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Why Material Selection Matters

Material selection is the most consequential decision in part design. The wrong material costs you twice - once when you build the prototype, and again when you redesign for production because the part failed in the field. This guide gives you the engineering framework to narrow hundreds of alloys down to the right one - backed by real property data, cost comparisons, and application-specific recommendations used by experienced mechanical engineers.

Section 1 of 9

The Material Selection Framework

Before opening a material database, answer these five questions in order. Each one eliminates entire material families and narrows your search.

Material selection is the most consequential decision in part design. The wrong material costs you twice - once when you build the prototype, and again when you redesign for production because the part failed in the field. This guide provides a structured framework for choosing materials across CNC machining, 3D printing, sheet metal, and injection molding.

We'll cover property trade-offs with real numbers, cost comparisons at different volumes, and the selection methodology that experienced mechanical engineers use to narrow hundreds of alloys down to the right one.

What loads does the part see?

Static, cyclic/fatigue, impact, or creep. This determines your minimum yield strength and fatigue endurance limit.

1.1

What environment does it operate in?

Temperature range, chemical exposure, UV, humidity, sterilization (autoclave, EtO, gamma).

1.2

What are the dimensional requirements?

Tight tolerances favor metals (stable, machinable). Large, complex shapes favor plastics or composites.

1.3

What are the weight constraints?

Strength-to-weight ratio (specific strength) is what matters, not absolute strength. Aluminum and titanium win here; steel wins on absolute cost.

1.4

What is the target cost at volume?

Raw material cost per kg varies 10× between commodity steels and aerospace titanium.

1.5

Pro Tip

Answer these five questions before opening any material database. Each one eliminates entire material families and narrows your search from hundreds of alloys to 2–3 candidates.

Section 2 of 9

Aluminum Alloys

Aluminum is the default CNC material for good reason: excellent machinability, good strength-to-weight, natural corrosion resistance, and moderate cost.

The two most common grades cover 80%+ of CNC aluminum work. Start with 6061-T6. Switch to 7075-T6 only when you need >40 ksi yield and can accept lower weldability and higher material cost. For cosmetic anodized parts, 6061 produces a cleaner finish.

Property6061-T67075-T6
Tensile strength310 MPa (45 ksi)572 MPa (83 ksi)
Yield strength276 MPa (40 ksi)503 MPa (73 ksi)
Elongation at break12–17%5–11%
MachinabilityExcellentGood (more tool wear)
WeldabilityGood (loses T6 temper in HAZ)Poor (stress-corrosion cracking risk)
Anodize qualityExcellent (clear, hard, color)Good (slight yellow tint)
Cost (plate, $/lb)$3–5$6–10
Best forStructural brackets, housings, fixturesHigh-load aerospace, bicycle frames, drone arms

Pro Tip

Selection rule: Start with 6061-T6. Switch to 7075-T6 only when you need >40 ksi yield and can accept lower weldability and higher material cost. For cosmetic anodized parts, 6061 produces a cleaner finish.

Section 3 of 9

Stainless Steel

Stainless steel grades range from free-machining (303) to marine-grade corrosion resistance (316L) to heat-treatable high-strength (17-4 PH).

Property303304316L17-4 PH (H900)
Tensile strength620 MPa515 MPa485 MPa1,310 MPa
Corrosion resistanceGoodVery goodExcellent (chloride environments)Good
MachinabilityBest (free-machining)ModerateModerateModerate
WeldingPoor (hot cracking)ExcellentExcellentGood (age after welding)
FDA food contactNoYesYesYes
Best forFittings, shafts, bushingsFood/medical housingsMarine, chemical processingHigh-strength structural

Pro Tip

Use 303 when machinability is king and corrosion requirements are moderate. Use 316L for anything involving salt water, chlorides, or bodily fluids. Use 17-4 PH when you need stainless corrosion resistance and heat-treatable high strength (130+ ksi).

Section 4 of 9

Carbon & Alloy Steels + Titanium

When cost matters more than corrosion resistance, carbon steel is the answer. When strength-to-weight is critical, titanium is unmatched.

Carbon and alloy steels dominate when cost matters more than corrosion resistance. Titanium (Ti-6Al-4V, Grade 5) delivers a strength-to-weight ratio that beats both aluminum and steel - 160 ksi tensile at 4.43 g/cm³ density (vs. 2.70 for aluminum, 7.85 for steel). But it's expensive ($25–$50/lb for bar stock) and difficult to machine (low thermal conductivity causes tool-tip heat buildup).

1018 (Low Carbon)

Easy to machine and weld. Case-hardenable. Best for pins, shafts, brackets where surface hardness + tough core is needed.

4.1

4140 (Alloy Steel)

Through-hardenable to HRC 28–32. Excellent fatigue resistance. Standard for gears, axles, and high-load shafts.

