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- 1. Economic Development Council 30 September 2008 Major General Charles R. Davis, USAF Program Executive Officer, F-35 Lightning II Program DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited.
- 2. VISION DELIVER AND SUSTAIN THE MOST ADVANCED, AFFORDABLE STRIKE FIGHTER AIRCRAFT TO PROTECT FUTURE GENERATIONS WORLDWIDE. MISSION STATEMENT BE THE MODEL ACQUISITION PROGRAM FOR JOINT SERVICE AND INTERNATIONAL COOPERATION. DELIVER TO OUR WAR FIGHTERS AN AFFORDABLE AND EFFECTIVE NEXT GENERATION STRIKE FIGHTER WEAPON SYSTEM AND SUSTAIN IT WORLDWIDE. DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited.
- 3. What Is F-35? Thenext generation “family” of strike fighters • F-16/F/A-18C “like” aero performance • Stealth Signature and Countermeasures • Advanced avionics, data links and adverse weather precision targeting • Increased range with internal fuel and weapons • Highly supportable, state of the art prognostics and health management Lethal Survivable Supportable Affordable DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. 3
- 4. JSF SDD Scope P&W F135 Interoperability CTOL GE/RR F136 CV STOVL 3 Services 8 International Partners Global Sustainment 2 Security Cooperation Domestic / International Participants Suppliers Team JSF Autonomic 3 Flight Test Integrated Logistics Facilities Training DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. 4
- 5. Leveraging Economies ofCommonality Total Ownership Cost Reduction Production Airframe System Development and 70-90% Common Demonstration Common or Cousin Parts Task/ Design Key to Cost Savings Commonality Common Core Key to SDD Propulsion Affordability Costs System Avionics System CTOL STOVL CV Total JSF ~100% Common Three Stand Alone Programs Operations & Support Joint ALGS Key to Reduced Training Delivering and O&S Savings Total Support Ownership Costs PBL Contract Integrated R&M Design DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. 5
- 6. Requirements: Service Needs •USAF: 1763 CTOL – Multi-role (primary air-to-ground) fighter to replace the F-16 and A-10 and to complement the F/A-22 • DoN: 680 CV/STOVL – USN - Multi-role, stealthy strike fighter to complement the F/A-18E/F – USMC - Multi-role, short takeoff, vertical landing strike fighter to replace the AV-8B and F/A-18C/D – DoN CV/STOVL mix TBD • UK (RN and RAF): 138 – Supersonic STOVL replacement for the Sea Harrier and GR-7 • International (Italy, Netherlands, Australia, Norway, Denmark, Canada, Turkey): 592 CTOL/STOVL • Requirements Document – JORD signed 13 March 00 • JROC Validated 11 April 00 • JROC Revalidated 18 October 01 – Annual JROC program review 13 Dec 04 and 16 Mar 06 DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. 6
- 7. JSF Enables TrueJoint/Coalition Operations Domestic and UK International Denmark F-35 F-16 Norway Joint F-16 Netherlands USAF Strike Italy Fighter A-10 Turkey Australia F/A-18 Canada F/A-18 USN Australia F-111 F/A-18 USMC AMX AV-8B Sea Harrier Italy Harrier RN/RAF Harrier GR7 Tornado DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. 7
