance both subsonic and supersonic, coupled
with excellent airfield performance.
Using the latest control technology with a high degree
of aerodynamic instability, and by extensive use of carbon
composite, the resulting airframe and engine are some
10-20% smaller and 30% lighter than its predecessors.
High thrust / weight + Low wing loading = Agility
Agility+ Integrated avionics = Combat superiority
Introduction
05
Eurofighter Typhoon has a foreplane/delta wing configuration
that is aerodynamically unstable. This gives the aircraft
advantages in:◆ Agility ◆ Supersonic performance
◆ Reduced drag ◆ Lift and STOL performance
Wingspan 10.95m (35ft 11in) Height 5.28m (17ft 4in)
Length Overall 15.96m (52ft 4in)
Wing Area 50.0m2 (538ft2)
04
General Characteristics
0706
Materials Surface AreaCFC 70%
GRP 12%
Metal 15%
Other 3%
Carbon Fibre Composites (CFC)
Glass Reinforced Plastic (GRP)
Aluminium Alloy
Titanium Alloy
Acrylic (ROHM 249)
General Characteristics
MassBasic Mass Empty 11,150 kg (24,582 lb)
Maximum Take-Off 23,500 kg (51,809 lb)
Maximum external load 7,500 kg (16,535 lb)
Design CharacteristicsSingle seat twin-engine, with a two-seat variant
Weapon Carriage 13 Hardpoints
G’ limits +9/-3 ‘g’
In-service life 25 years/6,000 Flying Hours*
Power Plants Two Eurojet EJ200 reheated turbofans max dry thrust class 60 kN (13,500 lb) max reheat thrust class 90 kN (20,000 lb)
Supercruise capability
*Based on demanding and realistic mission profiles
General Performance Characteristicswith a full Air-to-Air Missile FitCeiling > 55,000 ft
Brakes off to 35,000 ft / M1.5 < 2.5 minutes
Brakes off to lift off < 8 seconds
At low level, 200Kts to Mach 1.0 in 30 seconds
Maximum Speed Mach 2.0
Operational Runway Length < 700 m (2,297 ft)
Eurofighter Typhoon is both light and strong
based on adoption of modern construction and
manufacturing technology combined with
the use of advanced materials and
assembly techniques.
Utilities System◆ Integrated digital
system featuring seven distributed processors and a dual-redundant databus
◆ High fleet availability◆ Reduced pilot workload
Designed for Growth◆ Solid air-vehicle design◆ Highly adaptable platform◆ Planned technology insertion
Data Link◆ High-capacity secure digital information
distribution system
Sensor Fusion◆ Presents the pilot with a unified picture
of the world outside◆ Pilot concentrates on the fight not on the flight◆ Reduced pilot workload
Swing-Role◆ Rapid transition between Air-to-Air
and Air-to-Surface moding◆ Can always carry at least five Air-to-Air missiles
Low Observability◆ Airframe shaping absorbent materials and coatings◆ Hidden engine compressor faces◆ Supercruise capability◆ Semi-conformal carriage of BVRAAM missiles◆ Passive electro-optic sensors◆ Secure communications
0908
The Performance to Get the Job Done
Propulsion System◆ Twin-engine for safety and system redundancies◆ Excellent thrust-to-weight ratio◆ Supercruise capability◆ Low fuel consumption
Cockpit / HMI◆ Excellent all-round vision◆ Full glass cockpit◆ Helmet display and VTAS◆ High level of integration and automation
Air Intake◆ Chin location◆ High Performance at high angles
of attack/sideslip
Radar◆ Multi-role, multi-mode CAPTOR radar◆ Very high power◆ Extensive search and track volume◆ Highest performing type of its class
Avionics System◆ Highly integrated system◆ Modular technology◆ Rapid access to the overall tactical situation
Flight Control System◆ Carefree handling◆ Artificial stabilisation◆ Quadruplex digital Fly-By-Wire system
General Characteristics
Defensive Aids◆ Internally housed◆ All round prioritised
assessment◆ Fully automatic
response to singleor multiple threats
IRST / FLIR◆ Passive Air-to-Air target detection
and tracking for covert operation◆ Target acquisition and identification◆ Low level night navigation
Weapons Carriage◆ Maximum operational flexibility
and combat persistence◆ 13 well-spaced hardpoints◆ Internally mounted 27mm Mauser gun◆ Low drag and radar cross-sections◆ Semi-conformal BVRAAM missile carriage
1100
Multi-Role and Swing-RoleThe Eurofighter Typhoon can undertake all the following
missions and roles:
◆ Air Superiority
◆ Air-to-Surface
(including Air Interdiction, Close Air Support, Maritime
Attack, Suppression and Destruction of Enemy
Air Defences)
◆ Reconnaissance
Due to the flexibility of the design, future missions and
roles can be readily accommodated. This flexibility is based
on advanced avionics, sensors and weapon integration
techniques that are unique to this aircraft. Eurofighter
Typhoon is a genuine swing-role aircraft, with the ability to
carry out several roles during a mission, shifting between
Air-to-Surface and Air-to-Air roles. One aircraft for all
missions reducing costs, increasing effectiveness and
enhancing interoperability with allied Air Forces.
