Ti Grade 1

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Ti Grade 1 / UNS R50250 / AMS 4940

Ti Grade 1
UNS R50250 · W.Nr. 3.7025 · DIN 17850 Ti 1 · ASTM Grade 1 · COMMERCIALLY PURE (unalloyed) titanium, alpha phase. Ceilings: O 0.18% max · Fe 0.20% 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 LOWEST-OXYGEN and most ductile grade of the family. 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

Ti Grade 2

For what
It is bought where formability comes before strength: deep-drawn and heavily bent thin sheet parts, the cladding layer in explosion cladding, anode substrates in chlor-alkali electrolysis, sea-water and brackish-water heat exchanger tubes, expansion bellows and thin-wall chemical process equipment.
Forms
Round bar · flat bar · plate · sheet · thin sheet / foil · tube · forgings. All forms are supplied to order.
Standards
AMS (verified): 4940 – sheet, strip and plate; commercially pure, annealed, 25.0 ksi (172 MPa) yield strength. No verified AMS number was found for Grade 1 BAR or FORGINGS. ASTM: B265 / SB-265 (strip, sheet, plate) · B348 (bars and billets) · B338 (condenser and heat exchanger tubes, seamless and welded) · B861 (seamless pipe) · B862 (welded pipe) · B363 (welding fittings) · B381 Grade F-1 (forgings) · B863 (wire) · F67 Grade 1 (unalloyed titanium for surgical implants). EN / DIN: DIN 17850 Ti 1 (composition, W.Nr. 3.7025) · DIN 17860 (sheet/plate) · DIN 17862 (bar) · DIN 17864 (forgings). MIL: MIL-T-9046J CP-4 and AMS-T-9046B CP-4 (sheet, strip, plate) – the CP number runs OPPOSITE to the grade number. Welding: AWS A5.16 / SFA-5.16 ERTi-1.
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
Formability. The ASTM B265 floor is 24% elongation and the yield CEILING is 310 MPa; having a yield ceiling in the specification guarantees that the material will not arrive too hard and keeps the springback calculation of press and draw tooling stable.
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 1 IsStandards by Product FormASME Code Acceptance and MAXIMUM CODE TEMPERATURESProduct Forms With NO StandardChemical CompositionMechanical PropertiesPhysical PropertiesHeat Treatment and Thermal StabilityWeldingMachiningCorrosionFrequently Asked Questions



Commercially pure titanium – low oxygen. Ti Grade 1 is the purest form of titanium and is known as unalloyed titanium. The alloy contains 99.5% titanium and is known for its very high corrosion resistance, excellent biocompatibility, low density and good mechanical properties.

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: Being pure titanium, some difficulties can arise in terms of machinability, but machining is generally possible. The following are some important points regarding the machinability of Ti Grade 1.​‌​​‌​

Machining: It can be processed by conventional methods such as milling, turning and drilling. During the machining of titanium, however, it is important to allow for high temperatures and to use appropriate cutting tools. Machining at low speed and the use of cutting fluids are necessary, because titanium can generate high temperatures during cutting operations.

Welding: It can be welded by the TIG (Tungsten Inert Gas) and MIG (Metal Inert Gas) methods. It is important to use shielding gases such as argon during welding in order to prevent oxidation of the titanium. Post-weld heat treatment may be required, since some change in properties can occur in the weld zone.​‌​​‌​

Cold forming: Cold forming is generally suitable for Ti Grade 1. Operations such as plasma cutting and bending can also be carried out, but care should be taken during the process.

Hot forming: Hot forming is generally suitable for Ti Grade 1 and working at lower temperatures is recommended. It should be remembered that temperatures must not be too high.​‌​​‌​

Chemical Composition

C %​‌​​‌​≤ 0.08
N %​‌​​‌​≤ 0.03
Ti %​‌​​‌​Balance
Fe %​‌​​‌​≤ 0.20
O %​‌​​‌​≤ 0.18
H %​‌​​‌​≤ 0.015
Mechanical Properties at 20 °C

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Hardness HB 30≤ HB 120​‌​​‌​
0.2% Yield Strength Rp N/mm²≥ 170​‌​​‌​
Tensile Strength Rm N/mm²≥ 240​‌​​‌​
Elongation≥ 24%​‌​​‌​
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​‌​​‌​21
Electrical Resistivity Ω mm²/m​‌​​‌​0.47
Standards and Equivalents · Ti Grade 1
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Trade nameTi Grade 1​‌​​‌​
UNSR50250​‌​​‌​
AMS4940​‌​​‌​
Available formsRound bar · Flat bar · Plate · Sheet · Tube · Forgings
All forms are supplied to order.​‌​​‌​

What Titanium Grade 1 Is — and the ONE Thing That Separates It From Grade 2​‌​​‌​

Titanium Grade 1 (UNS R50250 / W.Nr. 3.7025 / DIN Ti 1 / commonly sold as Ti 99.8) is the softest and most ductile grade of unalloyed, commercially pure (CP) titanium. At room temperature it is single-phase HCP (α) titanium — there is no second phase, no precipitate and no hardening mechanism in it. It cannot be hardened by heat treatment. Its strength comes from exactly two sources: cold work and interstitial atoms.

