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.
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
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
DEFENCE METAL
C %
≤ 0.08
N %
≤ 0.03
Ti %
Balance
Fe %
≤ 0.20
O %
≤ 0.18
H %
≤ 0.015
Mechanical Properties at 20 °C
DEFENCE METAL
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/mm²
105
Physical Properties at 20 °C
DEFENCE METAL
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
DEFENCE METAL
Trade name
Ti Grade 1
UNS
R50250
AMS
4940
Available forms
Round 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)
DEFENCE METAL
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.
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).
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)
ASTM B338 / SB-338 — this is the family standard for condenser and heat-exchanger tube
Pipe
Seamless 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 fittings
ASTM 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 · castings
ASTM 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 implant
ASTM 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
Aerospace
AMS 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 consumables
Bare 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 IX
Titanium 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
Europe
DIN 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
HEAT TREATMENT — SCHEMATIC
DEFENCE METAL
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.
Returns a cold-worked structure to a fully recrystallized equiaxed alpha structure. Restores formability and corrosion resistance. The temperature stays BELOW the beta transus.
Temperature
650-760 °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.
Time
6 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.
Cooling
Air cool. NASA/DMIC states air or furnace cooling. Cooling rate does not set the strength; there is NO hardening by quenching.
Resulting hardness
Annealed condition. Specification minimums are written for this condition.
DEFENCE METAL
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.
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.
315 °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 it
Section 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 B31.3
Titanium 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 1
Most 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
DEFENCE METAL
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.
O ≤0.18 and Fe ≤0.20 — the two lines that define the grade. Grade 2: ≤0.25 and ≤0.30
Carbon · Nitrogen
C ≤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 · others
H ≤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
DEFENCE METAL
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
ASTM B348 / ASME SB-348 – annealed bars and billets
—
138
240
24%
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.
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)
≤310 MPa (45 ksi) — this line is an upper limit and it is enforced. Over-cold-worked material is rejected
Elongation · bend radius
A ≥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
DEFENCE METAL
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
DEFENCE METAL
Annealed sheet · typical band
Rm ~290–340 MPa · Rp0.2 ~170–250 MPa · elongation typically above 30 % — that last line is the commercial case for Grade 1
Elastic constants
E = 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 effect
A 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)
DEFENCE METAL
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
DEFENCE METAL
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
DEFENCE METAL
Annealing
538–704 °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 relief
538–593 °C · ~30 min · air cool, after welding, heavy machining or cold forming. Not forbidden — recommended for welded titanium vessels
Damaging phase window
None. 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
Forming
Finish 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
DEFENCE METAL
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
DEFENCE METAL
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 — slag and flux moisture mean inevitable contamination
Filler metal
AWS 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 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
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 not repaired, it is cut out
Trailing shield
Effectively 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
Cleanliness
The “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
DEFENCE METAL
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)
DEFENCE METAL
Cutting speed · feed
General 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 coolant
Sharp, 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 dwell
Titanium 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
DEFENCE METAL
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.
DEFENCE METAL
Grade
UNS
W.-Nr.
Oxygen max
Iron max
Nitrogen max
Tensile min MPa
Yield min MPa
Yield max MPa
Elongation min
Note
Ti Grade 1
UNS R50250
3.7025
0.18%
0.20%
0.03%
240
138
310
24%
Lowest oxygen, highest ductility. Deep drawing and explosion cladding work.
Ti Grade 2
UNS R50400
3.7035
0.25%
0.30%
0.03%
345
275
450
20%
The workhorse of commercially pure titanium. The most common grade for plate, tube and heat exchangers.
Ti Grade 3
UNS R50550
3.7055
0.35%
0.30%
0.05%
450
380
550
18%
The intermediate step. It is not in this card set; it is shown to complete the ladder.
Ti Grade 4
UNS R50700
3.7065
0.40%
0.50%
0.05%
550
483
655
15%
The strongest of the commercially pure family. It is absent from most pipe and tube specifications.
DEFENCE METAL
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.
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
DEFENCE METAL
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
Useful 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 acid
Outstanding 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 acid
ATTACKED 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
DEFENCE METAL
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
DEFENCE METAL
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 5
Moving 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 titanium
If 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.