Non-Ferrous Metals

Zinc Die Casting: Zamak Alloys, Hot Chamber Process, and Dimensional Accuracy

📅 March 25, 2026 ⏱ 36 min read 👤 metallurgyzone 🏷 dimensional accuracy   hot chamber die casting   Zamak  
March 25, 2026 · 12 min read · Non-Ferrous Metals

Zinc Die Casting: Zamak Alloys, Hot Chamber Process, and Dimensional Accuracy

Zinc die casting is the highest-volume precision metal casting process in the world by number of parts produced, enabled by a combination of properties unique to the Zamak alloy family: a low melting point near 380–390°C, exceptional fluidity, the ability to reproduce surface detail at sub-micrometre resolution, and a solidification shrinkage low enough to permit dimensional tolerances tighter than any other die casting metal. From automotive door handles, carburettors, and lock cylinders, to consumer electronics connectors, cosmetics packaging, and architectural hardware, Zamak castings are ubiquitous precisely because the hot chamber die casting process can produce complex, thin-walled, net-shape components at production rates exceeding 800 shots per hour with minimal post-processing.

Key Takeaways
  • Zamak alloys are Zn-4Al-Mg-Cu compounds named with the German acronym for zinc (Z), aluminium (A), magnesium (MA), and copper (K); all grades contain ~4 wt% Al as the primary alloying addition.
  • Hot chamber die casting is possible because zinc’s low liquidus (~380–390°C) does not attack the submerged steel gooseneck; aluminium’s higher liquidus (>580°C) destroys submerged iron components, requiring cold chamber machines.
  • Zamak 3 is the dominant grade (55–60% of all zinc die casting production): no copper, excellent ductility (10% elongation), best dimensional stability, and ideal electroplating substrate.
  • Zinc die castings age at room temperature as the as-cast supersaturated Zn-Al solid solution decomposes, causing small dimensional changes (0.01–0.07% linear shrinkage) that stabilise within 3–5 weeks; stabilisation annealing at 70–100°C is applied for precision parts.
  • Impurity control is critical: lead, cadmium, and tin above threshold levels (Pb > 0.004 wt%, Cd > 0.003 wt%, Sn > 0.002 wt%) cause catastrophic intergranular corrosion; special high-grade (SHG) zinc feedstock is mandatory.
  • The ZA alloy family (ZA-8, ZA-12, ZA-27) extends zinc casting to higher-strength structural and bearing applications at the cost of reduced castability and, for ZA-12 and ZA-27, incompatibility with hot chamber machines.
300 381 419 500 600 660°C Temperature (°C) 0 1 2 3 4 5 7 10 15 20 27 Aluminium content (wt%) 419°C (Zn) 660°C (Al) E (5.0% Al, 381°C) L + η(Zn) L + α(Al) η(Zn) + eutec. α(Al) + eutec. Liquid Zamak 3.5–4.3% ZA-8 ZA-12 ZA-27 Zn liquidus Al liquidus Eutectic (381°C) Zamak range (3.5–4.3%Al)
Fig. 1 — Zn-Al binary phase diagram showing the eutectic point at 5.0 wt% Al and 381°C. Zamak alloys (3.5–4.3 wt% Al, blue band) are hypoeutectic, solidifying as primary η-zinc dendrites followed by Zn-Al eutectic. ZA-8, ZA-12, and ZA-27 compositions are marked; ZA-27 falls in the aluminium-rich region and solidifies with primary α-aluminium dendrites. © metallurgyzone.com

The Zamak Alloy Family: Compositions and Grades

The four Zamak grades share a common base of approximately 4 wt% aluminium in a zinc matrix but differ primarily in copper content, which controls the strength-ductility-dimensional stability balance. All Zamak grades use special high-grade (SHG) zinc (≥99.99 wt% Zn) as the base metal, with aluminium added from high-purity ingot. Impurity limits are strictly enforced because lead, cadmium, and tin cause intergranular corrosion even at parts-per-thousand levels.

