Tag: laser powder bed fusion

  • Design for Laser Powder Bed Fusion: A Practical DfAM Guide

    Design for Laser Powder Bed Fusion: A Practical DfAM Guide

    Designing for laser powder bed fusion (LPBF) is not the same as designing a conventionally manufactured part and then sending the CAD file to a printer. LPBF performance depends on the interaction between geometry, orientation, supports, heat flow, recoating, powder removal, post-processing and inspection.

    A good LPBF design is not merely printable. It is buildable, removable, heat-treatable, machinable, inspectable and repeatable.

    Start with the complete manufacturing route

    Before optimizing geometry, define the route from powder to accepted hardware. The sequence commonly includes build preparation, printing, controlled cooling, depowdering, stress relief, removal from the build plate, support removal, heat treatment, hot isostatic pressing when required, machining, surface finishing, cleaning and inspection.

    Each downstream operation creates design requirements. A channel that can be printed but not depowdered is not manufacturable. A thin wall that survives the build but distorts during cut-off is not robust. A datum that cannot be machined or inspected is not production-ready.

    1. Part orientation is a multi-objective decision

    Orientation affects support volume, thermal gradients, surface roughness, dimensional accuracy, build height, recoater exposure, mechanical-property direction, powder removal and post-processing access. There is rarely one universally best orientation.

    Orientation objectiveWhy it mattersTypical trade-off
    Reduce support volumeLowers material, removal effort and witness marksMay increase build height or distortion
    Protect critical surfacesDown-facing surfaces are usually rougher and less accurateMay require more supports elsewhere
    Improve heat flowStable thermal paths reduce distortion and local overheatingCan increase contact with the build plate
    Limit recoater riskTall, thin or poorly anchored features may deflect or collideA safer orientation may use more space
    Enable machiningDatums and critical interfaces need tool access and stock allowanceMachining-friendly orientation may not minimize print time
    Enable inspectionInternal features need suitable access or validated NDT methodsSome optimized internal geometries are difficult to verify

    Use build simulation and engineering judgment, but validate critical orientations with representative builds. Simulation quality depends on accurate material, process and boundary-condition inputs.

    2. Overhang rules are process-specific

    The familiar “45-degree rule” is only a screening heuristic. The minimum self-supporting angle depends on alloy, layer thickness, scan strategy, feature length, local heat accumulation, machine architecture and required surface quality. Short bridges, thin walls and curved surfaces can behave differently from large flat overhangs at the same nominal angle.

    Instead of applying a single angle limit, classify features by risk:

    • Down-facing surfaces: prone to roughness, dross, dimensional error and local overheating.
    • Large horizontal areas: high risk of distortion and poor surface condition.
    • Thin cantilevers: vulnerable to curling and recoater interaction.
    • Internal overhangs: difficult to support, remove and inspect.
    • Bridges and enclosed channels: sensitive to span, shape, heat flow and powder evacuation.

    3. Supports are thermal and mechanical tools

    Metal LPBF supports do more than hold a part against gravity. They anchor the component, conduct heat to the build plate, resist residual-stress-driven distortion and stabilize vulnerable features against recoater forces.

    A support strategy should define:

    • Where strong anchoring is needed and where low-contact supports are sufficient
    • How heat will flow from local hot spots to the build plate
    • How supports will be accessed and removed
    • Which surfaces can tolerate support witness marks
    • Whether the part will remain stable during stress relief and build-plate removal
    • How support volume affects cost, powder recovery and machining

    Supports should be designed together with the cut-off and machining plan. Minimizing support volume at the expense of build stability often increases total cost.

    Example of LPBF support structures
    Support design example originally credited to Materialise Magics

    4. Design for thermal stability

    LPBF creates steep, repeated thermal gradients. Residual stress, distortion, delamination and cracking risk depend on geometry, material, heat flow and scan strategy. Designers cannot control every process variable, but geometry can reduce sensitivity.

    • Use gradual section transitions rather than abrupt changes in mass.
    • Avoid isolated heavy sections connected to thin walls.
    • Add generous radii where stress and heat concentrate.
    • Keep long unsupported edges and broad flat surfaces under control.
    • Consider sacrificial ribs, strongbacks or machining stock where distortion risk is high.
    • Coordinate thin-wall limits with the qualified supplier and parameter set.
    • Use symmetry cautiously: symmetric CAD does not guarantee symmetric thermal history.

