Browse Topic: Titanium alloys

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Titanium Alloy, Sheet and Strip, 15Mo - 3.0AI - 2.8Cb - 0.20SiAMS4897F (Current)04/14/2025
This specification covers a titanium alloy in the form of sheet and strip 0.125 inch (3.18 mm) and under in nominal thickness (see 8.6).
AMS G Titanium and Refractory Metals Committee
Material Specification
Titanium Alloy Bars and Forging Stock, 6.0Al - 4.0V Extra Low Interstitial, AnnealedAMS6932D (Current)04/14/2025
This specification covers a titanium alloy in the form of bars up through 10.000 inches (2540 mm) in nominal diameter or least distance between parallel sides, inclusive, with bars having a maximum cross-sectional area of 79 square inches (509.67 cm2), and stock for forging of any size (see 8.7).
AMS G Titanium and Refractory Metals Committee
Material Specification
Titanium Alloy, Sheet, Strip, and Plate, 5Al - 2.5Sn, Extra Low Interstitial, AnnealedAMS4909M (Current)04/14/2025
This specification covers a titanium alloy in the form of sheet, strip, and plate up to 1.000 inch (25.40 mm), inclusive (see 8.6).
AMS G Titanium and Refractory Metals Committee
Material Specification
Titanium Alloy Bars, Forgings, and Rings, 5Al - 2.5Sn, Extra Low Interstitial, AnnealedAMS4924K (Current)03/25/2025
This specification covers a titanium alloy in the form of bars, wire, forgings, flash-welded rings 4.000 inches (101.60 mm) and under in nominal diameter or least distance between parallel sides, and stock for forging and flash-welded rings of any size (see 8.6).
AMS G Titanium and Refractory Metals Committee
Material Specification
Minimizing Stress-Corrosion Cracking in Wrought Titanium Alloy ProductsARP982E (Current)03/25/2025
Primarily to provide recommendations concerning minimizing stress-corrosion cracking in wrought titanium alloy products.
AMS G Titanium and Refractory Metals Committee
Recommended Practice
Strain-Controlled High-Temperature (400°C) Low-Cycle Fatigue of Additive Manufactured Ti6Al4V Alloy05-18-03-002403/21/2025
The tensile and low-cycle fatigue (LCF) properties of Ti6Al4V specimens, manufactured using the selective laser melting (SLM) additive manufacturing (AM) process and subsequently heat-treated in argon, were investigated at elevated temperatures. Specifically, fully reversed strain-controlled tests were performed at 400°C to determine the strain-life response of the material over a range of strain amplitudes of industrial interest. Fatigue test results from this work are compared to those found in the literature for both AM and wrought Ti6Al4V. The LCF response of the material tested here is in-family with the AM data found in the literature. Scanning electron microscopy performed on the fracture surfaces indicate a marked increase in secondary cracking (crack branching) as a function of increased plastic deformation and demonstrating equivalent performance when compared to the wrought Ti6AL4V at RT (room temperature) at 1.4% strain amplitude and better performance when compared to the
Gadwal, Narendra Kumar, Barkey, Mark E., Hagan, Zach, Amaro, Robert, McDuffie, Jason G.
Journal Article
Titanium Alloy Tubing, Seamless, Hydraulic, 3Al - 2.5V, Texture Controlled, Cold Worked, Stress RelievedAMS4946G (Current)03/05/2025
This specification covers a titanium alloy in the form of seamless tubing (see 8.7).
AMS G Titanium and Refractory Metals Committee
Material Specification
Titanium Alloy Tubing, Seamless, Hydraulic, 3Al - 2.5V, Controlled Contractile Strain Ratio, Cold Worked, Stress RelievedAMS4945J (Current)03/05/2025
This specification covers a titanium alloy in the form of seamless tubing (see 8.7).
AMS G Titanium and Refractory Metals Committee
Material Specification
Titanium Alloy, Sheet, Strip, and Plate, 4.5AI - 3V - 2Fe - 2Mo, AnnealedAMS4899F (Current)03/05/2025
This specification covers a titanium alloy in the form of sheet, strip, and plate up through 4.000 inches (101.60 mm), inclusive (see 8.6).
AMS G Titanium and Refractory Metals Committee
Material Specification
Titanium Alloy Tubing, Seamless, Hydraulic, 3.0Al - 2.5V, Cold Worked, Stress RelievedAMS4944N (Current)03/05/2025
This specification covers a titanium alloy in the form of seamless tubing (see 8.6).
