Military Airframe, Land & Sea Based Applications for Titanium

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Military Airframe, Land & Sea Based Applications for Titanium Richard J. Harshman Chairman, President and Chief Executive Officer of ATI Titanium 2012 Atlanta, GA October 8, 2012

Forward Looking Statements This presentation contains forward-looking statements. Actual results may differ materially from results anticipated in the forward-looking statements. These and additional risk factors are described from time to time in the Company s filings with the Securities and Exchange Commission, including its Annual Report on Form 10-K for the year ended December 31, 2011. 2

Titanium s History in Defense Applications Abrams F-22 Submarines SR71 CH53K F-117 C-17 Howitzer F-35 Stilleto F-4 C-130 HMMWV Bradley Stryker A400M 1950s 1960s 1970s 1980s 1990s 2000s 2010s 3 Photos courtesy of DoD

Why Titanium? Performance Speed, mobility, maneuverability Compatibility with composites Payload Extends range & capacity Fuel efficiency Protection Enhanced survivability Optimum Design & Balanced Trades Payload Performance, Payload and Protection Drives Ti Usage in Military Applications 4

Challenges for Titanium in Military Applications Initial raw material cost Higher vs. traditional materials Life-cycle costs aren t typically considered Uncertainty of demand No long-term firm backlog Sequestration Government budget cuts 5

Military Airframe Programs Fighters F-35 F-15 Eurofighter F-22 Transports C-130 C-17 A400M Helicopters 6 Photos courtesy of DoD

Military Airframe Applications using Titanium Fasteners Brackets, Fittings & Clips Hydraulic Tubing Bulkheads Rear Spar Tail Fin Spars Lower Keel Chord Aileron Strongback Aft Keel Structure Engine Bay Doors Wing Clips & Brackets Aft Frame Spars & Structures Cockpit Window Surrounds Intake & Auxiliary Vent Doors Landing & Weapons Bay Doors Side of Body Chord Front Spar Pylon Castings Landing Gear & Tail Hook Components 7

Military Airframe Applications using Titanium Fasteners Small Bellow Components Structural Beams Tall Rotor Blades Rotor Yoke Rotor Hubs Spindles/Cuffs Root Fittings Stabilator Components Erosion Shields Structural Components Core of Blade Window Surrounds Belly Armor Hub Wing Plate 8

Military Airframe Applications using Titanium * * Fighter Jet Bulkheads * Rotor Hub Rotor Yoke *Photo courtesy of PCC Wyman Gordon 9

Examples of Titanium Uses in Land & Sea Defense Applications Existing Applications Abrams Main Battle Tank Leopard Main Battle Tank Bradley Fighting Vehicle MRAP Lightweight Howitzer CVN Aircraft Carriers USN Submarines Stryker Projected Future Applications GCV MAPV MPC Others 10 Photos courtesy of DoD

Land Defense Applications Examples of Titanium Uses Critical element in heavy armor recipes Add-on passive armor panels Reactive Armor Boxes Suspension components Hatches Howitzer components Gunner Protection Kits Structures on next generation vehicles Reactive Armor Boxes Bradley Fighting Vehicle* Example of titanium structure for future combat vehicles** 11 *Photo courtesy of DoD **Photo courtesy of AM General

Titanium: Military Vehicle s Lightweight Alternative Abrams M1A2 Main Battle Tank Replacement Components Turret blow-off panels Gunner's primary sight GPS cover NBC cover Engine top cover Turret pivot rack Commander's hatch Commander's independent thermal viewer TOTAL (1) Source: US Army ARDEC (1) Not including internal armor modifications Weight (Kg) Weight Saved RHA Steel Titanium (Kg) (%) 311 229 82 26% 227 160 67 30% 168 132 36 21% 498 358 140 28% 160 90 70 44% 80 56 24 30% 146 92 54 37% 1590 1117 473 30% Photo courtesy of DoD 12

Naval Programs Examples of Titanium Uses in Non-Aerospace Defense Mission module structures Pipe and fittings MAST components Fasteners Structural hardware components and systems Ship hull structural applications Castings for valve and pump bodies and internals Ti Pipe CVN* 13 *Photo courtesy of DoD Ti Impeller Virginia Class Submarine*

DoD has created MIL-DTL-46077G for Titanium Armor Reduced some processing requirements to further reduce costs Created a ballistic specification for 4 classes of non-aerospace Ti Class 1 and 2 are the same chemistries as Ti-6-4 ELI and standard grade 5 Class 3 allows for higher levels of oxygen Class 4 removes the requirement for aluminum and vanadium as long as it still falls into the alpha-beta range of alloys and meets all other requirements of the MIL-DTL-46077 specification. ATI 425 -MIL alloy falls in Class 4 ARL believes that the ATI 425 -MIL Alloy offers the best potential to increase applications for both commercial and military platforms * * ARL Report - The Design and application of Titanium Alloys to U.S. Army Platforms 2010 14

Military Airframe, Land & Sea Based Applications for Titanium Richard J. Harshman Chairman, President and Chief Executive Officer of ATI Titanium 2012 Atlanta, GA October 8, 2012