SINTS Blog Design and DFM

MIM Tolerances and Design Guidelines for Precision Metal Parts

Which tolerances survive sintering, which have to be machined, and the six design rules that decide whether a MIM part is straightforward or expensive.

Coordinate measuring machine inspecting a sintered metal component

The most common reason a MIM quotation comes back higher than expected is not tooling or material — it is tolerance. A drawing that applies a tight tolerance across every dimension pushes the part into a machining-dominated process chain, and the economics that made MIM attractive disappear before the quote is issued.

This guide covers what MIM holds as-sintered, where the practical limits sit for walls, holes and threads, and how to structure a drawing so the tight tolerances land only where they are needed.

Why MIM tolerances differ from CNC tolerances

A CNC machine positions a tool against a workpiece and holds the result to the machine's accuracy. Material is removed after the shape is fixed, so tolerance is a machine property.

MIM is the reverse. The shape is set in the mould, then the part shrinks by 15–20% during sintering. Tolerance is therefore the sum of mould accuracy, feedstock consistency, injection repeatability, shrinkage behaviour and furnace variation. Because shrinkage is proportional, the resulting tolerance is proportional too — which is why MIM tolerance is expressed as a percentage of the dimension rather than as a fixed band.

Once that is understood, the rest of MIM design guidance follows logically. Errors scale with size. Thin and thick sections behave differently. Features formed by thin core pins are as fragile as the pins. And anything requiring absolute accuracy rather than relative accuracy has to be machined after sintering.

The percentage rule, in numbers

Percentage-based tolerances are sometimes used for early comparisons. The table below shows the arithmetic at ±0.3% and ±0.5%; it does not establish an achievable tolerance. Review feature size, geometry, alloy, datums and any minimum absolute tolerance with the manufacturer.

Illustrative percentage arithmetic, not a tolerance capability table
DimensionAt ±0.3%At ±0.5%Practical reading
5 mm±0.015 mm±0.025 mmArithmetic only; minimum practical tolerance must be reviewed
10 mm±0.030 mm±0.050 mmArithmetic only; confirm with the supplier
20 mm±0.060 mm±0.100 mmIllustrative calculation; verify process capability
40 mm±0.120 mm±0.200 mmIllustrative calculation; verify process capability
60 mm±0.180 mm±0.300 mmIllustrative calculation; verify process capability

a tight tolerance on a small feature needs a specific capability review and an agreed control route; it may require secondary finishing

Wall thickness

Wall thickness is reviewed with material, flow length, local mass, debinding and distortion risk. Avoid abrupt transitions and unsupported features where practical; do not use one wall-thickness band as a universal tooling rule.

The more important rule concerns variation rather than absolute thickness. Where a thick boss or hub meets a thin wall, the two regions densify at different rates. Keeping the ratio between the thickest and thinnest section below roughly 3:1 avoids most defects; cores and lightening features are the standard way to bring a heavy section closer to the surrounding wall.

Design the section, not just the shape. A part with 2 mm walls and one 8 mm hub will sinter unevenly no matter how good the furnace is. Coring the hub, or accepting that it will need machining, is a design decision that belongs in the first drawing rather than the third sample.

Holes and bores

Hole feasibility depends on diameter, depth, core-pin support, orientation and material. Compare molded holes with drilling or other finishing where tooling becomes fragile or the required fit is critical.

Holes that run parallel to the mould opening direction are straightforward. Cross-holes are also possible in MIM — this is one of its advantages over press-and-sinter PM — but they require side-action tooling or additional mould complexity, which affects tooling cost. Where a cross-hole exists only to pass a pin or a wire and the tolerance is loose, forming it in the mould is usually cheaper than drilling later.

Threads

Small internal threads can be moulded using unscrewing cores, but the tooling is more complex and the thread form must tolerate the shrinkage. External threads can be formed when they are coarse enough to survive sintering without distortion.

For most industrial parts, threads tighter than about M3 or requiring a specific class of fit are cut or rolled after sintering. The general approach: state the thread on the drawing, expect the supplier to propose whether it is moulded or machined, and confirm which one appears in the quotation.

Undercuts, draft and radii

Undercuts and side features are formable in MIM using split tooling or side actions, unlike press-and-sinter PM where they generally are not. The cost is tooling complexity, so the design question is whether the feature can be moved to a direction that avoids a side action — often it can, with a small change to the surrounding geometry.

Draft angles let the part release from the mould cleanly. MIM generally requires less draft than die casting or forging, but surfaces parallel to the mould opening direction still benefit from a small amount — commonly about 0.5° to 1° on walls, more on textured surfaces. Where the drawing shows a zero-draft wall, expect the supplier to raise it.