AMS G Titanium and Refractory Metals Committee
Material Specification
Titanium Alloy, Forgings, 10V - 2Fe - 3AI, Consumable Electrode Melted, Single-Step Solution Heat Treated and Overaged, 140 ksi (965 MPa) Tensile StrengthAMS4987G (Current)02/25/2025
This specification covers a titanium alloy in the form of forgings 4.00 inches (101.6 mm) and under in nominal cross-sectional thickness and of forging stock of any size (see 8.6).
AMS G Titanium and Refractory Metals Committee
Material Specification
Advanced Parameter Forecasting for Titanium Grade 19 Machining in Automotive Applications2025-28-004502/07/2025
Electrochemical machining (ECM) is a remarkably effective technique for producing detailed designs in materials that can conduct electricity, regardless of their level of hardness. As the desire for high-quality products and the necessity for rapid design changes grow, decision-making in the industrial sector becomes increasingly intricate. This work focuses on Titanium Grade 19 and proposes the development of prediction models using regression analysis to estimate performance measurements in ECM. The experiments are designed using Taguchi's methodology, employing a multiple regression approach to produce mathematical equations. The Taguchi technique is utilized for the purpose of single-objective optimization in order to determine the optimal combination of process parameters that will optimize the rate at which material is removed. ANOVA is a statistical method used to assess the relevance of process factors that impact performance indicators. The suggested prediction technique for
Pasupuleti, Thejasree, Natarajan, Manikandan, Ramesh Naik, Mude, Silambarasan, R, D, Palanisamy
Technical Paper
Data-Driven Optimization of Titanium Grade 7 Machining for Automotive Applications2025-28-014302/07/2025
Electrochemical machining (ECM) is a highly efficient method for creating intricate structures in materials that conduct electricity, irrespective of their level of hardness. With the rising demand for superior products and the necessity for quick design modifications, decision-making in the industrial sector becomes increasingly complex. This study specifically examines Titanium Grade 7 and suggests creating prediction models through regression analysis to estimate performance measurements in ECM. The experiments are formulated based on Taguchi's ideas, utilizing a multiple regression approach to deduce mathematical equations. The Taguchi method is utilized for single-objective optimization in order to determine the ideal combination of process parameters that will maximize the material removal rate. ANOVA is a statistical method used to determine the relevance of process factors that affect performance measures. The suggested prediction technique for Titanium Grade 7 exhibits
Natarajan, Manikandan, Pasupuleti, Thejasree, Kumar, V, Krishnamachary, PC, Somsole, Lakshmi Narayana, Silambarasan, R
Technical Paper
Optimizing Titanium Alloy Grade 7 Machining with Grey Relational Analysis2025-28-004902/07/2025
Electrochemical machining (ECM) is a highly efficient method for creating intricate structures in materials that conduct electricity, irrespective of their level of hardness. Due to the growing need for superior products and the requirement for quick design adjustments, decision-making in production has become more complex. This study focuses on Titanium Grade 7 and suggests creating predictive models utilizing a Taguchi-grey technique to achieve multi-objective optimization in ECM. The trials are structured based on Taguchi's principles, utilizing Taguchi-grey relational analysis (GRA) to simultaneously maximize several performance indicators. This entails optimizing the pace at which material is removed, decreasing the roughness of the surface, and attaining precise geometric tolerances. ANOVA is used to assess the relevance of process variables that affect these measures. The suggested predictive technique for Titanium Grade 7 outperforms current models in terms of flexibility
Pasupuleti, Thejasree, Natarajan, Manikandan, Kumar, V, Sagaya Raj, Gnana, Krishnamachary, PC, Silambarasan, R
Technical Paper
Grey Relational Analysis for Multi-Objective Optimization in Aerospace Machining of Titanium Grade 192025-28-004702/07/2025
Electrochemical machining (ECM) is a highly efficient method for creating intricate structures in electrically conductive materials, irrespective of their hardness. Due to the growing need for superior products and quick design adjustments, decision-making in production has become increasingly complex. This study focuses on Titanium Grade 19 and proposes creating predictive models using a Taguchi-grey technique to achieve multi-objective optimization in ECM. The experiments are structured based on Taguchi's principles, utilizing Taguchi-grey relational analysis (GRA) to simultaneously optimize several performance indicators, including the material removal rate, surface roughness, and geometric tolerances. ANOVA is employed to assess the significance of process variables affecting these measures. The proposed predictive technique for Titanium Grade 19 outperforms current models in terms of flexibility, efficiency, and accuracy, providing enhanced capabilities for monitoring and control
Pasupuleti, Thejasree, Natarajan, Manikandan, Krishnamachary, PC, Katta, Lakshmi Narasimhamu, Silambarasan, R
Technical Paper
Titanium Alloy, Cold Rolled Sheet and Strip, 15V - 3Al - 3Cr - 3Sn, Solution Heat TreatedAMS4914J (Current)01/22/2025
This specification covers a titanium alloy in the form of sheet and strip up to and including 0.125 inch (3.18 mm) in nominal thickness.
