UNS R50700 · W.Nr. 3.7065 · DIN 17850 Ti 4 · ASTM Grade 4 · COMMERCIALLY PURE (unalloyed) titanium, alpha phase. Ceilings: O 0.40% max · Fe 0.50% max · N 0.05% 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 STRONGEST grade of the commercially pure family; all of that strength comes from raising the oxygen, iron and nitrogen ceilings. IT DOES NOT PRECIPITATION HARDEN AND IT DOES NOT QUENCH HARDEN: it is single-phase alpha.
It is bought where the corrosion behaviour of unalloyed titanium must be kept but Grade 2 cannot carry the load: dental implants and bone screws, surgical plates, airframe fasteners and clamps, cryogenic vessels, high-strength chemical process parts and pickling baskets.
Forms
Round bar · plate · sheet · strip · forgings · wire. All forms are supplied to order.
Standards
AMS (verified): 4901 – sheet, strip and plate; commercially pure, annealed, 70.0 ksi (485 MPa) yield strength · 4921 – bars, wire, forgings, flash welded rings and forging/ring stock up to 101.60 mm nominal diameter; commercially pure, 70 ksi (483 MPa) yield. ASTM: B265 / SB-265 (strip, sheet, plate) · B348 / SB-348 (bars and billets) · B381 Grade F-4 (forgings) · B863 (wire) · F67 Grade 4 (unalloyed titanium for surgical implants). EN / DIN: DIN 17850 Ti 4 (composition, W.Nr. 3.7065) · DIN 17860 (sheet/plate) · DIN 17862 (bar) · DIN 17864 (forgings). MIL: MIL-T-9046H Type 1 Composition B and MIL-T-9046J CP-1 (sheet, strip, plate) · MIL-T-9047G / AMS-T-9047A CP-70 (bar). Welding: AWS A5.16 / SFA-5.16 ERTi-4. 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
Strength gained while staying unalloyed. The minimum tensile strength is 550 MPa and the minimum yield strength is 483 MPa – 59% and 76% above Grade 2 respectively – and it is obtained without adding any alloying element such as aluminium or vanadium.
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 4 IsStandards by Product FormASME Code Acceptance and Maximum Code TemperaturesProduct Forms With NO StandardChemical CompositionMechanical PropertiesPhysical PropertiesHeat Treatment and Thermal StabilityWeldingMachiningCorrosionFrequently Asked QuestionsCommon Datasheet Errors and Purchasing Traps
Ti Grade 4 — commercially pure titanium, high oxygen.
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: Because Ti Grade 4 offers more mechanical strength and hardness than Ti Grade 2, it can be more difficult to machine. It can nevertheless be machined with suitable process conditions and techniques.
Machining: It can be processed by operations such as milling, turning and drilling. Because of the hardness and high melting point of titanium, machining at low speed is recommended. Cutting tools should generally be a hard alloy or carbide, and cutting fluids should be used to prevent the titanium from overheating.
Welding: It can be welded by the TIG (Tungsten Inert Gas) and MIG (Metal Inert Gas) methods. Using shielding gases such as argon during welding prevents oxidation.
Cold forming: It is suitable for cold forming operations and can be shaped by processes such as plasma cutting and bending.
Hot forming: It is also suitable for hot forming, but oxidation of the titanium must be prevented at high temperatures and carefully monitored.
Chemical Composition
DEFENCE METAL
C %
≤ 0.08
N %
≤ 0.05
Ti %
Balance
Fe %
≤ 0.50
O %
≤ 0.40
H %
≤ 0.015
Mechanical Properties at 20 °C
DEFENCE METAL
Hardness HB 30
≤ HB 200
0.2% Yield Strength Rp N/mm²
≥ 485
Tensile Strength Rm N/mm²
≥ 550
Elongation
≥ 15%
Modulus of Elasticity kN/mm²
106
Physical Properties at 20 °C
DEFENCE METAL
Density gr/cm³
4.51
Specific Heat Capacity J/kg K
540
Thermal ConductivityW/m K
18
Electrical Resistivity Ω mm²/m
0.55
Standards and Equivalents · Ti Grade 4
DEFENCE METAL
Trade name
Ti Grade 4
UNS
R50700
AMS
4901 · 4921
Available forms
Round bar · Flat bar · Plate · Sheet · Tube · Forgings All forms are supplied to order.
What Titanium Grade 4 Is — and Why “Commercially Pure” Is a Misleading Phrase
Titanium Grade 4 (UNS R50700 / W.Nr. 3.7065 / DIN designation Ti 4, often sold as Ti99.5) is the strongest of the four unalloyed (commercially pure, CP) titanium grades. And there is only one thing you need to understand about it: Grades 1, 2, 3 and 4 are the same metal. None of them contains an alloying addition — no chromium, no nickel, no aluminium, no vanadium. The only difference between them is the deliberately different ceiling placed on the interstitial elements: oxygen, iron, nitrogen and carbon.
Put differently, the alloying element in Grade 4 is oxygen. Oxygen occupies interstitial sites in the HCP (α) titanium lattice, locks slip planes and raises strength — at the cost of ductility, fracture toughness and cold formability. The oxygen ceiling in Grade 1 is 0.18 %; in Grade 4 it is 0.40 %. That single change lifts the minimum tensile strength from 240 MPa to 550 MPa, roughly 2.3×. The identity of the metal does not change and its corrosion behaviour is effectively unchanged; only the mechanical behaviour moves.
The commercial consequence in one sentence: Grade 4 is CP titanium that delivers about 1.75× the strength of Grade 2 while giving up nothing in corrosion resistance — and it pays for that in ductility, formability, supply chain and available product forms. That last item is the most valuable information on this page and almost no distributor sheet prints it: Grade 4 has no pipe specification, no tube specification and no casting specification.
