Ti Grade 2

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Ti Grade 2 / UNS R50400 / AMS 4902 / AMS 4941

Ti Grade 2
UNS R50400 · W.Nr. 3.7035 · DIN 17850 Ti 2 · ASTM Grade 2 · COMMERCIALLY PURE (unalloyed) titanium, alpha phase. Ceilings: O 0.25% max · Fe 0.30% max · N 0.03% max · C 0.08% max · H 0.015% max · each other element 0.10% max · other elements total 0.40% max · balance Ti. It is the most widely used grade of commercially pure titanium. IT DOES NOT PRECIPITATION HARDEN AND IT DOES NOT QUENCH HARDEN: it is single-phase alpha and strength cannot be added by heat treatment.
Not to be confused with

AISI 316LTi Grade 5Ti Grade 1

For what
It is bought for welded and formed equipment where corrosion resistance and moderate strength are both required: sea-water and brackish-water heat exchangers and condensers, chlorine and chlorine dioxide lines, hypochlorite and nitric acid service, chemical process tanks and piping, desalination…
Forms
Round bar · flat bar · plate · sheet · tube · forgings. All forms are supplied to order.
Standards
AMS (verified): 4902 – sheet, strip and plate up through 25.4 mm; commercially pure, annealed, 40.0 ksi (276 MPa) yield strength · 4942 – seamless tubing, annealed, 40 ksi yield · 4941 – WELDED tubing, annealed, 40 ksi yield · 4951 – welding wire, commercially pure. No verified AMS number was found for Grade 2 BAR or FORGINGS. ASTM: B265 / SB-265 (strip, sheet, plate) · B348 / SB-348 (bars and billets) · B338 / SB-338 (condenser and heat exchanger tubes) · B861 (seamless pipe) · B862 (welded pipe) · B363 (welding fittings) · B381 Grade F-2 (forgings) · B863 (wire) · B367 (castings) · F67 Grade 2 (surgical implants) · F467 (nuts) · F468 (bolts). EN / DIN: DIN 17850 Ti 2 (composition, W.Nr. 3.7035) · DIN 17860 (sheet/plate) · DIN 17862 (bar) · DIN 17864 (forgings). MIL: MIL-T-9046 / AMS-T-9046 CP-3 – the CP number runs OPPOSITE to the grade number. Welding: AWS A5.16 / SFA-5.16 ERTi-2. ASME Section IX P-No 51.
THE MIL-T-9046 / AMS-T-9046 CP NUMBERS RUN OPPOSITE TO THE ASTM GRADE NUMBERS: CP-1 = Grade 4 · CP-2 = Grade 3 · CP-3 = Grade 2 · CP-4 = Grade 1. If an old drawing says ‘CP-1’, that is Grade 4, not Grade 1.
Advantage
Breadth of product forms. Grade 2 is the only one of the three grades that appears in EVERY main ASTM product form: plate (B265), bar (B348), heat exchanger tube (B338), seamless pipe (B861), welded pipe (B862), fittings (B363), forgings (B381 F-2), wire (B863) and castings (B367).
Welding
Filler metal: matching commercially pure rod to AWS A5.16 / ASME SFA-5.16 – ERTi-1 for Grade 1, ERTi-2 for Grade 2, ERTi-4 for Grade 4. Preheat is NOT required and post-weld heat treatment is not mandatory (Corrosion Materials).
Limits
IT DOES NOT HARDEN BY HEAT TREATMENT. There is no quenching, no solution treatment and no ageing; when a drawing calls for a hardness value, this grade is the wrong choice. FORBIDDEN BAND – ABOVE 590-620 °C IN AIR: annealing or hot forming in air above this temperature produces oxide scale and a diffused-in oxygen layer (alpha case);
Compiled from manufacturer data sheets · confirm against the current specification before ordering

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On this page · click to jump
What Titanium Grade 2 IsStandards by Product FormASME Code Acceptance and MAXIMUM CODE TEMPERATURESProduct Forms With NO StandardChemical CompositionMechanical PropertiesPhysical PropertiesHeat Treatment and Thermal StabilityWeldingMachiningCorrosionFrequently Asked Questions



Ti Grade 2 is another commercially pure form of titanium and is known as unalloyed titanium. Like Ti Grade 1 it offers very high purity, but it provides higher strength in terms of mechanical properties. It contains 99.2% titanium and stands out for its corrosion resistance, light weight and biocompatibility.

The commercially pure titanium grades have an excellent strength-to-density ratio and good corrosion resistance. These properties make commercially pure titanium suitable for the manufacture of components in weight-saving structures carrying low mass forces, and also for components requiring high corrosion resistance. In addition, because of the low thermal expansion of titanium, thermal stresses in titanium structures are lower than in other metallic materials. Together with this property, titanium components are increasingly becoming the material of choice in a widening range of sectors. The materials are also widely used in the medical sector because of their exceptional biocompatibility.​‌​​‌​

Application areas: chemical industry, aerospace industry, medical applications.

Machinability: Because it has somewhat higher mechanical properties than pure titanium, it is also somewhat more difficult to machine, but it can be processed with conventional machining techniques. Machinability depends on factors such as the hardness of the alloy, its high melting point and the need to work at elevated temperature.​‌​​‌​

Machining: It can be processed by operations such as milling, turning and drilling, but machining at low speed is recommended. Cutting tools should generally be a hard alloy or carbide, and cutting and cooling fluids should be used to prevent the titanium from overheating.

Welding: It can be welded by the TIG (Tungsten Inert Gas) and MIG (Metal Inert Gas) methods. Oxidation should be prevented during welding by using shielding gases such as argon.​‌​​‌​

Cold forming: Cold forming operations are suitable for Ti Grade 2, and plasma cutting and bending operations can generally also be carried out.

Hot forming: It is suitable for hot forming, but temperatures should not be too high. Working at the lower end of the temperature range is generally recommended for titanium alloys.​‌​​‌​

Chemical Composition

C %​‌​​‌​≤ 0.08
N %​‌​​‌​≤ 0.03
Ti %​‌​​‌​Balance
Fe %​‌​​‌​≤ 0.30
O %​‌​​‌​≤ 0.25
H %​‌​​‌​≤ 0.015
Mechanical Properties at 20 °C

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Hardness HB 30≤ HB 150​‌​​‌​
0.2% Yield Strength Rp N/mm²≥ 275​‌​​‌​
Tensile Strength Rm N/mm²≥ 345​‌​​‌​
Elongation≥ 20%​‌​​‌​
Modulus of Elasticity kN/mm²105​‌​​‌​
Physical Properties at 20 °C

Density gr/cm³​‌​​‌​4.51
Specific Heat Capacity J/kg K​‌​​‌​520
Thermal ConductivityW/m K​‌​​‌​20
Electrical Resistivity Ω mm²/m​‌​​‌​0.48
Standards and Equivalents · Ti Grade 2
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Trade nameTi Grade 2​‌​​‌​
UNSR50400​‌​​‌​
AMS4902 · 4941 · 4942 · 4951​‌​​‌​
Available formsRound bar · Flat bar · Plate · Sheet · Tube · Forgings
All forms are supplied to order.​‌​​‌​

What Titanium Grade 2 Is — and Why It Is the De Facto Standard for Industrial Titanium​‌​​‌​