Zamak 2
Zn‑4Al‑1Cu‑0.035Mg
Highest hardness and creep resistance in the Zamak family. Used where hardness and bearing wear resistance are critical. Lowest elongation (7%) and poorest dimensional stability due to Cu-induced ageing.
UTS 328 MPa YS 230 MPa El. 7% 91 HRB
Zamak 3
Zn‑4Al‑0Cu‑0.035Mg
The most widely used Zamak grade (~55–60% of world production). No copper gives best dimensional stability, elongation, and electroplating quality. Standard general-purpose die casting alloy.
UTS 283 MPa YS 221 MPa El. 10% 82 HRB
Zamak 5
Zn‑4Al‑1Cu‑0.05Mg
Similar to Zamak 2 but with slightly different Cu and Mg balance. Intermediate strength and ductility. Widely used in Europe (EN 1774 AC44300) for automotive and hardware applications requiring higher strength than Z3.
UTS 328 MPa YS 228 MPa El. 7% 89 HRB
Zamak 7
Zn‑4Al‑0.01Cu‑0.01Mg
Ultra-high-purity variant of Zamak 3 with reduced Mg for improved ductility and better thin-wall formfill. Used for complex castings requiring maximum elongation and best corrosion resistance.
UTS 283 MPa YS 207 MPa El. 13% 80 HRB
Grade Al (wt%) Cu (wt%) Mg (wt%) Fe max Pb max Cd max Sn max ASTM / EN
Zamak 23.8–4.30.75–1.250.020–0.0500.1000.0040.0030.002B86 / AC43400
Zamak 33.8–4.30.25 max0.020–0.0500.1000.0040.0030.002B86 / AC43200
Zamak 53.8–4.30.75–1.250.030–0.0600.0750.0040.0030.002B86 / AC44300
Zamak 73.8–4.30.25 max0.005–0.0200.0750.0030.0020.001B86 / —
ZA-88.0–8.80.8–1.30.015–0.0300.0750.0040.0030.002B791 / —
ZA-1210.5–11.50.5–1.20.015–0.0300.0750.0040.0030.002B791 / —
ZA-2725.0–28.02.0–2.50.010–0.0200.0750.0040.0030.002B791 / —

Role of Each Alloying Element

Aluminium at ~4 wt% serves multiple simultaneous functions: it lowers the liquidus from 419°C (pure zinc) to ~385–390°C, refines the grain structure by acting as a nucleant for primary η-zinc dendrites, improves fluidity, reduces iron solubility in the melt (limiting die erosion), and contributes solid solution strengthening. The Zn-Al eutectic at 5.0 wt% Al and 381°C means Zamak alloys are slightly hypoeutectic and solidify through a two-phase (η-Zn + liquid) region before the eutectic reaction.

Magnesium at 0.02–0.06 wt% is critical for two functions: (1) it counteracts the embrittling effect of trace lead and tin impurities by preferentially scavenging them from grain boundaries; and (2) it contributes to grain boundary strengthening. However, excessive Mg above ~0.06 wt% causes hot shortness (intergranular cracking during solidification) and increases dross formation on the melt surface.

Copper at 0.75–1.25 wt% (Zamak 2 and 5) forms Cu-Zn-Al intermetallic phases that increase hardness, tensile strength, and creep resistance. However, copper accelerates the room-temperature ageing reaction and causes a larger and more prolonged dimensional change on ageing. For parts requiring tight long-term dimensional tolerance, Zamak 3 (no Cu) is preferred. Iron is an unavoidable contaminant; above 0.1 wt%, coarse Fe-Al intermetallic needle phases form that reduce ductility.

The Hot Chamber Die Casting Process

The hot chamber (gooseneck) die casting process is uniquely enabled by zinc’s low melting point and its benign interaction with iron and steel at casting temperature. The entire injection mechanism — pot, gooseneck, nozzle, and plunger — is permanently submerged in or adjacent to the molten zinc bath, eliminating the metal transfer step required in cold chamber machines and enabling cycle times two to four times faster than comparable aluminium HPDC.

Melt preparation
SHG zinc and master alloy ingots melted in steel crucible furnace. Drossing and temperature homogenisation.
420–440°C; ±3°C
Gooseneck fill
Plunger withdraws; molten zinc fills the gooseneck and shot sleeve through an inlet port submerged in the pot.
0.1–0.3 s
Injection
Hydraulic plunger advances, closing inlet port and forcing zinc through nozzle into the runner, gate, and die cavity.
10–50 m/s gate; 70–170 bar
Intensification & solidification
Plunger holds pressure while melt solidifies; intensification pressure minimises shrinkage porosity near gate.
0.5–2 s; 140–350 bar
Die opening & ejection
Die opens; ejector pins push casting from fixed half. Part temperature at ejection: 150–200°C.
0.5–1.5 s
Trimming & finishing
Flash, runner, and overflow trimmed in trim press or vibratory tumbling. Part ready for inspection or plating.
In-die trim (optional)
Hot chamber machine parameters (Zamak 3 reference values):