The CP Titanium Ladder — Interstitial Content Is the Only Variable
DEFENCE METAL
Grade 1 (R50250 / 3.7025)
O ≤0.18 % · Fe ≤0.20 % · N ≤0.03 %. Rm ≥240 MPa · Rp0.2 170–310 MPa · A ≥24 %. The most ductile, the softest. Deep drawing, rupture discs, anode structures. Never used where strength matters
Grade 2 (R50400 / 3.7035)
O ≤0.25 % · Fe ≤0.30 % · N ≤0.03 %. Rm ≥345 MPa · Rp0.2 275–450 MPa · A ≥20 %. The overwhelming majority of the world’s CP titanium is this grade. Heat-exchanger tube, vessel cladding, pipe, seawater hardware
Grade 3 (R50550 / 3.7055)
O ≤0.35 % · Fe ≤0.30 % · N ≤0.05 %. Rm ≥450 MPa · Rp0.2 380–550 MPa · A ≥18 %. The intermediate grade, chosen where Grade 2 is not strong enough and Grade 4 will not form. Far easier to source than Grade 4
Grade 4 (R50700 / 3.7065)
O ≤0.40 % · Fe ≤0.50 % · N ≤0.05 %. Rm ≥550 MPa · Rp0.2 483–655 MPa · A ≥15 %. The top of the CP family. The iron ceiling also rises here, from 0.30 to 0.50 % — so Grade 4 is not merely “more oxygen”, it is also more iron
Grade 5 / Grade 23 (R56400 / R56407)
No longer CP. Ti-6Al-4V is an α+β alloy: Rm ≥895 MPa (Gr 5) or ≥828 MPa (Gr 23 ELI). Comparing it with Grade 4 only makes sense on the strength axis; the corrosion, welding and heat treatment behaviours are entirely different. See the Ti Grade 5 ELI / Grade 23 page
Rp0.2 also has an UPPER limit — and almost nobody prints it
ASTM B265 and B348 define the yield strength of Grade 4 as a BAND of 483–655 MPa. The lower bound is what you expect; the upper bound is the line most datasheets quietly drop. The reason follows directly from the logic above: what pushes yield up is oxygen, and a very high yield means unacceptably low toughness and formability. A heat measuring Rp0.2 = 690 MPa is not “better” — it is out of specification and must be rejected. On the buying side this is one of the rare cases where the instinct “higher numbers are good” works against you.
The same logic applies to cold work. Grade 4 can be cold drawn above 950 MPa, but that is not the annealed specification condition and cannot be compared with ASTM B265 / B348 minimums. Cold-worked Grade 4 wire or bar is bought to a company specification — see the “forms with no standard” section below.
GRADE 4 IS OUT OF SCOPE. ASTM B338 covers 28 grades, ASTM B861 covers 34 grades and ASTM B862 covers 33 grades; Grade 4 is in none of them. If pipe or heat exchanger tube is required, the order must move to Grade 2 or Grade 3.
Castings
No casting grade corresponding to Grade 4 could be verified in ASTM B367.
MIL-T-9046H Type 1 Composition B · MIL-T-9046J CP-1 (sheet, strip, plate) · MIL-T-9047G and AMS-T-9047A CP-70 (bar). CP-1 and CP-70 both mean Grade 4.
European · inspection document
DIN 17850 Ti 4 (W.Nr. 3.7065, 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).
The Grade 4 standards map is an abridged version of the Grade 2 map — and the missing entries directly affect purchasing. The table below follows current ASTM scope texts; rows where the grade is absent from a specification are marked explicitly.
Standards by Product Form · Ti Grade 4 (R50700 / 3.7065)
DEFENCE METAL
Strip · sheet · plate
ASTM B265 Gr 4 / ASME SB-265 · AMS 4901 (unalloyed titanium sheet/strip/plate, annealed, defined by 70.0 ksi / 485 MPa yield) · MIL-T-9046 CP-1 · BS 3TA6
ASTM B863 Gr 4 — the scope text names Grade 4 explicitly. This, and not AWS A5.16, is the correct reference for structural wire
Seamless pipe
NONE. The ASTM B861 scope enumerates 34 grades and Grade 4 is not among them (Grades 1, 2, 2H, 3, 5, 7, 9, 11–29 and 33–38 are; 4 is not)
Welded pipe
NONE. The ASTM B862 scope enumerates 33 grades and Grade 4 is again absent
Heat-exchanger tube
NONE. ASTM B338 (condenser and heat-exchanger tube) currently covers 28 grades and Grade 4 is not one of them. [Conflict] Some older secondary listings print “ASTM B338 Gr 4”; the current scope text does not support it
Welding fittings
ASTM B363 (seamless and welded unalloyed and alloy titanium welding fittings, WPT classes). Coverage of Grade 4 could not be independently verified — confirm against the current edition before ordering
Flanges
There is no separate titanium flange specification. Titanium flanges are made from B381 F-4 forgings or B265 plate; dimensions and pressure class follow ASME B16.5. Titanium has no equivalent of the B462 used for nickel alloys
Bolts · nuts · studs
ASTM F468 (bolts, studs) and F467 (nuts) — nonferrous fasteners. Mill and distributor listings print F467/F468 Grade 4; the grade list could not be independently verified against the current ASTM scope text
Castings
NONE. The ASTM B367 grade list contains no grade C-4 (C-2, C-3, C-5, C-7, C-8, C-9, C-12, C-16, C-17, C-38). [Conflict] Some older cross-reference tables print “B367 Gr 4”; the current scope does not support it
Bare welding wire
AWS A5.16 ERTi-4 — the matching filler for Grade 4 base metal. DIN filler-metal number 3.7066
Covered electrode
NONE, and there never will be. Titanium is not welded by SMAW: slag and flux cannot protect the pool from oxygen and nitrogen. A supplier offering covered electrodes for titanium does not understand the metallurgy
Surgical implant
ASTM F67 (unalloyed titanium for surgical implants — R50250, R50400, R50550, R50700) · ISO 5832-2 · ASTM F1341 (unalloyed titanium wire for implants)
ASME Section IX
Titanium base metals fall in P-No. 51–53 and titanium filler metals in F-No. 51–56. The unalloyed grades group under P-No. 51; the grade-level assignment must be confirmed against the current edition of QW/QB-422
Europe
W.Nr. 3.7065 · DIN designation Ti 4 · DIN 17850 (semi-finished), 17860–17864 (sheet, bar, tube, wire), 17866, 1737 · aerospace material number 3.7064 · filler wire 3.7066
A subtlety worth knowing about AMS 4901: AMS does not name the grade the way ASTM does. It names it by guaranteed yield strength — the formal title of AMS 4901 is “Titanium Sheet, Strip and Plate, Commercially Pure, Annealed, 70.0 ksi (485 MPa) Yield Strength”. The same logic gives AMS-T-9047 CP-70 on the bar side. So the words “Grade 4” may never appear on an AMS certificate, and the buyer wrongly concludes the material is something else. It is the same metal under a different naming system.