- 8. Global Production System The Netherlands Norway Canada Dutch Space PHM Consortium Howmet Ben Marine Aeronamic Kitron Fokker - Elmo ASCO DY4 Mindready DAP Applica TNO NLR SP Aerospace FTG Dishon Cyclone Sun Electric Techni Metronor Megellan-Bristol Honeywell Eng Sys Brookx Hexagon Dutch Aero Corena DRS Technologies Axxiflex Kongsberg Herou Devtek Flextronics Eurocast Fokker - Aerostructures Avcorp Thales Cryogenics Thales Nederlands DNV EPM Technology CMC Electronics Magellan-Chicopee Denmark United Kingdom Systematic Software Engineering BAE SYSTEMS Smiths Terma Aerospace Goodrich GPV Maersk Logistics Microfiltrex Hamble Structures IFAD Corena HiQ Wise GKN Helmut Danish Aerotech Integrated Sys. Bruel & Kjaer Martin Baker Beaufort Samputensilli Italy Australia Aermacchi Cusinetti Alenia Broens Mecear Levett York Datamat Micro LTD Aerostaff Turkey Cablex Galileo Marconi Sirio Panel Piaggio Kalekalip Varley Metaltech Ferra Engr. Aerea Umbra Milsoft Ayesas Adecel Lovitt Moog - SBC BAE Australia UoP GKN Marand Oto Meleraia Havelsan TAI Aselsan Logic GPC Marconi Selenia Hawker de Havilland Magnaghi Mikes ALP Aviation Goodrich Services Segundo Mona Production Parts Vestel Gate Elektronik DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. 8
- 9. F-35 Lightning IIDescription • Key Attributes: CTOL Length: 51.4 ft – Stealth Wing Area: 460 ft2 – Integrated Avionics Weight (Empty): 29,036 lbs – A/G Munitions Internal Fuel: 18,840 lbs – LPI Intraflight DL Range: 626 nm – Adv A/C Survability • General Features – Single seat – Speed: 750 kts or 1.6M Length: 51.1 ft – Ceiling: 50,000 ft+ STOVL Wing Area: 460 ft2 – Engine: PW F135; GE F136 Weight (Empty): 32,161lbs • Sensors Internal Fuel: 14,003 lbs – Fully integrated open architecture system Range: 499 nm – A/G – A/A radar/SAR – Electro Optical A/G Targeting system – A/A IRST – Electronic Support Measures (ESM) Length: 51.4 ft – Short range EO spherical coverage CV Wing Area: 668 ft2 Weight (Empty): 32,072 lbs Internal Fuel: 20,085 lbs Range: 642 nm LETHAL SURVIVABLE SUPPORTABLE LETHAL SURVIVABLE SUPPORTABLE INTEROPERABLE INTEROPERABLE DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. 9
- 10. JSF Family OfAircraft One Program -- Three Variants Meeting Service and International Needs Larger Wing and Conventional Carrier Variant Horizontal Tail Area Take-Off and (CV) Landing (CTOL) Probe and Drogue Refueling (Basket) In-Flight Refueling Door (Boom) Strengthened Internal Landing Gear 25mm 4-Barrel and Tailhook Gattling Gun Centerline Wingfold and Gun Pod Ailerons Added with 25mm Gun Short Take-Off and Vertical Landing (STOVL) 3-Bearing Probe and Drogue Swivel Nozzle All variants § 450-600 nm Range Refueling (Basket) § 1.6 Max Mach (Limit) § Stealthy § Same Weapons Lift Fan § Similar Avionics § Similar Flight Envelope § Same Basic Engines Roll Posts DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. 10
- 11. Fighter Aircraft Generations 5thGen -- Integration of All-Aspect Stealth, Advanced Sensors and Weapons DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. 11
- 12. Advanced Stealth MustBe Designed-In Internal Fuel Tanks Curved Diverterless Inlets, Reduced Signature “Buried” Engine Axi-Symmetric Nozzle Fixed Array Radar Engine Inlets Composite Structure Full Line-of-Sight Blockage Aligned Edges Radar Absorbing Embedded Antennas Material (RAM) Reduced Signature Nozzles Internal Stores Carriage Large Capacity Internal Fuel Tanks Low Observable Seams, RAM Seals Weapons Carried Low-Emission Internally Radar and Avionics Embedded Aircraft Shaping Antennas and Edge Alignment Fundamental 5TH Design Features Can Not Be Retrofitted DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. 12