Air SuperiorityAir Superiority fighters have to be extremely agile in order
to meet the increasingly demanding requirements of
supersonic Beyond Visual Range (BVR) combat and
subsonic Within Visual Range (WVR) combat.
First Look First Shoot First Kill
Operational Capabilities
10
Design drivers for BVR combat Eurofighter Typhoon featuresLong range sensors CAPTOR Radar, MIDS, IRST, DASS
High specific excess power low drag EJ200 engines to accelerate to Mach 2.0
Supersonic sustained turn rate and agility Excellent aerodynamic and engine performance
Low detectability Low observability, MIDS, IRST
Combat persistence Excellent aerodynamic/engine performance and fuel capacity. Weapon load: minimum 4 BVRAAM (Meteor or AMRAAM)
Defensive aids Fully integrated Defensive Aids Sub System (DASS)
Human machine interface Highly integrated sensor suite and a sophisticated cockpit for pilot carefree handling
InterceptFlyout speed
Radius of action
Detect Target
Ground Control Intercept
& Combat
Air Patrol
Evade CounterfireDetect threat
missiles
Turn away/to beam/across
Accelerate to outrun threats
Dive to reduce missile range
Defensive aids to defeat missile
Re-engagementRegain energy
Turn and re-acquire opponents
Post LaunchEscape
manoeuveringand mid-course
guidance
LaunchMulti-targeting
ApproachGain energy
Identify and sort targets
Tactical manoeuvre
Deny situational awareness to
threat
2 3 4
5
67
1
1312
Beyond Visual Range (BVR)The BVR combat philosophy is characterised by the synergy
of a number of weapon system characteristics giving
Eurofighter Typhoon exceptional combat effectiveness; these
are, primarily, flight performance, weapons, sensors range,
and detectability.
Overview of BVR combat
Operational Capabilities
1514
Comparison of key BVR combat parameters
Comparison of key WVR combat parameters
Within Visual Range (WVR)Within Visual Range (WVR) – Eurofighter Typhoon’s airframe
and engine agility will be complemented by its systems’
agility, with features such as excellent cockpit view, highly
capable off-boresight Helmet Mounted Display (HMD)
system, advanced VTAS technology, and state-of-the-art
short-range missiles. The advanced ‘g’-protection system
ensures that the pilot can operate comfortably in a relaxed
‘g’ environment under prolonged agile manoeuvring at 9 ‘g’.