Melt temperature:         415–435°C (superheat 30–50°C above liquidus)
Die temperature:          165–220°C (cavity surface)
Injection velocity (gate): 20–50 m/s  (higher for thin-wall; lower for porosity control)
Intensification pressure: 140–350 bar
Cycle time (typical):     4–8 s (2–5 s for small parts)
Shots per hour:           400–900 (machine size dependent)
Machine sizes (locking force): 25–400 tonnes
Shot weight range:        5 g – 1.5 kg
Minimum wall thickness:   0.4–0.6 mm (achievable in production tooling)

Why Hot Chamber Works for Zinc but Not Aluminium

The metallurgical barrier to hot-chamber casting of aluminium is the reactivity of liquid aluminium with iron and steel at elevated temperature. Liquid aluminium dissolves iron at an accelerating rate above 680°C, forming Fe-Al intermetallic compounds (Fe₂Al₅, FeAl₃) that simultaneously erode the steel gooseneck and introduce iron contamination into the casting. At the casting temperatures required for A380 (660–700°C), a submerged steel gooseneck would be rendered unusable within hours. Zinc at 415–435°C dissolves iron at a negligible rate — iron solubility in liquid zinc at 420°C is only approximately 0.003 wt% — allowing the submerged injection system to survive indefinitely without significant erosion.

ZA-8 compatibility: ZA-8 (8 wt% Al) can be cast in hot chamber machines because, although it contains more aluminium, its casting temperature (440–460°C) is still below the threshold at which aluminium’s iron-dissolving rate becomes damaging. ZA-12 (12 wt% Al) requires a casting temperature of approximately 480–520°C, which begins to approach the erosion threshold; ZA-12 and ZA-27 are therefore processed only in cold chamber machines or by gravity/permanent mould casting.

Fluidity and Thin-Wall Casting Capability

Zinc alloys have among the highest fluidity of any casting metal, enabling wall thicknesses down to 0.4 mm in production tooling — a capability unmatched by aluminium or magnesium die casting alloys. Fluidity arises from three concurrent factors: low viscosity at casting temperature, a narrow freezing range (Zamak 3 freezes over only approximately 5–10°C below the eutectic at 381°C), and the low latent heat of solidification of zinc (112 J/g vs. 397 J/g for aluminium). The narrow freezing range means the alloy is nearly fully liquid until the eutectic reaction, after which it solidifies rapidly without leaving an extended mushy zone that would resist flow.

Comparative fluidity (spiral fluidity test at standard conditions):
  Zamak 3 (Zn-4Al):       ~900–1100 mm
  A380 aluminium:          ~600–750 mm
  Magnesium AZ91D:         ~600–700 mm
  Grey cast iron:          ~800–1000 mm

Minimum achievable wall thickness in die casting:
  Zinc (Zamak):            0.4–0.6 mm
  Aluminium (A380):        0.8–1.2 mm
  Magnesium (AZ91D):       0.6–0.8 mm

Solidification Microstructure of Zamak Alloys

The solidification microstructure of Zamak die castings consists of two principal constituents: primary η-zinc dendrites (a zinc-rich solid solution containing up to ~1 wt% Al at the eutectic temperature) and a Zn-Al eutectic phase filling the interdendritic spaces. In die cast components, the extreme cooling rates in the water-cooled die cavity produce a refined microstructure with dendrite cell sizes of 3–10 µm, similar in scale to HPDC aluminium.

A characteristic feature of Zamak hot chamber castings is the skin-core microstructural gradient: the outer skin (0.05–0.3 mm thick) solidifies almost instantaneously against the cold die face and is completely free of porosity and segregation, with an extremely fine grain size. This skin is the structurally strongest part of the casting and the ideal substrate for electroplating. The core solidifies more slowly and may contain fine interdendritic porosity and coarser eutectic regions. Any machining that removes the skin exposes the coarser, more porous core and severely degrades plating adhesion and corrosion resistance.

