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Material Selection Drives 40–60% of Total Part Cost

For CNC machined parts, the material you select determines raw stock price, cycle time, tool wear rate, and post-processing requirements. Choosing 6061-T6 aluminum over Ti-6Al-4V for a non-weight-critical bracket can reduce total part cost by 80–90%. This guide provides alloy-specific data — UTS, yield strength, density, machinability rating, cost per pound, and cycle-time multipliers — so you can make that decision with real numbers.

Section 1 of 6

Quick Decision Framework

Every CNC material decision starts with one dominant constraint — weight, strength, cost, or corrosion environment — and that single priority narrows the field to one or two alloy families. Weight-limited? Aluminum or titanium. Strength-limited? Steel or titanium. Cost-limited? Aluminum or carbon steel. Corrosion environment? Aluminum (anodized), stainless steel, or titanium. The table below maps each priority to the right alloy family and specific grade.

PriorityMaterial FamilyTop AlloyWhy
Lowest costCarbon steel12L14, 1018$1–2/lb ($2–4/kg) raw, machinability rating up to 170%
LightweightAluminum6061-T6, 7075-T62.70–2.81 g/cm³ vs. 7.85 g/cm³ for steel
High strengthAlloy steel4140, 4340UTS 95–108 ksi (655–745 MPa) heat-treated
Corrosion + lightweightAluminum6061-T6 + anodizeNatural oxide layer + anodize Type II/III per MIL-A-8625
Corrosion + strengthStainless steel304, 316LCr-Ni passivation layer, no coating required
Strength-to-weightTitaniumTi-6Al-4VComparable strength to heat-treated alloy steels at 57% of the weight
BiocompatibleTitanium or 316L SSTi-6Al-4V ELI, 316LISO 10993 biocompatible

Decision Tree: What Is Your Primary Constraint?

Weight

Al or Ti

6061-T6 for general use (2.70 g/cm³), Ti-6Al-4V when strength must also be high (4.43 g/cm³)

Strength

Steel or Ti

4140 (95 ksi) or 4340 (108 ksi) for cost-effective strength; Ti-6Al-4V (130 ksi) when weight is also a factor

Cost

Al or Steel

12L14 steel at $1–2/lb for small parts; 6061-T6 aluminum at $3–5/lb for the shortest cycle times

Corrosion

Al, SS, or Ti

6061-T6 + anodize for mild environments; 316L SS for chemical exposure; Ti for high-temp corrosion

Pro Tip

Most engineers over-specify material. Before selecting Ti-6Al-4V or 17-4 PH, ask: does this part actually need the higher strength, corrosion resistance, or temperature capability? In 70–80% of cases, 6061-T6 aluminum or 4140 steel meets the functional requirement at a fraction of the cost.

Section 2 of 6

Aluminum Alloys for CNC Machining

If you are new to CNC sourcing, start with aluminum — it is the most forgiving, fastest to machine, and cheapest to iterate on. Aluminum is the most frequently CNC-machined metal — typically 60–70% of job-shop volume. High machinability (90% for 6061-T6 relative to free-machining aluminum 2011-T3, rated 100%), low density (2.70 g/cm³), and natural corrosion resistance make it the default choice when strength requirements allow. The three workhorse alloys are 6061-T6, 7075-T6, and 2024-T3.

Property6061-T67075-T62024-T3
UTS, ksi (MPa)45 (310)83 (572)70 (483)
Yield strength, ksi (MPa)40 (276)73 (503)50 (345)
Density, g/cm³2.702.812.78
Machinability rating90%70%70%
Cost, $/lb ($/kg)$3–5 ($7–11)$5–8 ($11–18)$4–7 ($9–15)
Corrosion resistanceGood (anodizable)Fair (needs anodize)Poor (needs clad or anodize)
WeldabilityGood (TIG/MIG)PoorPoor
Fatigue resistanceModerateGoodExcellent
Primary useGeneral structural, enclosuresHigh-load brackets, toolingFatigue-critical, cyclic-load parts

Machinability rating relative to Al 2011-T3 = 100% (standard aluminum baseline). Mechanical properties per ASM Handbook Vol. 2.

