DISTRIBUTION STATEMENT A Approved for public release distribution

DISTRIBUTION STATEMENT A: Approved for public release; distribution is unlimited. IMPORTANT NOTICE: A hard copy of this document may not be the document currently in effect. The current version is always the version on the Lockheed Martin network. Bill Gigliotti 25 October 2014 © 2014 Lockheed Martin Corporation Use or disclosure of the information contained herein is subject to the restrictions of the Cover Page SFTE_SETP_25 Oct - 1

DISTRIBUTION STATEMENT A: Approved for public release; distribution is unlimited. F-35 Value Proposition © 2014 Lockheed Martin Corporation Use or disclosure of the information contained herein is subject to the restrictions of the Cover Page SFTE_SETP_25 Oct - 2

DISTRIBUTION STATEMENT A: Approved for public release; distribution is unlimited. The Strategic Advantage of Air Power “Not to have an adequate air force in the present state of the world is to compromise the foundations of national freedom and independence. ” Winston Churchill, 1933 Iraqi Army – Without Air Power Desert Storm Bosnia • Enemy Fighters Neutralized • Coalition Power Projection Achieved Coalition Forces – With Air Power Afghanistan • Freedom to Maneuver • Freedom from Attack • Freedom to Attack Iraqi Freedom Libya Air Power Is an Essential Core Competency © 2014 Lockheed Martin Corporation Use or disclosure of the information contained herein is subject to the restrictions of the Cover Page SFTE_SETP_25 Oct - 3

DISTRIBUTION STATEMENT A: Approved for public release; distribution is unlimited. Fighter Generations 5 th Generation 2005 4 th Gen F-35 Additions 1970 • Multi-Spectral Sensors • Interoperability • Weapon Types • Modernized Avionics 3 rd Gen 1 st Gen 2 nd Gen 1955 1945 • 1 st Jets • Supersonic • 1 st Radar Common Attributes 1960 • Multi-Role • Missiles • LO Treatments • Advanced Avionics • Guided Weapons • Advanced Stealth • Sensor Fusion • Net Enabled Ops • Fighter Performance • Adv. Sustainment Stealth Technology 1966 High & Fast 1983 Night, Non Maneuverable Air-Surface Only 2005 Maneuverable All Weather Operations 5 th Gen Capabilities & Effectiveness Are Superior To 4 th Gen © 2014 Lockheed Martin Corporation Use or disclosure of the information contained herein is subject to the restrictions of the Cover Page SFTE_SETP_25 Oct - 4

DISTRIBUTION STATEMENT A: Approved for public release; distribution is unlimited. VLO Stealth Must Be Designed In *Very Low Observable (VLO) Antennas F-35 A 18, 200 lb F-35 B F-35 A 13, 100 lbs lb 18, 500 F-35 C F-35 B 19, 200 lbs lb 14, 000 Reduced Signature F-35 C Nozzle Large Capacity Internal Fuel Tanks 20, 000 lbs Aircraft Shaping and Edge Alignment Curved Diverterless Inlets, “Buried” Engine Low Observable Seams, RAM Seals Low-Emission Radar and Avionics DAS Apertures EOTS / IRST Weapons Carried Internally Embedded / Internal Antennas and Sensors Fundamental 5 TH Design Features Cannot Be Retrofitted © 2014 Lockheed Martin Corporation Use or disclosure of the information contained herein is subject to the restrictions of the Cover Page SFTE_SETP_25 Oct - 5

DISTRIBUTION STATEMENT A: Approved for public release; distribution is unlimited. F-35 C – Carrier Variant Length Span Wing Area Internal Fuel © 2014 Lockheed Martin Corporation 51. 5 ft 43 ft 668 ft 2 19, 200 lb Use or disclosure of the information contained herein is subject to the restrictions of the Cover Page SFTE_SETP_25 Oct - 6

DISTRIBUTION STATEMENT A: Approved for public release; distribution is unlimited. F-35 C – Carrier Variant Larger Wing and Tails Probe and Drogue Refueling (Basket) Strengthened Landing Gear and Tailhook Wingfold and Ailerons Added © 2014 Lockheed Martin Corporation Use or disclosure of the information contained herein is subject to the restrictions of the Cover Page SFTE_SETP_25 Oct - 7

DISTRIBUTION STATEMENT A: Approved for public release; distribution is unlimited. Fifth-Gen Carrier Suitable Design Features Larger Wing Fuel Dump (Underside) Larger Vertical Tails Durable Structure Continuous Keel Tailhook to Nosegear Drag Optimized Contour ~20, 000 lb Internal Fuel Over the Nose View IPP Exhaust Rapid Power Response Refuel Probe Larger Horizontal Tails Supportable LO Ailerons for Low-Speed Roll Control © 2014 Lockheed Martin Corporation Weapon Bays Forward of MLG Heavy Carrier Stronger Catapult Weather Tailhook Landing Gear Launch Wing Fold Tiedown System Points Use disclosure the information contained herein subject the restrictions the Cover Page SFTE_SETP_25 Oct - 8 - 8 Use oror disclosure ofof the information contained herein isis subject toto the restrictions ofof the Cover Page