    Materials with high crack sensitivity or poor thermal conductivity may need tighter geometric constraints, platform preheating, specialized parameters or alternative processes.

    5. Plan powder removal from the first sketch

    Internal channels, lattices and cavities are valuable LPBF features, but trapped powder creates safety, mass, contamination and inspection risks. Powder-removal strategy should be designed, documented and verified.

    • Provide adequately sized and correctly located escape holes.
    • Avoid blind cavities unless trapped powder is explicitly acceptable.
    • Use channel cross-sections that are both printable and cleanable.
    • Consider line-of-sight, gravity, vibration, vacuum and fluid-cleaning access.
    • Account for powder agglomeration after thermal exposure.
    • Verify residual powder using the method required by the application.

    For safety-critical hardware, “we shook the powder out” is not a controlled process. Cleaning acceptance criteria belong in the manufacturing plan.

    6. Add machining allowance intentionally

    LPBF rarely delivers every surface at final tolerance and finish. Critical bores, sealing faces, bearing seats, threads, datums and interfaces commonly require machining.

    A machining-ready design identifies:

    • Functional datums and how they will be established
    • Surfaces that require stock allowance
    • Workholding features and fixture access
    • Tool approach, reach and collision constraints
    • How the part will be located after support removal or heat treatment
    • Which features should be printed near-net-shape versus machined from solid stock

    Uniform extra stock is not always best. Allowance should reflect expected distortion, surface orientation, feature size and the planned machining sequence.

    7. Design for inspection

    Inspection access is a design variable. Complex internal passages may be impossible to evaluate using conventional line-of-sight methods. X-ray computed tomography can provide powerful volumetric inspection, but part size, material density, wall thickness, resolution and scan time limit what it can detect.

    Define critical-to-quality features and credible defect modes before selecting NDT. Inspection should be matched to the required probability of detection, not chosen simply because a technology is available.

    8. Use lattices and topology optimization selectively

    Topology optimization and lattices can reduce mass or tailor stiffness, heat transfer and energy absorption. They can also increase file size, build time, surface area, powder-removal difficulty and inspection burden.

    Before adopting an optimized geometry, ask whether it:

    • Creates a measurable system-level performance gain
    • Can be built across the qualified process window
    • Can be cleaned and inspected
    • Can be represented and transferred reliably in the digital workflow
    • Can tolerate expected process variation and surface condition
    • Still offers value after supports, machining and qualification are included

    9. Material selection is process-route selection

    A familiar alloy designation does not guarantee familiar properties. LPBF microstructure and performance depend on powder, parameters, orientation, heat treatment and post-processing. Select materials based on validated data for the intended route, not on wrought handbook values.

    The design allowable, coupon plan and acceptance criteria must reflect the actual production process. For regulated applications, changes to powder source, machine model, parameter set or thermal treatment may require formal review or requalification.

    10. Build a production checklist

    1. Define loads, environment, life, failure modes and acceptance requirements.
    2. Select a qualified machine–material–parameter–post-process route.
    3. Choose orientation using thermal, support, surface, cost and inspection objectives.
    4. Review overhangs, thin walls, holes, channels and recoater-sensitive features.
    5. Complete support, depowdering, cut-off, heat-treatment and machining plans.
    6. Define datums, stock allowances, fixtures and inspection access.
    7. Run simulation where it adds value and validate with representative hardware.
    8. Freeze the digital definition and control manufacturing changes.
    9. Use process monitoring and witness specimens only as part of a defined quality plan.
    10. Capture lessons from build, post-processing and inspection and feed them back into design rules.

    Conclusion

    The strongest LPBF designs integrate product function with manufacturing reality. Orientation, support, heat flow, powder removal, machining and inspection are not downstream details; they are core design inputs. The goal is a stable process route that repeatedly produces acceptable hardware, not a one-time successful print.

    Related Addithive resources: NDT for Additive Manufacturing · AM Surface Finishing

    References and further reading

  • Surface Finishing for Metal Additive Manufacturing: Methods, Selection and Design Rules

    Surface Finishing for Metal Additive Manufacturing: Methods, Selection and Design Rules

    Metal additive manufacturing can produce geometries that conventional processes cannot, but the as-built surface is rarely the final engineering surface. Roughness, partially fused particles, stair-stepping, support scars, down-facing irregularities and near-surface defects can affect fatigue, sealing, friction, flow, cleaning, coating and dimensional performance.