Surface Finishing Options

  • Anodize Type II per MIL-A-8625: decorative + corrosion protection, 0.0002–0.001 in. (5–25 μm) thickness
  • Anodize Type III (hard) per MIL-A-8625: wear-resistant, 0.001–0.003 in. (25–75 μm), hardness up to 70 HRC equivalent
  • Chromate conversion per MIL-DTL-5541: conductive corrosion protection for EMI shielding applications

CNC Machining Considerations

  • High RPM spindle preferred: 15,000–30,000 RPM for optimal chip evacuation and surface finish
  • Aggressive feeds achievable: 0.004–0.010 in./tooth (0.10–0.25 mm/tooth) typical for 6061-T6
  • Built-up edge (BUE) risk at low spindle speeds — maintain SFM above 800 (250 m/min) to prevent material welding to the tool
  • Typical surface finish: Ra 32–63 μin. (0.8–1.6 μm) achievable with standard end mills at proper speeds

Pro Tip

Default to 6061-T6 unless you have a specific reason not to. It is the most available aluminum alloy (nearly every metal supplier stocks it in bar, plate, and sheet), machines with the fewest issues, and anodizes well. Reserve 7075-T6 for applications where the 40% higher yield strength (73 ksi vs. 40 ksi) justifies the 60–100% higher material cost and reduced weldability.

Section 3 of 6

Steel Alloys for CNC Machining

When your strength requirements exceed what aluminum can deliver (yield > 73 ksi / 503 MPa), steel is the next step — and choosing the right grade determines whether your part is machinable or a nightmare. Steel offers the broadest range of mechanical properties of any metal family — from 12L14 free-machining at 78 ksi (540 MPa) UTS to 17-4 PH precipitation-hardened at 135 ksi (930 MPa) in H1150 condition. The trade-off: higher density (7.85–8.00 g/cm³) and, for carbon steels, poor corrosion resistance without plating or coating.

Property101812L1441404340304 SS316L SS17-4 PH
UTS, ksi (MPa)63.8 (440)78 (540)95 (655)108 (745)73 (505)70 (485)135 (930)
Yield, ksi (MPa)53.7 (370)60 (415)60 (415)68 (470)31 (215)25 (170)105 (725)
Machinability70%170%65%50%45%36%48%
Cost, $/lb ($/kg)$1–2 ($2–4)$1–2 ($2–4)$1.50–3 ($3–7)$2–4 ($4–9)$3–5 ($7–11)$4–7 ($9–15)$6–10 ($13–22)
CorrosionPoorPoorPoorPoorExcellentExcellentGood
WeldabilityGoodPoor (leaded)Good (preheat)Fair (preheat)ExcellentExcellentFair
Primary useLow-cost structural, weldmentsHigh-volume turned parts, pinsGears, shafts, structuralHigh-toughness critical partsCorrosion-resistant process equip.Medical instruments, marineHigh-strength pins, shafts

17-4 PH properties shown for H1150 condition (over-aged for highest corrosion resistance among 17-4 PH conditions). 4140/4340 in annealed condition; heat-treated values are 20–40% higher.

Carbon & Alloy Steel CNC Notes

  • Carbide tooling recommended for alloy steels (4140, 4340) — HSS wears 3–5× faster
  • Typical SFM: 200–400 (60–120 m/min) for carbon steels; 100–250 (30–75 m/min) for alloy steels
  • 12L14 contains lead for chip-breaking — produces short, clean chips at high feed rates. Not weldable
  • Carbon steels require plating (zinc, nickel) or painting for corrosion protection in any humid environment

