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Hot Isostatic Press (HIP)

HIP & densification · Densification

Hot isostatic pressing applies high-temperature inert gas pressure uniformly to cast, sintered, and metal powder-bed-fusion parts.

3D printingCastingHigh cost $$$$Gas quench (N₂ / He)
Temperature510–1,220 °C950–2,228 °F
HardnessNo target
Case depthThrough section
Cycle time8–24 hVessel heat-up, pressurization, hold, depressurization, and cooling dominate turnaround.

HIP at a glance

Four scores, each 0–100 against every heat treatment in this catalog. Hardness is derived from the HRC target (20 HRC = 0, 70 HRC = 100) — treatments without a hardness target (anneals, stress relief, HIP, cryo) are not rated. Toughness, dimensional stability and cost are FabDigit's engineering assessment.

Hardness achievedNot rated—
Toughness retainedVery good75 / 100
Dimensional stabilityGood65 / 100
Relative costHigh95 / 100

What is HIP?

Hot isostatic pressing applies high-temperature inert gas pressure uniformly to cast, sintered, and metal powder-bed-fusion parts. It closes internal porosity and improves fatigue consistency, but it does not repair open-to-surface defects or replace alloy-specific solution and aging treatments.

How it works

Parts are heated below the alloy solidus in a pressure vessel while argon applies at least 100 MPa in standard AM cycles. Elevated temperature lowers flow stress; gas pressure drives creep and diffusion so isolated pores and internal lack-of-fusion defects shrink or bond. Pressure is isostatic, so sound external geometry changes little, although unsupported thin features can creep. Defects connected to the surface remain gas-filled and generally do not close. The HIP thermal exposure also changes grain size, phases, and residual stress, so titanium, nickel, stainless, cobalt-chrome, and aluminum each require a specific cycle and often a subsequent solution-and-age treatment.

Why specify it

  • ASTM F3301 AM cycles use at least 100 MPa inert-gas pressure
  • Can raise qualified PBF density toward 100%
  • Closes internal pores that reduce fatigue life
  • Applies pressure uniformly to complex cast and AM geometry
  • Covers alloy-specific temperatures from about 510 °C for AlSi10Mg to 1220 °C for Co-Cr-Mo

Where it falls short

  • Does not close defects connected to the external surface
  • Cannot remove inclusions or restore material missing from lack-of-build
  • High temperature can coarsen grains and alter precipitation state
  • Thin unsupported features can creep under pressure
  • Requires expensive pressure-vessel capacity and material-specific post-HIP heat treatment

The HIP cycle

Typical furnace parameters from the governing specifications and shop practice; the heat treater sets the exact recipe from the alloy, section size and required result.

Temperature510–1,220 °C (950–2,228 °F) — Material-specific ASTM F3301 envelope: AlSi10Mg 510–520 °C; Ti alloys 895–955 °C; Ni, 316L, and Co-Cr alloys use higher ranges.
Soak2–5 h — ASTM F3301 cycles are commonly 180 ± 60 min or 240 ± 60 min.
CoolingGas quench (N₂ / He)
AtmosphereHigh-pressure argon
Door to door8–24 h — Vessel heat-up, pressurization, hold, depressurization, and cooling dominate turnaround.

Stages

  1. 1Clean and inspect for surface-connected defects
  2. 2Load and evacuate pressure vessel
  3. 3Ramp temperature and argon pressure
  4. 4Hold at the alloy-specific qualified condition
  5. 5Controlled cool under inert pressure
  6. 6Apply solution and age treatment when required

What HIP does to the part

HardnessNo hardness target — the treatment is specified by condition, not by HRC.
Section affectedThe whole section transforms.
ToughnessClosing internal porosity usually improves ductility and fatigue scatter; final toughness still depends on alloy, grain structure, and post-HIP heat treatment.
DistortionMedium risk. Isostatic pressure preserves sound bulk geometry, but thin walls, trapped cavities, and near-solidus exposure can creep or collapse.
Surface after treatmentExternal as-built roughness remains; argon prevents bulk oxidation, but surface-connected pores remain open.
Machining sequenceMachine datums and critical surfaces after HIP when possible; remove sacrificial supports and allow for required post-HIP solution and aging cycles.

Specifications for HIP

The documents a drawing cites to define this treatment. Each links to a page explaining the standard, its classes and the tests it invokes.

StandardRoleClasses usedStatus
Standard Specification for Additive Manufacturing Nickel Alloy (UNS N07718) with Powder Bed Fusion
GoverningUNS N07718Active
Standard for Additive Manufacturing—Post Processing Methods—Standard Specification for Thermal Post-Processing Metal Parts Made Via Powder Bed Fusion
GoverningCondition HIPActive

Test and related methods: AMS 2750 (Pyrometry).

Drawing call-out

HOT ISOSTATIC PRESS PER ASTM F3301 CONDITION HIP FOR Ti-6Al-4V: 895–955 °C, 100 MPa MIN, 3 ± 1 H; COOL UNDER INERT GAS BELOW 425 °C; CERTIFY TIME, TEMPERATURE, AND PRESSURE

Which alloys take HIP?