STANDARDS BY PRODUCT FORM
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Product formStandards
Plate · sheet · stripAMS 4902 (commercially pure, annealed, 40.0 ksi / 276 MPa yield; up through 25.4 mm) · ASTM B265 / ASME SB-265 Grade 2​‌​​‌​
Round bar · flat bar · billetThere is NO verified AMS number for Grade 2 bar. ASTM B348 / ASME SB-348 Grade 2​‌​​‌​
Seamless tubingAMS 4942 (seamless tubing, annealed, 40 ksi yield) · ASTM B338 / ASME SB-338 Grade 2​‌​​‌​
Welded tubingAMS 4941 (WELDED tubing, annealed, 40 ksi yield) · ASTM B338 / ASME SB-338 Grade 2​‌​​‌​
PipeASTM B861 Grade 2 (seamless) · ASTM B862 Grade 2 (welded). The former ASTM B337 has been withdrawn.​‌​​‌​
Welding fittingsASTM B363 / ASME SB-363 (unalloyed titanium welding fittings)​‌​​‌​
ForgingsASTM B381 Grade F-2 · DIN 17864​‌​​‌​
Wire · welding wireAMS 4951 (commercially pure welding wire; the Grade 2 match is given by three sources) · ASTM B863 Grade 2 · AWS A5.16 / SFA-5.16 ERTi-2​‌​​‌​
Castings · fastenersASTM B367 Grade C-2 (castings) · ASTM F467 (nuts) · ASTM F468 (bolts)​‌​​‌​
Surgical implantsASTM F67 Grade 2 (UNS R50400, unalloyed titanium)​‌​​‌​
Pressure vessels · welding qualificationASME Section IX P-No 51 (UNS R50400) · used in ASME Section VIII and related sections through SB-265 / SB-338 / SB-348​‌​​‌​
European · inspection documentDIN 17850 Ti 2 (W.Nr. 3.7035, composition) · DIN 17860 (sheet/plate) · DIN 17862 (bar). EN 10204 is NOT a material specification; it defines the 3.1 / 3.2 document type.​‌​​‌​
AMS numbers are written first, ASTM afterwards. AMS 4900 (55 ksi yield) belongs to GRADE 3 and is written on none of these cards. AMS 4902 belongs to Grade 2, AMS 4901 and AMS 4921 to Grade 4, and AMS 4940 to Grade 1. The numbers are separated by yield strength, not by grade name. EN 10204 is not a material specification but a type of inspection document (2.2 / 3.1 / 3.2).

Titanium Grade 2 (UNS R50400 / W.Nr. 3.7035 / DIN Ti 2 / commonly sold as Ti 99.6) is the workhorse of unalloyed, commercially pure (CP) titanium. At room temperature it is single-phase HCP (α) titanium: no second phase, no precipitate, no hardening mechanism. It cannot be hardened by heat treatment. Its strength comes only from cold work and from interstitial atoms.​‌​​‌​

There is not a single deliberately added alloying element separating Grade 2 from Grade 1. Both are unalloyed titanium and their carbon, nitrogen and hydrogen ceilings are identical. Only two lines in the specification differ: oxygen (0.25 % versus 0.18 %) and iron (0.30 % versus 0.20 %). Those two lines take the minimum yield from 138 MPa to 275 MPa, roughly double — and that is what makes Grade 2 the only CP grade you can practically build a code calculation on.

The Unalloyed Titanium Family · Where Grade 2 Sits (ASTM B265)

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Grade 1
R50250 / 3.7025
O ≤0.18 % · Fe ≤0.20 %. Rm ≥240 MPa · Rp0.2 138–310 MPa · A ≥24 %, bend 1.5T–2T. The most ductile of the family: deep drawing, explosive cladding, anode substrate, lining. Of little use in a code calculation​‌​​‌​
Grade 2
R50400 / 3.7035
O ≤0.25 % · Fe ≤0.30 %. Rm ≥345 MPa · Rp0.2 275–450 MPa · A ≥20 %, bend 2T–2.5T, typical hardness ~80 HRB / ~145 HV. This is the overwhelming majority of industrial titanium: pressure vessels, piping, exchanger tube, flanges, forgings, tank lining. Stocked at every service centre — which is why its price per kilo is often below Grade 1. Grade 2H shares the same UNS and EXACTLY the same chemistry; the only difference is a minimum tensile guaranteed at 400 MPa (58 ksi) instead of 345 — not a new material, but a higher minimum accepted into the code​‌​​‌​
Grade 3 · Grade 4
R50550 / R50700
Gr 3: O ≤0.35 % · Rm ≥448–450 MPa · A ≥18 %. Gr 4: O ≤0.40 % · N ≤0.05 % · Fe ≤0.50 % · Rm ≥552 MPa · A ≥15 %. Formability drops sharply, corrosion behaviour is identical to Grade 2 — strength grades, not corrosion grades​‌​​‌​
Grade 5 · Ti-6Al-4V
R56400 / 3.7165
A different material altogether. An α+β alloy, Rm ≥895 MPa, heat treatable. It is NOT a corrosion upgrade — in reducing media and crevice corrosion it trails the CP grades, and it cannot be cold formed. Detail: Ti Grade 5 / ELI​‌​​‌​

What oxygen does — and why Grade 2 is the sweet spot

In titanium, oxygen is not an impurity — it is an alloying element. It sits interstitially in the HCP lattice, distorts it and blocks dislocation motion — solid solution strengthening in the strictest sense. Yield and tensile rise; elongation, formability and fracture toughness fall; the β transus shifts up (~888 °C in Grade 1, ~913 °C in Grade 2). Iron is a β stabiliser: it leaves a small amount of β at grain boundaries, and iron-rich regions are the weak points in reducing acid and in crevice corrosion.​‌​​‌​

Grade 2’s commercial dominance comes down to one sentence: its interstitial content holds the best balance between engineering-useful strength (275 MPa yield) and still-excellent ductility (20 % minimum, typically above 25 %). Grade 1 welds well but inflates wall thickness in a code calculation; Grades 3 and 4 give strength but cannot be formed and lose weld ductility. Grade 2 welds, forms AND passes the ASME calculation. No other unalloyed titanium grade does all three at once.

Standards by Product Form​‌​​‌​

Unlike the nickel alloys, titanium has an ASTM family numbered separately by product form — and Grade 2 is covered in EVERY specification in it. The table below can go straight onto a purchase order.

Standards by Product Form · Titanium Grade 2 (R50400 / 3.7035)

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Strip · sheet · plate
Bar · billet
ASTM B265 / SB-265 (strip, sheet, plate — annealed) · B348 / SB-348 (bar, billet)​‌​​‌​
Seamless and welded tube
(condenser · exchanger)
ASTM B338 / SB-338 — this is the family standard for seawater condenser and exchanger tube, and Grade 2 is its de facto principal grade​‌​​‌​
PipeSeamless ASTM B861 · welded ASTM B862. ASTM B337 was WITHDRAWN in 1997 and split into these two — do not accept a certificate citing B337​‌​​‌​
Fittings · forgingsASTM B363 / SB-363 (material) + ASME B16.9 (dimensions) — both must appear on the order; Grade 2 uses the WPT2 / WPT2S class codes (letter code not independently verified). Forgings: ASTM B381 / SB-381, F-prefixed — Grade 2 forging is F-2, and the great majority of titanium flanges are made from F-2. Removal of alpha case is an explicit requirement​‌​​‌​
Wire · castingsASTM B863 — titanium DOES have a real wire product specification, a meaningful advantage over the nickel alloys; but the grades covered change from edition to edition, so put the edition year on the order acknowledgement. Castings: ASTM B367 / SB-367 — grades are C-prefixed and Grade 2’s equivalent is C-2; this is the de facto grade for cast titanium valve and pump bodies​‌​​‌​
Surgical implant · aerospaceASTM F67 · in Europe EN ISO 5832-2, which defines six grades by tensile strength — the numbering is not the same as ASTM, so match on chemistry. Aerospace: AMS 4902 (sheet/strip/plate, annealed, 40.0 ksi yield) · AMS 4941 (welded tube) · AMS 4942 (seamless tube) · AMS 4951 (welding filler) · AMS-T-9046 (formerly MIL-T-9046J) class CP-3 = Grade 2. WARNING: the CP numbering runs INVERSE to the ASTM grade number (CP-3 = Gr 2, CP-4 = Gr 1, CP-1 = Gr 4)​‌​​‌​
Welding consumablesBare wire: AWS A5.16 ERTi-2 · W.Nr. filler 3.7036 (Grade 1 filler is ERTi-1 / 3.7026). There is NO covered electrode and there never will be — slag and coating moisture inevitably load titanium with oxygen and hydrogen​‌​​‌​
ASME Section IX · EuropeTitanium base metals sit at P-No. 51–53, unalloyed grades at P-No. 51; fillers at F-No. 51–56, ERTi-1/ERTi-2 at F-No. 51 (the band is verified; the grade-by-grade assignment could not be verified from a primary ASME table — confirm QW/QB-422 before writing a WPS). Europe: DIN 17850 Ti 2, material number 3.7035; product forms DIN 17860 (sheet/plate), 17862 (bar), 17863 (wire), 17864 (forgings). 3.7034 is the WL/aerospace number [D: some mill sheets print 3.7034 as the base-metal number — the base metal is 3.7035]. EN 10204 is NOT a material specification; it defines only the inspection-document type (2.2, 3.1, 3.2)​‌​​‌​

