DISTRIBUTION STATEMENT A: Approved for public release; distribution is unlimited. © 2014 Lockheed Martin Corporation SFTE_SETP_25Oct - 1 Use or disclosure of the information contained herein is subject to the restrictions of the Cover Page 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. DISTRIBUTION STATEMENT A: Approved for public release; distribution is unlimited. 25 October 2014 Bill Gigliotti © 2014 Lockheed Martin Corporation

DISTRIBUTION STATEMENT A: Approved for public release; distribution is unlimited. © 2014 Lockheed Martin Corporation SFTE_SETP_25Oct - 2 Use or disclosure of the information contained herein is subject to the restrictions of the Cover Page F-35 Value Proposition

DISTRIBUTION STATEMENT A: Approved for public release; distribution is unlimited. © 2014 Lockheed Martin Corporation SFTE_SETP_25Oct - 3 Use or disclosure of the information contained herein is subject to the restrictions of the Cover Page 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 Winston Churchill, 1933 Air Power Is an Essential Core Competency Iraqi Army – Without Air Power Bosnia Desert Storm Iraqi Freedom Libya Afghanistan Coalition Forces – With Air Power Freedom to Maneuver Freedom from Attack Freedom to Attack Enemy Fighters Neutralized Coalition Power Projection Achieved

DISTRIBUTION STATEMENT A: Approved for public release; distribution is unlimited. © 2014 Lockheed Martin Corporation SFTE_SETP_25Oct - 4 Use or disclosure of the information contained herein is subject to the restrictions of the Cover Page Fighter Generations 1st Jets1st Jets SupersonicSupersonic 1st Radar1st Radar Multi-RoleMulti-Role MissilesMissiles LO TreatmentsLO Treatments Advanced AvionicsAdvanced Avionics Guided WeaponsGuided Weapons 5 th Generation 2 nd Gen 4 th Gen 3 rd Gen 1 st Gen 5th Gen Capabilities & Effectiveness Are Superior To 4th Gen High & Fast Night, Non Maneuverable Air-Surface Only Stealth Technology Common Attributes Advanced StealthAdvanced Stealth Sensor FusionSensor Fusion Net Enabled OpsNet Enabled Ops Fighter PerformanceFighter Performance Adv. SustainmentAdv. Sustainment F-35 Additions Multi-Spectral SensorsMulti-Spectral Sensors InteroperabilityInteroperability Weapon TypesWeapon Types Modernized AvionicsModernized Avionics Maneuverable All Weather Operations

DISTRIBUTION STATEMENT A: Approved for public release; distribution is unlimited. © 2014 Lockheed Martin Corporation SFTE_SETP_25Oct - 5 Use or disclosure of the information contained herein is subject to the restrictions of the Cover Page F-35A18,500 lbs F-35B14,000 lbs F-35C20,000 lbs VLO Stealth Must Be Designed In Fundamental 5 TH Design Features Cannot Be Retrofitted F-35A 18,200 lb F-35B 13,100 lb F-35C 19,200 lb Weapons Carried Internally Embedded / Internal Antennas and Sensors Aircraft Shaping and Edge Alignment Low-Emission Radar and Avionics Low Observable Seams, RAM Seals Curved Diverterless Inlets, “Buried” Engine Large Capacity Internal Fuel Tanks *Very Low Observable (VLO) Reduced Signature Nozzle Antennas DAS Apertures EOTS / IRST

DISTRIBUTION STATEMENT A: Approved for public release; distribution is unlimited. © 2014 Lockheed Martin Corporation SFTE_SETP_25Oct - 6 Use or disclosure of the information contained herein is subject to the restrictions of the Cover Page F-35C – Carrier Variant Length 51.5 ft Span 43 ft Wing Area 668 ft 2 Internal Fuel 19,200 lb

DISTRIBUTION STATEMENT A: Approved for public release; distribution is unlimited. © 2014 Lockheed Martin Corporation SFTE_SETP_25Oct - 7 Use or disclosure of the information contained herein is subject to the restrictions of the Cover Page F-35C – Carrier Variant Strengthened Landing Gear and Tailhook Wingfold and Ailerons Added Larger Wing and Tails Probe and Drogue Refueling (Basket)

DISTRIBUTION STATEMENT A: Approved for public release; distribution is unlimited. © 2014 Lockheed Martin Corporation SFTE_SETP_25Oct - 8 Use or disclosure of the information contained herein is subject to the restrictions of the Cover Page Fifth-Gen Carrier Suitable Design Features Refuel Probe Heavy Weather Tiedown Points Larger Wing Drag Optimized Contour ~20,000 lb Internal Fuel Wing Fold Ailerons for Low-Speed Roll Control Larger Vertical Tails CarrierTailhook IPPExhaust Larger Horizontal Tails Stronger Landing Gear Catapult Launch System Rapid Power Response Durable Structure Weapon Bays Forward of MLG Continuous Keel Tailhook to Nosegear Supportable LO Over the Nose View Fuel Dump Fuel Dump (Underside) © 2014 Lockheed Martin Corporation Use or disclosure of the information contained herein is subject to the restrictions of the Cover Page SFTE_SETP_25Oct - 8