- 13. Advanced Stealth ProvidesSurvivability, Lethality and Mission Success Survivable Theater Access . . . . . . With Increased Lethality Advanced 4th Gen Air-to-Ground 5TH Gen Air-to-Air Legacy Advanced 4th Gen TACAIR 5TH Gen TACAIR Engaged / Shot by Reduced Force Ground Defenses Requirements Surprise Lost Surprise Maintained Mission Effectiveness 5TH Gen Access Assured Degraded / Lost Survivable Access Denied Lethal Stealth Shrinks Air-to-Air Detection Capability Lethal SAM Shots Reduced O&S Cost Baseline 15% • F-35 A-A Loss Exchange Ratio 95% Reduction Reduction (LER) Is 4x Over Advanced 4th 1st to 3rd Some 4th 5TH Generation Generation Fighters Generation Generation Fighters – All Fighters – Fighters – LO Aspect Stealth • First Look, First Shot, First Kill Conventional Enhancements DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. 13
- 14. F-22 and F-35- The World’s Only 5th Gen Fighters 5th Generation Fighters Uniquely Integrate Added Capabilities Added Capabilities Unique to the F-22 Unique to the F-35 · Stealth · Fighter · Sustained Supersonic Ops Performance · Targeting Flexibility · High Altitude Cruise · Internal · Persistence/Range · Extreme Agility Payload · Basing Options Combat Configuration Military Power · Information Subsonic Mission Radius – Service Profiles Fusion and F-35A 60 Situational F-16C 50 Awareness 40 F-35B Alt (K ft) · Sustainable F-22 30 AV-8B · Deployable F-15 20 F-35C 10 · Net-Enabled Operations F/A-18C SL Mach .4 .8 1.2 1.6 2.0 n.mi 200 400 600 800 USAF Combat Configuration– Legacy Has External Fuel Tanks DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. 14
- 15. Non-Technical Data CTOL & CV Weapons Carriage Requirements CTOL Internal Gun Store Fully Certified During SDD EXTERNAL WEAPONS EXTERNAL WEAPONS INTERNAL GBU-32 JDAM 1,000-lb GBU-10 Paveway II 2,000-lb LGB (MK-84 Warhead) 426 -Gallon Wing Tank (MK-83/BLU-110 Warhead) GBU-12 Paveway II 500-lb LGB GBU-24A/B Paveway III 2,000-lb LGB (MK-84 / BLU-109 Warhead) Stormshadow (MK-82 Warhead) GBU-38 JDAM 500-lb (MK-82 Warhead) GBU-16 Paveway II 1,000-lb LGB (MK-83 Warhead) GBU-31 JDAM 2,000-lb AGM-158 JASSM (MK-84 Warhead) MK-83 BLU-110 LDGP 1,000-lb LDGP MXU-648/CNU-88 Baggage Pod AGM-154A/C JSOW Glide Bomb MK-83 BSU-85 HDGP AGM-154A/C JSOW Glide Bomb CBU-103/105 WCMD GBU-38 JDAM 500-lb (MK-82 Warhead) MK-84 2,000-lb LD/HDGP AIM-120B/C AMRAAM Brimstone/Joint GBU-31 JDAM 2,000-lb Common Missile GBU-31 JDAM 2,000-lb MK-84 BSU-50 Ballute 2,000-lb HDGP (MK-84 Warhead) (BLU-109 Warhead) AIM-9X Sidewinder GBU-32 JDAM 1,000-lb AIM-120C AMRAAM AIM-132 ASRAAM GBU-12 Paveway II 500-lb LGB (MK-83/BLU-110 Warhead) BDU-57/58/60 (MK-82 Warhead) Laser-Guided Training Round Weapons Currently Under Development GBU-31 JDAM 2,000-lb MK-82 500-lb LD & HD (BLU-109 Warhead) CBU-99/100 Rockeye II UK 500# PGB Phase I SDB Cluster Munition CBU-103/105 WCMD Missionized Gun Brimstone/Joint Common Missile MK-76/MK-58/BDU-48 AIM-132 ASRAAM DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. 15
- 16. Meeting Key PerformanceParameters 240-4.7 CTOL 240-4.4; STOVL 240-4.3; CV 240-4.5 Combat Radius Mission Reliability CTOL CTOL CV CV STOVL STOVL USMC STOVL UK CV Recovery CTOL 240-4.4; STOVL 240-4.3; CV 240-4.5 Sortie Generation Rate Vpamin CTOL 240-4.7 CV STOVL Performance STO Distance STOVL USMC Flat Deck STOVL UK (HHH Fuel) Ski Jump 240-4.4; 240-4.5 (HMMH Fuel) Logistics Footprint—C-17 Loads VLBB CTOL STOVL USMC 240-4 240-4.4; 240-4.3; 240-4.5 Interoperability Logistics Footprint—Volume Net Ready Criteria CV 240-4.7 RF Signature STOVL USMC STOVL UK • CTOL 240-4.4; STOVL 240-4.3; Threshold Requirement CV 240-4.5 unless noted CE Performance Logistics Footprint—Weight • Contract Engine Deck Exceeds ORD Objective • Projected IOC Weight Empty Meets Rqmt/Exceeds Tripwire CV based on WSR 209 CE Meets Rqmt/In Tripwire Band • Data as of 2-26-08 STOVL USMC Does Not Meet Requirement DISTRIBUTION STATEMENT A. STOVL UK Approved for public release; distribution is unlimited. 16