ASME Code Acceptance and MAXIMUM CODE TEMPERATURES

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HEAT TREATMENT — SCHEMATIC

1 · STRESS RELIEF
Step​‌​​‌​1 · STRESS RELIEF
Summary​‌​​‌​Reduces residual stress left by cold forming, straightening, machining and welding. It does not change the grain structure and does not lower strength.
Temperature​‌​​‌​480-595 °C common band. ATI 538-593 °C · HonTitan 538-593 °C · NASA/DMIC 482-593 °C (900-1100 °F) · Corrosion Materials 482-593 °C (900-1100 °F). DIVERGING SOURCES: the RTI/RMI Titanium Alloy Guide gives an upper limit of 649 °C (1200 °F) and Zapp gives a lower limit of 450 °C. NO AVERAGE HAS BEEN TAKEN.
Time​‌​​‌​30 minutes to 2 hours. ATI 30 minutes · HonTitan 30 minutes to 2 hours · RTI 30-60 minutes · Zapp about 30 minutes · NASA/DMIC 15 minutes to 4 hours.
Cooling​‌​​‌​Air cool. Corrosion Materials states forced air or slow cooling; Zapp states inert gas or air.
Resulting hardness​‌​​‌​Hardness and strength are practically unchanged. Stress relief is NOT a hardening step.
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2 · ANNEALING (MILL ANNEAL · RECRYSTALLIZATION)
Step2 · ANNEALING (MILL ANNEAL · RECRYSTALLIZATION)​‌​​‌​
SummaryReturns a cold-worked structure to a fully recrystallized equiaxed alpha structure. Restores formability and corrosion resistance. The temperature stays BELOW the beta transus.​‌​​‌​
Temperature650-760 °C common band. Corrosion Materials 649-760 °C (1200-1400 °F) · HonTitan 649-760 °C for Grades 2-4 and 538-704 °C for Grade 1 · Zapp about 700 °C · ATI 538-704 °C. DIVERGING SOURCE: NASA/DMIC gives 704-871 °C (1300-1600 °F); the top of that band approaches the beta transus. NO AVERAGE HAS BEEN TAKEN.​‌​​‌​
Time6 minutes to 2 hours. Corrosion Materials 6 minutes to 2 hours · ATI 0.5-2 hours · HonTitan 0.5-2 hours · Zapp 3 minutes per mm of section thickness, minimum 15 minutes.​‌​​‌​
CoolingAir cool. NASA/DMIC states air or furnace cooling. Cooling rate does not set the strength; there is NO hardening by quenching.​‌​​‌​
Resulting hardnessAnnealed condition. Specification minimums are written for this condition.​‌​​‌​

3 · VACUUM or PROTECTIVE-ATMOSPHERE ANNEALING
Step​‌​​‌​3 · VACUUM or PROTECTIVE-ATMOSPHERE ANNEALING
Summary​‌​​‌​Not a separate strength step; it is step 2 carried out where a clean surface is required. It prevents alpha case formation and hydrogen pickup and lowers existing hydrogen.
Temperature​‌​​‌​Same as the annealing band, about 540-760 °C. NASA/DMIC gives 538-760 °C (1000-1400 °F) for hydrogen removal.
Time​‌​​‌​NASA/DMIC gives 2-4 hours at 0.5 micron vacuum. These figures come from a single source and are not written here as a binding time.
Cooling​‌​​‌​Cooling under vacuum or argon.
Resulting hardness​‌​​‌​Hardness is unchanged. NASA/DMIC reports that this cycle lowers 550 ppm hydrogen to 25-35 ppm; vacuum annealing is the only practical way to remove hydrogen.
The diagram is schematic; the time axis is NOT to scale. No published TTT/CCT curve was used, so no curve is drawn. THIS MATERIAL IS COMMERCIALLY PURE (alpha phase) TITANIUM: IT DOES NOT HARDEN BY HEAT TREATMENT. There is NO quench hardening, no solution treatment and no ageing step (nothing like H900 or H1025). Strength is set directly by the OXYGEN, IRON and NITROGEN content and by the amount of cold work. The three steps below were each verified separately. Commercially pure titanium is a single-phase alpha material. Total Materia, NASA/DMIC, RTI and HonTitan each state the same thing: in alpha and near-alpha alloys HIGH STRENGTH CANNOT BE DEVELOPED BY HEAT TREATMENT; only stress relief and annealing are used. Annealing is carried out BELOW the beta transus. HonTitan gives the beta transus as about 888 °C for Grade 1, 913 °C for Grade 2, 921 °C for Grade 3 and 949 °C for Grade 4; Carpenter gives 899-927 °C (1650-1700 °F) for Grade 2. A single per-grade figure could not be confirmed in four independent sources, so it is not written as binding. Hot forming is carried out at 480-540 °C (900-1000 °F) for severe operations according to Carpenter; Corrosion Materials gives 204-316 °C (400-600 °F). The two sources diverge and no average has been taken. Annealing or hot forming IN AIR above about 590-620 °C produces a visible oxide scale and a diffused-in oxygen layer (alpha case) (RTI/RMI). On fatigue- or fracture-critical parts this layer must be removed COMPLETELY, either mechanically (grinding, grit blasting) or chemically (molten alkaline descale followed by 5:1 to 10:1 HNO3-HF pickling). Cooling rate does not set the strength of this material. When a specification calls for a hardness value, these grades are not the right choice.

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The ceiling for titanium is strikingly low compared with the nickel alloys you are used to, and it is a CODE limit, not a metallurgical one. Grade 2 is metallurgically perfectly happy at 315 °C; the code stops there because there is no creep and long-term oxidation data behind it. Most of the family’s code lines were published through Grade 2 in the first place — it is the best-documented unalloyed titanium grade in ASME.

ASME Code Acceptance · Titanium Grade 2 (SB-265 / SB-338 / SB-348 / SB-381)

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MAXIMUM CODE TEMPERATURE315 °C (600 °F) — for all applications, published explicitly for SB-265 Grade 2 plate. There is no allowable stress above it; do not offer Grade 2 as a pressure-retaining component above 315 °C​‌​​‌​
Sections that accept itSection VIII Div. 1 and Div. 2 · Section III Class 2/3 · Section XII (transport tanks); one source also lists Section I (power boilers) for Grade 2 plate — all to 315 °C. The Section I row is single-sourced. ASME B31.3 is also in scope and is quoted with the same 315 °C ceiling (not independently verified — confirm Table A-1)​‌​​‌​
ASME B16.5 (flanges)TITANIUM IS NOT IN B16.5. The standard does not include titanium in its material groups, so there is no ready-made pressure–temperature table. A titanium flange is made to B16.5 dimensions, but its rating must be calculated per B16.5 Annex A, or designed as a gasket-dependent flange per VIII Div. 1 Appendix 2. This is the most overlooked item in titanium piping, and it is where the price difference comes from​‌​​‌​
Grade 2HASME-approved H grades: 2H, 7H, 16H, 26H (R50400, R52400, R52402, R52404). Grade 2H gives 400 MPa (58 ksi) minimum tensile and a higher allowable stress on identical chemistry. THERE IS NO SUCH THING AS GRADE 1H. Numerical allowable stresses are not published on this page — Section II Part D values are updated edition to edition; always take the design value from the code edition in force, never from a distributor sheet​‌​​‌​