AMS G Titanium and Refractory Metals Committee
Material Specification
Chemical Check Analysis Limits, Titanium and Titanium AlloysAMS2249K (Current)12/10/2024
This specification defines limits of variation for determining acceptability of the composition of cast or wrought titanium and titanium alloy parts and material acquired from a producer.
AMS G Titanium and Refractory Metals Committee
Material Specification
Titanium Alloy Sheet, Strip, and Plate, 6Al - 4V, Solution Heat TreatedAMS4903E (Current)12/10/2024
This specification covers a titanium alloy in the form of sheet, strip, and plate up through 2.000 inches (50.80 mm), inclusive (see 8.6)
AMS G Titanium and Refractory Metals Committee
Material Specification
Titanium Alloy, Bars, Wire, Forgings, Rings, and Drawn Shapes, 4Al - 2.5V -1.5 Fe, Annealed, Heat TreatableAMS6947C (Current)12/10/2024
This specification covers a titanium alloy in the form of bars, wire, forgings, flash-welded rings, and drawn shapes 4.000 inches (101.60 mm) and under and stock for forging, heading, or flash-welded rings of any size (see 8.6).
AMS G Titanium and Refractory Metals Committee
Material Specification
Titanium Alloy Bars, Wire, Forgings, Rings, and Drawn Shapes, 4Al - 2.5V -1.5 Fe, AnnealedAMS6948C (Current)12/10/2024
This specification covers a titanium alloy in the form of bars, wire, forgings, flash-welded rings, drawn shapes 5.000 inches (127.00 mm) and under, and stock for forging or flash-welded rings of any size (see 8.6).
AMS G Titanium and Refractory Metals Committee
Material Specification
Titanium Alloy, Ti-6Al-4V, Hot Isostatically Pressed (Low Temperature, High Pressure), Produced by Laser Powder Bed FusionAMS7028 (Current)12/03/2024
This specification covers an alpha-beta Ti-6Al-4V alloy produced by laser powder bed fusion (L-PBF) additive manufacturing and subjected to hot isostatic press (HIP) operation. Typically, this material is used for complex-shaped aerospace products made to near net shape dimensions. These products have been used typically for parts requiring operating strength up to 750 °F (399 °C), but usage is not limited to such applications.
AMS AM Additive Manufacturing Metals
Material Specification
Titanium Alloy Bars, Forgings, and Forging Stock 6.0Al - 2.0Sn - 4.0Zr - 6.0Mo Solution Heat Treated and AgedAMS6906D (Current)11/06/2024
This specification covers a titanium alloy in the form of bars up through 4.000 inches (101.60 mm) in nominal diameter or least distance between parallel sides, inclusive, and maximum cross-sectional area of 32 square inches (206.5 cm2), forgings of thickness up through 4.000 inches (101.60 mm), inclusive, and maximum cross-sectional area of 32 square inches (206.5 cm2), and stock for forging of any size (see 8.6).
AMS G Titanium and Refractory Metals Committee
Material Specification
Titanium Alloy, Round Bar and Wire, 3AI - 8V - 6Cr - 4Mo - 4Zr, Consumable Electrode Melted, Solution Heat Treated and Cold DrawnAMS4957H (Current)11/06/2024
This specification covers a titanium alloy in the form of round bar and wire 0.625 inch (15.88 mm) and under in nominal diameter or thickness (see 8.7).
AMS G Titanium and Refractory Metals Committee
Material Specification
Titanium Alloy Sheet, Strip, and Plate, 6Al - 6V - 2Sn, Solution Heat Treated and AgedAMS4990E (Current)11/06/2024
This specification covers a titanium alloy in the form of sheet, strip, and plate up through 4 inches (101.6 mm) (see 8.5).