Intermetallic Phases

Several intermetallic phases form in Zamak castings depending on composition and cooling rate:

  • ε-phase (CuZn₄): Forms in Zamak 2 and 5 from the copper addition; appears as small particles (1–5 µm) distributed in the eutectic. Increases hardness and creep resistance. Transforms to other Cu-Zn compounds during low-temperature ageing.
  • T’-phase (Cu₅Zn₈Al₅): Precipitates during room-temperature ageing in Cu-containing grades; contributes to the dimensional change observed during natural ageing.
  • FeAl₃ / Fe₂Al₅ needles: Form when Fe > 0.1 wt%; brittle platelets that reduce elongation and fatigue resistance. Controlled by maintaining Fe below specification limits through proper feedstock and minimising iron pickup from tools and furnace linings.
Optical micrograph of Zamak 3 zinc die casting showing primary eta-zinc dendrites and interdendritic Zn-Al eutectic phase with fine grain structure characteristic of hot chamber die casting solidification
Optical micrograph of a Zamak 3 hot chamber die casting (nital etch, ~200×) showing the characteristic microstructure: primary η-Zn dendrites (white/grey) surrounded by interdendritic Zn-Al eutectic (darker regions). The fine grain size (dendrite cell size 3–8 µm) is a direct consequence of the rapid cooling rate against the water-cooled die face. © Wikimedia Commons / public domain.

Dimensional Accuracy, Tolerances, and Ageing

Zinc die casting is renowned for producing the tightest dimensional tolerances achievable in any die casting process. The combination of low solidification shrinkage, low melt and die temperatures, narrow freezing range, and exceptional fluidity (enabling complete cavity fill without premature freeze-off) all contribute to this precision.

Solidification Shrinkage and Tolerance Capability

Solidification shrinkage comparison (volumetric, casting direction):
  Zamak 3:        ~1.0–1.3% linear
  Zamak 5:        ~1.1–1.4% linear
  A380 aluminium: ~0.5–0.7% in-cavity; ~1.2–1.5% total to ambient
  AZ91D magnesium:~0.8–1.0% linear

NADCA Product Standard dimensional tolerances (general):
                    Zinc       Aluminium   Magnesium
  Up to 25 mm:    ±0.05 mm   ±0.10 mm   ±0.08 mm
  25–75 mm:       ±0.07 mm   ±0.15 mm   ±0.12 mm
  75–150 mm:      ±0.10 mm   ±0.20 mm   ±0.18 mm
  Critical dims:  ±0.025 mm  ±0.05 mm   ±0.04 mm

Surface finish Ra:
  Zinc (hot chamber):    0.4–0.8 µm  (as-cast, polished die)
  Aluminium (HPDC):      0.8–1.6 µm
  Magnesium (HPDC):      0.6–1.2 µm

Room-Temperature Ageing and Dimensional Change

One of the few disadvantages of Zamak die castings compared to aluminium is their susceptibility to dimensional change during room-temperature ageing. As-cast Zamak contains a supersaturated η-zinc solid solution (approximately 1 wt% Al dissolved at the eutectic temperature, compared to near-zero at room temperature) that is thermodynamically unstable. Over days to weeks at ambient temperature, aluminium precipitates from the zinc-rich matrix, forming a two-phase structure of near-pure zinc and Al-rich zones. This decomposition is accompanied by a net linear contraction of 0.01–0.07%, depending on alloy grade and section thickness.

Zamak dimensional change during ageing (ASTM B86 data):

Grade       First 24h    First week    5 weeks    Stabilised
Zamak 2     −0.010%      −0.040%       −0.065%    −0.070% (largest change — Cu)
Zamak 3     −0.005%      −0.020%       −0.038%    −0.042%
Zamak 5     −0.008%      −0.030%       −0.055%    −0.060%
Zamak 7     −0.003%      −0.015%       −0.028%    −0.030% (lowest change)

Artificial stabilisation anneal:
  70–100°C for 3–6 hours immediately after casting
  → accelerates decomposition to completion within hours
  → part can be machined to final tolerances immediately after anneal
  → no further dimensional change at room temperature thereafter
Design and inspection implications: For precision components such as carburettor bodies, lock cylinders, or metrology fixtures, dimensional inspection must either be deferred until ageing is complete (≥5 weeks at ambient), or parts must be stabilisation-annealed before any precision machining or inspection. Inspecting un-aged Zamak castings to final tolerance will result in false accepts that subsequently move out of tolerance in service. ASTM B86 documents the typical dimensional change data for each alloy grade.