Radii serve the same purpose at internal corners, where a sharp corner concentrates stress during cooling and can cause cracking. A practical minimum inside radius is around 0.2–0.5 mm, and it is usually cheaper to add one than to argue about it.

How material affects tolerance

Shrinkage varies by alloy and by powder specification, so tolerance capability varies with the material. Austenitic 316L is well characterised and behaves predictably. Martensitic grades such as 420 and 440C are more sensitive to carbon content and atmosphere, and their sintering window is narrower. Magnetic grades require tighter control of carbon and oxygen, which can affect dimensional consistency as well.

The practical takeaway: the tolerance figures quoted above are a working baseline for well-characterised stainless grades. For less common alloys, the supplier should be asked what capability has actually been demonstrated, rather than what is theoretically possible.

Specifying tolerances in an RFQ

A drawing that produces a competitive MIM quotation usually has three tiers of tolerance.

  • Critical features — fits, bores, sealing surfaces, bearing journals. Mark these explicitly, and expect them to be machined after sintering.
  • Functionally significant dimensions — assembly clearances and general fits. Typically ±0.1 mm to ±0.3 mm, which is achievable as-sintered on most part sizes.
  • General dimensions — leave these at a general tolerance note rather than dimensioning every one. This is where a drawing either keeps MIM economical or makes it expensive.

Also state the datum structure. MIM parts are measured against datums established after sintering, and a well-defined datum scheme makes first-article inspection straightforward rather than a debate.

Design mistakes that cost money

  • Applying ±0.05 mm generally. It converts an economical forming part into an expensive machining part.
  • Heavy sections without coring. Thick hubs and bosses next to thin walls sinter unevenly and generate sink or porosity.
  • Very small or very deep holes. Thin core pins deflect and break, which shows up as tooling cost and downtime.
  • Sharp internal corners. They concentrate stress during cooling and cause cracking in the green or brown part.
  • Zero draft on tall walls. Ejection becomes difficult and surface finish suffers.
  • Tolerancing a feature that is not measured. Adding a tight tolerance to a cosmetic dimension buys inspection cost with no functional benefit.

Material standards and dimensional capability are different references. MPIF Standard 35-MIM and ASTM B883 address MIM materials; they do not establish one tolerance for every feature. The percentages in this guide are illustrative arithmetic, not a SINTS capability guarantee. Agree feature tolerances, datums and inspection methods from the actual drawing.

Conclusion

MIM tolerance is proportional, and that single property explains most of the design guidance: small dimensions are relatively accurate, large ones are not; section variation causes distortion; thin core pins set the hole limits; and only a handful of features should carry machining tolerances.

A well-structured MIM drawing concentrates precision where it functions, leaves general dimensions general, and states density, material and datums explicitly. That drawing is cheaper to make, cheaper to inspect and far less likely to require a tooling change after the first samples.

Related component families

These pages apply the tolerance framework to specific component types.

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Frequently Asked Questions

Practical answers for OEM sourcing and engineering teams.

What tolerances can MIM achieve?

On general dimensions MIM typically holds about ±0.3–0.5% of the dimension as-sintered, so the absolute tolerance changes with part size: a 10 mm feature carries roughly ±0.03–0.05 mm, while a 60 mm feature carries ±0.18–0.30 mm. Features needing tighter control — usually few on a well-designed part — are produced by a machining operation after sintering.

What wall thickness is possible with MIM?

MIM works comfortably with walls of about 1–3 mm. Below roughly 0.5 mm, cavity filling and green-part handling become difficult. Above about 4–5 mm, the interior sinters more slowly than the surface, risking porosity and sink. The more important variable is uniformity: keeping the ratio between the thickest and thinnest section below roughly 3:1 prevents most distortion problems.

What about holes and cross-holes?

Holes are formed by core pins in the mould, so the practical minimum diameter is around 0.3–0.5 mm, with depth limited to roughly three to four times the diameter for slender pins. Cross-holes are possible in MIM — unlike press-and-sinter PM — but they require side-action tooling or added mould complexity, which affects tooling cost. Where a cross-hole tolerance is loose, forming it in the mould is often cheaper than drilling afterwards.

How should I design for MIM shrinkage?

Shrinkage is compensated in the mould rather than in the drawing, so the design task is to keep the part's shrinkage predictable. Practical measures are uniform wall sections, generous radii at internal corners, adequate draft on tall walls, and avoiding heavy masses adjacent to thin walls. Keeping a consistent section allows the mould to compensate accurately.

When is secondary machining needed?

Secondary machining is normally required when a feature needs a tolerance tighter than about ±0.05 mm, when a surface must be flat or parallel to a degree that sintering cannot guarantee, when threads tighter than roughly M3 are required, or when a bore is a bearing or sealing surface. Identifying these features on the drawing at RFQ stage lets them be costed deliberately rather than discovered after the first samples.