Radar Range
EurofighterTyphoon
High EndLegacyFighter
vs
SustainedTurn Rate
Acceleration
Stealth
Persistence
MaximumFirepower
20406080100%
Radar Range
EurofighterTyphoon
EvolvedLegacyFighter
vs
SustainedTurn Rate
Acceleration
Stealth
Persistence
MaximumFirepower
20406080100%
Radar Range
EurofighterTyphoon
High EndThreatvs
SustainedTurn Rate
Acceleration
Stealth
Persistence
MaximumFirepower
20406080100%
Radar Range
EurofighterTyphoon
Other 4thGenerationFighter
vs
SustainedTurn Rate
Acceleration
Stealth
Persistence
MaximumFirepower
20406080100%
EurofighterTyphoon
High EndLegacyFighter
vs
Agility
SustainedTurn Rate
Acceleration
InstantaneousTurn Rate
Persistence
20406080100%
EurofighterTyphoon
EvolvedLegacyFighter
vs
Agility
SustainedTurn Rate
Acceleration
InstantaneousTurn Rate
Persistence
20406080100%
EurofighterTyphoon
High EndThreatvs
Agility
SustainedTurn Rate
Acceleration
InstantaneousTurn Rate
Persistence
20406080100%
EurofighterTyphoon
Other 4thGenerationFighter
vs
Agility
SustainedTurn Rate
Acceleration
InstantaneousTurn Rate
Persistence
20406080100%
Operational Capabilities
1716
One Aircraft Any MissionEurofighter Typhoon provides a diverse range of
options for all Air-to-Air and Air-to-Surface operations.
Customer Choice◆ 3 choices of SRAAM
◆ 2 choices of BVRAAM
◆ 2 choices of ARM (Anti-Radiation Missiles)
◆ 2 choices of Cruise Missiles
◆ 2 choices of Anti-Ship Missiles
◆ 2 choices of Mobile Target Missiles
◆ 3 choices of FF & Retarded bombs
Operational Capabilities
SIDEW
INDER
ASRA
AM
IRIS
-T10
00L
FUEL
TA
NK
27m
m M
AU
SE
R
LDP
RE
CC
E P
OD
MK
80 SE
RIE
S
2000L FUE
L TAN
K
AM
RA
AM
METEO
R
JSOW
JASSM
HARM
ALARM
TAUR
US
GB
U 10/16 PAV
EW
AY II
GB
U 24B
/24AB
/24UK
PAVEWAY
III
UK
100
0lb
BO
MB
GB
U 3
2 JD
AM
CLU
STE
R B
OM
BS
CB
LS-2
00
BR
IMS
TON
E
STO
RM
SH
ADO
WNSM
HARPOON
MAV
ERIC
K
AIR C
OMBAT TRAIN
ING P
OD
1918
Interdiction/Strike
Air Superiority
Suppression and Destruction
of Enemy Air Defences
Close Air Support
Multi-Role/Swing-Role
Maritime Attack
6 BVRAAM
2 SRAAM
27mm Mauser
2x2000L+1x1000Lor 3x1000L Fuel Tanks
2 Cruise Missiles
4 BVRAAM
2 SRAAM
27mm Mauser
2x2000L+1x1000LFuel Tanks
6 ARM
4 BVRAAM
2 SRAAM
27mm Mauser
1x1000L Fuel Tank
2 GBU 24 Paveway lll
2 ARM
3 BVRAAM
2 SRAAM
27mm Mauser
1 LDP
2x2000L+1x1000L Fuel Tanks
18 Brimstone
4 BVRAAM
2 SRAAM
27mm Mauser
1x1000L Fuel Tank
6 Anti-ship Missiles
4 BVRAAM
2 SRAAM
27mm Mauser
1x1000L Fuel Tank
Unmatched Capability
Operational Capabilities
Day 1 Day 2
Days of combat versus a Sophisticated Air Threat
Num
ber
of
Airc
raft
Day 3 Day 4 Day 5 Day 6
EurofighterTyphoon
Less CapableAircraft
Fleet EffectivenessFewer Eurofighter Typhoons are required to achieve the
same level of operational effectiveness, and with far fewer
losses when compared to a larger fleet of less capable
aircraft. This reduces both direct and indirect cost and
manpower levels.
Based on EADS Operational Simulation Analysis Tool
Comparison of the loss rate of a fleet of Eurofighter Typhoon with
a larger fleet of a less capable aircraft, versus an aggressor force,
in a typical high intensity scenario.