There is not a single deliberately added alloying element separating Grade 1 from Grade 2. Both are unalloyed titanium; both carry the same carbon, nitrogen and hydrogen ceilings. Only two lines in the specification differ: oxygen and iron. Those two lines set the strength, the ductility, the bend radius, the welding behaviour, the price and what code calculation you are allowed to do. Everything else on this page follows from that one fact.​‌​​‌​

The Unalloyed Titanium Family · The Only Variable Is Interstitial Content (ASTM B265)

Grade 1
R50250 / 3.7025​‌​​‌​
O ≤0.18 % · Fe ≤0.20 %. Rm ≥240 MPa · Rp0.2 138–310 MPa · A ≥24 %. The most ductile and best cold-forming member of the family. Deep drawing, explosive cladding, anode substrate, plate-heat-exchanger plate, lining. It is not for anyone who wants strength
Grade 2
R50400 / 3.7035​‌​​‌​
O ≤0.25 % · Fe ≤0.30 %. Rm ≥345 MPa · Rp0.2 275–450 MPa · A ≥20 %. The industry workhorse. Pressure vessels, piping, exchanger tube, flanges, forgings. The best-stocked grade there is — which is why its price per kilo is often below Grade 1
Grade 3 · Grade 4
R50550 / R50700​‌​​‌​
Gr 3: O ≤0.35 % · Rm ≥448–450 MPa · A ≥18 % — a niche grade whose real justification is not corrosion but a higher allowable stress in the code calculation. Gr 4: O ≤0.40 % · N ≤0.05 % · Fe ≤0.50 % · Rm ≥552 MPa · A ≥15 % — dental, medical, fasteners; formability drops sharply
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 in crevice corrosion it is worse than the CP grades, and it cannot be cold formed. Detail: Ti Grade 5 / ELI

What oxygen and iron actually do​‌​​‌​

In titanium, oxygen is not an impurity — it is an alloying element. It sits interstitially in the octahedral sites of 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. Going from Grade 1 to Grade 2 oxygen rises by only 0.07 percentage points, and in exchange the minimum yield goes from 138 MPa to 275 MPa — roughly double. Iron is capped for a different reason: 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 acids and in crevice corrosion. Grade 1’s 0.20 % ceiling means a cleaner single phase and noticeably better ductility.

The sentence worth publishing: Grade 1 is not a “purer” Grade 2. It is the grade chosen for a different engineering purpose. Grade 2 exists for strength and code calculability; Grade 1 exists for formability, weld ductility and cladding adhesion. Ordering the wrong one is expensive in both directions: put Grade 1 in a pressure vessel and your wall thickness grows for nothing; put Grade 2 into a deep-draw die and it tears.​‌​​‌​

Standards by Product Form

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STANDARDS BY PRODUCT FORM

Product formStandards
Plate · sheet · strip · thin sheet​‌​​‌​AMS 4940 (commercially pure, annealed, 25.0 ksi / 172 MPa yield) · ASTM B265 / ASME SB-265 Grade 1
Round bar · flat bar · billet​‌​​‌​There is NO verified AMS number for Grade 1 bar. ASTM B348 / ASME SB-348 Grade 1
Tube (condenser · heat exchanger)​‌​​‌​ASTM B338 / ASME SB-338 Grade 1 (seamless and welded)
Pipe​‌​​‌​ASTM B861 Grade 1 (seamless) · ASTM B862 Grade 1 (welded). The former ASTM B337 has been withdrawn.
Welding fittings​‌​​‌​ASTM B363 / ASME SB-363 (unalloyed titanium welding fittings)
Forgings​‌​​‌​ASTM B381 Grade F-1 · DIN 17864
Wire​‌​​‌​ASTM B863 Grade 1 (UNS R50250)
Surgical implants​‌​​‌​ASTM F67 Grade 1 (UNS R50250, unalloyed titanium)
Welding filler metal​‌​​‌​AWS A5.16 / ASME SFA-5.16 ERTi-1
European · inspection document​‌​​‌​DIN 17850 Ti 1 (W.Nr. 3.7025, 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).

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Unlike the nickel alloys, titanium has an ASTM family numbered separately by product form, and it covers Grade 1 almost completely. The table below can be used directly on a purchase order.