- 17. F-35 Capability Evolution 2014 Full Warfighting Capability 2012 Initial Warfighting Capability 2010 Basic Training Link to Rating Scale USMC USAF IOC IOC 2008 2010 2012 2014 DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. 17
- 18. JSF Top-Level SDDProgram Schedule FY 2003 2004 2005 2006 2007 2008 2009 2010 2011 2012 2013 2014 2015 CY 2003 2004 2005 2006 2007 2008 2009 2010 2011 2012 2013 2014 2015 Qtr 4 1 2 3 4 1 2 3 4 1 2 3 4 1 2 3 4 1 2 3 4 1 2 3 4 1 2 3 4 1 2 3 4 1 2 3 4 1 2 3 4 1 2 3 4 1 2 3 4 1 2 3 AS CDR 1 IOC USMC AS Air System PDR AS CDR 2 IOC USAF Program Events AS CDR 3 IOC USN CTOL FF Blk 1 DT&E Blk 2 Blk 2 DT&E OT&E First Flights STOVL FF Blk 3 DT&E Blk 3 IOT&E & CTOL (Opt) DT Complete Test Completion CV FF OT Complete DAB Program Reviews (DPRs) LRIP 1 Long Lead Full Funding LRIP 2 LL FF LRIP 3 LL FF LRIP 4 LL FF LRIP 5 LL FF Production LRIP 6 LL FF LRIP 7 LL FF LRIP 8 LL FF Multiyear Procurement (MYP) Contract 1 LL / EOQ MYP As of 17 Sept 08 DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. 18
- 19. JSF Acquisition Timeline 1990 1995 2000 2005 2010 2015 2020 2025 2030 2065 USMC ASTOVL USAF USN IOC Dates MRF JSF ATA JAST CDP NATF AX JSF SDD Derivatives and Enhancements System Development and Demonstration 10/01 F-35 PRECURSOR PROGRAMS: Award LRIP 1-7 Low Rate Initial Production 2027 2033 Advanced Short Takeoff Vertical Landing Multi-Role Fighter Advanced Tactical Aircraft Full Rate Production Naval Advanced Tactical Fighter Advanced Attack Joint Advanced Strike Technology Sustainment Concept Definition Phase F-35 Passing Through The Eye Of The Needle DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. 19
- 20. DISTRIBUTION STATEMENT A:Approved for public release; distribution is unlimited BF-1 Flight Test Results to Date Accomplishments • Envelope expansion – 30,000 feet, .6 Mach, 17 degrees AoA • Systems integration/risk reduction items discovered: – Electric system maturation – Landing gear loads above 200 kts – Fuel system performance/anomalies – Cabin pressure software anomaly – IPP bleed and burn exhaust temperatures – Nacelle vent fan anomaly • Capabilities proven Objectives – Engine and afterburner transients in flight • STOVL envelope expansion – Landing gear extension/retraction below 200 kts • First of variant systems integration – STOVL door system proven in flight • Initial LHD ship operations – Cabin pressure ops – Touch and go landings Status – Formation flying UA and PA • 16 Flts to date; – Max AB take off • Completing airworthiness below 30k ft • Reliability and maintainability – 6 Code One aircraft out of 11 flts • Commencing STOVL door opening – One “two sorties on same day” 18 July and aerial refueling flying qualities • Turned aircraft in 90 minutes testing DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. 20