Intergranular Corrosion of Zinc Die Castings

Intergranular corrosion (IGC) is the most serious long-term degradation mechanism for Zamak components and historically caused catastrophic failures in automotive, plumbing, and consumer products before the introduction of SHG zinc and modern impurity standards in the 1950s. Understanding its mechanism and prevention remains essential for specifying zinc die castings in corrosive environments.

Mechanism of Intergranular Corrosion

Lead, cadmium, and tin are virtually insoluble in solid zinc at room temperature and segregate to grain boundaries during solidification, forming thin continuous films. These grain boundary films are electrochemically different from the zinc matrix: lead and cadmium-rich boundaries are less noble (more anodic) in many environments, while tin can be cathodic, creating local galvanic cells at each grain boundary. In humid or aqueous environments, these cells drive selective dissolution of the grain boundary regions:

Impurity threshold limits (above which IGC risk is significant):
  Lead (Pb):    > 0.004 wt% (40 ppm)
  Cadmium (Cd): > 0.003 wt% (30 ppm)
  Tin (Sn):     > 0.002 wt% (20 ppm)
  Indium (In):  > 0.001 wt% (10 ppm)

Mechanism:  Pb/Cd/Sn → segregate to η-Zn grain boundaries on solidification
            → form continuous low-melting-point boundary films
            → anodic dissolution of boundary film in humid/wet environment
            → intergranular network cracks, swelling, strength loss
            → catastrophic failure in severe cases (50–90% strength loss)

Standard test: ASTM B428 (steam test) or ASTM B791 humidity exposure;
               measure dimensional change and mass loss after 10-day
               95°C / 98% RH exposure

Historical context: Pre-1950s zinc die castings used commercially pure zinc (99.9%) which routinely contained 0.02–0.10 wt% Pb from primary zinc smelting. Automotive parts produced before 1950 frequently exhibited IGC failure (called “zinc pest” or “zinc plague”) within 5–10 years. The introduction of SHG (special high grade, ≥99.99 wt% Zn) zinc from 1952 onwards, combined with strict specification of impurity limits in ASTM B86, essentially eliminated IGC from properly produced Zamak castings.

Scrap contamination risk: Recycled zinc die casting scrap is a major source of Pb, Cd, and Sn contamination, particularly from plated parts (Cd and Sn from plating baths) and from mixed-metal scrap. Zamak alloy ingot producers apply strict spectrometric analysis and blending protocols to maintain impurity levels below threshold. Foundries using reclaimed zinc alloy must verify that the reformulated alloy meets ASTM B86 impurity limits before use. Unapproved re-melt of plated zinc scrap directly into the casting furnace is a frequent root cause of IGC failures in practice.

Magnesium’s Role in Suppressing IGC

Magnesium at 0.02–0.06 wt% plays a critical protective role against IGC: it preferentially forms fine Mg-Pb and Mg-Pb-Zn intermetallic compounds in the grain boundary region, effectively sequestering lead impurities into discrete, less-harmful particles rather than allowing them to form continuous films. The protective effect is concentration-dependent: below ~0.02 wt% Mg the protection against Pb impurities is incomplete. This is why Zamak 7 (with very low Mg of 0.005–0.020 wt%) requires even stricter Pb limits (0.003 wt% max) to compensate for its reduced IGC protection, and why it mandates the use of the highest-purity zinc feedstock.

Mechanical Properties and Comparison with Competing Alloys

Property Zamak 3 Zamak 5 ZA-27 A380 Al AZ91D Mg
Density (g/cm³)6.606.605.002.741.81
UTS (MPa)283328400–425317230
Yield strength (MPa)221228370–385159160
Elongation (%)1071–33.53.0
Hardness (HRB)82891058073
Impact strength (J)5865144650
Liquidus (°C)387387484595598
Min. wall (mm)0.40.41.50.80.6
Casting processHot chamberHot chamberCold ch. / gravityCold chamberCold ch. / hot ch.
Electroplatable?ExcellentExcellentFairGoodRequires pre-treat

Specific Strength and the Density Penalty

Zinc’s high density (6.60 g/cm³ for Zamak 3, compared to 2.74 for A380 and 1.81 for AZ91D) is its principal disadvantage for weight-sensitive applications. On a specific strength basis (UTS/density), Zamak 3 at 283 MPa / 6.60 g/cm³ = 43 MPa·cm³/g compares unfavourably to A380 aluminium at 116 MPa·cm³/g and AZ91D magnesium at 127 MPa·cm³/g. For automotive body and structural applications where weight is paramount, aluminium and magnesium die castings have largely displaced zinc. Zinc retains its position in applications where its superior surface finish, dimensional accuracy, thin-wall capability, production rate, and electroplating quality justify the weight penalty — particularly in decorative hardware, precision locking mechanisms, electrical connectors, and small intricate components.