What an “H” grade is, and whether Grade 2H is worth buying

An H grade is a grade with identical chemistry but a raised minimum tensile strength. Grade 2H has exactly the same composition as Grade 2 — same UNS number, same O, Fe, C, N and H ceilings. The only difference is that the minimum tensile is guaranteed at 400 MPa (58 ksi) instead of 345 MPa (50 ksi); yield stays at 275 MPa and elongation at 20 % for both.
The justification is statistical. The Materials Technology Institute and the International Titanium Association reviewed first more than 400 commercial heats and later more than 5,200 commercial test reports, and showed that over 99 % already met the 58 ksi minimum. So an H grade is not a new material — it is strength that already existed being accepted into the code. In one published example, using Grade 2H under Section VIII Div. 2 (Class 2) rules gives roughly a 14 % material saving over Div. 1.
The practical answer: if you are building a thick-walled, large-diameter vessel and the design can move to Div. 2, ask for 2H — same metal, similar price, thinner wall. In thin sheet, exchanger tube and general piping the difference disappears in practice; there, specifying 2H only narrows your supplier pool.​‌​​‌​

Product Forms With NO Standard — the Commercially Valuable Section

Grade 2 is the most widely covered titanium grade; the gaps are few but expensive. This is the section your sales engineers should memorise.​‌​​‌​

Specification Gaps and Traps for R50400

Flanges​‌​​‌​There is no “ASTM titanium flange specification” — the titanium equivalent of ASTM B462 does not exist. A flange is made from a B381 F-2 forging or from B265 plate; dimensions are ASME B16.5 but the rating is calculated, not read off a table. “Class 150 titanium flange” is not a rating
Covered electrode (SMAW)​‌​​‌​Does not exist and is not technically possible. The honest answer to “titanium electrodes” is GTAW/ERTi-2 or GMAW; no covered electrode
Bolts · nuts · spring wire​‌​​‌​ASTM F467 (nuts) and F468 (bolts) include titanium grades, but Grade 2 coverage could not be independently verified. Besides, 275 MPa minimum yield is low for a highly preloaded joint; the practical route is Grade 4 or Grade 5, and titanium fasteners carry a real galling risk (a solid lubricant or coating is mandatory). Same for spring wire: B863 covers it but spring temper is not a defined strength class
Hardening by heat treatment​‌​​‌​Not a process gap — a physical impossibility. Grade 2 is single-phase α titanium; there is no solution treat plus age, so for surface hardness the route is anodising, nitriding or coating. Europe also has no current EN product-standard family for titanium; what is actually used is the DIN 17850 family plus the ASTM B series, and the practical answer is ASTM chemistry with an EN 10204 3.1 certificate

Chemical Composition​‌​​‌​

For unalloyed titanium, “composition” means writing down the interstitial ceilings. There are five lines on the certificate; two of them (oxygen, iron) define the grade.

Chemical Composition · ASTM B265 / B348 / B338 Grade 2 (weight %)

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Oxygen · IronO ≤0.25 and Fe ≤0.30 — the two lines that define the grade. Grade 1: ≤0.18 and ≤0.20; Grade 3: O ≤0.35. Grade 2H chemistry is identical to Grade 2 — H is not a chemistry class but a mechanical-guarantee class​‌​​‌​
Carbon · NitrogenC ≤0.08 · N ≤0.03 — both identical to Grade 1. Nitrogen is roughly twice as potent a strengthener as oxygen, which is why its ceiling is so low​‌​​‌​
Hydrogen · othersH ≤0.015 (150 ppm) — same as Grade 1; this line is the first line of defence against hydrogen embrittlement. Other elements ≤0.1 each, ≤0.4 total; balance titanium — hence the trade name Ti 99.6​‌​​‌​
Source conflict [D]Some mill sheets print the carbon ceiling as 0.10 %. The current ASTM B265 value is 0.08 % — 0.10 is a leftover from an older edition. Write 0.08 % with the edition year on the order​‌​​‌​
ASTM versus DIN/EN Divergences — the Ones That Matter on a Certificate

Chemistry​‌​​‌​There is no divergence in chemistry. DIN 17850 Ti 2 and ASTM B265 Grade 2 use the same ceilings: O ≤0.25 · Fe ≤0.30 · C ≤0.08 · N ≤0.03 · H ≤0.015. The problem is not chemistry, it is mechanicals
Tensile strength​‌​​‌​THIS IS THE TRAP. ASTM B265 gives only a minimum (Rm ≥345 MPa); DIN Ti 2 gives a RANGE (390–540 MPa). So a heat conforming to ASTM can fall below the DIN lower limit (360 MPa) or exceed its upper limit (560 MPa). Tell a customer who wants dual certification this at order stage
Yield and elongation​‌​​‌​ASTM B265: 275–450 MPa (40–65 ksi) — a maximum as well as a minimum. The commonly published DIN Ti 2 value is ≥270 MPa (the source labels it a 1.0 % offset; take care comparing with Rp0.2). The ASTM maximum is the line most buyers miss: heavily cold-worked, “stronger” Grade 2 does not conform. Elongation: ASTM A ≥20 % versus DIN ≥22 %, so an ASTM B265 Grade 2 certificate does NOT automatically mean DIN 17850 Ti 2 conformity
Numbers and certificate​‌​​‌​3.7035 = DIN 17850 Ti 2 (base metal) · 3.7034 = WL/aerospace · 3.7036 = welding FILLER wire. [D: several mill sheets print the Grade 2 base metal as 3.7034 — a common error.] On the certificate, EN 10204 3.1 is the European norm in practice; 3.2 (third party) may be required for PED pressure equipment

Mechanical Properties​‌​​‌​

STRENGTH VALUES
Yield (MPa)Tensile (MPa)ASTM B265 / ASME SB-265 – annealed strip, sheet and plate345275ASTM B348 / ASME SB-348 – annealed bars and billets345275AMS 4902 – annealed sheet, strip and plate (up through 25.4 mm)276AMS 4941 (welded tubing) and AMS 4942 (seamless tubing) – annealed276
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ConditionHardnessYield MPaTensile MPaElongation
ASTM B265 / ASME SB-265 – annealed strip, sheet and plate—​‌​​‌​275-450345​‌​​‌​20%
ASTM B348 / ASME SB-348 – annealed bars and billets​‌​​‌​—275​‌​​‌​34520%​‌​​‌​
AMS 4902 – annealed sheet, strip and plate (up through 25.4 mm)—​‌​​‌​276—​‌​​‌​—
AMS 4941 (welded tubing) and AMS 4942 (seamless tubing) – annealed​‌​​‌​—276​‌​​‌​——​‌​​‌​
In the chart, a value given as a range is drawn at its lower bound; the full range is in the table. All rows are for the ANNEALED condition. Commercially pure titanium has no other heat treatment condition; there is no condition code such as H900 or QT650. THE HARDNESS COLUMN IS DELIBERATELY EMPTY. Commercially pure titanium is not ordered by hardness and ASTM B265 / B348 give no hardness minimum or maximum. RTI gives about 70 / 82 / 90 / 100 HRB (Grades 1-4) and ATI gives about 80 HRB for Grade 2 and about 100 HRB for Grade 4; four independent sources could not be found, so no value is written in the table. THE YIELD STRENGTH ALSO HAS A MAXIMUM in the specification. ASTM B265 gives both a minimum and a maximum for yield; material that arrives too hard is rejected as well. For a buyer running forming tools that ceiling matters as much as the floor. ASTM B265 bend radius requirement: for Grade 1, 1.5T below 1.78 mm thickness and 2T between 1.78 and 4.75 mm · for Grade 2, 2T and 2.5T · for Grade 4, 2.5T and 3T. Reduction of area (RA) is not written in the table: the sources give 25%, 30% and 35% for Grade 4 and contradict each other.