    Surface finishing should not be treated as a cosmetic operation added after printing. It is part of the manufacturing route and should be planned during design.

    Why AM surfaces are difficult

    Surface condition depends on more than layer thickness. Process category, alloy, powder size, energy input, orientation, local heat flow, support strategy, recoating, scan parameters and post-build handling all contribute. The same part can contain several different surface states:

    • Up-facing surfaces: often smoother and more dimensionally stable than unsupported down-facing areas.
    • Down-facing surfaces: vulnerable to dross, partially fused powder and geometric sag.
    • Vertical walls: affected by layer stair-stepping, contour strategy and powder adhesion.
    • Support-contact regions: retain witness marks and local damage after removal.
    • Internal channels: may be inaccessible to conventional tools and difficult to inspect after finishing.
    • Machined stock surfaces: intentionally printed oversized so final geometry is created later.

    Because surface requirements vary by function, a single roughness target for the complete part is usually inefficient. A better approach classifies surfaces by engineering need.

    Start with functional surface requirements

    Surface functionWhat mattersTypical finishing route
    Structural fatigue surfaceNotches, attached particles, near-surface defects and residual stressMachining or controlled material removal, followed by polishing or peening where justified
    Sealing faceFlatness, waviness, roughness and dimensional controlMachining, grinding, lapping or honing
    Bearing or sliding interfaceGeometry, roughness direction, hardness and wearMachining, grinding, honing, superfinishing or coating
    Fluid channelPressure loss, debris retention, cleanability and geometry preservationAbrasive-flow, chemical/electrochemical or specialized internal finishing
    Biological interfaceCleanliness, controlled texture and biocompatibilitySelective machining, blasting, chemical treatment and validated cleaning
    Coating substrateAdhesion, contamination, oxide state and target profileBlasting, machining, cleaning or chemical preparation
    Cosmetic surfaceVisual uniformity and touchBlasting, tumbling, polishing or coating

    Mechanical finishing methods

    Machining

    CNC milling, turning, drilling, reaming, grinding and EDM remain the most reliable methods for creating tight tolerances and functional interfaces. Machining is commonly used for datums, bores, sealing faces, threads and mounting surfaces.

    Designers should define machining stock, workholding, tool access and the datum strategy before printing. AM parts can contain residual stress, thin walls and interrupted surfaces that make machining less stable than a wrought blank. Heat treatment and build-plate removal sequence can materially change the final geometry.

    Abrasive blasting

    Bead, grit or shot blasting can remove loose particles and create a more uniform appearance. It is fast and scalable for accessible surfaces, but it does not create precision geometry. Media type, pressure, angle and contamination control must suit the alloy and final application.

    Mass finishing and vibratory finishing

    Tumbling and vibratory systems use media and relative motion to smooth exposed edges and surfaces. They work well for smaller robust parts, but can round sharp features, damage thin sections and provide uneven access to recessed geometry.

    Abrasive-flow machining

    Abrasive media is forced through a passage to remove high points and smooth internal channels. It can improve flow performance in manifolds and heat exchangers, but material removal is geometry-dependent. Process development should verify that critical wall thickness and channel shape remain within limits.

    Peening and surface mechanical treatments

    Shot peening, laser shock peening and related methods can modify near-surface residual stress and improve fatigue performance in suitable applications. Peening does not automatically remove surface-connected defects and should not be used as a substitute for required machining or inspection.

    Chemical and electrochemical finishing

    Chemical polishing

    Chemical polishing removes material through a controlled reaction across exposed surfaces. It can reach complex areas without direct tool contact, but the rate depends on alloy chemistry, solution condition, temperature, flow and local geometry. Entrapped chemicals, selective attack and dimensional loss must be controlled.

    Electropolishing

    Electropolishing removes material electrochemically and preferentially smooths peaks. It is widely used for stainless steels and selected nickel, cobalt-chromium, titanium and other alloys with appropriate electrolytes. Electrical contact, current distribution, shielding and access determine uniformity. Deep blind passages may remain difficult.

    Both chemical and electrochemical routes require validated cleaning and waste-control procedures. For medical, aerospace or fluid-service components, residual chemicals and altered surface chemistry can be as important as roughness.