Eurofighter Typhoon wins and survives
2120
Continuous Enhancementsfor Future DemandsEurofighter Typhoon is designed to maintain operational
dominance well into the 21st century. At present the
enhancement and technology insertion is focused on the
following capabilities:
System of Systems◆ Interoperability
◆ Communications
◆ Wide Band Data Links, including imagery
◆ Reconnaissance
◆ Exploitation of Intelligence Surveillance Target Acquisition and Reconnaissance (ISTAR) assets
Reach◆ Conformal fuel tanks
◆ Larger external tanks
◆ Improved engine efficiency
Precision Attack◆ Increased Weapon inventory
◆ Enhanced Nav/Attack sensors
◆ Improved target detection/ identification
◆ Air Superiority
◆ Thrust vectoring and thrust increase up to 20%
Operational Capabilities
Combat Simulation
2322
Survivability◆ Advanced DASS
◆ Stand-off capability
◆ Signature reduction (engine, airframe and RF)
◆ Covert terrain following
◆ Improved co-ordination and safety with friendly forces
Human Machine Interface◆ Improved helmet display leading to HUD removal
◆ 3D Audio for immediate spatial perception of threats
◆ Increased DVI control envelope and vocabulary
Affordability◆ Increased Robustness
◆ Enhanced Maintenance and Field Support
◆ Open architecture to facilitate technology insertion
Deployability◆ Minimised logistic footprint
◆ Improved availability
Operational Capabilities
2524
The Avionics System has been designed to ensure that
the pilot is presented with all the information needed in
the cockpit, at all stages of flight. The solution – a highly
distributed computing capability linked by high-speed
conventional (MIL-STD-1553, MIL-STD-1760B) and
fibre-optic databuses (STANAG 3910) will further evolve
to make maximum use of the rapid developments in
computing power.
Sensor Fusion The heart of the system is the Sensor Fusion that
processes the information received by the main aircraft
sensors. This information is correlated and presented clearly
to the pilot to allow safe and efficient single seat operation
in the swing-role environment. The high level of integration
and sharing of information between the sub-systems gives
the pilot an autonomous ability to assess rapidly the overall
tactical situation and respond efficiently to threats.
Multifunction Information
and Distribution System
Sub-System
Defensive Aids
Identification
Friend/Foe
Search andTr
ack
Infra-R
ed
Rad
arS
yste
ms
MIDS
IFF
IRSTD
ASS
RA
DA
R
Avionics and Sensors
2726
Individual Sensors
RadarThe CAPTOR Radar is the best performing type of its class.
This multi-mode pulse-Doppler Radar is the first airborne
Radar in NATO with three as opposed to two processing
channels. The third channel is used in a jamming scenario
for sidelobe nulling, interference blanking and jammer
classification.
The Radar provides Air-to-Air and Air-to-Surface features.
Main Air-to-Air features◆ Search Modes – Range While Search (RWS), Velocity
Search (VS) and multiple target Track While Scan (TWS)
◆ Lock-Follow Modes, which are tailored for long range
tracking and short range tracking for use in visual
identification or gun attacks
◆ Air Combat Acquisition Modes allowing a choice of
boresight, vertical scan HUD field of view or slaved
acquisition
Main Air-to-Surface features ◆ Search Modes – Ground Map, High Resolution Map,
Ground Moving Target Identification and Sea Surface
Search and Track While Scan
◆ Track Modes – Fixed Target Track and Moving Target Track
◆ Air-to-Surface Ranging
◆ Terrain Avoidance
IRST – Infra-Red Search and Track The PIRATE IR sensor provides the Avionics System with
more information but in a frequency band complementary
to that of the radar. Passive Air-to-Air target detection and
tracking performance in the IRST mode provides totally
covert-tracking capabilities. PIRATE also fully supports
Air-to-Surface operations in the Forward Looking Infra-Red
(FLIR) mode, with ground and target imagery as required
during operations where passive operations are also needed.
DASS – Defensive Aids Sub-System The DASS monitors and responds to the outside world.
It is installed internally and provides the pilot with all-round
prioritised assessment of Air-to-Air and Surface-to-Air
threats, with fully automatic response to multiple threats;
manual override is available. Space and computing power
expansions will house continuous evolution for future
threats, enhance Eurofighter Typhoon’s survivability and
greatly increase overall mission effectiveness.