Standards by Product Form · Titanium Grade 1 (R50250 / 3.7025)

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Strip · sheet · plate
Bar · billet
ASTM B265 / ASME SB-265 (strip, sheet, plate — supplied annealed) · ASTM B348 / SB-348 (bar and billet)​‌​​‌​
Seamless and welded tube
(condenser · exchanger)
ASTM B338 / SB-338 — this is the family standard for condenser and heat-exchanger tube​‌​​‌​
PipeSeamless ASTM B861 · welded ASTM B862. ASTM B337 was WITHDRAWN in 1997 and split into these two; do not accept a current certificate citing B337​‌​​‌​
Welding fittingsASTM B363 / SB-363 (material) + ASME B16.9 (dimensions) — both go on the order​‌​​‌​
Forgings (disc · ring · block)ASTM B381 / SB-381 — grades carry an F prefix: Grade 1 forging is F-1, Grade 2 forging is F-2. Removal of alpha case is an explicit requirement of the standard​‌​​‌​
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, whose grades use a separate C prefix (C-2, C-3 …) — a Grade 1 equivalent could not be independently verified as in scope​‌​​‌​
Surgical implantASTM F67 · in Europe EN ISO 5832-2, which defines six grades separated by tensile strength. The numbering is not identical to ASTM — match on chemistry, not on the number​‌​​‌​
AerospaceAMS 4940 (sheet, strip, plate — “Commercially Pure, Annealed, 25.0 ksi (172 MPa) yield“) · AMS-T-9046 (formerly MIL-T-9046J) class CP-4 = Grade 1. WARNING: the CP numbering runs INVERSE to the ASTM grade number (CP-4 = Gr 1, CP-3 = Gr 2, CP-1 = Gr 4)​‌​​‌​
Welding consumablesBare wire: AWS A5.16 ERTi-1 · W.Nr. filler 3.7026 (Grade 2 filler is ERTi-2 / 3.7036). There is NO covered electrode and there never will be — slag and coating moisture inevitably load titanium with oxygen and hydrogen​‌​​‌​
ASME Section IXTitanium base metals sit in the P-No. 51–53 band, unalloyed grades at P-No. 51; fillers in 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 against the current QW/QB-422 before writing a WPS​‌​​‌​
EuropeDIN 17850 Ti 1, material number 3.7025; product forms DIN 17860 (sheet/plate), 17862 (bar), 17863 (wire), 17864 (forgings). 3.7024 is the WL/aerospace number. EN 10204 is NOT a material specification; it only defines the inspection-document type. The correct wording is “ASTM B265 Gr 1, certified to EN 10204 3.1“​‌​​‌​

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. Unalloyed titanium is metallurgically perfectly happy at 315 °C; the code stops there because there is no creep and long-term oxidation data behind it.

ASME Code Acceptance · Unalloyed Titanium (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 and quoted as the titanium family ceiling. There is no allowable stress above it​‌​​‌​
Sections that accept itSection VIII Div. 1 and Div. 2 · Section III Class 2/3 · Section XII (transport tanks) — all to 315 °C. One source also lists Section I (power boilers) for Grade 2 plate; single-sourced, confirm in the current Section II Part D​‌​​‌​
ASME B31.3Titanium is in scope and is quoted with the same 315 °C ceiling. Not independently verified — confirm against B31.3 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 single most overlooked item in titanium piping​‌​​‌​
Code coverage for Grade 1Most of the rows above were verified through Grade 2. That Grade 1 is separately listed in the same sections could not be independently verified; confirm the R50250 line in Section II Part D before ordering. In any case most designers move to Grade 2 anyway, because Grade 1’s 138 MPa minimum yield inflates the wall thickness. Note also that the ASME-approved H grades are 2H, 7H, 16H and 26H — THERE IS NO SUCH THING AS GRADE 1H​‌​​‌​

What an “H” grade is, and why Grade 1 was left out

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; the only difference is that the minimum tensile is guaranteed at 400 MPa (58 ksi) instead of 345 MPa (50 ksi). Yield is 275 MPa and elongation 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. Grade 1 is outside this programme — because Grade 1 is not bought for strength in the first place.​‌​​‌​

Product Forms With NO Standard — the Commercially Valuable Section

Titanium has fewer gaps than the nickel alloys, but they sit in different places and cost more when you hit them. This is the section your sales engineers should memorise.​‌​​‌​

Specification Gaps and Traps for R50250

Flanges​‌​​‌​There is no “ASTM titanium flange specification”. The titanium equivalent of ASTM B462 does not exist. A titanium flange is made from a B381 forging (F-1 / F-2) or from B265 plate; the dimensions are ASME B16.5, but the pressure–temperature rating cannot be read off a table — it has to be calculated
Grade 1 castings​‌​​‌​B367 covers unalloyed titanium castings, but casting grades use a separate C-prefixed numbering and a casting grade equivalent to Grade 1 could not be independently verified as in scope. In practice cast titanium valve and pump bodies are supplied as Grade 2 / C-2
Bolts · nuts · spring wire​‌​​‌​ASTM F467 (nuts) and F468 (bolts) include titanium grades, but Grade 1 coverage could not be independently verified — and it is meaningless anyway: you cannot hold preload with a 138 MPa minimum yield. The route is Grade 2, 4 or 5. Same for spring wire: B863 covers it but spring temper is not a defined strength class. And there is no “Grade 1H”
Hardening by heat treatment​‌​​‌​Not a process gap — a physical impossibility. Grade 1 is single-phase α titanium; there is no solution treat plus age. For surface hardness the route is anodising, nitriding or coating
A current EN product standard​‌​​‌​Europe has no current EN product-standard family for titanium of the kind stainless steel enjoys; what is actually used is the DIN 17850 family plus the ASTM B series. 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 1 (weight %)