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.
Two separate questions must not be conflated here. First: “has ASME adopted the material specification?” Second: “has ASME published a design stress for this grade?” The answer to the first is yes, to the second unverified — and in code work it is the second that decides.
Code Status · Ti Grade 4
DEFENCE METAL
Material specification adoption
ASME SB-265 and SB-348 are the Section II Part B counterparts of ASTM B265 and B348, and Grade 4 is in their grade lists. So far, no problem
Design stress (II-D) listing
Could not be verified — and probably does not exist. The Titanium Association’s 2020 code presentation states that “currently 17 different titanium alloy grades are approved for Section VIII, Division 1 pressure vessel construction” and its stress charts show Grades 1, 2, 2H, 12 and 28. Grade 4 is never mentioned. For code work, Grade 4 should not be offered as a pressure-boundary material without confirming the current ASME II Part D Table 1B
Published temperature range
The Section VIII Div. 1 allowable stress curves in that same presentation are plotted to 600 °F (315 °C). That is the order of the code ceiling for titanium — a surprise for buyers used to the 800–1000 °F of nickel alloys
Approved “H” grades
The four H grades accepted into Section VIII Div. 1 are 2H, 7H, 16H and 26H. There is no “4H”. H grades have identical chemistry but a higher guaranteed minimum tensile strength and exist primarily for pressure vessel use
Practical conclusion
If you need a code titanium vessel, piping system or heat exchanger, the answer is almost always Ti Grade 2 (or Gr 12 / Gr 7 / Gr 28). Grade 4 is an engineering material, not a code material
Non-code use: outside the pressure codes Grade 4 is used widely and without difficulty. The limitation is administrative, not metallurgical — present it as a listing gap, not a material defect.
Product Forms With NO Standard — the Commercially Valuable Section
This is the section your sales engineers should memorise. Grade 4 enquiries most often stall here, and an honest answer is worth far more than a lost order.
Specification Gaps for R50700
DEFENCE METAL
Pipe — seamless and welded
No ASTM pipe specification exists. Grade 4 is absent from the scope lists of B861 (seamless) and B862 (welded). A request for “ASTM B861 Grade 4 pipe” cannot be met. The honest answer has three branches: (1) move to Gr 2 or Gr 3 pipe (code work requires this anyway); (2) have bored/machined pipe made from B348 Gr 4 bar — chemistry conforms to B348, dimensions and mechanicals are by agreement; (3) if strength is genuinely critical, move to Ti Grade 5 ELI or Gr 9 (Ti-3Al-2.5V) pipe — Gr 9 exists precisely for this gap
Heat-exchanger tube
Grade 4 is not in the B338 scope. And here honesty helps: this is not a loss. What decides a heat-exchanger tube is corrosion resistance and expandability, not strength. Grade 2 and Grade 4 have identical corrosion resistance; Grade 2 expands far better and costs far less. A customer asking for Grade 4 tube is usually asking the wrong question
Castings
B367 has no C-4 grade. The titanium casting world runs effectively on C-2 (unalloyed) and C-5 (Ti-6Al-4V). There is no such standardised product as a “Grade 4 cast valve body”. Options: take a C-2 casting and accept lower mechanicals; take a C-5 casting and accept that it is no longer CP titanium; or machine from B348 Gr 4 bar
Cold-drawn / spring wire
Partly covered — know the distinction.ASTM B863 Grade 4 is a real structural wire specification. But B863 covers annealed and defined drawn conditions; heavily cold-worked spring temper in the >950 MPa region is a company-specification matter. And AWS A5.16 ERTi-4 is a welding consumable specification and is not a substitute for structural wire — confusing the two is common
Covered electrode
Does not exist and will not — titanium is not welded by SMAW
Flange specification
There is no titanium-specific flange material specification. The role B462 plays for nickel alloys is taken by B381 forgings and B265 plate. The order line should read: “ASME B16.5 Class ___ WN RF flange, material ASTM B381 Gr F-4“
These gaps all come from one commercial fact: Grade 4 belongs to the strength market, not the corrosion market — and there Ti-6Al-4V and Ti-3Al-2.5V already offer better answers. The real market for Grade 4 is sheet, bar, wire, forgings and implants.