Wing tip ESM/ECM pods
Wing tip ESM/ECM pods
Chaff dispenser
Front missile warner
Front missile warner
Laser warner
Laser warner
Chaff dispenser
Flare dispenser
Flare dispenser
Rear missile warner
Towed decoy
Avionics and Sensors
2928
Navigation Features
Automatic Terrain Following Eurofighter Typhoon allows automated and inherently
covert operation down to 100ft. Integrated lateral cueing
and vertical commands allow safe manoeuvre with 3D
situational awareness.
Navigation Aids ◆ Global Positioning System (GPS) for full digital interface
with individual satellite tracking channels
◆ Improved anti-jam capabilities
◆ Inertial Navigation System (INS) with GPS
Landing Aids ◆ Instrumented Landing System – ILS
◆ Microwave Landing System (MLS) area Navigation
◆ Differential Global Navigation Satellite System operation
Communications◆ Electronic Counter Measures (ECM) resistant with
secure and non-secure UHF and VHF dual redundancy
◆ A reversionary control facility is provided
MIDS – Multifunction Information and Distribution System MIDS is a communication system that allows all the elements
– where Eurofighter Typhoon is one – of a command and
control system to share the same information, and contribute
data whenever required. Over huge ranges, and in any
direction, the Eurofighter Typhoon pilot can listen to, and see,
all the data known on friendly and enemy forces, airfields,
command decisions or mission changes. Eurofighter
Typhoon will have the capacity to absorb all of this, analyse
it, fuse it and remain the most effective platform for present
and future swing-role operations.
Electro-Optic Targeting System Autonomous operations for Eurofighter Typhoon will be
greatly enhanced by the addition of on-board target
detection, recognition and identification, using the latest
technology EO sensors complemented by on-board laser
tracking supporting target designation for self or third party
operations. Future generations of targeting and tracking
sensors will be readily integrated into Eurofighter Typhoon
through the evolving avionics and weapon system
architecture. As with the IRST/FLIR, multi-spectral
operations will be key to future operational capability.
AutopilotThe Eurofighter Typhoon autopilot is designed for both
cruising and to free the pilot in tactical situations. The
autopilot provides basic track, heading, altitude and airspeed
modes, and allows the pilot to fly optimum attack profiles
automatically. In fact, advanced modes such as auto-climb,
auto-attack, and auto-approach are available. The autopilot
is an integrated part of the pilot’s tactical control.
Avionics and Sensors
Mk.16A Ejection Seat The Mk.16A is a solid state ejection seat which offers
high comfort levels, and is integrated with an On-Board
Oxygen Generation System, chemical defence, and
communication systems.
General FeaturesFive major display surfaces: 3 Multi-function Head Down
Displays (MHDD), a Head-Up Display (HUD) and a Helmet
Mounted Display (HMD), provide the pilot with all the
tactical information he needs for all stages of his mission.
Night Vision Enhancement (NVE) devices are an integral part
of the full HMD. Voice, Throttle And Stick (VTAS) technology
gives the pilot optimum intuitive controls and enhances the
efficiency of the single seat operation.
3130
Cockpit At all stages of the design of the Eurofighter Typhoon
cockpit, the needs of the single-seat pilot have been
paramount. High workload situations have been analysed
to establish priorities and to automate tasks. The priorities
of head-in and head-out operations were established,
and displays and moding designed, such that only the
necessary information is presented to the pilot.
Life Support System and Aircrew EquipmentAssembly (AEA)The life support system provides pressure breathing and
‘g’-protection so that ‘pilot-straining’ is not necessary under
high ‘g’-force.
Avionics and Sensors
3332
The PowerplantTwin EnginesEurofighter Typhoon is equipped with twin EJ200 engines
to increase safety in peacetime and redundancy in war.
The high reliability and subsequent availability ensure
operational costs are reduced.
Design PrioritiesThe EUROJET team achieved the following design priorities:
◆ Air-to-Air combat superiority
◆ High-speed interception
◆ High performance in dry and reheat operation,
including supercruise capability in maximum dry
◆ Carefree handling throughout an extensive flight envelope
◆ Growth potential
Main CharacteristicsThe overall design provides a small lightweight engine with high strength and high temperature capability.