Stainless Steel CNC Notes

  • 304 and 316L austenitic grades work-harden rapidly — avoid dwelling or rubbing without cutting
  • Flood coolant is critical: stainless conducts heat poorly, causing tool-tip temperatures above 1,200°F (650°C)
  • 316L offers higher pitting and crevice corrosion resistance vs. 304 (2.5% Mo content) — required for marine and chemical environments
  • Passivation per ASTM A967 after machining restores the chromium oxide layer removed during cutting

Pro Tip

If you need both corrosion resistance and high strength, consider 17-4 PH stainless before jumping to titanium. In H1150 condition, 17-4 PH reaches 135 ksi (930 MPa) UTS with good corrosion resistance — at $6–10/lb ($13–22/kg) vs. $15–30/lb ($33–66/kg) for Ti-6Al-4V. The machining cycle time is also roughly 2× faster than titanium.

Section 4 of 6

Titanium Alloys for CNC Machining

Titanium is justified only when no other metal can meet the combined requirements for strength, weight, and corrosion resistance — and that justification must account for 5–8× longer machining cycles and 10–30× higher raw material cost vs. aluminum. Ti-6Al-4V achieves 130 ksi (896 MPa) UTS at 4.43 g/cm³, roughly 57% of steel's weight. Raw material costs $15–30/lb ($33–66/kg), and cycle times run 5–8× longer than aluminum. Why? Titanium's thermal conductivity is extremely low — 6.7 W/m·K vs. 167 W/m·K for 6061-T6 aluminum. This means cutting heat cannot dissipate through the workpiece and concentrates at the tool tip, accelerating wear. Combined with titanium's low elastic modulus (114 GPa, roughly half of steel's 200 GPa), the material springs back after the cutter passes, causing chatter, poor surface finish, and unpredictable tolerances unless feeds, speeds, and workholding are dialed in precisely.

PropertyTi-6Al-4V (Grade 5)CP Grade 2
UTS, ksi (MPa)130 (896)50 (345)
Yield strength, ksi (MPa)120 (828)40 (275)
Density, g/cm³4.434.51
Machinability rating22%30%
Cost, $/lb ($/kg)$15–30 ($33–66)$10–18 ($22–40)
Cycle time vs. aluminum5–8×3–5×
Corrosion resistanceExcellent (all environments)Excellent
BiocompatibilityYes (ELI grade for implants)Yes (per ISO 10993)
Max service temp600°F (315°C)500°F (260°C)

Ti-6Al-4V per AMS 4928 (bars), AMS 4911 (sheet). CP Grade 2 per ASTM B348. ELI = Extra Low Interstitials, required for implant applications.

CNC Machining Considerations

  • Low thermal conductivity: heat concentrates at the tool tip — flood coolant is mandatory, not optional
  • Typical cutting speeds: 100–200 SFM (30–60 m/min) vs. 800–1,200 SFM (250–370 m/min) for aluminum
  • Low elastic modulus (16 Msi / 110 GPa) causes spring-back — use sharp tools and maintain positive rake angles
  • Titanium is reactive with most tool coatings at high temps — uncoated carbide or AlTiN-coated inserts are typical

When Titanium Is Worth the Cost

  • Medical implants: Ti-6Al-4V ELI is the standard for load-bearing implants requiring osseointegration
  • High-temperature applications: service above 400°F (200°C) where aluminum loses temper and steel is too heavy
  • Aggressive corrosion environments: salt water, chloride solutions, or acidic environments where even 316L SS pits
  • Weight-critical + high-load: when both strength above 83 ksi (572 MPa) and density below 5 g/cm³ are required simultaneously

Cost Reality Check

A simple bracket that costs $40–80 in 6061-T6 aluminum (at quantity 10) will typically cost $300–600+ in Ti-6Al-4V at the same quantity — roughly 5–8× more when combining material cost ($15–30/lb / $33–66/kg vs. $3–5/lb / $7–11/kg) and cycle time (5–8× longer). Verify that the application truly demands titanium's properties before specifying it.