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Oxygen · IronO ≤0.18 and Fe ≤0.20 — the two lines that define the grade. Grade 2: ≤0.25 and ≤0.30​‌​​‌​
Carbon · NitrogenC ≤0.08 · N ≤0.03 — both identical to Grade 2. 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 2; 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 99.8​‌​​‌​
Source conflict [D]Some mill sheets print the carbon ceiling as 0.10 %. The current ASTM B265 value is 0.08 % — the 0.10 figure 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 1 and ASTM B265 Grade 1 use the same ceilings: O ≤0.18 · Fe ≤0.20 · 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 ≥240 MPa. DIN Ti 1 gives a RANGE: Rm 290–410 MPa. So a heat that conforms to ASTM can fall below the DIN lower limit (say 260 MPa) or exceed its upper limit (430 MPa). Tell a customer who wants dual certification this up front
Yield strength​‌​​‌​ASTM B265: 138–310 MPa (20–45 ksi) — it has a maximum as well as a minimum. The commonly published DIN Ti 1 value is ≥200 MPa. The ASTM maximum is the line most buyers miss: heavily cold-worked, “stronger” Grade 1 does not conform
Elongation​‌​​‌​ASTM B265 A ≥24 % (50 mm) versus DIN Ti 1 ≥30 % — DIN is the harder target
Numbers and certificate​‌​​‌​3.7025 = DIN 17850 Ti 1 (base metal) · 3.7024 = WL/aerospace · 3.7026 = welding FILLER wire. Three different documents, permanently confused on datasheets. 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 plate240138ASTM B348 / ASME SB-348 – annealed bars and billets240138AMS 4940 – annealed sheet, strip and plate172
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ConditionHardnessYield MPaTensile MPaElongation
ASTM B265 / ASME SB-265 – annealed strip, sheet and plate—​‌​​‌​138-310240​‌​​‌​24%
ASTM B348 / ASME SB-348 – annealed bars and billets​‌​​‌​—138​‌​​‌​24024%​‌​​‌​
AMS 4940 – annealed sheet, strip and plate—​‌​​‌​172—​‌​​‌​—
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.

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Never mix specification minima with typical mill values. Purchasing works from the minima; typicals are a guarantee of nothing and, if substituted for the specification, cause trouble on the first certificate.

Specification Minima · ASTM B265 Grade 1 (annealed, room temperature)

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Tensile and yield minimaRm ≥240 MPa (35 ksi) · Rp0.2 ≥138 MPa (20 ksi)​‌​​‌​
Yield Rp0.2 · MAXIMUM≤310 MPa (45 ksi) — this line is an upper limit and it is enforced. Over-cold-worked material is rejected​‌​​‌​
Elongation · bend radiusA ≥24 % (50 mm). Bend radius 1.5T (t <1.8 mm) · 2T (1.8–4.75 mm); the coupon must bend through 105° without fracture (ASTM E290); Grade 2 is 2T / 2.5T. Hardness is typically ~70 HRB / ~120 HV (Gr 2: ~80 HRB / ~145 HV) — typical, not a specification requirement​‌​​‌​
MIL / AMS differs [D]AMS-T-9046 CP-4 and AMS 4940 give the yield minimum as 25 ksi (172 MPa) — above ASTM’s 20 ksi. Do not rely on the ASTM minimum for an aerospace order​‌​​‌​
DIN 17850 Ti 1 · A SEPARATE SYSTEM — DO NOT MIX THE ROWS

Tensile strength Rm​‌​​‌​290–410 MPa (a range) — its minimum is above ASTM’s 240 MPa, and there is an upper limit as well
Yield and elongation​‌​​‌​Yield ≥200 MPa (the source labels this a 1.0 % offset; take care when comparing with Rp0.2) · elongation ≥30 % — harder than ASTM’s 24 %. Practical consequence: an ASTM B265 Grade 1 certificate does NOT automatically mean DIN 17850 Ti 1 conformity; if dual certification is wanted, say so at order stage
Typical Mill Values — NOT GUARANTEED

​‌​​‌​

Annealed sheet · typical bandRm ~290–340 MPa · Rp0.2 ~170–250 MPa · elongation typically above 30 % — that last line is the commercial case for Grade 1​‌​​‌​
Elastic constantsE = 103–105 GPa [D] — roughly half that of steel, so twice the deflection at the same section. Compressive modulus ~110 GPa · shear ~45 GPa · Poisson 0.37 — Grade 2 data, single-sourced; 0.32–0.37 is also quoted for Poisson​‌​​‌​
Bauschinger effectA drop of up to 25 % in compressive yield after stretching has been reported. If a cold-formed titanium part carries compressive load, this is a real design item​‌​​‌​
What Happens Hot (unalloyed titanium · typical trend)