Never mix specification minima with typical mill values. Purchasing works from the minima; typicals guarantee nothing.​‌​​‌​

Specification Minima · ASTM B265 Grade 2 and 2H (annealed, room temperature)

Tensile strength Rm​‌​​‌​Grade 2: ≥345 MPa (50 ksi) · Grade 2H: ≥400 MPa (58 ksi) — that is the only difference. Minimum yield Rp0.2 is ≥275 MPa (40 ksi) for both, and the yield MAXIMUM is ≤450 MPa (65 ksi) — an upper limit that is enforced; over-cold-worked material is rejected
Elongation · bend · hardness​‌​​‌​A ≥20 % (50 mm) for Grade 2 and 2H alike. Bend radius 2T (t <1.8 mm) · 2.5T (1.8–4.75 mm); the coupon must bend through 105° without fracture (ASTM E290) — Grade 1 is 1.5T / 2T. Hardness typically ~80 HRB / ~145 HV (typical, not a requirement; Grade 1 ~70 HRB, Grade 4 ~100 HRB)
DIN 17850 Ti 2 · A SEPARATE SYSTEM — DO NOT MIX THE ROWS

​‌​​‌​

Tensile strength Rm390–540 MPa (a range) — its minimum is above ASTM’s 345 MPa, and there is an upper limit as well​‌​​‌​
Yield and elongationYield ≥270 MPa (labelled a 1.0 % offset) · elongation ≥22 % — harder than ASTM’s 20 %. Practical consequence: if dual certification is wanted, say so at order stage; the heat selection changes​‌​​‌​
Typical Mill Values — NOT GUARANTEED

Annealed sheet · typical band​‌​​‌​Rm ~400–480 MPa · Rp0.2 ~300–400 MPa · elongation typically above 25 %. One published mill typical: tensile ~483 MPa (70 ksi) at 20 °C — far above the minimum. That is precisely the statistical case for Grade 2H
Elastic constants​‌​​‌​E = 105 GPa — roughly half that of steel, so twice the deflection at the same section. Compressive modulus ~110 GPa · shear ~45 GPa · Poisson 0.37 (single-sourced; 0.32–0.37 is also quoted for Poisson — verify before using it in a critical calculation)
Bauschinger effect​‌​​‌​A drop of up to 25 % in compressive yield after stretching has been reported — if a cold-formed part carries compressive load, this is a real design item. Creep/fatigue: no numerical curves are published on this page; unalloyed titanium is not a creep alloy and the code ceiling is 315 °C anyway
What Happens Hot

​‌​​‌​

Measured trendUnalloyed titanium weakens fast and becomes more ductile fast as it heats. Published Grade 2 data: typical tensile ~483 MPa (70 ksi) at 20 °C falls to ~228 MPa (33 ksi) at 300 °C — roughly half — while elongation rises to 43 %​‌​​‌​
What the code saysAbove 315 °C (600 °F) there is no code allowable stress. Even if mechanical data reaches 400 °C, the design temperature stops at 315 °C. These are two separate numbers; label each of them​‌​​‌​
Oxidation in airAbove ~540 °C alpha case becomes a practical problem; above 649 °C (1200 °F) oxygen pick-up embrittles the metal. The limit usually published as safe in oxygen-bearing environments is ~371 °C (700 °F)​‌​​‌​

Physical Properties

Physical Properties · Titanium Grade 2

​‌​​‌​

Density4.51 g/cm³ (0.163 lb/in³) — 57 % of steel, 1.7 × aluminium. Melting range 1,649–1,671 °C​‌​​‌​
β transus~913 °C (1,675–1,680 °F), with a normal ±15 °C uncertainty from interstitial content. Grade 1 is ~888 °C — oxygen stabilises α, so the transus moves up. One source gives the alpha transus as 877–904 °C​‌​​‌​
Modulus of elasticity105 GPa (15.0–15.2 × 10³ ksi) — roughly half that of steel​‌​​‌​
Thermal conductivity~16–22 W/m·K [D: sources diverge badly — 16.4 · 20.8 · 21.8 · 22 W/m·K have all been published; quote the band, not a single number]. WARNING: some machining sources give ~7 W/m·K — that figure is for Ti-6Al-4V​‌​​‌​
Thermal expansion8.6 × 10⁻⁶ /K (20 °C) · 8.7 (0–200 °C) · ~9.7 (500 °C). About half that of stainless steel — in a titanium tube / steel tubesheet combination that difference is stress​‌​​‌​
Specific heat · resistivity
magnetic · surface film
Specific heat ~520–526 J/kg·K · resistivity ~0.52 µΩ·m (52 µΩ·cm) (another source gives 54–60 µΩ·cm). Non-magnetic — the reason for its use in MRI equipment and mine-hunting vessels. The TiO₂ film that forms spontaneously is nanometres thick and re-forms within milliseconds if damaged, provided oxygen or water is present​‌​​‌​

Heat Treatment and Thermal Stability

The most important sentence first: Grade 2 cannot be hardened by heat treatment. In single-phase α titanium there is no solution treat plus age, no martensite, no precipitate. The purpose of heat treatment is to soften, to relieve stress and to stabilise dimensions.​‌​​‌​

Heat Treatment · Grade 2

Annealing​‌​​‌​538–704 °C · 0.5–2 h · air cool; one published mill recipe is 704 °C (1,300 °F) · 2 hours, and a mill anneal band of 650–760 °C is also quoted. The β transus (~913 °C) must NEVER be exceeded. The atmosphere must be vacuum or inert gas; annealing in air produces alpha case, which then has to be removed
Stress relief​‌​​‌​538–593 °C · ~30 min · air cool, after welding, heavy machining or cold forming. Not forbidden — recommended for welded titanium vessels. There is NO damaging phase window: titanium has no equivalent of the σ, μ, Ni₄Mo or γ′ precipitates — the only enemies are oxygen, nitrogen and hydrogen entering through the surface
Forming​‌​​‌​Finish forging 316–649 °C; deep drawing and spinning 204–538 °C, 480–540 °C for severe operations; 25–40 % reduction below the β transus tidies the microstructure. Grade 2 cold forms well, but not as well as Grade 1: bend radius 2T–2.5T, and springback is far greater than in steel — allow generous overbend
Alpha Case, Hydrogen and Iron — Titanium’s Three Real Surface Damages

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Alpha caseThe oxygen-rich, hard and brittle α layer that forms when titanium is heated in air; grey-white or powdery, it directly destroys fatigue life and ductility, and it forms in air annealing, unshielded welding, hot forging and laser/plasma cutting. The only cure is removal — and pickling with HF carries a hydrogen pick-up risk​‌​​‌​
HydrogenCeiling 0.015 % (150 ppm). Hydrogen is not soluble in α titanium; it precipitates as TiH₂ platelets and lowers toughness. Wet filler wire, oily surfaces, damp gas and the HF pickling bath are the main sources. Iron contamination: free iron smeared onto titanium starts local corrosion in service — steel brushes, bench tops, slings and shared wheels are forbidden, and a titanium shop must be physically separated from steel​‌​​‌​

Welding

Welding titanium is not difficult; welding it CLEAN is. Grade 2 welds easily in metallurgical terms — single phase, no hardening, no preheat, no cracking. The entire risk is in one place: molten and hot titanium absorbs oxygen, nitrogen and hydrogen greedily.​‌​​‌​

Welding · Titanium Grade 2

Suitable processes​‌​​‌​GTAW (TIG) dominant · GMAW · PAW · EBW and LBW · spot, seam and flash resistance welding (acceptable even without a protective atmosphere). Covered electrode (SMAW) and submerged arc (SAW) are NOT used
Filler metal​‌​​‌​AWS A5.16 ERTi-2 (W.Nr. 3.7036, AMS 4951). Rule: the filler must match the base metal or be one grade BELOW it — never above. Welding Grade 2 with ERTi-1 is acceptable; the reverse is not. Welding an alloyed base metal (Gr 7, Gr 12) with generic ERTi-2 dilutes the alloy
Shielding gas​‌​​‌​Argon, 99.995 % minimum; preferably 99.999 % (5.0). Helium or Ar-He for deeper penetration. Under no circumstances a mixture containing CO₂, O₂ or H₂. Flow: ~14–19 L/min with a large gas-lens torch (No. 12–16 cup); ~7–9.5 L/min with a standard No. 8 cup to avoid turbulence
Back purge · trailing shield​‌​​‌​Back purge is MANDATORY on pipe and tube. The bore is fully argon purged and the ends sealed with aluminium tape. A titanium pipe weld whose root ran unshielded is scrap — it is cut out, not repaired. A trailing shield is likewise effectively mandatory: weld metal and HAZ must stay under argon until they are too cool to take colour
Preheat · interpass
stress relief​‌​​‌​
There is no preheat and none is needed. Keep interpass temperature low; a numerical code limit could not be independently verified, and the working rule on the floor is to wait, after each pass, until the weld has cooled under gas to a level where it will not take colour. Stress relief is not forbidden — it is recommended: 538–593 °C · ~30 min · air cool
Cleanliness · after welding​‌​​‌​The “white glove rule”: acetone or MEK first, then a stainless brush or carbide burr dedicated to titanium only. No tool that has touched steel touches titanium. Handle with clean nitrile gloves and wipe the filler wire with acetone immediately before use. After welding: any alpha case on the bead is removed by taking material off; where shielding was adequate the weld metal builds the same TiO₂ film as the parent and no different corrosion behaviour is expected
WELD COLOUR — the Only Valid Quick Acceptance Test on the Floor