Chemical Composition
ASTM B265 / B348 / B381 / B863, Grade 4 (R50700), weight %:N ≤0.05 · C ≤0.08 · H ≤0.015 · Fe ≤0.50 · O ≤0.40 · residuals 0.1 each, 0.4 total · Ti balance. There are no alloying additions.
What Each Interstitial Actually Does
DEFENCE METAL
Oxygen (≤0.40 %)
The principal strengthener. It enters interstitial sites in the α lattice and locks slip systems. It raises strength, lowers ductility and fracture toughness, worsens ductile-to-brittle behaviour and raises the β transus. The entire Grade 1 → Grade 4 story is this one element
Iron (≤0.50 %)
The second strengthener and the only β stabiliser present, allowing a little β phase at grain boundaries. The ceiling is 0.30 % in Grades 2 and 3 but rises to 0.50 % in Grade 4
Nitrogen (≤0.05 %)
Roughly twice as potent an embrittler as oxygen per unit weight — hence a ceiling one eighth of oxygen’s. Nitrogen is picked up from air during welding and heat treatment, which is largely why the shielding regime exists
Carbon (≤0.08 %)
Limited solubility; above it TiC forms
Hydrogen (≤0.015 %)
This is the only genuinely dangerous one, and its ceiling is a safety limit rather than a product property. 0.015 % = 150 ppm, which sits right on the hydrogen solubility limit of unalloyed titanium (~100–150 ppm). Above it, brittle titanium hydride precipitates
Divergences Between Specifications — What Actually Matters on a Certificate
DEFENCE METAL
Residual total
[Conflict] The ASTM table generally gives 0.1 each / 0.4 total; one mill datasheet distinguishes 0.40 for AMS 4921 and 0.30 for ASTM B348. Both are published. The order must state which specification governs
ASTM vs AMS
The chemistry is effectively identical; the difference is in naming and acceptance testing. The AMS route (4901 sheet, 4921 bar) brings aerospace traceability, tighter sampling and a yield guarantee. Material certified to ASTM is not automatically AMS compliant.
ASTM F67 (implant)
For Grade 4 the chemical limits are identical to B265/B348. What F67 adds is not chemistry but microstructure, grain size, surface and traceability requirements. Saying “F67 = purer titanium” is wrong
ISO 5832-2
The ISO counterpart of the unalloyed titanium implant standard, paired with ASTM F67. ISO 5832-3 is Ti-6Al-4V and has nothing to do with Grade 4 — the two are frequently confused
Hydrogen by form
The hydrogen ceiling can vary by product form. Read this line from the table in the specification actually ordered, not from a generic “0.015” habit
ASTM B348 / ASME SB-348 – annealed bars and billets
—
483
550
15%
AMS 4901 – annealed sheet, strip and plate
—
483-485
—
—
AMS 4921 – annealed bars, wire, forgings and rings (up to 101.60 mm)
—
483
—
—
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.
483–655 MPa (70–95 ksi) — this is a BAND, not a floor
Elongation
≥15 %
Reduction of area
≥30 %
Bend radius
Grade 4 requires the largest bend radius of the CP grades; the number depends on thickness — read the bend table
Typical Mill Values — NOT GUARANTEED
DEFENCE METAL
Yield (typical)
480–635 MPa (70–92 ksi)
Tensile (typical)
655–690 MPa (95–100 ksi) — clearly above the minimum
Elongation (typical)
20–25 % (min 15 %)
Reduction of area (typical)
38–51 % (min 30 %)
Cold worked
>950 MPa — this is NOT the annealed specification condition; do not compare it with ASTM minimums
Hardness
~100 HRB · a European mill sheet gives HB30 ≤200. Do not confuse HRB with HRC: 100 HRB is roughly 20 HRC, and a reader who takes “100” for HRC reaches an absurd conclusion. Always print the scale
Fatigue
CP titanium is one of the few materials that shows a true endurance limit in high-cycle fatigue. A numerical endurance limit for Grade 4 could not be independently verified; ask the mill for a curve
Elevated-Temperature Behaviour
DEFENCE METAL
General trend
CP titanium loses strength rapidly with temperature. Expect to be below half the room-temperature values around 300 °C, and creep starts far lower. Grade 4 is not a high-temperature material
Numerical data
[Unverified] One European mill page publishes values for 315 °C and 425 °C, but which CP grade those rows belong to could not be independently verified. Do not use those numbers in design — for hot service ask the mill for curves by grade and form
Oxidation / alpha case
Heating in air above roughly 600 °C produces a hard, brittle oxygen-enriched surface layer — alpha case. It severely reduces fatigue life and must be removed by pickling or machining. Vacuum or inert-atmosphere heat treatment is preferred
Cryogenic
Unalloyed titanium gains strength at low temperature but loses toughness, and that loss tracks interstitial content directly. Grade 4 is the worst cryogenic performer of the CP family. For cryogenic work the right choice is Grade 1 / Grade 2 or Ti-6Al-4V ELI
Physical Properties
Physical Properties · Ti Grade 4 (room temperature)
DEFENCE METAL
Density
4.51 g/cm³ (0.163 lb/in³) — about 57 % of steel, roughly 1.7× aluminium. This single number is why most applications buy titanium
Melting point
~1660–1670 °C (two independent sources; no single exact value)
Modulus of elasticity
~103–106 GPa (15.0 × 10³ ksi). About half that of steel — twice the deflection for the same section. It governs design (buckling, stiffness) and machining (the part springs away)
Thermal conductivity
[Conflict] Published values scatter between 17.2, 18 and 22 W/m·K. The order of magnitude is reliable: about one third of steel, roughly one twentieth of copper. For an exact value use the mill certificate
Specific heat
~526–540 J/kg·K
Thermal expansion
~9.4 × 10⁻⁶ /K (0–200 °C). Markedly lower than stainless steel (316L ~16 × 10⁻⁶) — a genuine advantage against carbon steel in clad construction and tubesheets
Electrical resistivity
~0.55 µΩ·m (55 µΩ·cm) — high, and it must be accounted for in anode structures
Magnetic response
Non-magnetic (paramagnetic). This underpins MR compatibility and non-magnetic hardware requirements
β transus
~935–963 °C (1715–1765 °F); one source gives 949 °C. α transus ~891–918 °C. This band sets the hot-working and heat treatment ceiling — entering the β field means grain coarsening and loss of ductility
Critical note
The β transus rises with oxygen. The same physics is why the low-oxygen ELI grades have a lower β transus than Grade 5
Heat Treatment and Thermal Stability
Start with the most important negative fact: Grade 4 cannot be hardened by heat treatment. Unalloyed titanium has no precipitation hardening, takes no benefit from martensitic transformation, and there is no solution-treat-and-age (STA) route. Strength comes from only two places: interstitial content (grade selection) and cold work. If a datasheet prints “solution treated and aged” for Grade 4, that sheet has put Ti-6Al-4V data in the wrong place.