AMS G Titanium and Refractory Metals Committee
Material Specification
Titanium Alloy, Sheet and Strip, 4Al - 2.5V - 1.5Fe, Electron Beam Single Melted. AnnealedAMS6949B (Current)11/06/2024
This specification covers a titanium alloy in the form of sheet and strip up to 0.143 inch (3.63 mm), inclusive, in nominal thickness (see 8.6).
AMS G Titanium and Refractory Metals Committee
Material Specification
Forgings, Titanium Alloys Heat-Treated, Finished-Part Properties: Short-Traverse Tensile, Fracture Toughness, and Longitudinal Time-Dependent-TensionAMS4938B (Current)11/06/2024
This specification establishes requirements for titanium forgings of any shape or form from which finished parts are to be made (see 2.4.4, 8.3, and 8.6).
AMS G Titanium and Refractory Metals Committee
Material Specification
Titanium Alloy Bars, Forgings and Forging Stock 3.0Al - 2.5V AnnealedAMS6940C (Current)10/11/2024
This specification covers a titanium alloy in the form of bars up through 1.000 inch (25.40 mm) in diameter or least distance between parallel sides, inclusive, forgings of thickness up through 1.000 inch (25.40 mm), inclusive, high-strength fastener stock up through 1.250 inch (31.75 mm), inclusive, and stock for forging of any size (see 8.7).
AMS G Titanium and Refractory Metals Committee
Material Specification
Titanium Alloy Sheet 6Al - 4V Driver SheetAMS4932E (Current)08/23/2024
This specification covers a titanium alloy in the form of sheet.
AMS G Titanium and Refractory Metals Committee
Material Specification
Comprehensive Analysis of Titanium Alloy Machining with 2–7% Carbon Nanotube-Infused Cubic Boron Nitride Grinding Wheel Utilizing Full-Factorial Design2024-01-507908/12/2024
This research explores the experimental analysis of titanium alloy using an innovative approach involving a 2–7% carbon nanotube (CNT)-infused cubic boron nitride (CBN) grinding wheel. Employing a full-factorial design, the study systematically investigates the interactions among varied wheel speed, workpiece feed rate, and depth of cut, revealing compelling insights. The integration of CNTs in the CBN grinding wheel enhances the machining performance of titanium alloy, known for its high strength and challenging machinability. The experiment varies CNT infusion levels to assess their impact on material removal rate (MRR) and surface finish. Significantly, MRR is influenced by CNT content, with 5% and above demonstrating optimal performance. The 7% CNT-CBN wheel exhibits a remarkable 61% improvement in MRR over the conventional CBN wheel. Interaction studies highlight the pivotal role of depth of cut, indicating that slower speeds and feeds, combined with increased depth of cut
Stephen, Deborah Serenade, Sethuramalingam, Prabhu
Technical Paper
Titanium Alloy, Sheet, Strip, and Plate, 6Al - 4V, AnnealedAMS4911S (Current)08/01/2024
This specification covers a titanium alloy in the form of sheet, strip, and plate up through 4.000 inches (101.60 mm), inclusive, in thickness (see 8.6).
AMS G Titanium and Refractory Metals Committee
Material Specification
Approval and Control of Premium-Quality Titanium AlloysAMS2380H (Current)07/26/2024
This specification covers the procedures for approval of products of premium-quality titanium alloys and the controls to be exercised in producing such products.
AMS G Titanium and Refractory Metals Committee
Material Specification
Titanium Alloy Bars, Forgings, and Forging Stock, 7.0Al - 4.0Mo, AnnealedAMS6915D (Current)07/26/2024
This specification covers a titanium alloy in the form of bars up through 6.000 inches (152.40 mm), inclusive, in nominal diameter or least distance between parallel sides, forgings of thickness up through 6.000 inches (152.40 mm), inclusive, and stock for forging of any size (see 8.6).
AMS G Titanium and Refractory Metals Committee
Material Specification
Titanium Alloy Bars, Forgings, and Forging Stock 3Al - 8V - 6Cr - 4Mo - 4Zr Solution Heat TreatedAMS6920E (Current)07/25/2024
This specification covers a titanium alloy in the form of bars up through 4.000 inches (101.60 mm) in nominal diameter or least distance between parallel sides, inclusive, forgings of thickness up through 4.000 inches (101.60 mm), inclusive, and stock for forging of any size (see 8.6).