    Thermal and energy-based finishing

    Laser polishing

    Laser polishing locally remelts a thin surface layer so surface tension redistributes material. It can smooth selected accessible regions without abrasive media, but the thermal cycle can change microstructure, residual stress, oxide condition and dimensions. Line-of-sight access and parameter development are required.

    Plasma and electrochemical plasma processes

    Plasma-based finishing methods can reduce roughness on suitable conductive materials and complex shapes. Their effectiveness depends strongly on chemistry, current density, edge effects and process access. They are specialized processes rather than universal solutions.

    Internal-channel finishing

    Internal channels are one of AM’s strongest design advantages and one of its hardest post-processing problems. A channel can be printable but impossible to depowder, finish, clean or inspect. The finishing strategy should answer:

    • Can media or fluid reach every surface and exit completely?
    • Will bends, branches or changes in section create uneven removal?
    • Can the process preserve minimum wall thickness and calibrated flow area?
    • How will residual abrasive, chemical or powder be verified?
    • Can CT, flow testing or other methods confirm the finished geometry?

    For critical channels, coupons and representative flow artifacts are usually more useful than generic roughness samples.

    Surface finishing and fatigue

    As-built metal AM surfaces can reduce fatigue performance because attached particles, valleys, support scars and near-surface imperfections act as local stress concentrators. The improvement obtained from finishing depends on how much material is removed and whether the controlling defect is actually eliminated.

    A polished appearance does not prove that subsurface lack of fusion or porosity has been removed. Fatigue-critical routes should connect surface treatment with material allowables, residual stress, heat treatment, inspection and representative testing.

    How to select a finishing process

    1. Define function. Specify why the surface needs treatment: tolerance, sealing, fatigue, flow, wear, coating, cleaning or appearance.
    2. Map accessibility. Separate open, recessed, internal and support-contact surfaces.
    3. Set material-removal limits. Protect thin walls, sharp features, lattices and calibrated flow areas.
    4. Choose the sequence. Heat treatment, HIP, support removal, machining, polishing, peening, coating and cleaning can interact.
    5. Validate on representative geometry. Flat coupons rarely reproduce internal channels, downskin or support scars.
    6. Measure more than Ra. Use the parameters and spatial scales that correlate with function.
    7. Verify cleanliness and integrity. Finishing must not introduce contamination, cracks, embedded media or unacceptable dimensional loss.

    Common mistakes

    • Specifying one roughness value for all surfaces regardless of function
    • Adding finishing only after the geometry and orientation are frozen
    • Assuming every internal passage can be polished uniformly
    • Using polishing to hide process instability rather than correcting the build route
    • Ignoring fixture, datum and tool-access requirements
    • Failing to account for removed material in tolerance and wall-thickness analysis
    • Evaluating visual appearance without checking fatigue, cleanliness or dimensional performance

    Conclusion

    Surface finishing is one of the main bottlenecks between a successful AM build and an accepted production part. No method is best for every surface. The correct route combines design, orientation, machining access, controlled material removal, cleaning and inspection around the actual functional requirement.

    Related Addithive resources: Design for LPBF · NDT for Additive Manufacturing

    References and further reading

  • Metal Additive Manufacturing Process Selection: A Practical Guide

    Metal Additive Manufacturing Process Selection: A Practical Guide

    Metal additive manufacturing is not one process. Laser powder bed fusion, electron-beam powder bed fusion, directed energy deposition, wire-arc systems, binder jetting and bound-metal extrusion solve different manufacturing problems. Selecting the wrong route can create avoidable cost, qualification and post-processing burdens.

    Process selection should begin with the component requirement and the complete production route — not with the machine already available.

    The first decision: what problem is AM solving?

    A strong metal AM application normally has at least one clear value driver: complex internal geometry, part consolidation, expensive material savings, low-volume tooling avoidance, rapid iteration, repair, feature addition, digital inventory or a significant performance improvement.

    If the only argument is that the part can be printed, the business case is incomplete. Conventional machining, casting, forging, sheet fabrication or a hybrid route may remain more robust and economical.