Heat Treatment Regimes · Ti Grade 4
DEFENCE METAL
Annealing
[Conflict, both published] One US producer gives 595–760 °C, 2 hours, air cool; two European sources give 600–700 °C and “~700 °C, 3 minutes per mm, minimum 15 minutes soak”. The ranges overlap; the European side is narrower and lower. Follow the specification ordered
Stress relief
[Conflict]540–595 °C, 15–30 minutes, air cool (US producer) or 450–600 °C, ~30 minutes (European mills). Recommended after welding and heavy machining; stress relief of titanium is not forbidden, unlike some nickel-molybdenum alloys
Atmosphere
The decisive item. Any heat treatment in air produces alpha case. Inert gas or vacuum is mandatory; if done in air the case must be removed (pickling or machining allowance). This is the most commonly skipped step
Hydrogen removal
Hydrogen picked up during pickling or faulty welding is removed by vacuum annealing. Solubility ~100–150 ppm; above that, brittle hydride precipitates
β annealing
Not used. Above the β transus (~935–963 °C) you get grain coarsening and loss of ductility with nothing to gain. Hot forming is also kept below the transus
Recrystallisation
Annealing gives back the strength of cold-worked Grade 4. So an order for “>950 MPa cold-worked Grade 4” implies the part will not be annealed afterwards — assess it together with the welding plan
The good news on thermal stability: Grade 4 has no damaging phase window. There is no sigma phase, no ordering embrittlement, no 475 °C embrittlement, no carbide sensitisation. The thermal risk in titanium is not phase transformation but contamination — pickup of oxygen, nitrogen and hydrogen. That is why everything discussed in titanium heat treatment is furnace atmosphere and cleanliness.
Welding
What governs titanium welding is not technique but environment. Molten and hot titanium absorbs oxygen, nitrogen and hydrogen from air without saturating, and every interstitial picked up embrittles the weld irreversibly. Grade 4 is the most sensitive grade of the family in this respect, because its chemistry already sits at the top of the interstitial ceiling: every extra ppm of oxygen eats into an already narrow ductility margin.
Welding Parameters and Rules · Ti Grade 4
DEFENCE METAL
Process
GTAW (TIG) dominates and is the standard choice for unalloyed titanium. GMAW for heavy sections; plasma, electron beam, laser, resistance and diffusion welding are all applied successfully. SMAW and oxy-acetylene are NOT used
Filler metal
AWS A5.16 ERTi-4 (matching) · DIN 3.7066. A common and often preferred alternative is the one-step-softer ERTi-2 — the weld becomes more ductile than the base metal and cracking risk drops where strength is not critical. When joining dissimilar grades, the filler follows the lower-strength side
Shielding gas
Pure argon (or argon-helium). Purity: 99.999 % (5.0) ideal, 99.995 % the practical floor. Never a mixture containing CO₂ or oxygen. Use a gas lens and a large ceramic cup (#12–#16); a small cup creates turbulence and draws in air
Triple shielding
(1) torch shield · (2)trailing shield — the bead must stay protected while it cools · (3)back purge — mandatory on pipe and tube. A titanium weld with an unprotected root is not acceptable
Colour acceptance
In titanium, bead colour is a quality measure, not cosmetics.Bright silver = perfect shielding. Light straw / gold = acceptable, slight surface oxide. Blue / purple = risky, rejected by most specifications. Grey / white powdery = scrap — brittle alpha case has formed; this is removal, not repair
Cleanliness
Ninety percent of the weld is preparation. Degrease with acetone or MEK, then use brushes and wheels dedicated to titanium only. Iron contamination causes galvanic attack and crack initiation. Lint-free gloves; fingerprints cause porosity
Preheat · interpass
No preheat is required or recommended. Keep interpass temperature low — hot metal absorbs more gas. Keep heat input low; avoid wide weaving
After welding
Stress relief is recommended (450–600 °C band), in a protective atmosphere or vacuum. No post-weld operation is forbidden
Tungsten and arc
DCEN · high-frequency arc start is mandatory — scratch starting contaminates with tungsten. Extend post-flow; the bead must stay under argon until it falls below roughly 400 °C
Post-weld strength: a Grade 4 weld approaches base-metal strength, but grain growth and reduced HAZ ductility are normal. An ERTi-2 weld is deliberately softer than the base metal — a considered choice, not a defect.