General behaviour​‌​​‌​Unalloyed titanium weakens fast and becomes more ductile fast as it heats; it is not a creep alloy. Measured example (Gr 2): 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 says​‌​​‌​The trend is the same for Grade 1 from a lower starting point; Grade 1’s elevated-temperature tensile table could not be independently verified — do not invent numbers. Above 315 °C (600 °F) there is no code allowable stress; even if mechanical data reaches 400 °C, the design temperature stops at 315 °C
Oxidation in air​‌​​‌​Above ~540 °C alpha-case formation 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 · Unalloyed Titanium Grade 1

Density​‌​​‌​4.51 g/cm³ (0.163 lb/in³) — 57 % of steel, 1.7 × aluminium. Melting range 1,649–1,671 °C (3,000–3,040 °F)
β transus​‌​​‌​~888 °C (1,630 °F ±14 °C). [D: one source gives 881 °C for the same 1,630 °F; 1,630 °F converts exactly to 888 °C. An uncertainty of ±15 °C with interstitial content is normal.] Grade 2 is ~913 °C — oxygen stabilises α, so the transus moves up
Modulus of elasticity​‌​​‌​103–105 GPa [D]
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; unalloyed titanium conducts markedly better
Thermal expansion​‌​​‌​8.6 × 10⁻⁶ /K (20 °C) · 8.7 (0–200 °C) · ~9.7 (500 °C). About half that of stainless steel — in a titanium/steel tubesheet that difference is stress
Specific heat · resistivity​‌​​‌​Specific heat ~520–526 J/kg·K · electrical resistivity ~0.52 µΩ·m (52 µΩ·cm) (Grade 2 data); another source gives 54–60 µΩ·cm for the unalloyed grades
Magnetic · surface film​‌​​‌​Non-magnetic — the reason for its use in MRI equipment and mine-hunting vessels. The TiO₂ film that forms spontaneously on the surface 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 1 cannot be hardened by heat treatment. In single-phase α titanium there is no solution treat plus age, no martensite, no precipitate. Heat treatment has three purposes and all three are to soften, to relieve stress and to stabilise dimensions.

Heat Treatment · Grade 1

​‌​​‌​

Annealing538–704 °C · 0.5–2 h · air cool. A mill anneal band of 650–760 °C is also quoted. The β transus (~888 °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 — a tolerance plan that ignores this does not work​‌​​‌​
Stress relief538–593 °C · ~30 min · air cool, after welding, heavy machining or cold forming. Not forbidden — recommended for welded titanium vessels​‌​​‌​
Damaging phase windowNone. Titanium has no equivalent of the σ, μ, Ni₄Mo or γ′ precipitates of the nickel alloys — the only enemies are oxygen, nitrogen and hydrogen entering through the surface​‌​​‌​
FormingFinish forging band 316–649 °C; heating band for deep drawing and spinning 204–538 °C; 25–40 % reduction below the β transus tidies the microstructure. In cold forming Grade 1 is the best of the family: bend radius 1.5T–2T. But because the modulus is low, springback is markedly greater than in steel — allow generous overbend in the die​‌​​‌​
Alpha Case, Hydrogen and Iron — Titanium’s Three Real Surface Damages

Alpha case​‌​​‌​The oxygen-rich, hard and brittle α layer that forms when titanium is heated in air. Grey-white, powdery or coloured, it directly destroys fatigue life and ductility, and it forms in air annealing, unshielded welding, hot forging, laser/plasma cutting and on an overheated grinding surface. The only cure is to remove it: pickling (HF/HNO₃) or machining — and because pickling uses HF it carries a hydrogen pick-up risk
Hydrogen​‌​​‌​Ceiling 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 shielding 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 grinding wheels are all forbidden — a titanium shop must be physically separated from steel

Welding​‌​​‌​

Welding titanium is not difficult; welding it CLEAN is. Metallurgically Grade 1 is the easiest of the family to weld — single phase, no hardening, no preheat, no cracking tendency. The entire risk sits in one place: molten and hot titanium absorbs oxygen, nitrogen and hydrogen greedily.