    The main metal AM process families

    ProcessBest suited toTypical strengthsPrimary constraints
    Laser powder bed fusion (PBF-LB/M or LPBF)Small-to-medium complex parts requiring fine features and strong material performanceHigh geometric detail, mature alloy routes, complex internal channelsHigh equipment and powder cost, supports, residual stress, limited build rate, extensive post-processing
    Electron-beam powder bed fusion (PBF-EB/M)Reactive alloys and production parts that benefit from elevated build temperatureLower residual stress for suitable alloys, no laser optics, effective for some titanium applicationsCoarser surface/detail, narrower supplier ecosystem, vacuum and material limitations
    Powder directed energy deposition (DED)Repair, feature addition, multi-axis deposition and medium-to-large near-net shapesLocal material addition, repair capability, multi-material potentialLower resolution, machining required, powder efficiency and shielding complexity
    Wire DED / DED-Arc / WAAMLarge metal structures and high-deposition-rate near-net shapesHigh deposition rate, low-cost wire feedstock, large scaleHigh heat input, distortion, coarse finish, substantial machining and process control
    Metal binder jettingBatch production of smaller sinter-based parts and geometries compatible with debinding/sinteringNo attached thermal supports during printing, high nesting potential, broad powder routesGreen-part fragility, shrinkage, distortion, furnace capacity and sintering qualification
    Bound-metal material extrusionPrototypes, tooling and low-volume parts where accessibility matters more than speed or propertiesLower entry barrier, simpler material handling, office/workshop workflowsDebinding and sintering, shrinkage, limited feature/property envelope, lower throughput
    Sheet lamination / ultrasonic additive routesSpecialized laminates, embedded features and selected multi-material structuresLow bulk thermal load, unique material combinationsNiche equipment, interface control, limited general-purpose adoption

    A practical selection framework

    1. Part envelope and local feature size

    Start with the complete bounding box, but do not stop there. Minimum wall, hole, channel, lattice and edge requirements may eliminate a process even when the part fits inside the machine. LPBF offers finer feature control than DED, while large wire or powder DED systems can exceed conventional powder-bed envelopes.

    2. Material and property maturity

    Ask whether the required alloy has a controlled feedstock specification, validated parameter set, heat-treatment route and relevant property data. A process may technically deposit an alloy without being suitable for a production or safety-critical program.

    The most mature route is often better than the most novel one. Qualification evidence, powder or wire availability, thermal-processing capacity and supplier experience materially change program risk.

    3. Geometry and design intent

    • Internal channels and compact complexity: favor LPBF when dimensions, powder removal and inspection are manageable.
    • Large near-net structures: favor wire or powder DED when machining can create final interfaces.
    • Repair or local feature addition: favor DED, particularly with multi-axis access and a controlled substrate.
    • High part count per batch: may favor binder jetting if the sintering route is stable.
    • Simple prismatic geometry: is often better machined, forged, cast or fabricated.

    4. Surface condition and tolerance

    As-built capability should be separated from final part capability. LPBF can produce finer surfaces and features than DED, but critical interfaces commonly require machining. WAAM and other high-deposition-rate processes are generally near-net-shape methods. Binder-jetted metal parts may achieve useful detail, yet sintering shrinkage and distortion must be included in the dimensional strategy.

    Create a surface-by-surface plan: as-built, machined, polished, coated or otherwise finished. Then evaluate whether the geometry provides access for the required operation.

    5. Production rate and batch economics

    Deposition rate alone is not production rate. Total lead time includes setup, printing, cooling, depowdering, debinding, sintering, heat treatment, cut-off, support removal, machining, cleaning, inspection and queue time.

    Binder jetting can place many parts in a build, but furnace capacity and sintering cycle time can become the bottleneck. Multi-laser LPBF can raise output, but build preparation, qualification and downstream operations still determine effective capacity. DED can deposit quickly, but heavy machining may reduce the net advantage.

    6. Material utilization

    Processes using wire typically offer high feedstock utilization. LPBF reuses a large fraction of unmelted powder, but powder conditioning, contamination control, sieving and refresh rules affect true yield. Binder jetting can pack many parts efficiently, but handling loss and sintering scrap matter. Compare the full buy-to-use ratio rather than quoting only printer waste.

    7. Post-processing and facility capability

    Process selection must include the equipment and expertise surrounding the printer. Consider:

    • Stress-relief and heat-treatment furnaces
    • Hot isostatic pressing where required
    • Depowdering and powder-safe handling
    • Debinding and sintering capacity
    • Build-plate removal and support removal
    • Five-axis machining, EDM, grinding and finishing
    • Cleaning and contamination controls
    • Dimensional metrology, material testing and NDT

    A theoretically attractive print route can fail commercially when the local post-processing chain is immature or overloaded.