Machining
Titanium is not difficult because it is hard; it is difficult because it does not carry heat away and because it is chemically active. Thermal conductivity is about a third of steel — nearly all the heat generated in the cutting zone stays at the tool tip instead of in the chip. Hot titanium also reacts with carbide and wears the tool chemically. On top of that comes the low modulus: the workpiece springs away from the tool.
CP titanium machines more easily than Ti-6Al-4V but presents a different problem: it is gummy. Grade 4 is the best machining CP grade because its higher strength gives cleaner chip breaking — Grades 1 and 2 are stickier.
60–120 m/min for CP titanium (this falls to 45–100 m/min for Ti-6Al-4V). One producer gives 12–40 m/min (40–130 fpm) for HSS tooling
Feed
0.08–0.15 mm per tooth.Rule: never feed lightly. A thin chip keeps the heat in the cut; a thick chip carries it out. The classic mill prescription is “low speed, heavy feed”
Tooling
Fine-grain carbide (0.5–0.8 µm), 6–8 % cobalt.AlTiN PVD coating or uncoated preferred; CVD coatings are not recommended. Sharp, positive-rake geometry is essential — uncoated carbide with a polished rake face often outperforms coated
Coolant
Copious coolant is mandatory. Through-tool delivery at 70 bar and above is preferred; external coolant never reaches the cutting zone
Fluid choice
Use non-chlorinated fluid. Chlorinated residue plus later heating means stress corrosion cracking risk; where unavoidable it must be removed completely before heat treatment or welding
Rigidity · dwell
With half the modulus of steel, workpiece and fixture rigidity are critical; thin walls deflect and chatter. And a stationary tool burnishes the surface — keep feeding
FIRE WARNING
Fine titanium chips and dust are flammable, and once burning, water does not extinguish them — it makes them worse. Do not let chips accumulate, collect dry grinding dust, and keep a Class D (metal fire) extinguisher on hand. This is the number one safety item in a titanium shop
Corrosion — Where It Excels, 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.
First, the single most important sentence: the corrosion resistance of Grade 4 is effectively identical to Grades 1, 2 and 3. Interstitial content changes mechanical behaviour; it does not change the passive film. So everything below applies to all CP titanium grades. The claim “Grade 4 is stronger so it corrodes less” is false and must not be made in a sales conversation.
Titanium’s resistance comes from a spontaneously formed TiO₂ passive film that repairs itself within seconds in the presence of ppm levels of oxygen or moisture. Every strength and every weakness of titanium reduces to one question: does the environment let that film re-form?
Where it excels
Seawater:negligible corrosion to 260 °C (500 °F). No pitting, no attack even under biofouling. A condenser tube exposed for 16 years to polluted seawater was slightly discoloured with no evidence of corrosion. Erosion-corrosion: outstanding — it withstands flow velocities of 30 m/s, decisive in the pump and condenser duties that eliminate copper alloys and stainless steels. Oxidising environments: nitric acid, oxidising chlorides, chlorinated water, hypochlorite, chlorine dioxide, chlorate, perchlorate — full resistance. Fatigue: titanium suffers no significant loss of fatigue strength in seawater.
WHERE IT FAILS — this section is mandatory
Environments Where Titanium Fails (with numerical limits)
DEFENCE METAL
Hydrofluoric acid and free fluoride
ABSOLUTE PROHIBITION. Titanium corrodes rapidly even at very dilute concentrations. It is not used in any fluoride-bearing solution at pH < 7. Fluorine gas is likewise not recommended. Exception: fully complexed fluorides pose no risk. This is titanium’s number one disqualifier
Reducing acids — HCl
Unalloyed titanium withstands roughly 7 % HCl at room temperature; that resistance falls considerably near boiling. For comparison: Gr 12 ~9 %, Gr 7 (Ti-0.2Pd) ~27 % — which is exactly what the palladium is for
Reducing acids — H₂SO₄
Unalloyed titanium: ~20 % at 0 °C, ~5 % at room temperature. In boiling sulphuric acid, high corrosion rates are seen even around 0.5 % concentration. Gr 7 reaches ~45 % at room temperature and ~7 % boiling
Phosphoric acid
Unalloyed: up to 30 % at room temperature, ~10 % at 60 °C, ~2 % at 100 °C. Gr 7: ~80 % / ~15 % / ~6 %. Here temperature matters more than concentration
DRY CHLORINE
Dry chlorine attacks titanium rapidly and can cause IGNITION if the moisture content is very low. Numerical threshold: about 1 % water is generally sufficient for passivation under static conditions at room temperature; approximately 1.5 % moisture is required at 199 °C (390 °F). In wet chlorine titanium is excellent — the difference between two states of the same gas is the most dangerous misconception about titanium. The same rule applies to bromine and iodine
Red fuming nitric acid
ABSOLUTE PROHIBITION.A pyrophoric reaction product forms and has caused serious accidents. Published threshold: the pyrophoric reaction develops when water content is below 1.34 % AND NO₂ content is above 6 %
Anhydrous methanol
Unalloyed titanium suffers stress corrosion cracking in methanol whose water content is below 1.5 %. This is the single most important exception to the generalisation that titanium is immune to SCC in aqueous service. Anhydrous halogenated organics and nitrogen tetroxide carry similar risk
Crevice corrosion
In neutral saturated chloride brine, unalloyed titanium shows crevice attack at about 93 °C (200 °F) and above; it is unlikely below 70 °C (158 °F). The practical seawater threshold is ~82 °C (180 °F). The threshold falls as acidity rises. Gr 12 and Gr 7 have shown no crevice attack in neutral saturated brine to 316 °C (600 °F) — that is the grade decision for hot gasketed flanges and tubesheets
Hydrogen embrittlement