DISTRIBUTION STATEMENT A: Approved for public release; distribution is unlimited. F-35 Specifications F-35 A CTOL 51. 4 ft / 15. 7 m 14. 4 ft / 4. 38 m 35 ft / 10. 7 m 460 ft 2 / 42. 7 m 2 22. 5 ft / 6. 86 m 29, 300 lb 18, 200 lb / 8278 kg 18, 000 lb / 8, 160 kg • 25 mm GAU-22/A Cannon • Two AIM-120 C Air-to-Air Missiles • Two 2, 000 -lb GBU-31 JDAM Guided Bombs F-35 B STOVL 51. 2 ft / 15. 6 m 14. 3 ft / 4. 36 m 35 ft / 10. 7 m 460 ft 2 / 42. 7 m 2 21. 8 ft / 6. 65 m 32, 300 lb 13, 100 lb / 6, 125 kg 15, 000 lb / 6, 800 kg • Two AIM-120 C Air-to-Air Missiles • Two 1, 000 -lb GBU-32 JDAM Guided Bombs F-35 C CV 51. 5 ft / 15. 7 m 14. 7 ft / 4. 48 m 43 ft / 13. 1 m 668 ft 2 / 62. 1 m 2 26. 3 ft / 8. 02 m 34, 800 lb 19, 200 lb / 8, 960 kg 18, 000 lb / 8, 160 kg • Two AIM-120 C Air-to-Air Missiles • Two 2, 000 -lb GBU-31 JDAM Guided Bombs Speed (Full Internal Weapons Load) Combat Radius (Internal Fuel) 70, 000 lb Class F 135 -PW-100 40, 000 lb Max. 25, 000 lb Mil. Vertical N/A Mach 1. 6 (~1, 200 mph) >590 nm / 1, 093 km 60, 000 lb Class F 135 -PW-600 38, 000 lb Max. 26, 000 lb Mil. 40, 500 lb Vertical Mach 1. 6 (~1, 200 mph) >450 nm / 833 km 70, 000 lb Class F 135 -PW-100 40, 000 lb Max. 25, 000 lb Mil. Vertical N/A Mach 1. 6 (~1, 200 mph) >600 n. mi / 1, 100 km Range (Internal Fuel) >1, 200 nm / 2, 200 km >900 nm / 1, 667 km >1, 200 n. mi / 2, 200 km Max g-Rating 9. 0 7. 5 Length Height Wingspan Wing area Horizontal Tail Span Weight Empty Internal Fuel Capacity Weapons Payload Standard Internal Weapons Load Maximum weight Propulsion* (Uninstalled Thrust Ratings) © 2014 Lockheed Martin Corporation Use or disclosure of the information contained herein is subject to the restrictions of the Cover Page SFTE_SETP_25 Oct - 9

DISTRIBUTION STATEMENT A: Approved for public release; distribution is unlimited. F-35 C Comparison (USN) F/A-18 C F-35 C Length 56 ft Span 40 ft 5 in (w/missiles) Wing Area 400 ft 2 Internal Fuel 10, 860 lb Spot Factor 1. 0 © 2014 Lockheed Martin Corporation Length 51. 5 ft Span 43 ft Wing Area 668 ft 2 Internal Fuel Spot Factor F/A-18 E 19, 200 lb 1. 20 Length 60 ft 1 in Span 44 ft 8 in Wing Area 500 ft 2 Internal Fuel 14, 400 lb Spot Factor 1. 23 Use or disclosure of the information contained herein is subject to the restrictions of the Cover Page SFTE_SETP_25 Oct - 10

DISTRIBUTION STATEMENT A: Approved for public release; distribution is unlimited. F-35 Master Schedule CY Low-Rate Initial Production and Multiyear Procurement 2006 2007 2008 2009 2010 As of 15 Oct 2014 2011 2012 2013 2014 2015 2016 2017 2018 2019 LRIP 1 (2) LRIP 2 (12) LRIP 3 (17) LRIP 4 (32) LRIP 5 (32) LRIP 6 (36) LRIP 7 (35) LL LRIP 8 (43) LL LRIP 9 LRIP 10 Planned Production • Air Force 1, 763 F-35 A • Dept of Navy 680 F-35 B/F- LRIP 11 FR 1 35 C • International 800 -1, 500 First Flights F-35 B F-35 A Development F 35 C USMC IOC Air System 2 A SW Fleet Releases F-35 A 2 B USAF IOC 3 I USN IOC 3 F F-35 B DT Flight Test Base Stand-Up F-35 C F-35 MS Eglin Edwar ds Cherry Point Nellis Yuma Luke Ogde Beaufo n Time rt © 2014 Lockheed Martin Corporation IT Iwakun i Hill NAS West ISR JP IT AF Ops 2 NO UK AU TR NL KR Now Use or disclosure of the information contained herein is subject to the restrictions of the Cover Page SFTE_SETP_25 Oct - 11

DISTRIBUTION STATEMENT A: Approved for public release; distribution is unlimited. Questions © 2014 Lockheed Martin Corporation Use disclosure the information contained herein subject the restrictions the Cover Page Use oror disclosure ofof the information contained herein isis subject toto the restrictions ofof the Cover Page SFTE_SETP_25 Oct - 12