- 21. DISTRIBUTION STATEMENT A:Approved for public release; distribution is unlimited AA-1 Flight Test Results to Date Accomplishments • 38,000 feet, .97 Mach, 22 degrees AoA • Risk reduction items discovered: – Electrical System – Flight Controls – Environmental Systems – Escape System • Capabilities proven – Air refueling door open handling qualities – Engine and afterburner transients Objectives – Landing gear extension/retraction • Risk reduction/confirmation – Speedbrake design • Basic envelope expansion – Power / Thermal Management System • Systems integration / reliability – Fire Protection System • Reliability and maintainability Status – 37 Code I aircraft out of 46 flts • 52 flts to date – Ten times flew back-to-back days • EAFB deployment week of 29 Sep 08 – Three “two sorties on same day” • Turned aircraft in 60 minutes last time DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. 21
- 22. SDD Tasks toComplete Test Labs CATB F-35 40,000 Hours 2124 Hours 8949 Hours 524 Flights 4986 Flights Verify 460 JCS Contract Specification Requirements 1554 Verification Objectives (VO) 3116 Success Criteria (SC) DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. 22
- 23. 2008/2009 Milestones Aug SepOct Nov Dec Jan Feb Mar Apr May Jun Jul Aug Sep Oct Nov Dec AF-1 BF-2 1st BF-4 1st BF-3 1st Flight AF-2 1st CF-1 1st CF-2 1st Power On Flight Flight Flight Flight Flight AA-1 Launch AF-1 AJ-1 AF-1 1st CJ-1 BF-2 to EAFB Rollout AF-2 CF-3 1st Rollout Rollout Delivered Flight Delivered to Test to Test Flight BF-3 ALIS AG-1 1.0.2 Delivered AF-3 AF-3 1st Rollout CF-1 Flight Delivery to Test Rollout Rollout AF-4 BF-5 Rollout Rollout Maintenance BF-5 1st BF-4 Training CG-1 Flight Rollout CDR Delivered CF-2 to Test Rollout BH-1 Delivered to Test CATB 1st Integrated CF-3 Flt Rollout As of 9 Sept 08 DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. 23
- 24. DRAFT Update F-35 Production Profile BLK 0.5 BLK 1 BLK 2 BLK 3 LRIP 1LRIP 2LRIP 3LRIP 4LRIP 5LRIP 6LRIP 7LRIP 8 MY 1 MY 2 MY 3 MY 4 Buy Year 2007 2008 2009 2010 2011 2012 2013 2014 2015 2016 2017 2018 2019 2020 2021 2022 2023 2024 2025 2026 2027 2028 2029 2030 2031 2032 2033 2034 Deliv ery Year 2010 2010 2011 2012 2013 2014 2015 2016 2017 2018 2019 2020 2021 2022 2023 2024 2025 2026 2027 2028 2029 2030 2031 2032 2033 2034 2035 2036 TOTAL USAF - CTOL 2 6 8 12 24 42 48 60 80 80 80 80 80 80 80 80 80 80 80 80 80 80 80 80 80 80 80 41 1763 DoN - CV 4 6 15 17 20 19 50 50 50 50 50 50 50 38 25 25 9 680 DoN - STOVL 6 8 14 13 25 25 30 31 UK - STOVL 2 1 0 6 1 8 11 12 13 12 12 7 2 1 1 12 13 13 11 138 IT - S TOV L 4 3 3 3 3 14 14 12 1 57 IT - CTOL 2 3 11 11 11 11 12 12 1 74 AS - CTOL 4 8 15 15 15 15 15 13 100 CA - CTOL 16 16 16 16 16 80 DK - CTOL 8 8 8 8 8 8 48 NL - CTOL 1 1 6 10 10 12 12 12 12 9 85 NO - CTOL 8 12 12 12 4 48 TR - CTOL 10 10 10 12 12 10 10 10 10 6 100 TOTAL 2 12 19 32 47 118 132 199 230 231 230 219 181 159 150 143 120 117 118 102 91 80 80 80 80 80 80 41 3173 • Reflects PB09 QTY Profile with Adjusted Navy/Marine Breakout FY 14/15 - As of 18 Sept 08 DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. 24
- 25. USAF Force Structure PMAI 1600 F-15 A/B 1400 F-117 F-22 F-X 1200 1000 F-35 F-16 ROLLUP 800 600 400 F-15 E F-15 C/D 200 A/OA-10 0 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. 25
- 26. F-35 Global CoalitionBasing Operational Locations: 52 Bases, 9 Ships, 156 Squadrons Aircraft USAF 1763 DoN 680 BAE Partners 682 Total 3125 NGC LM Prime Contractors OEMs FET Pratt & Whitney BAE Northrop Grumman Lockheed Martin Depots / FRCs F-16 Locations F/A-18 Locations AV-8B Locations F-35 Requires Global Supply Chain Solution DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. 26