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Bright silver · light strawACCEPT. Bright silver: shielding was perfect. Light straw/gold: superficial oxidation, removable with Scotch-Brite​‌​​‌​
Dark blue/purple · grey/whiteDark blue or purple: REJECT — significant oxidation, properties degraded, rejected in aerospace and pressure equipment. Grey or white powdery: SCRAP — that is alpha case, a brittle ceramic-like layer, cut out and rewelded, never cleaned off​‌​​‌​
Pre-production tack testEvery shift, before production starts, run a few tacks on clean scrap titanium. If the tack is bright silver, carry on. A rainbow halo, a blue tint or haze means STOP: gas leak, moisture in the line or a bad batch of gas. This single habit prevents most titanium welding scrap​‌​​‌​

Machining

Grade 2 is the easiest unalloyed grade in the titanium family to machine — but “easy” is a relative word here. Its higher oxygen makes it break chips more cleanly than Grade 1; even so, Grade 2 work hardens the instant it is rubbed, concentrates heat at the cutting edge and destroys a dull tool quickly.​‌​​‌​

Starting Parameters (CP titanium · family guidance)

Cutting speed · feed​‌​​‌​General starting band ~55–98 m/min (180–320 SFM) · roughing ~49–67 m/min · finishing ~61–91 m/min (for comparison, Ti-6Al-4V slot roughing runs 120–160 SFM). Feed 0.08–0.13 mm/tooth (12.7 mm end mill) — NEVER reduce the feed, low feed means rubbing and rubbing means work hardening
Tooling · coolant
never dwell​‌​​‌​
Sharp, positive-rake carbide coated AlTiN or TiAlN; high-pressure through-tool coolant is preferred, flood is acceptable, dry cutting is not done. Retract the drill fully on every peck — a drill sitting at the bottom of the hole hardens it and breaks the tool on the next pass. Short tools, rigid machine: the low modulus means the workpiece flexes too
FIRE — With Titanium This Is a Procedure, Not a Warning

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DO NOT USE WATERThe risk is in fine chips, grinding dust and swarf; bulk titanium does not ignite. A titanium fire is Class D: water and CO₂ make it worse — use dry sand or a Class D extinguisher, collect chips in closed metal containers, and note that wet titanium dust generates hydrogen​‌​​‌​
Pure oxygenTitanium burns in pure oxygen. Published threshold: a risk of ignition at oxygen concentrations above 35 % at elevated temperature and pressure. Do not offer titanium for oxygen service​‌​​‌​
Dry chlorineIn dry chlorine gas titanium corrodes rapidly and can ignite; passivation requires ~1 % water in the gas. In a chlor-alkali plant the dry chlorine line is forbidden territory for titanium​‌​​‌​

Corrosion — Why It Is Good, and WHERE IT FAILS

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COMPARISON
A single criterion: the annealed-condition SPECIFICATION LIMITS of ASTM B265 / ASME SB-265 (and of ASTM B348, which carries the same values). Chemical ceilings from Table 1, tensile values from Table 2. These are limits, not typical values; producer typicals run higher.

GradeUNSW.-Nr.Oxygen maxIron maxNitrogen maxTensile min MPaYield min MPaYield max MPaElongation minNote
Ti Grade 1​‌​​‌​UNS R502503.7025​‌​​‌​0.18%0.20%​‌​​‌​0.03%240​‌​​‌​138310​‌​​‌​24%Lowest oxygen, highest ductility. Deep drawing and explosion cladding work.​‌​​‌​
Ti Grade 2UNS R50400​‌​​‌​3.70350.25%​‌​​‌​0.30%0.03%​‌​​‌​345275​‌​​‌​45020%​‌​​‌​The workhorse of commercially pure titanium. The most common grade for plate, tube and heat exchangers.
Ti Grade 3​‌​​‌​UNS R505503.7055​‌​​‌​0.35%0.30%​‌​​‌​0.05%450​‌​​‌​380550​‌​​‌​18%The intermediate step. It is not in this card set; it is shown to complete the ladder.​‌​​‌​
Ti Grade 4UNS R50700​‌​​‌​3.70650.40%​‌​​‌​0.50%0.05%​‌​​‌​550483​‌​​‌​65515%​‌​​‌​The strongest of the commercially pure family. It is absent from most pipe and tube specifications.
​‌​​‌​

Additional information
IliskiAs the OXYGEN CEILING rises from 0.18% to 0.40%, the minimum tensile strength rises from 240 MPa to 550 MPa (+129%) and the minimum elongation falls from 24% to 15%. The iron ceiling also rises from 0.20% to 0.50%. THIS INCREASE HAS NOTHING TO DO WITH HEAT TREATMENT; all four grades use the same heat treatment cycle.​‌​​‌​
MechanismOxygen and nitrogen enter the octahedral interstitial sites of the hexagonal close-packed alpha lattice and create an asymmetric lattice distortion; the resulting stress field impedes dislocation glide (interstitial solid solution strengthening). Iron stabilises a small amount of beta phase. The MDPI Crystals 2025 review gives a critical oxygen threshold of about 0.46% for pure titanium, above which room-temperature elongation collapses sharply. The 0.40% ceiling of Grade 4 sits just below that threshold.​‌​​‌​
WarningAll four grades are defined in ASTM with the same base elements; the difference is ONLY the oxygen, iron and nitrogen ceilings. If an order is placed simply as ‘commercially pure titanium’, it is undefined which strength class will arrive. The grade number and the UNS number must both be written.​‌​​‌​
The minimum yield of Grade 1 DEPENDS ON THE SPECIFICATION: the ASTM B265 / ASME SB-265 table gives 138 MPa (20 ksi), while AMS 4940 requires 172 MPa (25 ksi). Two different floors apply to the same grade; an order must not be written without stating which specification governs. The carbon (0.08%) and hydrogen (0.015%) ceilings are identical in all four grades; they contribute nothing to the strength ladder. Grade 3 is not in this card set. It is shown only in the comparison table because it is the third step of the ladder.

All of titanium’s corrosion resistance rests on one thing: the spontaneously formed TiO₂ passive film. That film is extremely stable, tightly adherent and self-healing — but only if oxygen or water is present. If the environment feeds the film, titanium is close to untouchable; if it cannot, titanium is an ordinary active metal. Grade 1 and Grade 2 behave practically identically in corrosion; the grade is chosen for strength and code, not for corrosion.​‌​​‌​

WHERE IT IS EXCELLENT

Seawater​‌​​‌​Grade 2’s flagship duty and its single largest use worldwide. Titanium tubing exposed for 16 years in a surface condenser on polluted seawater showed no corrosion beyond slight discolouration. General corrosion resistance is published to 260 °C (500 °F); another source says 315 °C (600 °F) [D]. There is no practical velocity limit — erosion-corrosion is not the constraint it is with copper alloys
Oxidising environments​‌​​‌​Nitric acid, chromic acid, oxidising chlorides, hypochlorite, wet chlorine. These feed the film, and titanium here beats 316L and most nickel alloys; a published rate in chlorine environments is of the order of 0–0.065 mpy. It is also fully resistant to stress-corrosion cracking in aqueous chloride solutions — the boiling MgCl₂ scenario that is a nightmare in stainless is a non-issue (AISI 316L cracks, super duplex is limited) — and alkaline media and most organics are untroubled
Ferric / cupric ions​‌​​‌​In titanium these are INHIBITORS, not a threat. Fe³⁺ and Cu²⁺ passivate titanium in reducing acid: in 20 % sulphuric they prevent corrosion. This is the exact opposite of the nickel-molybdenum alloys (the Hastelloy B family), where the same ions are the number one cause of failure. Anyone copying datasheets across alloy families gets this line backwards
Sour service (NACE)​‌​​‌​One source states Grade 2 is approved for sour service under NACE MR-01-75. Single-sourced; could not be verified against the current NACE MR0175 / ISO 15156-3 text. Before taking on H₂S work, read the table in force yourself — its temperature, chloride and pH limits included
Acid Limits · Unalloyed Titanium (pure acid, uninhibited)