◆ Digital Electronic Control Unit (DECU)
◆ Bypass ratio 0.4
◆ Overall pressure ratio 26:1
◆ Thrust / Weight ratio 10:1
◆ Overall length 4m (157 in)
◆ Inlet diameter 0.74m (29 in)
Main Aircraft Systems
3534
Flight Control SystemThe FCS is a full authority, quadruplex digital Fly-by-WireSystem that provides:◆ Stability and control augmentation
◆ Excellent handling characteristics
◆ High agility
◆ Carefree handling/manoeuvring
It is designed to enable the pilot to concentrate on the tactical
tasks and to fly the aircraft ‘head-up’ in combination with the
HOTAS concept applied to cockpit design. Emergency
features have been also embodied in the system design to
ensure maximum safety of operation. These include:◆ Low speed auto recovery
◆ Emergency ‘g’ override
◆ ‘g’ onset limitation
◆ Dis-Orientation Recovery Capability (DORC)
◆ Automatic reversion
The system is designed to provide the necessary
measurement (Air Data System) computation and surface
actuation required to perform all required manoeuvres
ensuring carefree handling and manoeuvring capabilities.
The System is also designed to provide higher mode
functionalities including:◆ Autopilot
◆ Auto-throttle
◆ Flight Director Modes
The System is controlled by four Flight Control Computers
and features primary and secondary actuation to ensure
control along all axis (pitch, roll and yaw). The aerodynamic
configuration is automatically trimmed to achieve an optimum
compromise between performance and manoeuvrability.
Built-in Growth PotentialA first stage of planned engine growth, changes in the
pressure rating, fan and core engine technology will produce
a 25% increase in dry power and a 10% increase in reheat
power. This performance improvement may also be traded
off to extend engine life up to 30% maintaining present
performances. Such trade off will be possible through DECU
settings to fully exploit the advantages of the improved
design in line with Operational Requirements. Further engine
growth is also envisaged, with further increases in pressure
and an upgraded engine core to produce additional power
with and without reheat.
5 Stages HighPressure RatioCompressor (HPC)
3 StagesLow Pressure RatioCompressor (LPC)
Digital ElectronicControl Unit (DECU)
Anular Combustion Chambertechnology
Highly efficient reheat system
Convergent/Divergentadapted Nozzle
Main Aircraft Systems
Single Stage HighPressure Turbine andSingle Stage Low TurbinePressure
3736
Primary control surfaces
Secondary control surfaces
Pitch control is provided by symmetric operation of
foreplanes and wing flaperons, while roll control is primarily
achieved through differential operation of wing flaperons.
Yaw control is primarily provided by the fin mounted rudder.
Cross feeds among the various actuation systems are
also implemented to optimise aircraft performance and
handling qualities.
The FCS also features automatic reversion through various
back-up modes. It is integrated with other systems through
the avionics (STANAG 3910) and utility control (STANAG 3838)
data buses.
Utilities Control SystemThe Utilities Control System (UCS) is integrated within the
overall system architecture. It provides continuous control
monitoring and faults detection for Eurofighter Typhoon
general systems reducing pilot workload and increasing
fleet availability.
Other Systems◆ Secondary Power System (SPS)
◆ Hydraulic System
◆ Fuel System
◆ Electrical Power Generation System
◆ Environmental Control System (ECS)
◆ Integrated Monitoring and Recording System (IMRS)
◆ Landing Gear System
◆ Fire Protection System
◆ External Lighting System
◆ Ice Detection and Protection System
Rudder
Outboard flaperon
Inboard flaperon
Leading edge slats
Nose wheel steering
Foreplane
Air intake vary cowl
Main Aircraft Systems
3938
To reverse the trend of ever increasing through-life support
costs, and to demonstrate absolute commitment to cost of
ownership, Industry was contracted to give equal priority
to Operational Performance and Integrated Logistic Support
from the outset of the programme.
This holistic approach to the operation and support of
the total weapon system has resulted in an aircraft that
demonstrates and surpasses all previous maintenance
expectations.
Swing-role capability coupled with unprecedented reliability,
low levels of maintenance and a vastly reduced logistics tail,
enhance aircraft availability and lethality and permit rapid
deployment worldwide.