Surface Finishing: Electroplating and Coating

Zinc die castings provide an unmatched substrate for electroplating among the die casting metals, because the smooth, porosity-free skin produced in the hot chamber process replicates the polished die surface at sub-micrometre accuracy. The standard plating sequence for bright decorative chromium on Zamak is:

  • Alkaline cleaning: Removes die lubricant and surface contamination without attacking the zinc substrate.
  • Copper strike (cyanide or acid pyrophosphate bath): A thin 3–8 µm copper deposit seals micropores and provides a uniform base for subsequent layers.
  • Bright acid copper (15–30 µm): Builds thickness, levels surface defects, and provides the bright reflective finish needed for chrome.
  • Semi-bright or bright nickel (8–15 µm): Corrosion barrier and brightness amplifier; a duplex nickel system (semi-bright + bright) provides cathodic protection of the zinc substrate.
  • Chromium (0.2–0.5 µm): Final decorative and wear-resistant layer. Traditional hexavalent chromium is being replaced by trivalent chromium (Cr III) plating for environmental compliance (RoHS, ELV Directive).
Skin integrity is critical for plating quality: The dense, defect-free skin of a hot chamber zinc die casting extends only 0.1–0.3 mm below the surface. Any machining through this skin exposes the subsurface zone which contains interdendritic porosity and gas inclusions. These surface defects trap plating solutions (causing blistering), prevent uniform copper adhesion, and produce visible plating defects under the bright decorative finish. All surfaces to be plated must remain in the as-cast condition; drilling, tapping, and milling for assembly must be confined to surfaces not visible in the final product.
Hot Chamber Process Schematic and Zamak Ageing Curves Molten Zn (420°C) Gooseneck Plunger Cavity Steel furnace pot Die Water-cooled Hot Chamber Cycle 1. Plunger up → Zn fills gooseneck 2. Plunger down → seals port, injects 3. Intensification → solidification 4. Die opens → eject → trim → repeat Cycle time: 4–8 s | 400–900 shots/hr Room-Temperature Ageing (Dimensional Change) 0 −0.02 −0.04 −0.06 −0.08% Linear shrinkage (%) 0 1 2 3 5 8 12w Time (weeks at room temperature) Stabilised Zamak 2 (1% Cu, max change) Zamak 5 (1% Cu) Zamak 3 (0% Cu) Zamak 7 (low Mg, min. change)
Fig. 2 — Left: Schematic of the hot chamber die casting process showing the submerged gooseneck, plunger, nozzle, and water-cooled die. The key advantage over cold chamber is that the injection mechanism is permanently immersed in molten zinc, enabling rapid 4–8 second cycle times. Right: Room-temperature ageing dimensional change curves for the four Zamak grades showing the progressive linear shrinkage (%) over 12 weeks. Cu-bearing Zamak 2 and 5 exhibit the largest change; low-Mg Zamak 7 the smallest. The yellow band marks the stabilisation zone (3–5 weeks). © metallurgyzone.com

ZA Alloys: Higher-Strength Zinc Casting

The ZA (Zinc-Aluminium) alloy series — ZA-8, ZA-12, and ZA-27 — represents a progression beyond the Zamak family to significantly higher aluminium contents and correspondingly higher strength, at the cost of higher density and reduced hot-chamber castability. ZA-27 with 27 wt% Al achieves a UTS of 400–425 MPa and hardness of 105 HRB, making it competitive with many aluminium die casting alloys on an absolute strength basis, though its density of 5.0 g/cm³ still exceeds aluminium (2.7 g/cm³).

ZA alloys have excellent bearing and wear properties due to the hard Al-rich phases dispersed in the softer zinc matrix, enabling use as lightly-loaded sleeve bearings and bushings without lubrication in applications such as agricultural equipment, food processing machinery, and light industrial gearboxes. ZA-12 exhibits a particularly attractive combination of strength (UTS ~290–320 MPa), good elongation (1–2%), and self-lubricating bearing behaviour. For further reading on solidification and phase diagram fundamentals underlying ZA alloy behaviour, see the Iron-Carbon Phase Diagram article for phase diagram interpretation principles and Grain Boundaries for grain boundary segregation relevant to IGC.