Section 5 of 6

Head-to-Head Comparison Table

This table gives you every number you need to make a material trade-off decision — print it and keep it next to your workstation. All six alloys, nine properties, side by side. Use real data instead of rules of thumb.

Property6061-T6 Al7075-T6 Al4140 Steel304 SS316L SSTi-6Al-4V
UTS, ksi (MPa)45 (310)83 (572)95 (655)73 (505)70 (485)130 (896)
Yield, ksi (MPa)40 (276)73 (503)60 (415)31 (215)25 (170)120 (828)
Density, g/cm³2.702.817.858.008.004.43
Strength-to-weight (UTS/ρ)16.729.512.19.18.829.3
Machinability90%70%65%45%36%22%
Cost, $/lb ($/kg)$3–5 ($7–11)$5–8 ($11–18)$1.50–3 ($3–7)$3–5 ($7–11)$4–7 ($9–15)$15–30 ($33–66)
Cycle time factor1.0×1.3×1.5×2.2×2.8×5–8×
Corrosion resistanceGood (anodized)FairPoor (needs plating)ExcellentExcellentExcellent
Max service temp300°F (150°C) continuous250°F (121°C)800°F (427°C)1,500°F (816°C)1,500°F (816°C)600°F (315°C)

Strength-to-weight = UTS (ksi) ÷ density (g/cm³). Cycle time factor relative to 6061-T6 aluminum = 1.0×. Machinability ratings use material-family baselines: aluminum alloys relative to 2011-T3 (100%), steels and titanium relative to AISI B1112 (100%). All properties at room temperature per ASM Handbook.

Key Takeaways from the Comparison

Strength-to-Weight Champion

7075-T6 aluminum (29.5) and Ti-6Al-4V (29.3) are virtually tied for strength-to-weight ratio — both roughly 2.4× that of 4140 steel (12.1). If weight is the primary driver and you don't need titanium's corrosion or temperature capability, 7075-T6 is the cost-effective alternative.

Cost-Performance Leader

4140 steel delivers the most strength per dollar: 95 ksi UTS at $1.50–3/lb. For applications where weight and corrosion are not concerns, 4140 outperforms every other alloy on cost-normalized strength.

Machinability Spread

The machinability gap is massive — 6061-T6 at 90% vs. Ti-6Al-4V at 22%. That 4× difference translates directly to cycle time: a part that takes 15 minutes in aluminum takes 75–120 minutes in titanium. Factor this into your total part cost calculation, not just raw material price.

Pro Tip

Do not select material based on UTS alone. For deflection-limited designs (brackets, frames, housings), elastic modulus matters more than strength. Steel (29 Msi / 200 GPa) is 3× stiffer than aluminum (10 Msi / 69 GPa) — a steel bracket deflects one-third as much as an identically-shaped aluminum bracket under the same load.

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Section 6 of 6

Application Selection by Industry

Your industry determines which material properties dominate the selection — biocompatibility for medical, weight savings for EV, and corrosion resistance for renewable energy all lead to different answers.Below are alloy recommendations for the most common CNC-machined components in each industry.

Robotics

Structural frames6061-T6 Al

Low weight, good stiffness-to-weight

High-load joints7075-T6 Al

40% higher yield than 6061

Gears & pinions4140 steel

Hardened to 28–32 HRC for wear

High-strength pins17-4 PH SS

135 ksi UTS (H1150), corrosion-resistant

Medical Devices

Surgical instruments316L SS

Biocompatible, autoclavable

ImplantsTi-6Al-4V ELI

ISO 10993, osseointegration

Equipment housings6061-T6 Al

Lightweight, lower cost

Process fixtures304 SS

Corrosion-safe for cleanroom

Semiconductors

Wafer handling fixtures6061-T6 Al

Non-magnetic, lightweight, anodizable

Process chamber parts304 SS

Corrosion-resistant in chemical vapor

Thermal management6061-T6 Al

High thermal conductivity (96 BTU/hr·ft·°F)