Re
liability
Maintainability
Support System
Training
Test
abili
ty
LO
W
C
OS
TO F O W
NE
RS
HI
P
HI
GH
AV A I L A
BI
LI
TY
Integrated Logistics Support
4140
Key Aspects of the Eurofighter TyphoonTotal Weapon SystemIntegrated Logistics Support:
SupportabilityThe extensive use of prognostic and Built-In Test equipmentand high weapon system reliability, together with a lowrequirement for scheduled maintenance has reducedmaintenance man-hours to less than half that required onother combat aircraft in-service.
AvailabilityHigh inherent Reliability and Maintainability, coupled withrapid turnaround times, and ease of deployment, result inconsistent high levels of operational readiness.
AffordabilityLife cycle costs are minimised by flexible cost-effectivesupport solutions tailored to the needs and existinginventory of an individual Air Force.
Weapon System Operational SupportEurofighter Typhoon operators are given access andinvolvement in the enhancement of the weapon systemthrough membership of the International Weapon SystemSupport System (IWSSS) and the associated in-countryNational Support Centre. Membership of the IWSSS offersall Eurofighter Typhoon nations the unique opportunity to have a permanent presence within the central Air Force/Industry management organisation.
TrainingEurofighter Typhoon has an extremely comprehensive suiteof aircrew and ground-crew training aids ranging fromcomputer based training classrooms to integrated linked Full Mission Simulators. This allows air forces to achieve upto 30% combat-ready training in a synthetic environment.
Ground OperationsThe aircraft implementation of advanced built-in test anddiagnostic features into the aircraft has substantially reducedthe number of Ground Support Equipment (GSE) compared to previous aircraft. The remaining suite of state-of-the-art GSE was developed according to the same stringent standardsas the aircraft, thus ensuring performance and reliability.Depending on the needs of an individual Air Force, off-aircraftequipment maintenance can be supported with a full suite ofGSE or through cost-effective industrial support arrangements.
Ground Support SystemThe Ground Support System (GSS) gives all operators aleading edge mission and engineering data management,which provides rapid seamless bi-directional data flow fromthe operational and maintenance centres to the aircraft andback. The GSS is linked to the National Support Centre and Industry, thus facilitating continuous on-line data andintelligence transfer.
Technical Publications Technical publications have been developed as structureddata modules allowing rapid adaptation to the needs of an individual Air Force and forming the basis of a paperlesscockpit and paperless maintenance environment.
Deployment CapabilityFrom the outset Eurofighter Typhoon was designed for rapid worldwide deployment with minimum dependency on air-transportable specialist ground support equipment.
Integrated Logistics Support
Eurofighter Typhoon is now in full production and will enterservice in 2002. The four partner nations have ordered 620aircraft with a further option for 90 aircraft.
Spain 87 AircraftItaly 121 AircraftGermany 180 AircraftUnited Kingdom 232 Aircraft
Export campaigns are currently underway around the worldwith the aim to capture 50% of the realistic market for newcombat aircraft, currently estimated at 800 units.
There are seven Development Aircraft (DA1-7) in the flighttest programme. Each aircraft is designed to meet specificobjectives. This unique testing programme has deliveredoutstanding results combining application of syntheticenvironment and flight-testing to reduce the cost andschedule for entry to service testing and qualification.
The recent addition of three Instrumented Production Aircraft(IPA) to the flight test programme has clearly demonstratedthe effectiveness of the manufacturing and final assemblyprocess ahead of series production. In addition the IPA fleetwill significantly enhance the test flight programme providingclearance of delivery standard aircraft.