AMS G Titanium and Refractory Metals Committee
Material Specification
Design and Optimization of Lightweight Alloys for Automotive ApplicationsSAE-PP-0040007/22/2024
Effective integration of lightweight materials is becoming more and more important to the automobile industry as a means of improving vehicle efficiency, performance, and sustainability. A key element in accomplishing these goals is the use of lightweight alloys, which are distinguished by their high strength-to-weight ratios and customized mechanical properties. Using databases and computer tools like CES EduPack, this study investigates the design and optimization of lightweight alloys for automotive body panels, guaranteeing that the materials chosen are both economically and environmentally sustainable. The results of the study offer insightful data on developing more efficient automobile alloys in the future, advancing the field of sustainable automobile technology.
Al-Ezzi, Athil
Pre-Print Article
Titanium Alloy Direct Deposited Products 6Al - 4V AnnealedAMS4999B (Current)07/03/2024
This specification covers metal products fabricated by direct metal deposition.
AMS AM Additive Manufacturing Metals
Material Specification
Titanium Alloy Forgings, 8Al - 1Mo - 1V, Solution Heat Treated and StabilizedAMS4973K (Current)06/26/2024
This specification covers a titanium alloy in the form of forgings up to 4.000 inches (101.60 mm), inclusive, and forging stock (see 8.6).
AMS G Titanium and Refractory Metals Committee
Material Specification
Effect of Fatigue Loads on behavior of 2024 Aluminum for Aircraft Hydraulic Applications2024-26-043106/01/2024
Hydraulic systems in aircraft largely comprise of metallic components with high strength to weight ratios. Some examples of such material include Aluminum and Titanium alloys which are typically chosen for low and high-pressure applications respectively. For aircraft fluid conveyance products, hydraulic conduits are fabricated by axisymmetric turning to support flow conditions. The hydraulic conduits can have grooved interfaced design within for placement of elastomeric sealing components. This article presents a systematic study carried out on common loads experienced by fluid carrying conduits and the failure modes induced. Firstly, a static structural analysis was carried out on each of the geometries of the test articles to identify the locations having areas of high stress concentration. Test articles of various wall thicknesses and internal diameters were pressure impulse tested at different conditions of side loads to identify cycle numbers till failure and failure locations. On
Paidimarri, Vishal, Jacob, Krupa, Harish, Uppu, Hovis, David
Technical Paper
Identification, Titanium and Titanium Alloy Wrought ProductsAMS2809B (Current)05/24/2024
This specification covers procedures for identifying wrought products of titanium and titanium alloys.
AMS G Titanium and Refractory Metals Committee
Material Specification
Enhanced Ultrasonic Immersion Inspection for Titanium Alloy and other Metal Alloy BilletsAMS2628C (Current)05/17/2024
This specification covers procedures for ultrasonic immersion inspection of premium-grade wrought titanium and titanium alloy round billet 5 inches (127 mm) and over in nominal diameter (see 2.6.1). Metal alloy billets other than titanium may be tested to this specification with the use of suitable reference standards.
AMS K Non Destructive Methods and Processes Committee
Material Specification
Surface Properties of Shot-Peened and Plasma Sprayed Powder-Coated Alpha-Beta Titanium Alloy Implants2024-01-506005/15/2024
The paramount importance of titanium alloy in implant materials stems from its exceptional qualities, yet the optimization of bone integration and mitigation of wear and corrosion necessitate advanced technologies. Consequently, there has been a surge in research efforts focusing on surface modification of biomaterials to meet these challenges. This project is dedicated to enhancing the surface of titanium alloys by employing shot peening and powder coatings of titanium oxide and zinc oxide. Comparative analyses were meticulously conducted on the mechanical and wear properties of both treated and untreated specimens, ensuring uniformity in pressure, distance, and time parameters across all experiments. The outcomes underscore the efficacy of both methods in modifying the surface of the titanium alloy, leading to substantial alterations in surface properties. Notably, the treated alloy exhibited an impressive nearly 12% increase in surface hardness compared to its untreated counterpart
Balasubramanian, K., Bragadeesvaran, S. R., Raja, R., Jannet, Sabitha
Technical Paper
Titanium Alloy Welding Wire, 5Al - 2.5SnAMS4953J (Current)04/25/2024
This specification covers a titanium alloy in the form of welding wire (see 8.5).