Welding · Titanium Grade 1

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Suitable processesGTAW (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 — slag and flux moisture mean inevitable contamination​‌​​‌​
Filler metalAWS A5.16 ERTi-1 (W.Nr. 3.7026). Grade 2 base metal is welded with ERTi-2. Rule: the filler must match the base metal or be one grade BELOW it — never above, or the weld metal ends up more brittle than the parent​‌​​‌​
Shielding gasArgon, 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 purgeMANDATORY 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 not repaired, it is cut out​‌​​‌​
Trailing shieldEffectively mandatory. Weld metal and HAZ must stay under argon until they are too cool to take colour; apart from short tacks, clean welding is impossible without it​‌​​‌​
Preheat · interpass
stress relief
There is no preheat and none is needed — with no hardening transformation there is no cold-cracking risk. Keep interpass temperature low; a numerical code limit could not be independently verified, and the working rule on the shop 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​‌​​‌​
CleanlinessThe “white glove rule”: chemical cleaning with acetone or MEK first, then a stainless brush or carbide burr dedicated to titanium only. No tool that has touched steel touches titanium. Handle only with clean nitrile gloves; wipe the filler wire with an acetone rag immediately before use​‌​​‌​
WELD COLOUR — the Only Valid Quick Acceptance Test on the Floor

Bright silver · light straw​‌​​‌​ACCEPT. Bright silver: shielding was perfect. Light straw/gold: superficial oxidation, removable with Scotch-Brite
Dark blue / purple​‌​​‌​REJECT. Significant oxidation, properties degraded — rejected in aerospace and pressure equipment
Grey / white powdery​‌​​‌​SCRAP. This is alpha case — a brittle, ceramic-like layer. It is not cleaned off; it is cut out and rewelded
Pre-production tack test​‌​​‌​Every shift, before production starts, run a few tacks on a clean piece of scrap titanium. If the tack is bright silver, carry on. If you see a rainbow halo, a blue tint or haze, STOP: there is a gas leak, moisture in the line or a bad batch of gas. This single habit prevents most titanium welding scrap

Machining​‌​​‌​

Grade 1 is the hardest grade in the titanium family to machine — and because that is counter-intuitive, it is constantly planned wrong. Being soft does not make it easier; on the contrary it goes “gummy”: the chip smears onto the tool instead of breaking, forms a built-up edge (BUE) and ruins the surface. Grade 2, with its higher oxygen, breaks chips more cleanly.

Starting Parameters (CP titanium · family guidance)

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Cutting speed · feedGeneral starting band ~55–98 m/min (180–320 SFM) · roughing ~49–67 m/min · finishing ~61–91 m/min. 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 and coolantSharp, positive-rake carbide coated AlTiN or TiAlN; on Grade 1 edge sharpness matters more than anything — the moment it dulls, the material is smeared rather than cut. High-pressure through-tool coolant is preferred; flood is acceptable, dry cutting is not done​‌​​‌​
Never dwellTitanium work hardens the instant it is rubbed. Retract the drill fully on every peck; a drill that sits at the bottom of the hole hardens it and breaks the tool on the next pass. Short tools, short overhang, rigid machine — the low modulus means the workpiece flexes too​‌​​‌​
FIRE — With Titanium This Is a Procedure, Not a Warning

DO NOT USE WATER​‌​​‌​The risk is in fine chips, grinding dust and swarf — bulk titanium does not ignite, high surface-to-volume material does. 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; do not send grinding dust to a wet collector — wet titanium dust generates hydrogen
Pure oxygen​‌​​‌​Titanium 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 chlorine​‌​​‌​In dry chlorine gas titanium corrodes rapidly and can ignite; passivation requires the gas to contain ~1 % water. In a chlor-alkali plant the dry chlorine line is forbidden territory for titanium

Corrosion — Why It Is Good, and WHERE IT FAILS​‌​​‌​

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.
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GradeUNSW.-Nr.Oxygen maxIron maxNitrogen maxTensile min MPaYield min MPaYield max MPaElongation minNote
Ti Grade 1UNS R50250​‌​​‌​3.70250.18%​‌​​‌​0.20%0.03%​‌​​‌​240138​‌​​‌​31024%​‌​​‌​Lowest oxygen, highest ductility. Deep drawing and explosion cladding work.
Ti Grade 2​‌​​‌​UNS R504003.7035​‌​​‌​0.25%0.30%​‌​​‌​0.03%345​‌​​‌​275450​‌​​‌​20%The workhorse of commercially pure titanium. The most common grade for plate, tube and heat exchangers.​‌​​‌​
Ti Grade 3UNS R50550​‌​​‌​3.70550.35%​‌​​‌​0.30%0.05%​‌​​‌​450380​‌​​‌​55018%​‌​​‌​The intermediate step. It is not in this card set; it is shown to complete the ladder.
Ti Grade 4​‌​​‌​UNS R507003.7065​‌​​‌​0.40%0.50%​‌​​‌​0.05%550​‌​​‌​483655​‌​​‌​15%The strongest of the commercially pure family. It is absent from most pipe and tube specifications.​‌​​‌​

Additional information
Iliski​‌​​‌​As 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.
Mechanism​‌​​‌​Oxygen 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.
Warning​‌​​‌​All 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.