DISTRIBUTION STATEMENT A: Approved for public release; distribution is unlimited. © 2014 Lockheed Martin Corporation SFTE_SETP_25Oct - 9 Use or disclosure of the information contained herein is subject to the restrictions of the Cover Page F-35 Specifications F-35A CTOLF-35B STOVLF-35C CV Length51.4 ft / 15.7 m51.2 ft / 15.6 m51.5 ft / 15.7 m Height14.4 ft / 4.38 m14.3 ft / 4.36 m14.7 ft / 4.48 m Wingspan35 ft / 10.7 m 43 ft / 13.1 m Wing area460 ft2 / 42.7 m2 668 ft2 / 62.1 m2 Horizontal Tail Span22.5 ft / 6.86 m21.8 ft / 6.65 m26.3 ft / 8.02 m Weight Empty29,300 lb32,300 lb34,800 lb Internal Fuel Capacity18,200 lb / 8278 kg13,100lb / 6,125 kg19,200 lb / 8,960kg Weapons Payload18,000 lb / 8,160 kg15,000 lb / 6,800kg18,000 lb / 8,160 kg Standard Internal Weapons Load 25 mm GAU-22/A Cannon Two AIM-120C Air-to-Air Missiles Two 2,000-lb GBU-31 JDAM Guided Bombs Two AIM-120C Air-to-Air Missiles Two 1,000-lb GBU-32 JDAM Guided Bombs Two AIM-120C Air-to-Air Missiles Two 2,000-lb GBU-31 JDAM Guided Bombs Maximum weight70,000 lb Class60,000 lb Class70,000 lb Class Propulsion* (Uninstalled Thrust Ratings) F135-PW ,000 lb Max. 25,000 lb Mil. Vertical N/A F135-PW ,000 lb Max. 26,000 lb Mil. 40,500 lb Vertical F135-PW ,000 lb Max. 25,000 lb Mil. Vertical N/A Speed (Full Internal Weapons Load) Mach 1.6 (~1,200 mph) Mach 1.6 (~1,200 mph) Mach 1.6 (~1,200 mph) Combat Radius (Internal Fuel)>590 nm / 1,093 km>450 nm / 833 km>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

DISTRIBUTION STATEMENT A: Approved for public release; distribution is unlimited. © 2014 Lockheed Martin Corporation SFTE_SETP_25Oct - 10 Use or disclosure of the information contained herein is subject to the restrictions of the Cover Page Length51.5 ft Span43 ft Wing Area668 ft 2 Internal Fuel 19,200 lb Spot Factor1.20 Length60 ft 1 in Span44 ft 8 in Wing Area500 ft 2 Internal Fuel14,400 lb Spot Factor1.23 F-35C Comparison (USN) F/A-18E Length56 ft Span40 ft 5in (w/missiles) Wing Area400 ft 2 Internal Fuel10,860 lb Spot Factor1.0 F/A-18CF-35C

DISTRIBUTION STATEMENT A: Approved for public release; distribution is unlimited. © 2014 Lockheed Martin Corporation SFTE_SETP_25Oct - 11 Use or disclosure of the information contained herein is subject to the restrictions of the Cover Page F-35 Master Schedule As of 15 Oct 2014 CY LRIP 1 (2) LRIP 2 (12) LRIP 3 (17) LRIP 8 (43) LRIP LRIP 11 FR1 Time Now LRIP 10 F-35BF-35AF-35C First Flights Low-Rate Initial Production and Multiyear Procurement Base Stand-Up Development Eglin Yuma Edwards Nellis Luke USN IOCUSAF IOCUSMC IOC UK Iwakuni Hill NAS West IT JP ISR NO IT AU Planned Production Air Force1,763 F-35A Air Force1,763 F-35A Dept of Navy680 F-35B/F-35C Dept of Navy680 F-35B/F-35C International800-1,500 International800-1,500 Planned Production Air Force1,763 F-35A Air Force1,763 F-35A Dept of Navy680 F-35B/F-35C Dept of Navy680 F-35B/F-35C International800-1,500 International800-1,500 Ogden Air System SW Fleet Releases Cherry Point DT Flight Test F-35BF-35B F-35AF-35A F-35CF-35C 2B3F3I2A LRIP 6 (36) LRIP 7 (35) LL LRIP 5 (32) LRIP 4 (32) F-35MSF-35MS AF Ops 2 KR TR NL LL Beaufort

DISTRIBUTION STATEMENT A: Approved for public release; distribution is unlimited. © 2014 Lockheed Martin Corporation SFTE_SETP_25Oct - 12 Use or disclosure of the information contained herein is subject to the restrictions of the Cover Page Questions © 2014 Lockheed Martin Corporation Use or disclosure of the information contained herein is subject to the restrictions of the Cover Page SFTE_SETP_25Oct - 12 DISTRIBUTION STATEMENT A: Approved for public release; distribution is unlimited.