High-purity gas fittings316L SS

Electropolished, ultra-clean surfaces

EV / Automotive

Battery enclosures6061-T6 Al

Lightweight, thermal dissipation

Drivetrain components4140 steel

High fatigue strength, heat-treatable

Motor housings6061-T6 Al

Non-magnetic, good machinability

Suspension brackets7075-T6 Al

High strength-to-weight for unsprung mass

Renewable Energy

Solar tracker brackets6061-T6 Al

Corrosion-resistant, anodizable

Marine wind components316L SS

Salt-spray corrosion resistance

Inverter housings6061-T6 Al

EMI shielding with chromate conversion

High-load mounting304 SS

Outdoor durability without coatings

Pro Tip

When in doubt, start with 6061-T6 aluminum for prototypes. It is the lowest-risk material choice: fast to machine (cycle time baseline 1.0×), readily available, and easy to finish. Validate your design with aluminum prototypes first, then switch to steel or titanium for production only if functional testing proves aluminum is insufficient.

Further Reading

Common Questions

Frequently Asked Questions

Which is stronger — aluminum, steel, or titanium?
It depends on the alloy. Ti-6Al-4V titanium has the highest ultimate tensile strength at 130 ksi (896 MPa). 4340 alloy steel reaches 108 ksi (745 MPa). 7075-T6 aluminum peaks at 83 ksi (572 MPa). However, on a strength-to-weight basis, titanium and 7075-T6 aluminum are nearly identical — approximately 29.3 and 29.5 ksi·cm³/g respectively — both roughly 2.4× the strength-to-weight ratio of 4140 steel (12.1 ksi·cm³/g).
Is titanium worth the cost for CNC parts?
Titanium is worth the cost when the application demands either (a) the highest strength-to-weight ratio, (b) biocompatibility for medical implants, or (c) corrosion resistance at elevated temperatures above 400°F (200°C). Ti-6Al-4V costs 5–10× more than 6061-T6 aluminum when accounting for raw material ($15–30/lb / $33–66/kg vs. $3–5/lb / $7–11/kg) plus 5–8× longer cycle time. For most structural applications where weight is not critical, 4140 steel provides comparable strength at 10–20% of the total machining cost.
What is the most cost-effective CNC machining material?
12L14 free-machining steel ($1–2/lb / $2–4/kg, 170% machinability rating) and 6061-T6 aluminum ($3–5/lb / $7–11/kg, 90% machinability) are the most cost-effective metals to CNC machine. 12L14 has the lowest raw-material cost; 6061-T6 offers the shortest cycle times due to aluminum's high machinability. Choose based on whether you need steel's strength (63.8 ksi / 440 MPa for 1018) or aluminum's weight savings (2.70 g/cm³ vs. 7.85 g/cm³) and corrosion resistance.
Can I substitute aluminum for steel to save cost?
Yes, if the application allows. 7075-T6 aluminum has similar tensile strength to some carbon steels (83 ksi / 572 MPa) at one-third the weight — but at 3–5× the raw material cost. 6061-T6 is the more cost-effective substitution: lower material cost than 7075, easier to machine, and readily anodizable. Verify that the aluminum alloy meets stiffness requirements — aluminum's elastic modulus (10 Msi / 69 GPa) is one-third that of steel (29 Msi / 200 GPa), so deflection-limited designs may not benefit from the switch.
What material should I use for CNC machined medical device parts?
316L stainless steel and Ti-6Al-4V ELI are the primary choices for patient-contact medical devices. 316L is cost-effective ($4–7/lb / $9–15/kg), biocompatible per ISO 10993, and autoclavable. Ti-6Al-4V ELI (Extra Low Interstitials) is used for implants requiring osseointegration — it has higher fatigue endurance (~500 MPa vs. ~260 MPa for 316L) and is fully biocompatible per ISO 10993. For non-patient-contact equipment housings and fixturing, 6061-T6 aluminum offers lighter weight at lower cost.

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