gripen briefing farnborough 2010
TRANSCRIPT
GRIPEN AROUND THE WORLD
“ The Gripen system will be the backbone of the Swedish Air Force for more than the next 30 years and my Government is commited to continued additional development of the system.”
Mr. Sten Tolgfors, Minister for Defence
GRIPEN DEVELOPMENT 2010
The main development plan is as earlier outlined. • The MS20 order came as expected• Studies for MS21 underway
Swedish government have during 2010 put Gripen related orders onSaab for a value of more than 3 000 MSEK• Continuous support of Gripen’s operational capacity.• Development of avionics system.• For upgrade and further development of the reconnaissance system.• System maintenance of Gripen.• Development of the existing Gripen fleet (MS20).
GRIPEN DEVELOPMENT
Gripen A/B
Gripen C/D
Gripen NG
1995 2000 2005 2010 2015
Demonstrator
Gripen C/D
TRADITIONAL UPGRADE PHILOSOPHY
timeacquisition MLUSystem FOC
Evolving Fighter capability
Desired capability levelTraditional MLU - Mid Life Upgrade and minor upgrades as provided by manufacturer
GRIPEN UPGRADE PHILOSOPHY
timeacquisitionSystem FOC
Customer adapted upgrades
Evolving Fighter capability
2-3 year cycle
Desired capability level
GRIPEN NG - FIGURES & FACTS
Length: 14.1 mWingspan: 8.6 mMax T/O weight: 16 500 kgThrust: + 22 000 lbPayload: 7 200 kgMax fuel: 7 100 kgSuper Cruise: > M 1.2GLIMIT: -3 G / + 9 G
Max Range: > 2200 NmLanding Distance: < 500 m Combat TurnAround: < 10 minEngine replacement: < 1 hourCost per flight hour < $ 4000
REACH
REACH
450 Gallons external tank
INCREASE INTERNAL FUELNew and moved main gearOld main gear bay – 900 kg extra fuel
NEW 450 Gallons EXTERNAL TANKOptimized for minimized dragSuper Sonic drop tanks
REACH (cont.)
Gripen NG unrefuelled Combat Radius700 nm (1300 km) + 30 min CAP4 x RR2 x IR Internal + External Fuel
Gripen NG unrefuelled Ferry Range2200 nm (4000 km)Internal + External Fuel
Gripen NG unrefuelled Combat Radius700 nm (1300 km) + 30 min CAP4 x RR2 x IR Internal + External Fuel
Gripen NG unrefuelled Ferry Range2200 nm (4000 km)Internal + External Fuel
REACH (cont.)
RETRACTABLE TELESCOPIC PROBEMinimized dragMinimized RCS
AIR TO AIR REFUELLINGC -130 HerculesKC -135Airbus 310 MRTTKDC-10Boeing 707
BUDDY - BUDDY REFUELLING
ACCESS
ACCESS
ADVANCED REAR SEAT Sensor SharingElectronic AttackAir Battle ManagementUCAV Lead
SUPERIOR SELF PROTECTIONMissile Approach- / Laser Warning SystemTowed DecoyEnhanced ESM • Wider bandwidth• DRFM
CBRN PROTECTION
SENSORSHARING
AWARENESS
AWARENESS
ES 05 RAVEN
q partnership2nd Generation AESA Swash PlateA-A, A-G and ECM Modes
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Gripen
RAVEN ES-05 –LATEST GENERATION AESA RADAR FOR THE GRIPEN NG
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A collaborative venture
• Collaboration between SELEX Galileo, Radar & Advanced Targeting, and Saab, EDS and Aeronautics
• Heads of Agreement signed in March 2009
• Business agreement May 2010
• Close cooperation built on overall radar experience, AESA experience and Gripenarchitecture
• Doing “Different things” – driving efficiency, timescales and costs
ES-05 Raven
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Builds on established technologyClear route map to future capability
High PerformanceInnovative WFOR solution
The Gripen NG AESA radar - high performance, high availability
Wide field of regard system optimised for multi-role/swing role operations