Industrial Applications and Selection Criteria

Application Alloy Critical Requirement Why Zinc vs. Alternatives
Decorative automotive trim (door handles, badges)Zamak 3Plating quality, surface finishSuperior plating substrate vs. Al or Mg
Lock cylinders, padlocksZamak 3 or 5Dimensional accuracy, thin walls, securityTightest tolerances; 0.4 mm wall achievable
Carburettors, fuel system parts (legacy)Zamak 3Dimensional stability, fuel resistanceStable dimensions after ageing; good machinability
Connector housings, electrical bracketsZamak 3 or 7Complex form, thin wall, high volume800+ shots/hr; intricate geometry capability
Cosmetics packaging closuresZamak 3Mirror plating, weight feel, luxury aestheticHigh density gives premium tactile feel; mirror-plate quality
Architectural hardware (handles, hinges)Zamak 5Strength, plating, corrosion resistanceHigher strength than Z3; excellent plating
Lightweight structural componentsZA-27Specific strength, casting precisionHighest strength zinc; 400+ MPa UTS
Bearings & bushingsZA-12Wear resistance, self-lubricationHard Al-rich phases provide wear resistance

For context on competing non-ferrous casting processes, the Aluminium Casting Alloys article covers A380, A356, and A319 in detail. Related surface protection methods applicable to both zinc and aluminium castings are covered in the Corrosion Mechanisms article. For hardness testing of zinc and ZA alloys per ASTM B86, see Hardness Testing Methods.