4.2

A2 / D2 Tool Steel

Air-hardening, wear-resistant. Use for fixtures, die components, and wear surfaces. HRC 58–62 achievable.

4.3

Ti-6Al-4V (Grade 5)

Use titanium when: weight savings directly impacts product performance (aerospace, medical implants, racing), the operating temperature exceeds 200°C (aluminum softens), or biocompatibility is required.

4.4

Pro Tip

Carbon steel needs surface treatment (plating, black oxide, paint) for corrosion resistance. Factor in finishing cost when comparing against stainless or aluminum.

Section 5 of 9

Engineering Plastics

Plastics offer lower density, electrical insulation, and chemical resistance that metals can't match. The trade-off is lower stiffness, creep under sustained load, and tighter temperature limits.

MaterialTensile StrengthMax Service TempChemical ResistanceCost ($/lb)Best For
Delrin (POM)69 MPa (10 ksi)90°C (195°F)Good (not strong acids)$4–8Gears, bushings, snap-fits, low-friction guides
Nylon 6/682 MPa (12 ksi)100°C (212°F)Good$4–7Structural clips, cable ties, wear pads
PEEK100 MPa (14.5 ksi)260°C (500°F)Excellent$70–120Aerospace, medical implants, semiconductor
UHMWPE40 MPa (5.8 ksi)80°C (176°F)Excellent$6–10Wear strips, guides, food-contact surfaces
Polycarbonate (PC)63 MPa (9.1 ksi)120°C (248°F)Moderate$3–6Transparent housings, impact-resistant covers
ABS40 MPa (5.8 ksi)80°C (176°F)Moderate$2–4Consumer enclosures, injection-molded housings

Pro Tip

Start with Delrin for precision mechanical parts (lowest moisture absorption, best dimensional stability). Use Nylon when you need higher strength and can tolerate ~2% moisture absorption. Use PEEK only when temperature or chemical environment demands it - it's 10–15× the cost of Delrin.

Section 6 of 9

Composites: Carbon Fiber, Glass & Kevlar

Composites offer the highest specific stiffness and strength of any material class, but they bring manufacturing complexity.

Composites are not CNC-machined from billet - they're laid up, cured, and then trimmed. Only use composites when specific stiffness or specific strength requirements cannot be met by aluminum or titanium, and the program volume justifies tooling for lay-up molds. For one-off prototypes, machined aluminum is almost always faster and cheaper.

Carbon Fiber Reinforced Polymer (CFRP)

Specific stiffness 3–5× aluminum. Used in drone frames, satellite structures, sporting goods. Expensive ($50–$200/lb for prepreg).

6.1

Glass Fiber Reinforced Polymer (GFRP)

60% of CFRP stiffness at 20% of the cost. Excellent for enclosures, non-structural panels, and PCB substrates (FR-4 is GFRP).

6.2

Kevlar (Aramid)

Exceptional impact and abrasion resistance. Difficult to machine (fibers fuzz rather than shear cleanly). Best for protective housings and ballistic applications.

6.3

Pro Tip

When to use composites: Only when specific stiffness or specific strength requirements cannot be met by aluminum or titanium, and the program volume justifies tooling for lay-up molds.

Section 7 of 9

Material Selection by Application

Use this application matrix to quickly find the right material for your specific use case - with alternatives and materials to avoid.

ApplicationFirst ChoiceAlternativeAvoid
Structural bracket (general)Al 6061-T6Steel 1018 (higher load)Plastics (creep under sustained load)
Precision bearing housingAl 7075-T6 or SS 303Bronze (for self-lubricating bushings)Carbon steel (corrosion without plating)
Medical instrumentSS 316L or Ti-6Al-4VPEEK (non-metallic alternative)Aluminum (anodize can flake in sterilization)
Consumer electronics enclosureAl 6061-T6 (premium) or ABS (injection)PC (impact resistance + transparency)SS (too heavy for handheld)
Semiconductor wafer handlingAl 6061-T6 (hard anodized) or PEEKCeramic (alumina, silicon carbide)Carbon steel (particle generation)
Outdoor/marineSS 316L or Al 5052-H32Titanium (corrosion-free, weight matters)Carbon steel, 7075 (pitting corrosion)
High-temp (>200°C)Inconel 718 or Ti-6Al-4VPEEK (to 260°C continuous)Aluminum (softens above 150°C)

Pro Tip

When your application doesn't fit a single row, prioritize the operating environment first (temperature, chemicals, moisture), then narrow by load requirements, and let cost break the tie.

Section 8 of 9

Material Cost Comparison

Raw material cost varies significantly by alloy, form factor (plate, bar, tube), and market conditions. These ranges reflect typical 2024–2025 pricing for small-lot purchases.