Verdict per material family, with the grades that behave differently. Each family links to its datasheets in the material library. Typical grades: Ti-6Al-4V, Ti-6Al-4V ELI, Co-28Cr-6Mo, Inconel 718, Inconel 625, 316L, AlSi10Mg, A356.

Material familyVerdictNotes
YesAlSi10Mg and cast aluminum use low-temperature alloy-specific HIP cycles.
  • AlSi10Mg 510–520 °C under ASTM F3301
  • A356 uses supplier-qualified cycles
YesSintered binder-jet parts can be further densified if pores are sealed from vessel gas.
YesCo-28Cr-6Mo PBF and implant parts have ASTM F3301 HIP requirements.
  • 1185–1220 °C, 100 MPa minimum
YesMetal powder-bed-fusion parts are a principal ASTM F3301 application.
  • Ti-6Al-4V, IN718, IN625, 316L, Co-Cr-Mo, AlSi10Mg
YesInconel 718 and 625 are routinely HIP processed before final heat treatment.
  • ASTM F3055 covers PBF UNS N07718
YesPowder-consolidated refractory metals are established HIP applications.
  • Cycle and capsule design are alloy-specific
Yes316L PBF has an ASTM F3301 HIP window of 1120–1163 °C at 100 MPa minimum.
  • 316L
  • 17-4 PH needs post-HIP aging control
YesTool, stainless, and alloy-steel cast or powder parts can be densified with alloy-specific cycles.
  • H13 and 316L require different cycles
YesTi-6Al-4V and ELI are standard aerospace and medical HIP substrates.
  • ASTM F3301: 895–955 °C, 100 MPa minimum
YesTungsten heavy-alloy powder compacts can be densified by qualified HIP cycles.
With carePossible only with specialized low-temperature cycles and strict safety controls.
LimitedPossible in powder metallurgy, but zinc vapor pressure and chemistry require specialized control.
LimitedSintered bronze can be densified with a qualified cycle.
LimitedPowder and cast copper alloys can be HIP consolidated using proprietary alloy-specific cycles.
LimitedPowder precious metals can be consolidated, but economics and alloy-specific cycles govern.
NoLow melting and vapor-pressure behavior make conventional metal HIP impractical.

Design rules for HIP

What to decide on the drawing before the part goes to the heat treater.

  1. Seal or remove surface-connected porosity before relying on HIP.Pressurized argon enters an open defect and prevents a closing pressure differential.
  2. Select a material-specific ASTM F3301 cycle.AlSi10Mg uses about 510–520 °C while Co-Cr-Mo uses 1185–1220 °C.
  3. Plan solution and aging treatment after HIP when required.The HIP soak can dissolve or overage strengthening precipitates.
  4. Support thin walls and large flat areas.Hot material can creep even under nominally uniform pressure.
  5. Specify acceptance by density, CT, metallography, or mechanical testing.HIP machine records prove the cycle, not that every original defect closed.
  6. Provide venting strategy for intentional cavities.A sealed cavity can collapse while an open cavity communicates with vessel pressure.

HIP versus the alternatives

Treatments engineers weigh against HIP, and when each wins.

TreatmentHardnessToughnessStabilityCostChoose it when
HIP
this page
—7565$$$$—
—7595$when only residual-stress reduction is needed and internal porosity is acceptable
—9055$$$when phase condition and corrosion properties, not pore closure, are the objective

Cost, lead time and applications

Relative cost

Hot Isostatic Press (HIP) is a high-cost treatment ($$$$) relative to the other heat treatments in this catalog.

Heat treatment is priced per lot with a furnace minimum. The exact figure appears on the instant quote once the part is uploaded.

Lead time

Added lead time7–21 working days
Furnace time8–24 h

What HIP is used for

  • Flight-critical PBF Ti-6Al-4V parts
  • PBF Inconel 718 turbomachinery
  • Medical cobalt-chrome implants
  • 316L valve and manifold bodies
  • AlSi10Mg AM structures
  • Nickel-superalloy investment castings

HIP — frequently asked

What pressure does HIP use?

ASTM F3301 Condition HIP cycles use inert atmosphere at not less than 100 MPa. Commercial equipment often operates in the 100–200 MPa range, but the drawing must state the alloy-specific requirement.

What temperature does HIP use?

There is no universal temperature: AlSi10Mg uses about 510–520 °C, Ti alloys 895–955 °C, 316L 1120–1163 °C, and Co-Cr-Mo 1185–1220 °C under ASTM F3301. Applying the wrong alloy cycle can damage microstructure or geometry.

How long is a HIP hold?

ASTM F3301 commonly specifies 180 ± 60 minutes for titanium and 240 ± 60 minutes for several nickel, stainless, and cobalt alloys. Total vessel time is longer because heating, pressurization, cooling, and depressurization are included.

Does HIP remove all AM porosity?

It can close isolated internal pores and bring a qualified PBF material toward full density. It generally cannot close defects that remain connected to the external surface because vessel gas reaches both sides.

Does HIP increase hardness?

Not inherently, so this record has no hardness score. Hardness may rise or fall with alloy phase changes, and nickel or precipitation-hardening alloys commonly need solution and aging treatment after HIP.

Will HIP change dimensions?

Sound bulk geometry changes little under isostatic pressure, but porous regions shrink and thin unsupported features can creep. Critical surfaces are commonly machined after HIP.