Eurofighter Typhoon – Key Milestone Achievements
4342
IPA1 15/04/02 1st Flight IPA1 Hartley, Keith
IPA3 08/04/02 1st Flight IPA3 Worning, Christian
IPA2 05/04/02 1st Flight IPA2 Cheli, Maurizo
DA-4 14/03/97 1st Flight DA4 Reeh, Derek
DA-5 24/02/97 1st Flight DA5 Schirdewahn, Wolfgang
DA-7 27/01/97 1st Flight DA7 Bragagnolo, Napoleone
DA-6 31/08/96 1st Flight DA6 De Miguel Gonzalez, Alf
DA-3 04/06/95 1st Flight DA3 Bragagnolo, Napoleone
DA-2 06/04/94 1st Flight DA2 Yeo, Christopher J
DA-1 27/03/94 1st Flight DA1 Weger, Peter
A/C Date Activity Pilot
Data
45
The task of developing and producing the Eurofighter
Typhoon Weapon System is based on an international
partnership of Governments, Industry and Air Forces.
Eurofighter is Europe’s largest defence programme.
The NATO Eurofighter and Tornado Management Agency
(NETMA) is the prime customer for the Eurofighter Typhoon
Weapon System representing the four Governments
participating in this quadrilateral programme.
Eurofighter GmbH is the Prime Contractor for the
Eurofighter Typhoon Weapon System responsible for
coordinating the activities of the four European Partner
Companies (EPCs) and delivering the Weapon System
to NETMA.
Organisation and Structure
44
Italy United KingdomSpainGermany
N E T M A
4746
A-A Air-to-Air
A/C Aircraft
A-S Air-to-Surface
AEA Aircrew Equipment Assembly
AMRAAM Advanced Medium Range Air-to-Air Missile
ASRAAM Advanced Short Range Air-to-Air Missile
BVR Beyond Visual Range
BVRAAM Beyond Visual Range Air-to-Air Missile
CFC Carbon Fibre Composites
DASS Defensive Aids Sub-Systems
DECU Digital Electronic Control Unit
DORC Dis-Orientation Recovery Capability
DVI Direct Voice Input
ECM Electronic Counter Measures
ECS Environmental Control Unit
ESM Electronic Support Measures
EO Electro-Optic
FCS Flight Control System
FLIR Forward Looking Infra-Red
GPS Global Positioning System
GSE Ground Support Equipment
GSS Ground Support System
GRP Glass Reinforced Plastic
HEA Helmet Equipment Assembly
HMD Helmet Mounted Display
HMI Human Machine Interface
Glossary
49
The material presented in this publication is provided to acquaint you withthe general characteristics of our product. It is not an offer and does notconstitute a commitment, a warranty or representation. The detail typespecification, which is part of the purchase agreement, will define the finalconfiguration and capabilities of the product.
www.eurofighter.com
Dimensions / MassWingspan 10.95m (35ft 11in)
Length overall 15.96m (52ft 4in)
Height 5.28m (17ft 4in)
Wing Area 50.0m2 (538ft2)
Basic Mass Empty 11,150 kg (24,582 lb)
Maximum Take-off 23,500 kg (51,809 lb)
Maximum external load 7,500 kg (16,535 lb)
Design CharacteristicsSingle seat twin-engine, with a two-seat variant
Weapon Carriage 13 Hardpoints
G’ limits +9/-3 ‘g’
In-service life 25 years/6,000 Flying Hours*
Power Plants Two Eurojet EJ200 reheated turbofans
max dry thrust class 60 kN (13,500 lb)
max reheat thrust class 90 kN (20,000 lb)
Maximum Speed Mach 2.0
*Based on demanding and realistic mission profiles
48
HOTAS Hand-On-Throttle-And-Stick
HUD Head-Up Display
IFF Identification Friend/Foe
ILS Instrumented Landing System
IMRS Integrated Monitoring and Recording System
INS Inertial Navigation System
IPA Instrumented Production Aircraft
IRST Infra Red Search & Track
ISTAR Intelligence Surveillance Target Acquisitionand Reconnaissance
IWSSS International Weapon System Support System
MIDS Multifunction Information and Distribution System
MLS Microwave Landing System
MHDD Multifunction Head Down Display
NVE Night Vision Enhancement
RWS Range While Search
S-A Surface-to-Air
SEAD Suppression of Enemy Air Defences
SPS Secondary Power System
SRAAM Short Range Air-to-Air Missile
STOL Short Take-Off and Landing
TWS Track While Scan
UCS Utilities Control System
VTAS Voice Throttle And Stick
VS Velocity Search
WVR Within Visual Range