Comprehensive mode suite for both A/A and A/G including interleaved operation
High availability and reliability
Clear route map to future capability
Builds on established technology from the European leaders in AESA radars
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Progress
• Raven 1000P (Raven ES-05 prototype) flew on Gripen NG within 12 months from go ahead
• Preliminary Design Review Complete
• Indian Air Force & FMV/SwAF Evaluation
• ATMOS Collaboration agreement
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Raven 1000P Air to Ground SAR Linköping Airport – 2 May 2010
Array of Corner Reflectors
RAVEN 1000P AIR TO GROUND SARLinköping Airport – 2 May 2010
AWARENESS
NETCENTRICWorld leader in data links Fully integrated• Land• Ship• Air• Space
Revolutionary fighter linkSensor sharingSensor fusionUnderstand the battle before take off
Example: SATCOM – LINK 16 – FIGHTER LINK (TIDLS) – DIGITAL CAS LINK (VMF)
FIRE POWER
TAURUS KEPT 350(Stand off weapon)DWS 39
(Stand off weapon)MRPS(Recce pod)
AGM-154 JSOW(Stand off weapon)
RECCELITE(Recce pod)
RBS15(Anti Ship missile)
DJRP(Recce Pod)
BRIMSTONE(Air-to-Surface Missile)
AGM-65 Maverick(Air-to-Surface Missile)
JDAM/JDAM-ER GBU-31/-32/-38(Smart Bomb)
BOQ-X300(ECM Pod)
FUEL DROP TANKMETEOR(Air-to-Air RR Missile)R-DARTER
(Air-to-Air RR Missile)
AIM-9X SIDEWINDER(Air-to-Air IR Missile)
AIM-9 SIDEWINDER(Air-to-Air IR Missile)
DERBY(Air-to-Air RR Missile)
SDB GBU39/B(Smart Bomb)
PYTHON 4/5(Air-to-Air IR Missile)
IRIS-T(Air-to-Air IR Missile)
A-DARTER(Air-to-Air IR Missile)
AIM-132 ASRAAM(Air-to-Air IR Missile)
AIM-120 AMRAAM(Air-to-Air RR Missile
Paveway IIIGBU-22/-24 (Smart Bomb)
Paveway IIGBU-10/-12/-16 (Smart Bomb)
Paveway IVGBU 49(Smart Bomb)
LITENING GIIIFLIR/LDP Pod
EHUD/FPR(AACMI Pod)
SPICE(Smart Bomb) Mk80 Series
(General Purpose Bombs)
FLEXIBILITY OF FIRE POWER
SEA GRIPEN
THE NAVALISED GRIPEN
SEA GRIPEN
ROAD BASE EXPERTS
Typical runway (45 x 2400m)
Swedish Road base (17 x 800m)
Gripen needs 9 x 600m
… without arrester hook or brake chute
35 Draken 37 Viggen 39 Gripen
REQUIREMENTS
• Low landing speed (<150 Kn)
• High pitch & roll rate authority
• High precision glide slope control
• High precision landing capability
• High sink rate clearance
• High ground steering authority
• High wheel brake capacity
• Assisted brake system
• Arrester hook
• Strengthened airframe
ROAD BASE LANDING REQ.
CARRIER LANDING REQ.
Yes Yes
Yes Yes
Yes Yes
Yes Yes
Yes Yes
Yes
Yes NoYes No
No Yes
Gripencapabilities
(…Today 15 fts)
(ABS on every wheel)
Tilted canards
Yes Yes
(…Today ~125-160 kn)
Emergency Tail Hook(NG customer req.)
Yes
Due to new gear installation
POSSIBILITIES…
GRIPEN DEMONSTRATOR PROGRAMME
FLIGHT TESTSPhase 1• First flight May 27 2008• Phase 1: 79 flights performed• Flight envelope
• Speed Mach 1,6+• Super cruise Mach 1,2+• Load factor Max• Angle of Attack Max• External stores Medium and Heavy
Phase 2• First flight 27 October 2009• 73 flights performed (total of >175 flights)• Flight tests of the MAW system, AESA radar, Sat. Com.
and increased internal fuel successfully completed• In country evaluation in India successfully completed
INDIA - IN COUNTRY EVALUATIONFerry flight
Linköping, Sweden
Kechkemet, Hungary
Athens, Greece
Hurgada, Egypt
Riyadh, Saudi Arabia
Musquat, Oman
Jamnagar, India
Landing for refueling
Landing/refueling and overnight stay