AMS G Titanium and Refractory Metals Committee
Material Specification
Titanium Alloy Bars, Forgings, and Flash-Welded Rings, 5Al - 2.5V - 4Sn - 1Co - 0.8Fe AnnealedAMS6903 (Current)04/25/2024
This specification covers a titanium alloy in the form of bars, forgings, and flash-welded rings up through 12.000 inches (304.80 mm), inclusive, in diameter or least distance between parallel sides, and stock of any size for forging or flash-welded rings. Bars, forgings, and flash-welded rings with a nominal thickness of 3.000 inches (79.20 mm) or greater shall have a maximum cross-sectional area of 113 square inches (729 cm2) (see 8.5).
AMS G Titanium and Refractory Metals Committee
Material Specification
Titanium Alloy Bars, Forgings and Forging Stock, 6.0Al - 6.0V - 2.0Sn, Solution Heat Treated and AgedAMS6935D (Current)04/25/2024
This specification covers a titanium alloy in the form of bars up through 4.000 inches (101.60 mm) in nominal diameter or least distance between parallel sides, inclusive, forgings of thickness up through 4.000 inches (101.60 mm), inclusive, with bars and forgings having a maximum cross-sectional area of 32 square inches (204.46 cm2), and stock for forging of any size (see 8.6).
AMS G Titanium and Refractory Metals Committee
Material Specification
Titanium Alloy, Sheet, Strip, and Plate 4Al - 2.5V - 1.5Fe AnnealedAMS6946E (Current)04/01/2024
This specification covers a titanium alloy in the form of sheet, strip, and plate 0.020 inch (0.50 mm) through 2.10 inches (53.3 mm), inclusive, in nominal thickness (see 8.5).
AMS G Titanium and Refractory Metals Committee
Material Specification
Titanium Alloy Bars, Wire, and Rings, 8Al - 1Mo - 1V, Solution Heat Treated and StabilizedAMS4972K (Current)04/01/2024
This specification covers a titanium alloy in the form of bars, wire, flash-welded rings up through 4.000 inches (101.60 mm), inclusive, in diameter or least distance between parallel sides, and stock for flash-welded rings or heading of any size (see 8.6).
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Material Specification
Titanium Alloy Sheet, Strip, and Plate 6Al - 2Sn - 4Zr - 2Mo - 0.08Si Duplex AnnealedAMS4919K (Current)04/01/2024
This specification covers a titanium alloy in the form of sheet, strip, and plate 0.025 to 3.000 inches (0.64 to 76.20 mm), inclusive, in nominal thickness (see 8.6).
AMS G Titanium and Refractory Metals Committee
Material Specification
Titanium Alloy, Bars, Wire, and Rings 5Al - 2.5Sn Annealed, 110 ksi (758 MPa) Yield StrengthAMS4926R (Current)04/01/2024
This specification covers a titanium alloy in the form of bars, wire, flash-welded rings 4.000 inches (101.60 mm) and under in nominal diameter or least distance between parallel sides and 16 square inches (103 cm2) and under in cross-sectional area, and stock of any size for flash-welded rings (see 8.7).
AMS G Titanium and Refractory Metals Committee
Material Specification
Titanium Alloy Bars, Wire, Forgings, and Rings 4.5Al - 3V - 2Fe - 2Mo AnnealedAMS4964D (Current)03/27/2024
This specification covers a titanium alloy in the form of bars, wire, forgings, flash-welded rings, and stock for forgings or flash-welded rings up through 6.000 inches (152.40 mm) in nominal diameter or distance between parallel sides (see 8.6).
AMS G Titanium and Refractory Metals Committee
Material Specification
Titanium Alloy, Extrusions and Flash Welded Rings, 6Al - 4V, Solution Heat Treated and AgedAMS4934J (Current)03/04/2024
This specification covers a titanium alloy in the form of extruded bars, shapes, and flash-welded rings up through 3.000 inches (76.20 mm), inclusive, in nominal diameter or least distance between parallel sides, and stock for flash-welded rings of any size (see 8.7).
AMS G Titanium and Refractory Metals Committee
Material Specification
Titanium Alloy Bars, Forgings, and Forging Stock, 5Al - 2.5Sn, Extra Low Interstitial, AnnealedAMS6901D (Current)03/01/2024
This specification covers a titanium alloy in the form of bars up through 4.000 inches (101.60 mm), inclusive, in nominal diameter or least distance between parallel sides, forgings of thickness up through 4.000 inches (101.60 mm), inclusive, and stock for forging of any size (see 8.7).
AMS G Titanium and Refractory Metals Committee
Material Specification
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