Three conditions must occur together: (1) temperature above 77 °C (170 °F) — below that, pickup is so slow it has no practical significance in the absence of severe tensile stress; (2)pH < 3 or pH > 12, or a surface damaged by abrasion; (3) impressed potential more negative than −0.70 V. Solubility limit ~100–150 ppm; absorption of several hundred ppm means embrittlement and cracking under stress. Even in hydrogen gas, 2 % moisture at 800 psi and 157 °C prevented absorption
Galvanic couples
Titanium sits at the noble end of the seawater galvanic series and is the CATHODE in nearly every couple. It is not harmed itself; it ACCELERATES corrosion of coupled aluminium, zinc, magnesium, carbon steel and some stainless steels. And because it is cathodic, it charges itself with hydrogen. Rule: single-metal construction; if impossible, insulate, cathodically protect, or use small titanium area with large less-noble area
Pure oxygen · fire
Titanium can ignite and burn in high-pressure oxygen. Published threshold: ignition cannot be induced even at very high pressure when the oxygen content of the environment is below 35 %. However, once started, the reaction propagates at far lower oxygen levels than were needed to start it. High-oxygen service requires a separate engineering assessment for titanium
Hot salt SCC (>250 °C)
In the 250–500 °C band, with halide salt deposit and stress present together, stress corrosion cracking can be produced in the laboratory in titanium alloys. The experiments concentrate on α+β and near-α alloys (such as Ti-8Al-1Mo-1V); the mechanism is not reported as a significant issue for unalloyed titanium. Even so: a salty fingerprint plus a 300 °C furnace is an avoidable risk
Anhydrous / strongly reducing conditions
The passive film either never forms or cannot repair; corrosion is then rapid. This is precisely where the belief that titanium is “immune to corrosion” breaks down: titanium needs water
The honest summary your page should carry: titanium is the material of oxidising and chloride-bearing environments, and there it is unmatched. It is not the material of reducing acids, fluoride or anhydrous environments. Those two sentences prevent the great majority of titanium sales errors.
Frequently Asked Questions
We use Grade 2. Does moving to Grade 4 make sense?
There is one honest criterion: is the part governed by thickness or by corrosion? If strength sets the wall thickness, Grade 4 delivers a real gain: yield rises from 275 MPa to 483 MPa, i.e. 75 % higher. You can reduce section, cut weight and sometimes drop a size step. For load-bearing implants, diving and defence hardware, fasteners and structural brackets the switch makes sense. If corrosion allowance, expandability or forming sets the thickness, the switch is pointless and harmful. The corrosion resistance of the two grades is identical — Grade 4 does not last longer in any environment. The prices you pay are real: elongation drops from 20 % to 15 %, bend radii grow, deep drawing gets harder, and the margin for error in welding narrows. And the argument is usually settled by supply: Grade 2 is in stock worldwide in every form; Grade 4 is a niche material with long lead times, a higher price per kilogram, and no pipe, tube or casting forms at all. Choose Grade 4 when strength is genuinely required and the form is sheet, bar, wire or forging. If you are on the fence, do not skip Grade 3: it is often the compromise you actually want and it is easier to find.
I need Grade 4 pipe or heat-exchanger tube. Which specification do I order to?
Short answer: there isn’t one. And saying so is far better than taking an order you cannot fill. None of the ASTM specifications for seamless pipe (B861), welded pipe (B862) or heat-exchanger tube (B338) lists Grade 4 in its grade table. B861 enumerates thirty-four grades, B862 thirty-three, B338 twenty-eight — Grade 4 is in none of the three. Some older cross-reference tables print “B338 Gr 4”; the current scope texts do not support it. There are four real options.(1) If the duty is corrosion-driven — which for a heat exchanger it almost always is — move to Grade 2 tube; the corrosion resistance is identical, expandability is far better, and price and delivery are not comparable. (2) If pressure is genuinely high, look at Grade 9 (Ti-3Al-2.5V): that alloy exists precisely for the “high-strength titanium pipe” requirement and is within the B861/B862 scope. (3) For small quantities, have bored/machined pipe made from B348 Gr 4 bar — chemistry conforms to B348, tolerances and mechanicals are by agreement, and the certificate cannot say “B861”. (4) If strength is the requirement and corrosion is secondary, Ti Grade 5 ELI pipe is within the B861/B862 scope. Never write “ASTM B861 Gr 4” in a written quotation. No such line exists and it will be rejected at third-party inspection.
Is Grade 4 good enough for an implant, or should I buy Ti-6Al-4V ELI?
Both are implant materials and the choice depends on what you are making — there is no “better” one. What speaks for Grade 4 is that it is unalloyed. It contains no aluminium and no vanadium. The long-running debate about vanadium release is the main line of criticism aimed at Ti-6Al-4V ELI; Grade 4 sits entirely outside it. The specification route is clean too: ASTM F67 and ISO 5832-2. Dental implant roots, bone screws and plates are Grade 4’s largest market — and in dental implants Grade 4 is effectively the standard. What speaks for Ti-6Al-4V ELI is mechanical. Yield 759 MPa (483 MPa for Grade 4), tensile 828 MPa (550 MPa), and — the real point — markedly better fracture toughness and fatigue behaviour. For load-bearing implants that will see millions of cycles over years — hip stems, spinal instrumentation, intramedullary nails — the choice is usually ELI, via ASTM F136 and ISO 5832-3. The practical dividing line: if the section can be generous and metallurgical simplicity is wanted, Grade 4; if section is constrained and cyclic load is high, Grade 23 (ELI). Do not position Grade 4 as “the cheap implant titanium” — it is a different engineering choice, not a lower one.