    8. Qualification and change control

    For aerospace, medical, energy and defense applications, qualification may dominate the decision. Define who owns process approval, what evidence is required, how machine equivalency is handled and which changes trigger revalidation.

    The cheapest prototype route may not be the lowest-risk production route. A qualified supply chain, stable machine platform and experienced service provider can outweigh a small difference in print cost.

    Process comparison matrix

    CriterionLPBFEB-PBFPowder DEDWire DED / WAAMBinder jettingBound-metal extrusion
    Feature resolutionHighMediumLow–mediumLowMediumMedium
    Typical part scaleSmall–medium; increasingly large systems existSmall–mediumMedium–largeLarge–very largeSmall–medium batch partsSmall–medium
    Deposition/build rateLow–mediumMediumMedium–highHighHigh print throughput; sintering dependentLow
    Attached supportsOften requiredLimited/process-dependentNot conventional supports; fixturing/substrate strategy requiredNot conventional supports; fixturing/substrate strategy requiredNot during printingProcess-dependent
    Final machining needCommonCommonUsually extensiveUsually extensiveApplication-dependentCommon for precision interfaces
    Thermal distortion riskMedium–highLower for suitable preheated routes but still design-dependentHighHighPrimarily during sinteringPrimarily during sintering
    Repair capabilityLimitedLimitedStrongStrong for suitable geometryNoNo
    Qualification maturityHigh for selected alloys and industriesEstablished in selected nichesEstablished for repair and selected buildsGrowing, with aerospace standards emergingGrowing; highly route-dependentLimited for critical applications

    Application-driven recommendations

    Choose LPBF when

    • The part requires fine metal features, internal channels or compact geometric complexity.
    • Production volume is modest and part value is high.
    • A qualified alloy and post-processing route exists.
    • Support removal, powder removal and inspection are feasible.

    Choose electron-beam PBF when

    • The alloy and application benefit from a hot, vacuum-based powder-bed process.
    • Residual-stress reduction and productivity for suitable geometries outweigh surface/detail limitations.
    • The supplier ecosystem and material route are available.

    Choose powder DED when

    • The requirement is repair, cladding, feature addition or a medium-to-large near-net shape.
    • Multi-axis deposition and local material placement provide value.
    • Machining and inspection are planned from the beginning.

    Choose wire DED or WAAM when

    • The component is large and deposition rate matters more than fine resolution.
    • Wire feedstock is available and the geometry can tolerate substantial machining.
    • Heat input, distortion, interpass control and toolpath planning can be managed.

    Choose binder jetting when

    • Many parts can be nested in a batch and the geometry is compatible with depowdering and sintering.
    • The organization has powder-metallurgy or metal-injection-molding expertise.
    • Shrinkage compensation, furnace loading and dimensional control have been demonstrated.

    Choose bound-metal extrusion when

    • The objective is accessible prototyping, tooling or low-volume metal parts.
    • The required properties and tolerance can be achieved after debinding, sintering and machining.
    • Low capital complexity matters more than high throughput.

    Questions to ask a machine supplier or service bureau

    1. What exact machine–material–parameter–post-process route supports the quoted properties?
    2. Which dimensions are as-built and which assume machining?
    3. What are the demonstrated minimum walls, holes and channels for this alloy and orientation?
    4. How are powder or wire batches controlled and traced?
    5. What is the historical first-pass yield for comparable parts?
    6. Which operations are performed internally and which are subcontracted?
    7. What are the largest recurring causes of nonconformance?
    8. How are machine maintenance, calibration and parameter changes controlled?
    9. What inspection methods are validated for the critical defect modes?
    10. What capacity constraint will dominate at the target annual volume?

    Conclusion

    Metal AM process selection is a systems-engineering decision. Part size, geometry, material maturity, final tolerances, post-processing, inspection, production rate and qualification must be evaluated together. The best process is the one that delivers accepted parts reliably at the required scale — not the one with the most impressive printer specification.

    Related Addithive research: Metal AM Supply Chain Map · Aerospace AM Qualification Guide

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    References and further reading