- 27. Eglin F-35 BeddownTimeline CY2006 CY2007 CY2008 CY2009 CY2010 CY2011 EIS 4Q 1Q 2Q 3Q 4Q 1Q 2Q 3Q 4Q 1Q 2Q 3Q 4Q 1Q 2Q 3Q 4Q 1Q 2Q 3Q 4Q EIS ROD RFT MILCON Design 15%, 35%, 65%, 95% …. Build OPS/AMUs, ATC etc. Outfit # 1318, #1309 Sim/Supply/ Ready for Training Add/Alter – O&M Plan & Design #1344, #1404 Hangars Mar 2011 (Fly & Mx) 1st CTOL Arrival – Mar 2010 1st STOVL Arrival – Oct 2010 1st CV Arrival – Jan 2012 ACC 33 FW 30 Sep 09 Standup AETC 33 FW 1 Oct 09 Personnel JSF Prg Ofc Site Activation Initial Cadre & Commanders AETC Program Integration Office USN & USMC Fleet Integration Team Instructors OT&E, Ops 1 Students DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. 27
- 28. Eglin Operations Scopeand Context 2016 2006 Aircraft 159 (113 JSF) 108 (54 F-15s) Student output (2016) 186 / FY • Pilots 1,950 / FY • Mx Total Air Traffic Control Ops 415,200 206,900 (at all three airfields) 33 FW ATC Ops / yr at 121,300 29,206 Eglin Main only 33 FW Sorties / day (year) 123 (30,000) 40 (8,300) 1st F-35 – Mar 10 Last F-15C 33 FW Timing 113th – Jun 15 Departs Sep 09 DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. 28
- 29. 2010 Significant Events •Delivered 14 Aircraft To ITC 4000 3500 Cumulative Training • Facilities construction nearing 3000 2500 completion 2000 1500 38 Pilots • US EW Reprogramming Facility up and 1000 500 326 Maintainers running—serves all three services 0 2008 2010 2011 2012 2013 2014 2015 120000 100000 Flight Hours (Cum) 80000 60000 40000 20000 2,611 Flt Test Hrs 505 LRIP Hrs 0 2008 2010 2011 2012 2013 2014 2015 DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. 29
- 30. Eglin Reprogramming Center JSF Reprogramming Facility Reports Tracks Integrated Core Processing Images OwnShip Sensors – Onboard Fusion Image Multi- Georegistration Processing BDI/BDA Spectral Sensor Sensor Stimulator Subsystem Trackers Image Radar Radar ATC/ATR Geolocation Prep EW EW Fusion CNI Intel Orgs CNI Server EOTS EOTS Correlation Assignment Update DAS DAS Tier 1 (onboard) System Tr ack File VS Simulated Validation & Models CATB Threat Environment FIRE CM CONTROL EXT. DATA PHM MISSION PVI F-35 Controller COMM. COLLECTION & STORES Mission Data Link to Government Facilities AFEWES CM Response CM Dispenser SMS HMD Verification Suppliers Files CM Stimulator Payload Simulator Weapon Simulators LMT-D-2 0-14 (e.g., Threat Threat Data Production Data) Intel Intel Support Support Theater Requirements Data Sensor/Alg Sets Engineering Theater Data Operations Reports Sets F-35 LM Team Development Air System Mission E- 1 – Threa t Products Mission Planning (Data & Data Files Capabilities) Mission JCS Appendix E-1 *(~80 threats today) Debrief Sensor Recordings F-35 Operations *(7 theatres; > 5,000 threats F-35 Development Post-SDD) DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. 30
- 31. 2012 Events • FlightTesting at Three Sites 4000 3500 Cumulative Training • Training Export Certification 3000 2500 and Accreditation approved 2000 159 Pilots 1500 • Achieved ITC Full Capacity 1000 500 1,590 Maintainers • Partner Reprogramming Lab 0 2008 2010 2011 2012 2013 2014 2015 Underway – All US and International 120000 Reprogramming activities 100000 Flight Hours (Cum) will be at Eglin 80000 60000 16,930 LRIP Hrs 40000 6,980 Flt Test Hrs 20000 0 2008 2010 2011 2012 2013 2014 2015 DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. 31