Is Grade 4 really harder to weld than Grade 2?
The process is the same; the margin for error is narrower. Both grades are welded with the same equipment, the same gas and the same process (GTAW). Neither needs preheat or a special interpass regime. The difference is chemical margin: the oxygen ceiling of Grade 2 is 0.25 %, that of Grade 4 is 0.40 %. Grade 4 therefore starts at the top of its interstitial budget; every additional oxygen and nitrogen atom picked up from air during welding can push ductility below acceptable levels in Grade 4 even at a level Grade 2 would tolerate. Elongation is already working against a 15 % minimum. In practice this means three things. First, trailing shield and back purge are not negotiable; a set-up that “gets by” on Grade 2 will not do on Grade 4. Second, the colour acceptance criterion must be applied more strictly — a blue bead on Grade 4 is a clear reject. Third, filler selection must be deliberate: matching ERTi-4 preserves strength but also moves the weld toward the brittle side, while one-step-softer ERTi-2 makes the weld more ductile than the base metal and reduces cracking risk. Where strength is not critical, ERTi-2 is often the better engineering decision — but it means the joint will be weaker than the parent metal, and that must be agreed at order stage.
Common Datasheet Errors and Purchasing Traps
1. “ASTM B338 Grade 4 heat-exchanger tube” — WRONG. The current B338 scope enumerates 28 grades and Grade 4 is not among them. Some older secondary listings say otherwise; the scope text governs. 2. “ASTM B861 / B862 Grade 4 pipe” — WRONG.Grade 4 is absent from the grade list of both specifications. Grades 1, 2, 2H, 3, 5, 7, 9, 11–29 and 33–38 are there; 4 is skipped. This is a deliberate scope decision, not a typographical omission. 3. “ASTM B367 Grade C-4 casting” — WRONG. The B367 grade list is C-2, C-3, C-5, C-7, C-8, C-9, C-12, C-16, C-17, C-38. There is no C-4. 4. “Grade 4 is hardened by heat treatment / solution treated and aged” — WRONG.There is no STA route in unalloyed titanium. Strength comes from interstitial content and cold work. Such a line is a sign that Ti-6Al-4V data has migrated onto the wrong page. 5. Dropping the upper bound of the yield band. ASTM Grade 4 yield is the band 483–655 MPa. Most sheets print only “≥483 MPa”. A heat exceeding 655 MPa is out of specification — it is not “stronger, therefore better”. 6. Hardness scale confusion. Grade 4 is typically ~100 HRB, roughly 20 HRC. A reader who takes “100” for HRC imagines a material that does not exist. Always print the scale. 7. Confusing β transus with α transus. For Grade 4 the β transus is ~935–963 °C and the α transus ~891–918 °C; one source gives a single value of 949 °C. These depend on the grade’s oxygen content and are not the same as Grade 2’s — there is no single “titanium β transus”. 8. Thermal conductivity conflict. Published values scatter across 17.2 / 18 / 22 W/m·K, depending on measurement temperature and which CP grade the source meant. Do not publish a single exact figure; give the order of magnitude. 9. “Titanium is immune to corrosion” — DANGEROUSLY WRONG. Titanium fails in hydrofluoric acid, in free fluoride, in dry chlorine, in red fuming nitric acid and in anhydrous methanol, and it has concentration and temperature thresholds in reducing acids (~7 % HCl, ~5 % H₂SO₄ at room temperature). Never put that sentence in a quotation. 10. Treating wet and dry chlorine as the same. Titanium is excellent in wet chlorine; dry chlorine attacks it and can ignite it. Thresholds: ~1 % water at room temperature, ~1.5 % at 199 °C. The difference between two states of the same gas is critical. 11. Using AMS and ASTM interchangeably.AMS 4901 and AMS 4921 identify the grade by 70 ksi yield, not by the words “Grade 4”, and their acceptance testing, sampling and traceability requirements differ from ASTM. A plate certified to ASTM B265 is not automatically compliant with AMS 4901. 12. “Grade 4 is ASME approved” — incomplete and misleading.SB-265 and SB-348 do include Grade 4 as a material specification; but code design requires a published allowable stress in ASME II Part D, and such a listing for Grade 4 could not be verified in this research. The Titanium Association’s code presentation speaks of 17 approved titanium grades for VIII-1 and its charts show Gr 1, 2, 2H, 12, 28; Grade 4 is never mentioned. For code work, do not offer Grade 4 without confirmation from the current II-D edition. 13. Taking “Ti99.5” for a purity guarantee. It is a naming convention from the DIN tradition (the Ti 1 / Ti 2 / Ti 3 / Ti 4 sequence), not an analysis result. What the specification guarantees is interstitial ceilings, not a percentage purity. 14. Believing “F67 = purer Grade 4”.The Grade 4 chemical limits in ASTM F67 are identical to B265/B348. What F67 adds is microstructure, grain size, surface and traceability requirements. It tightens inspection, not chemistry. 15. Confusing ISO 5832-2 with ISO 5832-3.5832-2 is unalloyed titanium (the ISO counterpart for Grade 4); 5832-3 is Ti-6Al-4V. If you see “ISO 5832-3” on a Grade 4 datasheet, that sheet has merged data from two different materials. 16. An offer of titanium covered electrodes.Titanium is not welded by SMAW and no such AWS classification exists. A supplier offering them is selling either another material or a fiction. 17. Ignoring the chip fire risk.Fine titanium chips and grinding dust are flammable and are not extinguished by water. It is the item almost never printed on a datasheet and the one with the most concrete consequence on the shop floor.