Cryogenic propellant tanks
Fusion welds and repairs in 2219 tanks for liquid oxygen and liquid hydrogen on launch vehicles.
2319 is the matching filler metal for welding 2219 aluminium, the high-copper alloy used in launch-vehicle tanks and hot-running airframe structure. It is classified as ER2319 / R2319 under AWS A5.10 and supplied to AMS 4191 for aerospace work. Metline supplies 2319 MIG spools and TIG cut lengths with full certification to customers worldwide.

Most high-strength 2xxx and 7xxx alloys crack when fusion welded, because the weld solidifies over a wide temperature range and tears as it shrinks. 2219 is an exception, and 2319 is the filler that makes the most of it: its chemistry is essentially that of 2219 with extra titanium, so the weld bead can be heat-treated with the parent metal and responds in the same way.
The titanium (0.10 – 0.20 %) and zirconium (0.10 – 0.25 %) act as grain refiners in the weld pool. A finer, equiaxed weld structure resists hot cracking and gives better ductility than a coarse columnar one. Magnesium is held to a very low level, because even small amounts in an aluminium-copper weld widen the freezing range and raise crack sensitivity.
The result is a filler that gives higher weld strength in 2219 than the general-purpose 4043 silicon filler, especially when the welded part is solution treated and aged after welding. That is why it is specified for cryogenic propellant tanks, pressure vessels and hot structures built from 2219 sheet, plate, extrusions and forgings.
Limits below follow the AWS A5.10 / ISO 18273 classification (S Al 2319, AlCu6MnZrTi). The certificate for each lot reports the actual analysis. Note that a simple list of "typical" percentages, such as Cu 6.3 %, is a nominal figure, not a specification limit.
| Element | Limit | Purpose in the weld |
|---|---|---|
| Copper (Cu) | 5.8 – 6.8 | Matches 2219; provides heat-treatable strength |
| Manganese (Mn) | 0.20 – 0.40 | Strength and grain control |
| Titanium (Ti) | 0.10 – 0.20 | Grain refiner in the weld pool; higher than in 2219 |
| Zirconium (Zr) | 0.10 – 0.25 | Grain refinement and crack resistance |
| Vanadium (V) | 0.05 – 0.15 | Elevated-temperature strength |
| Silicon (Si) | 0.20 max | Impurity |
| Iron (Fe) | 0.30 max | Impurity |
| Magnesium (Mg) | 0.02 max | Kept low to limit hot cracking |
| Zinc (Zn) | 0.10 max | Impurity |
| Beryllium (Be) | 0.0003 max | Limited for welder health |
| Others each / total | 0.05 / 0.15 | |
| Aluminium | Remainder |
Weld strength is a property of the joint, not of the wire. It depends on the base metal and temper, joint design, process, heat input and whether the assembly is heat-treated afterwards. For that reason AWS A5.10 classifies filler by chemistry and AMS 4191 adds aerospace controls on composition, cleanliness, dimensions and packaging, while joint strength is qualified through your welding procedure (for example under AWS D17.1 for aerospace fusion welding).
As a guide, 2219 joints welded with 2319 and left as-welded develop roughly the strength of the solution-treated, naturally aged parent metal in the heat-affected zone. Re-solution treating and ageing the complete weldment recovers a large part of the T8 strength. Weld ductility is markedly better than with 4043, and toughness at cryogenic temperature is good.
Earlier data sheets quoted "tensile ≥ 450 MPa, yield ≥ 370 MPa" for 2319 wire. Those values describe neither a filler classification nor a typical 2219 weld and should not be used for design.
| Form | Common diameters | Packaging |
|---|---|---|
| MIG (GMAW) wire | 0.8, 1.0, 1.2, 1.6 mm (0.030, 0.035, 3/64, 1/16 in) | Precision-layer-wound spools, 0.5 – 7 kg, sealed with desiccant |
| TIG (GTAW) rod | 1.6, 2.4, 3.2, 4.0 mm (1/16, 3/32, 1/8, 5/32 in) | 914 mm (36 in) cut lengths in sealed tubes or cartons |
| Larger rod / wire | up to about 12 mm | Coils or straight lengths for special processes |
| Electron-beam / laser wire | to process requirement | Small spools, cleanliness-controlled |
Each spool or tube is labelled with the classification, diameter, lot number and specification. Aerospace orders are traceable from the certificate to the cast and drawing lot.
Fusion welds and repairs in 2219 tanks for liquid oxygen and liquid hydrogen on launch vehicles.
Welded 2219 frames, ducts and brackets in engine bays and high-speed airframes.
Aerospace and ground-support pressure vessels where high joint ductility is required.
Welded 2219 casings and structures that see heat and vibration.
Approved repairs on 2219 parts; occasionally specified for 2014 and 2024 repairs under engineering approval.
Wire-arc additive manufacturing research and production of 2219-type parts uses 2319-chemistry wire.
| Factor | 2319 | 4043 | 4145 |
|---|---|---|---|
| Main alloying | Cu 6.3 %, Ti, Zr, V | Si 5 % | Si 10 %, Cu 4 % |
| Best for | 2219 welds needing strength and ductility | General 6xxx and cast-alloy welding | Crack-sensitive 2xxx repairs, brazing |
| Responds to post-weld heat treatment | Yes, like 2219 | Limited | Limited |
| Weld ductility on 2219 | High | Low | Low |
| Hot-crack resistance | Good on 2219 | Very good | Excellent |
4043 is easier to weld with and more forgiving of fit-up, but the silicon-rich weld is brittle on 2219 and does not age-harden with it. For qualified aerospace 2219 work, 2319 is the standard choice.
It is the matching filler for welding 2219 aluminium, mainly in aerospace tanks, pressure vessels and hot structures. It gives better weld strength and ductility on 2219 than 4043 and responds to post-weld heat treatment.
Almost. 2319 has the same copper, manganese, zirconium and vanadium ranges as 2219 but more titanium (0.10 – 0.20 %) to refine the weld grain and reduce hot cracking.
AWS A5.10 classifies it as ER2319 (wire) and R2319 (rod); AMS 4191 is the aerospace material specification. EN ISO 18273 lists it as S Al 2319 (AlCu6MnZrTi).
No. It is designed for 2219. Use 4043 or 5356 for 6xxx alloys and 5183 or 5556 for 5xxx alloys.
Usually hydrogen from moisture or hydrated oxide on the joint or wire. Clean the joint immediately before welding, keep wire sealed and dry, and check shielding gas quality.
MIG wire is commonly 0.8 – 1.6 mm and TIG rod 1.6 – 4.0 mm in 914 mm lengths; other sizes up to about 12 mm can be supplied on request.
Send the form, diameter, quantity and specification. We reply with availability, certification and freight to your site.