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Hydrochloric acidUseful resistance to about 7 % at room temperature; at boiling, above 2 % the rate is 280 mpy (~7.1 mm/y) — it effectively dissolves. Ferric ion moves the limit up​‌​​‌​
Sulphuric acid~20 % at 0 °C · ~5 % at room temperature · high corrosion at boiling with as little as 0.5 %. Ferric and cupric ions prevent corrosion in a 20 % solution​‌​​‌​
Phosphoric acid~30 % at room temperature · ~10 % at 60 °C · ~2 % at 100 °C. Void in phosphoric acid containing halides​‌​​‌​
Nitric acidOutstanding resistance across the whole concentration range at sub-boiling temperatures — the acid titanium is strongest in, with a published advantage over 304L in concentrated nitric. But see red fuming nitric below​‌​​‌​
Hydrofluoric acidATTACKED RAPIDLY AT EVERY CONCENTRATION, EVEN VERY DILUTE. NOT RECOMMENDED. Fluoride dissolves the TiO₂ film; passivity simply ceases to exist. This is titanium’s most absolute limit​‌​​‌​
WHERE IT FAILS — Publish This at Least as Prominently as the Good News

1 · Hydrofluoric acid and fluorides​‌​​‌​An absolute prohibition. Even dilute HF dissolves the film. Fluoride pickling baths, HF-bearing process streams, fluorine chemistry — titanium is not there. Note: titanium pickling baths are themselves HF/HNO₃ mixtures; they work because they are controlled, short and nitric-rich — that is not a service environment
2 · Reducing acids​‌​​‌​HCl and H₂SO₄ above the limits in the table. Deaerated, oxidant-free, hot reducing acid is titanium’s classic weakness; the answer is palladium-bearing titanium (Grade 7/16) or the nickel-molybdenum family (Hastelloy B-3)
3 · Dry chlorine gas​‌​​‌​Rapid attack and a risk of IGNITION. Passivation needs ~1 % water in the gas. Wet chlorine is excellent for titanium; dry chlorine is lethal — the most overlooked material selection error in chlor-alkali plants
4 · Hydrogen embrittlement​‌​​‌​It happens when three conditions are met SIMULTANEOUSLY: (a) temperature above 77 °C (170 °F) — below that hydrogen pick-up is too slow to matter; (b) pH <3 or pH >12 — in between the oxide film does not pass hydrogen; (c) a mechanism generating hydrogen at the surface: a galvanic couple, impressed-current cathodic protection, corrosion of the titanium itself, or dynamic abrasion. In near-neutral brines the threshold quoted is a potential more negative than −0.70 V (SCE). Do not accidentally make the titanium a cathode, and do not over-protect it
5 · Crevice corrosion — a temperature threshold​‌​​‌​Unalloyed titanium is open to local pitting and crevice corrosion in seawater above ~82 °C (180 °F) (one source gives 80 °C; the same source cites above 75 °C and above 1,000 ppm in hot halide or sulphate solutions as the risk condition). Under gaskets, in tubesheet holes, under deposits — the classic places; low pH pulls the threshold down further. In hot brine the answer is Grade 7 (Pd) or Grade 12
6 · Red fuming nitric acid (RFNA)​‌​​‌​Not used — risk of a pyrophoric reaction. Intergranular attack produces finely divided metallic particles that can ignite spontaneously. Published hazardous window: water <1.34 % and NO₂ >6 %
7 · Pure oxygen, methanol and other prohibitions​‌​​‌​Anhydrous methanol: once water falls below 1.5 %, unalloyed titanium cracks by stress corrosion in methanol. Titanium BURNS in pure oxygen — a risk of ignition at oxygen concentrations above 35 % at elevated temperature and pressure has been published; the limit regarded as safe is ~371 °C (700 °F), and above 649 °C (1200 °F) oxygen pick-up embrittles it. Also: molten chloride salt baths, alkaline peroxide solutions and liquid mercury are published prohibitions
8 · Galvanic coupling — the danger runs the other way​‌​​‌​In seawater titanium is passive (~0.0 V SCE) and is not attacked itself — but it eats THE OTHER MEMBER of the couple. Connect a titanium exchanger to a carbon steel shell, to aluminium bronze or to ordinary stainless and what corrodes is the other metal; with a large titanium cathode area the effect is severe. Titanium tubes in a steel tubesheet is a classic field failure
The Upgrade Path — What to Answer When Grade 2 Is Not Enough

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Grade 7 (R52400)Grade 2 + ~0.15 % palladium (0.12–0.25 %). Published as moving the seawater crevice threshold to ~250 °C (pH >1), and usable to 27 % HCl at 25 °C, 45 % H₂SO₄ and ~80 % phosphoric. Cost 2–3 ×. This is the direct corrosion upgrade for Grade 2​‌​​‌​
Grade 16 · 26 · 11 · 17Grade 16 (R52402) = Grade 2 + 0.04–0.08 % Pd: most of Grade 7’s benefit, 20–35 % cheaper. Grade 26 (R52404, 0.08–0.14 % Ru) escapes the palladium price and is approved as ASME 26H. Grades 11 and 17 are Grade 1 + palladium — for when formability is also required​‌​​‌​
Grade 12 (R53400)Ti-0.3Mo-0.8Ni, no palladium. Crevice resistance to ~120 °C in hot chloride brines; strong-acid resistance is below Grade 7’s, cost ~1.3–1.5 ×. Right if the driver is crevice corrosion, wrong if it is acid​‌​​‌​
NOT Grade 5Moving to Grade 5 for strength is not a corrosion upgrade — in most environments it is a DOWNGRADE. Ti-6Al-4V trails the CP grades in reducing acids and crevice corrosion and cannot be cold formed​‌​​‌​
NOT titaniumIf hot reducing acid is mixed with an oxidant, the answer is the nickel-chromium-molybdenum family: C-276 or C-22. In hot sulphuric the high-nickel alloy 825 is considered. If HF is present, no titanium grade works​‌​​‌​

Frequently Asked Questions

The customer wants Grade 2H. We have Grade 2 in stock. Can we certify it as 2H?​‌​​‌​

Chemically yes; mechanically only if that heat’s tensile value genuinely meets it. Grade 2H has exactly the same chemistry and the same UNS number (R50400) as Grade 2; it is not a separate material. The difference is one line: the minimum tensile is guaranteed at 400 MPa (58 ksi) instead of 345 MPa. Yield (275 MPa) and elongation (20 %) are unchanged.
The good news: in practice most Grade 2 heats already exceed that. The published statistic is clear — over 99 % of more than 5,200 commercial test reports met the 58 ksi minimum, which is exactly why the H grade exists. A typical mill value is of the order of ~483 MPa (70 ksi) at 20 °C.
But procedure matters. If the actual tensile value on the heat’s original certificate meets 400 MPa and the mill dual-marked it as 2H, there is no problem. If it does not — or if the certificate only states “≥345 MPa” without the actual value — you cannot sell the material as 2H; ask the supplier for the actual tensile value or for a new certificate dual-marked as 2H.
And ask one more question: does the customer actually need 2H? Its only benefit is a higher code allowable stress, hence a thinner wall. On a thick-walled, large-diameter Div. 2 vessel that is meaningful — one published example gives ~14 % material saving over Div. 1. In thin sheet, exchanger tube and general piping the difference disappears, and there the 2H requirement only narrows the supplier pool.