- 32. 2014 Events • Trained375 Pilots and 3421 4000 Cumulative Training Maintainers 3500 3000 • Delivered 236 Production 2500 2000 375 Pilots Aircraft 1500 1000 500 3,421 Maintainers • Completed DT&E Verification 0 2008 2010 2011 2012 2013 2014 2015 • Accomplished NDP Compliance Certification and 120000 Accreditation 100000 Flight Hours (Cum) 80000 60000 95,939 LRIP Hrs 40000 20000 0 2008 2010 2011 2012 2013 2014 2015 DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. 32
- 33. Eglin Eglin AircraftBeddown (All (Latest Plan) F-35 Deliveries Variants) 120 113 100 USN 15 80 Oct 2014: CTOL CV # Aircraft squadrons reach CTOL 60 capacity USAF 78 STOVL Jun 2014: STOVL squadron 40 reaches capacity 20 USMC 20 0 2011 2012 2013 2014 2015 2016 Fiscal Year Training Squadrons & Ramp Space reach capacity in June 2015 DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. 33
- 34. Pilot Throughput (Academic Training Facility) Numbers are based on 2008 bed down Fiscal Year 2010 2011 2012 2013 2014 2015 2016 2017 USAF 4 6 15 29 46 71 89 99 USMC 2 16 19 29 46 49 56 69 USN 8 11 18 21 28 31 UK 3 2 0 9 10 10 16 NETHERLANDS 2 3 2 7 9 9 9 ITALY 1 2 2 3 5 9 10 AUSTRALIA 3 12 9 6 Train in Australia TURKEY 4 5 5 Train in Turkey NORWAY 4 10 CANADA 6 10 DENMARK 8 10 TOTAL 6 28 49 77 145 179 230 264 Pilot training capacity reaches max capability of 186 in late 2015 DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. 34
- 35. Maintainer Annual Throughput (Academic Training Facility) Fiscal Year 2010 2011 2012 2013 2014 2015 2016 2017 USAF 71 65 116 216 341 486 630 823 (CC, Av, Wpn) USMC 55 164 187 208 371 394 535 604 USN 53 81 237 321 409 456 UK 26 21 13 85 Train in UK NETHERLANDS 12 12 0 77 Train in Netherlands ITALY 71 72 168 214 AUSTRALIA 48 98 Train in Australia TURKEY 45 Train in Turkey NORWAY TBD CANADA TBD DENMARK 192 192 TOTAL 126 267 389 566 1325 1273 1934 2298 Academic Facility can support maintenance training until fall 2016 DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. 35
- 36. Eglin AFB PopulationFY07-FY16 40000 * 132 Internationals Arrive FY10-FY16 Totals (Net Growth =7767) 36113 35000 34891 33447 30000 28292 25211 25000 Family Members Family Members 20000 15000 Active Duty Military Active Duty Military 10000 DoD Civilians DoD Civilians 5000 CME Contractors CME Contractors 0 FY07 FY08 FY09 FY10 FY11 FY12 FY13 FY14 FY15 FY16 36 DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. 36
- 37. AIMPOINT 2014: GlobalOps CY 2008 2010 2012 2014 Aircraft (SDD+LRIP) 2 24 77 242 Flight Hours (SDD+LRIP) 190 3,100 23,300 91,300 Aircraft Shore Sites 2 4 6 12 Site Activation Underway 13 20 25 17 Pilots Trained 8 (ITF) 8 94 340 Maintainers Trained 234 (ITF) 144 1,478 3,309 ITC/PTC 1 1 4? Pilot Training Devices 2 15 26 Mx Training Devices 9 13 DSOR Decisions 5 9 27 43 Sub-System Capability 13 (of 48) 30 (of 48) Field Support Eng 3 10 24 65 Service Bulletins 87 262 437 Global Spares Value (TY$M)230 1,055 2,380 4,673 PBAs/PPRs 2 6 8 12 OEM PBL Suppliers 5 12 19 PBL TRANSITION IBC SITE TRAINING EXPANSION ALGS OPERATIONS ACTIVATION EXECUTION Sustainment ... Globally Supported And Delivered DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. 37
- 38. Questions? Lockheed Martin AeronauticsCompany DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. DISTRIBUTION STATEMENT A.Approved for public release; distribution is unlimited. 38