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All of titanium’s corrosion resistance rests on one thing: the spontaneously formed TiO₂ passive film. That film is extremely stable, tightly adherent and — the critical point — self-healing, but only if oxygen or water is present in the environment. Every piece of good news and every piece of bad news below follows from that one sentence. 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 — both build the same TiO₂ film. Grade 1’s slightly lower iron gives a marginal edge in some environments; do not turn that into a sales argument.​‌​​‌​

WHERE IT IS EXCELLENT

Seawater​‌​​‌​The family’s flagship duty. 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]
Oxidising environments​‌​​‌​Nitric acid, chromic acid, oxidising chlorides, hypochlorite, wet chlorine. These feed the film, and titanium here beats 316L and most nickel alloys
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
Chloride SCC · alkalis · organics​‌​​‌​Fully resistant to stress-corrosion cracking in aqueous chloride solutions — the boiling MgCl₂ scenario that is a nightmare in stainless is a non-issue for titanium (for comparison, AISI 316L cracks and super duplex is limited). Alkaline media and most organics are untroubled; cavitation and erosion resistance are high and there is no practical velocity limit
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. The limit moves up if ferric ion is present​‌​​‌​
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. These limits are void in phosphoric acid containing halides​‌​​‌​
Nitric acidOutstanding resistance across the whole concentration range at sub-boiling temperatures. This is the acid titanium is strongest in — 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 right answer there is the nickel-molybdenum family (Hastelloy B-3) or the palladium titanium grades (7/11/16/17)
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 in practice; (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 of the surface. In near-neutral brines a cathodic potential more negative than −0.70 V (SCE) is quoted as the threshold. Practical consequence: 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). 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 · Anhydrous methanol​‌​​‌​Stress-corrosion cracking once water falls below 1.5 %
8 · Pure oxygen​‌​​‌​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); above 649 °C (1200 °F) oxygen pick-up embrittles it. Also: molten chloride salt baths, alkaline peroxide solutions and streams containing liquid mercury are all published prohibitions
9 · 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 not the titanium but the other metal; because the titanium cathode area is large, the effect is severe. Titanium tubes in a steel tubesheet is a classic field failure
The Upgrade Path — What to Answer When Grade 1 Is Not Enough

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Grade 11 (R52550)Grade 1 + 0.12–0.25 % palladium. It keeps Grade 1’s formability and raises resistance to reducing acid and crevice corrosion dramatically. This is the direct corrosion upgrade for Grade 1. The cheap version is Grade 17 (R52252): 0.04–0.08 % Pd​‌​​‌​
Grade 7 (R52400)Grade 2 + ~0.15 % Pd. Published as moving the crevice threshold in seawater to ~250 °C (at pH >1), and usable to 27 % HCl at 25 °C and 45 % H₂SO₄. Cost 2–3 × Grade 2. The cheap version is Grade 16 (0.04–0.08 % Pd, 20–35 % cheaper); to escape the palladium price there is also Grade 26 (ruthenium-bearing, approved as 26H)​‌​​‌​
Grade 12 (R53400)Ti-0.3Mo-0.8Ni, no palladium. Crevice resistance to ~120 °C in hot chloride brines; its strong-acid resistance is below Grade 7’s. Cost ~1.3–1.5 ×​‌​​‌​
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​‌​​‌​

Frequently Asked Questions

Is oxygen really the only difference between Grade 1 and Grade 2? Then why does the price run the other way?​‌​​‌​

Yes — only two lines in the specification differ: oxygen and iron. Grade 1 is O ≤0.18 % and Fe ≤0.20 %; Grade 2 is ≤0.25 % and ≤0.30 %. The carbon, nitrogen and hydrogen ceilings are identical, and there is no deliberately added alloying element in either.
The consequence is not small: that 0.07 percentage point of oxygen roughly doubles the minimum yield, from 138 MPa to 275 MPa. The price is that minimum elongation falls from 24 % to 20 % and the bend radius goes from 1.5T–2T to 2T–2.5T.
The reason the price runs the other way is volume, not metallurgy. Grade 2 is the overwhelming majority of industrial titanium consumption and is stocked at every service centre; Grade 1 is melted to a narrower oxygen window and is usually a smaller batch. So its price per kilo is often above Grade 2’s, its lead time is longer and the thickness range is narrower.
Practical advice: if the reason is deep drawing, explosive cladding, an anode substrate or a very tight bend radius, Grade 1 is a genuine requirement. If the reason is “purer, therefore better corrosion resistance”, the reason is weak: both grades build the same TiO₂ film and behave the same in practice. In that case Grade 2 is faster, cheaper and more useful in a code calculation.

