Infographic showing five estimator inputs leading to low, medium or high additive manufacturing qualification burden and an evidence package.

AM Qualification Effort Estimator

Estimate the relative qualification burden of an aerospace or space additive-manufactured part before you commit to a full evidence program. Select five inputs below. The tool returns a directional Low / Medium / High burden and a starter evidence checklist.

Infographic showing five estimator inputs leading to low, medium or high additive manufacturing qualification burden and an evidence package.
The estimator combines criticality, alloy/process maturity, inspection burden and application context into a directional planning score.
Select the inputs and run the estimator.

Directional planning aid only. It is not an FAA, NASA, military or OEM approval decision.

How the score works

The tool scores five drivers that tend to expand the evidence burden: criticality, novelty of the alloy/data package, novelty of the process configuration, difficulty of inspection and certification intensity of the application. Low novelty and low consequence produce a lower score; stacked novelty and criticality push the program toward High.

ScoreInterpretationPlanning implication
0–4: LowBounded evidence burdenFocus on traceability, process control, acceptance criteria and targeted verification.
5–9: MediumStructured qualification campaignPlan dedicated material/process data, NDT substantiation, configuration control and component testing.
10–18: HighQualification is a major program workstreamEngage approval stakeholders early; build a formal evidence architecture and change/equivalence strategy.

Evidence checklist

  • Defined and traceable feedstock specification
  • Qualified machine/process parameter envelope
  • Heat treatment / HIP / machining / surface-finish controls
  • Material property and variability dataset appropriate to failure modes
  • Defect characterization and defect-tolerance linkage where relevant
  • NDT/CT capability and acceptance limits
  • Machine and supplier equivalence strategy
  • Component-level verification / substantiation tests
  • Production acceptance plan
  • Configuration and change-control rules

Why this is directional—not a certification calculator

No generic calculator can determine whether a part is qualified or certified. The actual basis depends on the component, failure consequence, design organization, authority, program, existing data and manufacturing configuration. This tool is intended for early program screening: it helps teams identify where evidence work is likely to accumulate before schedule and budget are committed.

Method basis

The framework is informed by the 2026 NASA/FAA/NIST CM4QC strategy and NIST’s broader work on AM material, process and part qualification. CM4QC’s central direction is to reduce qualification time and cost by maturing computational-materials approaches while preserving the evidence rigor required for aviation safety.