MaterialCost per lb (bar stock)Relative to Al 6061
Al 6061-T6$3–51.0×
Al 7075-T6$6–102.0×
SS 304$4–71.3×
SS 316L$5–91.7×
17-4 PH$8–142.5×
Ti-6Al-4V$25–508–12×
Inconel 718$30–6010–15×
Delrin (POM)$4–81.3×
PEEK$70–12020–30×

Pro Tip

Raw material cost is only part of the equation. Titanium and Inconel are expensive to machine (slow speeds, high tool wear), so the total part cost is 3–5× the raw material premium. Factor in machining cost when comparing materials.

Section 9 of 9

Common Material Selection Mistakes

Avoid these pitfalls that burn budget and delay schedules. Each mistake has real cost implications.

1

Defaulting to stainless steel "because it won't rust"

Anodized aluminum resists corrosion in most indoor environments at 1/3 the weight and 1/2 the cost. Reserve stainless for chloride exposure, food contact, or autoclave sterilization.

2

Specifying 7075 when 6061 works

7075 is stronger, but harder to machine, can't be welded reliably, and costs 2× more. Use it only when you've proven 6061 can't meet your strength requirement.

3

Ignoring thermal expansion

If your assembly uses mixed materials (aluminum housing + steel shaft), calculate the differential thermal expansion across your operating range. Al expands at 23.6 µm/m·°C vs. 12 µm/m·°C for steel - a 100°C delta on a 200 mm bore creates a 0.23 mm fit change.

4

Choosing PEEK for cost savings vs. metal

PEEK is $70–120/lb and machines slowly. It's justified for weight, chemical resistance, or radiolucency - not because "plastic is cheaper than metal."

5

Not specifying the temper/condition

"Aluminum 6061" without "-T6" means the shop may use -O (annealed), which has half the strength. Always callout the full material designation on your drawing.

Pro Tip

Create a "material requirements" checklist on your drawing title block: alloy + temper, surface treatment, hardness range, and special test/cert requirements. This prevents assumptions from creeping in.

Summary

Conclusion

Material selection is an engineering decision, not a materials science exercise. Start with the functional requirements (loads, environment, tolerances), narrow to 2–3 candidate materials using the tables above, then let cost and availability break the tie.

Al 6061-T6

General CNC Parts

When in doubt, prototype in aluminum 6061-T6. It machines fast, costs little, and performs well in the vast majority of applications.

SS 316L or Ti-6Al-4V

Corrosive / Medical / Food

For chloride exposure, food contact, sterilization, or biocompatibility requirements. Factor in 2–3× higher machining costs.

Titanium or PEEK

Weight-Critical / High-Temp

Upgrade to a higher-performance material only when test data proves 6061 isn't sufficient. Consider total program cost, not just material price.

When in doubt, prototype in aluminum 6061-T6. It machines fast, costs little, and performs well in the vast majority of applications. Upgrade to a higher-performance material only when test data proves 6061 isn't sufficient.

Further Reading

Common Questions

Frequently Asked Questions

What is the best default material for CNC machined parts?
Aluminum 6061-T6 is the default for good reason: excellent machinability, good strength-to-weight, natural corrosion resistance, and moderate cost ($3–5/lb). It machines fast, anodizes well, and performs in the vast majority of applications. Switch to a higher-performance material only when test data proves 6061 isn't sufficient.
When should I use stainless steel instead of aluminum?
Use stainless steel when your part will be exposed to chloride environments (salt water, bodily fluids), requires FDA food-contact compliance, needs autoclave sterilization, or requires tensile strength above 45 ksi. For indoor applications with moderate corrosion requirements, anodized aluminum is lighter and cheaper.
How much does titanium cost compared to aluminum?
Ti-6Al-4V bar stock costs $25–50/lb vs. $3–5/lb for Al 6061-T6 - roughly 8–12× more for raw material. But the total part cost premium is even higher (3–5× the raw material premium) because titanium machines slowly due to low thermal conductivity and causes high tool wear.
What engineering plastic should I start with for CNC parts?
Start with Delrin (POM) for precision mechanical parts - it has the lowest moisture absorption and best dimensional stability among common engineering plastics. Use Nylon 6/6 when you need higher strength and can tolerate ~2% moisture absorption. Use PEEK only when temperature (>150°C) or chemical environment demands it - it costs 10–15× more than Delrin.
When are composites worth the cost and complexity?
Only when specific stiffness or specific strength requirements cannot be met by aluminum or titanium, AND the program volume justifies tooling for lay-up molds. CFRP offers 3–5× the specific stiffness of aluminum but costs $50–$200/lb for prepreg. For one-off prototypes, machined aluminum is almost always faster and cheaper.
What happens if I don't specify the temper on my material callout?
The shop may use the cheapest or most available condition. For example, "Aluminum 6061" without "-T6" could mean -O (annealed), which has roughly half the yield strength (12 ksi vs. 40 ksi). Always callout the full material designation including temper/condition on your drawing.

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