The specification says “Titanium Grade 2, ASME Section VIII, 400 °C design temperature”. Can we supply it?​‌​​‌​

Not as a pressure-retaining component — and the reason is a code limit, not a metallurgical one. Do not confuse the two.
Metallurgically Grade 2 is untroubled at 400 °C: no phase transformation, no embrittlement window, the β transus far away (~913 °C). The material simply gets weaker — published typical data show tensile falling from ~483 MPa at 20 °C to ~228 MPa at 300 °C, while elongation rises to 43 %.
The problem is code coverage, and the ceiling is surprisingly low: 315 °C (600 °F). That figure applies to unalloyed titanium for all applications — VIII Div. 1 and Div. 2, III Class 2/3, Section XII. Above it there is no code allowable stress, so you have no number to design with at 400 °C.
And the most forgotten item is flanges. ASME B16.5 does not cover titanium. A titanium flange is made to B16.5 dimensions but its rating must be calculated per Annex A; “Class 300 titanium flange” is not a rating on its own — and a significant part of the price difference in the quotation comes from that engineering work.
Realistic answers: get the design temperature brought down to 315 °C; if 400 °C is genuinely required, leave the titanium family for a nickel alloy with code coverage above it (alloy 825, C-276); or use the titanium as a non-pressure-retaining lining or cladding on a code-approved backing — on the seawater and chloride side this is a very common and very economical solution. What you must not do is quote “titanium is good to 500 °C” from a catalogue and let it turn into a design temperature.

We are using Grade 2 tube in a seawater exchanger. What should we watch for?​‌​​‌​

Grade 2 is the world’s de facto standard for this duty — but there are three traps, and all three are about system design, not corrosion data.
First, galvanic coupling, and it runs the opposite way to most people’s intuition. Titanium is passive in seawater and is not attacked itself; but it accelerates the other member of the couple. Connect a titanium tube bundle to a carbon steel tubesheet, to aluminium bronze or to ordinary stainless, and what corrodes is not the titanium but the other metal — and because the titanium cathode area is large, the effect is severe. The fix is to make the whole wetted surface titanium, to use insulation or coating, or to design a deliberate sacrificial anode scheme.
Second, cathodic protection and hydrogen. If you try to solve the galvanic problem with impressed-current cathodic protection, you make the titanium a cathode and generate hydrogen on its surface. Above 77 °C and in the pH <3 or >12 region that leads to hydrogen embrittlement; in near-neutral brine the threshold quoted is a potential more negative than −0.70 V (SCE). Do not over-protect the titanium.
Third, temperature and crevices. Grade 2’s general corrosion resistance in seawater is outstanding, but crevice corrosion is a real risk above ~82 °C (180 °F) and low pH pulls the threshold down further. The risky places are under gaskets, in the tube-to-tubesheet roll zone and under deposits. If there is hot brine, the right answer is not Grade 2 but Grade 7 / Grade 16 (palladium-bearing) or Grade 12.
And a bonus — the most common real cause of failure in the field: titanium’s modulus is 105 GPa, half that of steel, which means twice the deflection and a lower natural frequency at the same geometry. In seawater exchangers flow-induced vibration and support spacing cause more failures than corrosion does. Choose the tube wall thickness for vibration, not for corrosion allowance — in titanium the corrosion allowance is effectively zero anyway.

Can we offer Grade 2 for our hydrochloric acid line?​‌​​‌​

Most probably not — and this is the most common way titanium gets misapplied.
Titanium’s window in HCl is narrow: useful resistance runs to about 7 % at room temperature. At boiling, above 2 % the corrosion rate reaches the order of 280 mpy (~7.1 mm/y) — the material effectively dissolves. In sulphuric the window is narrower still: ~5 % at room temperature, ~20 % at 0 °C, and high corrosion at boiling with as little as 0.5 %.
The reason in one sentence: to heal itself the TiO₂ film needs oxygen or an oxidant in the environment, and a deaerated, hot, reducing acid does not have one.
But there is an important exception, and you have to ask the right question: is there ferric or cupric ion in the stream? In titanium, Fe³⁺ and Cu²⁺ are not a threat but INHIBITORS — they passivate titanium in reducing acid; published data show ferric or cupric ion preventing corrosion in 20 % sulphuric. A real process line with carbon steel upstream often generates those ions already. This is the exact opposite of the Hastelloy B family, where the same ions are the number one cause of failure.
A practical route: ask the customer in writing for concentration, temperature, aeration state and a ferric/cupric analysis. If the acid is dilute, cold and carries an oxidant, Grade 2 can work — but write those conditions into the order acknowledgement. If the acid is hot, concentrated or deaerated, the right answer is Grade 7 or Grade 16 (palladium-bearing titanium), or outside the family altogether Hastelloy B-3. And if there is hydrofluoric acid or fluoride in the stream, no titanium grade works — that one is not negotiable.

Common datasheet errors — check these before you order​‌​​‌​

1. “Grade 2H is a different alloy” — WRONG. Its chemistry and UNS number (R50400) are identical to Grade 2. The only difference is that the minimum tensile is guaranteed at 400 MPa instead of 345; yield and elongation are unchanged.
2. The AMS-T-9046 / MIL-T-9046 “CP” numbering runs INVERSE. CP-3 = Grade 2, CP-4 = Grade 1, CP-1 = Grade 4. Assuming “CP-1 must be the purest” is the most common and most expensive misreading.
3. Material-number confusion. 3.7035 = DIN 17850 Ti 2 (base metal), 3.7034 = WL/aerospace, 3.7036 = welding FILLER wire. Several mill sheets print the base metal as 3.7034 [D].
4. The ASTM minimum and the DIN range get mixed. ASTM B265 Grade 2 gives only Rm ≥345 MPa; DIN Ti 2 sets both a lower and an UPPER limit at Rm 390–540 MPa. A heat conforming to ASTM may fail DIN — from below or from above.
5. The YIELD MAXIMUM gets overlooked. ASTM B265 Grade 2 yield is 275–450 MPa; 450 MPa is an upper limit and it is enforced. Over-cold-worked, “stronger” Grade 2 does not conform.
6. ASTM B337 is still quoted as the pipe specification — it was WITHDRAWN in 1997. The correct references are B861 (seamless) and B862 (welded).
7. “ASME B16.5 Class 150 titanium flange” is taken for a rating — it is NOT. B16.5 does not cover titanium. The flange is made to B16.5 dimensions; the rating is calculated per Annex A.
8. Thermal conductivity gets copied from the wrong family. The ~7 W/m·K figure is for Ti-6Al-4V; the band published for unalloyed titanium is ~16–22 W/m·K [sources diverge across 16.4 · 20.8 · 21.8 · 22].
9. Ferric and cupric ions are taken for a threat — in titanium they are INHIBITORS. Fe³⁺ and Cu²⁺ passivate titanium in reducing acid; this is the exact opposite of the Hastelloy B family.
10. “Titanium does not corrode” — WRONG and dangerous. It dissolves in HF at every concentration, ignites in dry chlorine, burns in pure oxygen, cracks in anhydrous methanol, forms a pyrophoric product in RFNA, embrittles with hydrogen above 77 °C under cathodic charging and suffers crevice corrosion in seawater above 82 °C.
11. Hardness scale, carbon ceiling and modulus. Grade 2 is ~80 HRB (~145 HV); reading “80” as HRC produces nonsense. The carbon ceiling is often printed as 0.10 % — the current ASTM B265 value is 0.08 %. And the modulus is 105 GPa, roughly half that of steel — twice the deflection at the same section, which is why flow-induced vibration causes more seawater-exchanger failures than corrosion.
12. Hardening by heat treatment gets offered. Grade 2 is single-phase α titanium; it cannot be hardened. For surface hardness the route is anodising, nitriding or coating.
13. Allowable stresses get taken from a distributor sheet. ASME Section II Part D values are updated edition to edition. Always take the design value from the code edition in force.
14. “Grade 2 is NACE approved” gets published as a one-liner. One source states that Grade 2 is approved for sour service under NACE MR-01-75, but this is single-sourced and could not be verified against the current ISO 15156-3 text. Before taking on H₂S work, read the table in force yourself, including its temperature, chloride and pH limits.

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Related grades

Ti Grade 4  ·  Ti Grade 5  ·  Ti Grade 5 ELI  ·  Ti Grade 1  ·  All titanium alloys →​‌​​‌​

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