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Non-Ferrous Titanium
Titanium Scrap
Grade: VariousVery High Tier
Aerospace-grade titanium clippings, turnings, solids
Market Price EstimateUpdated Daily
$12,500/ MT
+950 (8.2%)vs yesterday
Verified specifications & market data
Chemical Composition
Elemental breakdown by percentage weight.
Standard composition limits
Values represent maximum allowed percentage unless otherwise noted.
Physical Properties
Material form, density, and contamination specifications.
Ultra-premium aerospace/medical-grade titanium alloy scrap; jet engine components (compressor blades, discs), airframe structural material, landing gear, aerospace fasteners; medical implants and surgical instruments; post-industrial aerospace manufacturing waste; extreme material purity and traceability requirements; direct aerospace/medical processor supply; ultra-concentrated, tightly-controlled supply chain
Acceptable Inclusions
- Aerospace titanium alloys (Ti-6Al-4V, Ti-5Al-2.5Sn, pure Ti)
- Thin protective oxide layer
- Minimal manufacturing handling residue
- Known aerospace alloy composition; documented certification
- Aerospace-certified scrap
Prohibited Materials
- Mixed titanium alloys (must be single type or cross-compatible grade)
- Non-aerospace titanium (commodity Ti prohibited)
- Steel or ferrous contamination (>0.05%)
- Composite materials (non-metallic)
- Unknown material composition or alloy type
- Corroded or oxidized material (>15% surface loss)
- Unauthorized or non-certified aerospace material
- Cadmium or toxic element contamination
Quality Assurance
Testing protocols, sampling methods, and acceptance criteria.
Sampling Protocol
frequencyStratified sampling from position, alloy type, form
maximumQuantity500+ individual samples per shipment
minimumQuantity5-20 tonnes or 200-500 material samples minimum
percentage30-50% of lot
stratificationSample across material form; alloy type; position in shipment; coverage
Acceptance Limits
all Criteria Must Passsingle criterion ; aerospace zero-defect standard ; - =
alloy IdentificationConfirmed as Ti-6Al-4V, Ti-5Al-2.5Sn, pure Ti, or specifically aerospace alloy
aluminum LimitAl within specification
carbon LimitC <0.1%
certification AuthenticAerospace documentation authentic; traceability ; CoC valid and ; alloy authenticity ; AS9100/ status
hydrogen LimitH <0.015%
iron LimitFe <0.3%
material Integritycontamination ; single aerospace alloy type ; aerospace-authentic ; composition aerospace-compliant; impurity violations
mechanical Propertiesmechanical properties aerospace specification for specific alloy
nitrogen LimitN <0.05%
oxygen LimitO <0.25%
titanium ContentTi within specification
vanadium LimitV within specification
Weight Tolerance
measurementVerified by certified aerospace-grade scale; weight certificate aerospace-standard for specialty shipment
variance±0.5% from purchase order weight
Required Test Methods
Visual Inspection & Aerospace Certification Documentation
CRITICAL
Purpose
- confirm aerospace-grade titanium (NOT commodity Ti)
- verify AS9100/NADCAP documentation
- assess authenticity rigorous
- identify alloy type visually
Acceptance Criteria
- Aerospace titanium character unmistakable
- AS9100/NADCAP documentation complete and valid
- material authentic aerospace-grade
- alloy type clearly identifiable
- thin oxide protective layer characteristic
- zero rust/corrosion
Procedure
- 100% visual inspection + RIGOROUS documentation review
- verify aerospace titanium characteristics
- examine aerospace certification documents
- cross-reference with OEM records
- identify alloy family
- assess oxidation characteristic aerospace-acceptable
- verify heat number visible
Alloy Type Identification
CRITICALABSOLUTE
Purpose
- confirm Ti-6Al-4V, Ti-5Al-2.5Sn, pure Ti, or APPROVED aerospace titanium
- EXCLUDE commodity/non-aerospace material
Acceptance Criteria
- Confirmed as Ti-6Al-4V, Ti-5Al-2.5Sn, pure Ti, or specifically approved aerospace alloy
Comprehensive ICP-AES Elemental Analysis
CRITICALMANDATORYEXTREME
Purpose
- verify ALL elements to aerospace AMS specifications
- accuracy ±0.01-0.05% for critical elements (Ti, Al, V)
- aerospace zero-defect precision
Acceptance Criteria
- ALL elements within AMS specifications
- ZERO impurities beyond tolerance
- alloy composition VERIFIED aerospace-compliant
- no alloying violations
- aerospace specification
Oxygen/Nitrogen/Hydrogen Ultra-Sensitive Analysis
CRITICAL
Purpose
- detect ppm-level and ppb-level O/N/H embrittlement elements
- assess CATASTROPHIC mechanical property degradation risk
- hydrogen stress-corrosion cracking extreme concern
Acceptance Criteria
- O <0.25%, N <0.05%, H <0.015% (ppb-level)
- aerospace embrittlement limits
- hydrogen embrittlement risk
- stress-corrosion cracking
- mechanical safety
Mechanical Properties Testing
CRITICALMANDATORY
Purpose
- verify material mechanical properties match aerospace specification (tensile strength, yield strength, hardness, fatigue, stress-rupture)
Acceptance Criteria
- Mechanical properties MEET aerospace standard for specific alloy
- stress-rupture capability verified
- fatigue resistance documented
- aerospace performance qualification
Procedure
- Tensile testing, hardness testing, fatigue assessment, stress-rupture testing for ALL lots (no minimum threshold)
- aerospace mechanical integrity
Material Certification Verification
ABSOLUTE
Purpose
- Verify authentic aerospace documentation
- Certificate of Conformance (CoC) validity
- traceability chain completeness
- aerospace authentication
Acceptance Criteria
- Valid aerospace CoC
- alloy/heat number verification
- traceability chain COMPLETE and
- authenticity CONFIRMED aerospace-certified
- aerospace specification DOCUMENTED explicit