The customer specification says “Titanium Grade 1, 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.
Metallurgically unalloyed titanium is untroubled at 400 °C: no phase transformation, no embrittlement window, the β transus far away (~888 °C). The material simply gets weaker — published typical data for Grade 2 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. There is no code allowable stress above it.
A second coverage problem: most of the code rows on this page were verified through Grade 2; that Grade 1 (R50250) is separately listed in the same sections could not be independently verified. Confirm the R50250 line in Section II Part D before ordering. In practice most designers move to Grade 2 anyway: a 138 MPa minimum yield inflates the wall thickness.
The third and most forgotten item is flanges. ASME B16.5 does not cover titanium. There is no ready-made pressure–temperature table; a titanium flange is made to B16.5 dimensions but its rating has to be calculated per B16.5 Annex A. “Class 300 titanium flange” is not a rating on its own.
Realistic answers: get the design temperature brought down to 315 °C; move to Grade 2 or Grade 2H for strength (2H guarantees 400 MPa minimum tensile on identical chemistry, and in one published example gives a 14 % material saving under Div. 2 Class 2 rules); or use the titanium as a non-pressure-retaining lining on a code-approved backing material. 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 want Grade 1 plate for explosive cladding onto steel. Why not Grade 2?​‌​​‌​

Because explosive cladding is a forming process, and Grade 1 is the most formable grade in the family. A thin titanium plate is driven onto the backing plate at very high velocity by explosive energy; a metallurgical bond forms at the interface, but the price is very high local plastic deformation in the impact zone. Grade 1’s minimum elongation is 24 % and its bend radius 1.5T–2T; Grade 2, at 20 % and 2T–2.5T, is markedly stiffer and more prone to cracking at the wave front. The same logic applies to deep drawing, spinning, pressing plate-heat-exchanger plates and tank lining.
Three warnings. (1) If the backing steel is to be stress relieved after cladding, make sure the temperature suits the titanium side too: 538–593 °C is safe; an anneal at 650 °C or above carried out in air produces alpha case on the titanium surface. (2) No steel tool may touch the clad surface — free iron contamination starts local corrosion in service. (3) Seam welds are made with ERTi-1 under full argon shielding and back purge; an unshielded root pass is scrap, not a repair.
And let us be honest: if the part will not be formed, the premium you pay for Grade 1 buys nothing. For flat plate, pipe, flanges and pressure vessels, Grade 2 is the better choice on every count.

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

1. “Grade 1 and Grade 2 have the same chemistry” — WRONG. Two lines differ: oxygen (0.18 / 0.25 %) and iron (0.20 / 0.30 %). Those two lines double the minimum yield.
2. The AMS-T-9046 / MIL-T-9046 “CP” numbering runs INVERSE. CP-4 = Grade 1, CP-3 = Grade 2, CP-1 = Grade 4. Assuming “CP-1 must be the purest” is the most common and most expensive misreading.
3. AMS number confusion. Grade 1’s aerospace sheet specification is AMS 4940 (“25.0 ksi yield”); AMS 4901 is Grade 4 at 70 ksi yield; AMS 4902 is Grade 2. Some distributor tables assign AMS 4901 to both Grade 1 and Grade 4 and thereby contradict themselves in the same table.
4. The material-number triplet. 3.7025 = DIN 17850 Ti 1 (base metal), 3.7024 = WL/aerospace, 3.7026 = welding FILLER wire. The same triplet exists on the Grade 2 side: 3.7035 / 3.7034 / 3.7036.
5. The ASTM minimum and the DIN range get mixed. ASTM B265 Grade 1 gives only Rm ≥240 MPa; DIN Ti 1 sets both a lower and an UPPER limit at Rm 290–410 MPa. A heat that conforms to ASTM may fail DIN — from below or from above.
6. The YIELD MAXIMUM gets overlooked. ASTM B265 Grade 1 yield is 138–310 MPa; 310 MPa is an upper limit and it is enforced. There is no such product as “high-strength Grade 1”.
7. There is no “Grade 1H”. The ASME-approved H grades are 2H, 7H, 16H, 26H.
8. ASTM B337 is still quoted as the pipe specification — it was WITHDRAWN in 1997. The correct references are B861 (seamless) and B862 (welded).
9. “B16.5 Class 150 titanium flange” is taken for a rating — it is NOT. B16.5 does not cover titanium; the rating is calculated per Annex A.
10. 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].
11. 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.
12. “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 red fuming nitric acid, embrittles with hydrogen above 77 °C under cathodic charging and suffers crevice corrosion in seawater above 82 °C.
13. Hardness scale and carbon ceiling. Grade 1 is ~70 HRB (~120 HV); reading “70” as HRC produces nonsense. And the carbon ceiling is often printed as 0.10 % — the current ASTM B265 value is 0.08 %.
14. Hardening by heat treatment gets offered. Grade 1 is single-phase α titanium; it cannot be hardened. For surface hardness the route is anodising, nitriding or coating.
15. The modulus is assumed to be steel-like. It is 103–105 GPa, roughly half that of steel — twice the deflection at the same section. In titanium design stiffness almost always governs before strength.

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Related grades

Ti Grade 2  ·  Ti Grade 4  ·  Ti Grade 5  ·  Ti Grade 5 ELI  ·  All titanium alloys →​‌​​‌​

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