Frequently Asked Questions

What is Zamak and what does the name mean?
Zamak is a family of zinc-aluminium die casting alloys standardised by the New Jersey Zinc Company in the 1920s. The name is a German-language acronym: Z = Zink (zinc), A = Aluminium, MA = Magnesium, K = Kupfer (copper). All Zamak alloys contain approximately 4 wt% aluminium as the primary alloying element, with minor additions of magnesium (0.02–0.06 wt%) and, in Cu-bearing grades (Zamak 2 and 5), approximately 1 wt% copper. The four principal grades are Zamak 2 (1.0 wt% Cu), Zamak 3 (0 Cu — the most widely used, ~55% of world production), Zamak 5 (1.0 wt% Cu), and Zamak 7 (ultra-high purity, very low Cu and Mg).
Why is hot chamber die casting used for zinc but not for aluminium?
Hot chamber die casting uses a submerged steel gooseneck and plunger permanently immersed in the molten metal. This is viable for zinc because zinc’s low casting temperature (~415–435°C) does not dissolve iron at a significant rate — iron solubility in zinc at 420°C is only ~0.003 wt%. Aluminium alloys must be cast at 660–700°C, at which temperature aluminium dissolves iron rapidly, forming Fe-Al intermetallic compounds that erode the submerged mechanism and contaminate the casting. A steel gooseneck in molten aluminium at casting temperature would be destroyed within hours. Aluminium therefore requires cold chamber machines where the injection mechanism is separate from the furnace.
What dimensional tolerances can zinc die castings hold compared to aluminium?
Zinc die castings achieve significantly tighter dimensional tolerances than aluminium HPDC. Per NADCA Product Standards, Zamak 3 achieves general tolerances of ±0.05 mm on dimensions up to 25 mm, compared to ±0.10 mm for aluminium HPDC. Critical tolerances reach ±0.025 mm for zinc vs. ±0.05 mm for aluminium. This advantage arises from zinc’s lower solidification shrinkage (~1.0–1.3% linear vs. ~1.2–1.5% total for A380), lower die and melt temperatures (reducing thermal distortion), narrow freezing range enabling complete cavity fill without premature solidification, and the ability to remain in the die longer before ejection without hot-tearing risk. Surface finish is also superior: Ra 0.4–0.8 µm for zinc vs. 0.8–1.6 µm for aluminium HPDC.
What is zinc die casting ageing and how does it affect dimensions?
Zinc die castings undergo natural room-temperature ageing as the as-cast supersaturated Zn-Al solid solution decomposes: aluminium precipitates from the zinc-rich matrix, causing a net linear contraction of 0.01–0.07% that stabilises after 3–5 weeks. Cu-bearing grades (Zamak 2, 5) exhibit larger changes than Zamak 3 or 7. For precision components, artificial stabilisation annealing at 70–100°C for 3–6 hours immediately after casting accelerates decomposition to completion, allowing final machining and inspection without subsequent dimensional drift. Dimensional inspection on un-aged castings to tight tolerances produces false accepts that move out of tolerance in service.
What causes intergranular corrosion in zinc die castings and how is it prevented?
Intergranular corrosion in zinc die castings is caused by lead, cadmium, or tin impurities above critical thresholds (Pb > 0.004 wt%, Cd > 0.003 wt%, Sn > 0.002 wt%). These elements segregate to grain boundaries during solidification and form electrochemically active continuous films that corrode preferentially in humid environments, eventually causing network cracking, swelling, and catastrophic strength loss (“zinc pest”). Prevention requires special high-grade (SHG) zinc feedstock (≥99.99 wt% Zn), strict scrap management to avoid plated scrap remelting, and spectrometric verification per ASTM B86. Magnesium at 0.02–0.05 wt% provides partial protection by forming Mg-Pb intermetallics that sequester lead impurities from grain boundaries.
How does aluminium content affect the mechanical properties of Zamak alloys?
Aluminium at ~4 wt% in Zamak alloys lowers the liquidus from 419°C (pure Zn) to ~385–390°C, refines the grain structure, improves fluidity, and provides solid solution strengthening. The Zn-Al eutectic at 5.0 wt% Al and 381°C is the thermodynamic reference: Zamak alloys at ~4 wt% Al are slightly hypoeutectic. Copper additions (Zamak 2 and 5, ~1 wt% Cu) increase hardness and creep resistance by forming Cu-Zn-Al intermetallic phases, at the cost of slightly reduced elongation and larger room-temperature ageing dimensional change. In the ZA family, increasing Al from 4% (Zamak) to 8, 12, and 27% progressively raises strength, hardness, and liquidus temperature while reducing density from 6.6 to 5.0 g/cm³ for ZA-27.
What is the ZA alloy family and how does it differ from Zamak?
The ZA alloys contain significantly more aluminium than Zamak: ZA-8 (8 wt% Al), ZA-12 (12 wt% Al), and ZA-27 (27 wt% Al). Higher Al raises strength substantially — ZA-27 achieves 400–425 MPa UTS vs. ~283 MPa for Zamak 3 — but also raises liquidus temperature, making ZA-12 and ZA-27 incompatible with hot chamber machines (they require cold chamber or gravity casting). ZA alloys have superior bearing and wear resistance due to hard Al-rich phases in the microstructure, are used for lightly-loaded bushings and bearings without lubrication, and have lower density than Zamak (5.0 g/cm³ for ZA-27 vs. 6.6 g/cm³ for Zamak 3). ZA-8 can be hot-chamber cast and occupies a middle ground between Zamak and the higher-Al ZA grades.
What surface finishing options are available for zinc die castings?
Zinc die castings accept an exceptionally wide range of surface finishes. Electroplating is the most common: the standard decorative bright chromium sequence is copper strike (3–8 µm) → bright acid copper (15–30 µm) → duplex nickel (8–15 µm) → chromium (0.2–0.5 µm). Other options include nickel-only, brass, bronze, and PVD coatings. Powder coating over zinc phosphate conversion coating is widely used for corrosion protection without decorative plating. The critical requirement for plating quality is preserving the as-cast skin layer (0.1–0.3 mm): machining through this dense, defect-free skin exposes subsurface porosity that causes plating blistering and adhesion failure. Trivalent chromium (Cr III) has largely replaced hexavalent chromium (Cr VI) for environmental compliance with RoHS and ELV regulations.

Recommended References

ASM Handbook Vol. 15: Casting
Authoritative reference covering zinc die casting processes, Zamak and ZA alloy metallurgy, hot chamber mechanics, microstructure, and defect analysis.
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Die Casting Engineering — Andresen
Comprehensive treatment of hot and cold chamber die casting processes, tooling, die design, alloy selection, and defect prevention for zinc, aluminium, and magnesium.
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Zinc Handbook — Porter (ASM)
The definitive single-volume reference on zinc metallurgy: alloy systems, phase diagrams, mechanical properties, corrosion, galvanising, and die casting applications.
View on Amazon
Fundamentals of Metal Casting — Groover
Accessible graduate-level text covering casting process fundamentals, solidification theory, shrinkage, fluidity, and process-property relationships for all casting metals.
View on Amazon

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