Material Properties Chart
Compare tensile strength, yield strength, density, thermal conductivity, and machinability across 25+ CNC-machined metals and engineering plastics. Side-by-side reference with SI and Imperial units.
25+ Metals & Plastics
Dual SI / Imperial Units
Machinability & Cost
Material Properties
Key properties at a glance
Reference Chart
Metals & Engineering PlasticsWhat Is a Material Properties Chart?
A material properties chart compares the key mechanical, physical, and thermal properties of engineering materials side by side, helping engineers select the right material for CNC machining.
Material properties are measurable characteristics — tensile strength, density, thermal conductivity, hardness — that determine how a material performs under load, heat, and environmental exposure. For CNC machining, these properties also influence machinability, tooling selection, surface finish, and final part cost.
Strength & Stiffness
Tensile strength, yield strength, and elastic modulus determine load capacity and deflection. Yield strength is the more important design value — once a part yields, it’s permanently deformed.
Physical Properties
Density (weight), thermal conductivity (heat flow), and thermal expansion (dimensional change with temperature) drive material selection in weight-critical, thermal, and precision applications.
Machinability & Cost
Machinability ratings (1–10) and relative cost columns help estimate cycle time and total part cost. A material with excellent strength can be uneconomical if it machines poorly.
Material Properties Comparison: Metals & Plastics
Compare tensile strength, density, thermal conductivity, and machinability across 25+ CNC-machined materials in dual SI/Imperial units.
Note: Property values are typical for the indicated temper and condition. Individual mill heats may differ. Values compiled from ASM Handbook, ASTM specifications, and manufacturer typical mill cert data. For critical applications, verify against material test reports (MTRs) from your supplier.
Metals — Mechanical & Physical Properties
Tensile and yield strength in both MPa and ksi. Density in g/cm³ (lb/in³ in parentheses). Machinability: 10 = easiest to machine (C360 brass). Relative cost vs. 6061-T6 aluminum baseline.
| Material Family | Alloy / Grade | Tensile (MPa / ksi) | Yield (MPa / ksi) | Density (g/cm³) | Elongation (%) | Elastic Modulus (GPa) | Hardness | Therm. Cond. (W/m·K) | Machinability | Rel. Cost |
|---|---|---|---|---|---|---|---|---|---|---|
| Aluminum | 6061-T6 | 310 / 45 | 276 / 40 | 2.70 (0.098) | 17 | 69 | 95 HB | 167 | 8 | $ (baseline) |
| 7075-T6 | 572 / 83 | 505 / 73 | 2.81 (0.101) | 11 | 72 | 150 HB | 130 | 7 | $$ | |
| 2024-T3 | 470 / 68 | 325 / 47 | 2.78 (0.100) | 20 | 73 | 120 HB | 121 | 6 | $$ | |
| 5052-H32 | 230 / 33 | 193 / 28 | 2.68 (0.097) | 12 | 70 | 60 HB | 138 | 6 | $ | |
| 5083-O | 310 / 45 | 230 / 33 | 2.66 (0.096) | 12 | 71 | 75 HB | 117 | 5 | $$ | |
| MIC-6 (cast) | 166 / 24 | 105 / 15 | 2.71 (0.098) | 3 | 71 | 65 HB | 142 | 8 | $$ | |
| Stainless | 303 (ann.) | 620 / 90 | 240 / 35 | 8.00 (0.289) | 50 | 193 | 150 HB | 16.2 | 8 | $$ |
| 304 (ann.) | 515 / 75 | 205 / 30 | 7.93 (0.286) | 40 | 193 | 150 HB | 16.2 | 4 | $$ | |
| 316 (ann.) | 550 / 80 | 240 / 35 | 8.00 (0.289) | 50 | 193 | 150 HB | 16.3 | 4 | $$$ | |
| 17-4 PH (H900) | 1310 / 190 | 1170 / 170 | 7.80 (0.282) | 10 | 196 | 42 HRC | 17.9 | 4 | $$$$ | |
| 416 (ann.) | 517 / 75 | 276 / 40 | 7.75 (0.280) | 30 | 200 | 160 HB | 24.9 | 9 | $$ | |
| 440C (hard.) | 760 / 110 | 450 / 65 | 7.65 (0.276) | 2 | 200 | 58 HRC | 24.2 | 3 | $$$ | |
| Carbon / Alloy Steel | 1018 (cold drawn) | 440 / 64 | 370 / 54 | 7.87 (0.284) | 15 | 205 | 126 HB | 51.9 | 7 | $ |
| 1045 (cold drawn) | 625 / 91 | 530 / 77 | 7.87 (0.284) | 12 | 205 | 179 HB | 51.9 | 6 | $ | |
| 4140 (ann.) | 655 / 95 | 417 / 60 | 7.85 (0.284) | 26 | 205 | 197 HB | 42.6 | 6 | $$ | |
| 4140 (Q&T 32 HRC) | 1035 / 150 | 885 / 128 | 7.85 (0.284) | 15 | 205 | 32 HRC | 42.6 | 4 | $$$ | |
| 4340 (ann.) | 745 / 108 | 470 / 68 | 7.85 (0.284) | 22 | 205 | 217 HB | 44.5 | 5 | $$$ | |
| Tool Steel | A2 (air-hardened) | 1480 / 215 | 1240 / 180 | 7.86 (0.284) | 12 | 205 | 60 HRC | 26.0 | 3 | $$$$ |
| D2 (hardened) | 1730 / 251 | 1520 / 220 | 7.70 (0.278) | 2 | 210 | 62 HRC | 20.0 | 2 | $$$$ | |
| O1 (oil-hardened) | 1380 / 200 | 1170 / 170 | 7.85 (0.284) | 2 | 210 | 61 HRC | 32.0 | 3 | $$$ | |
| Titanium | Ti-6Al-4V (Gr5) | 900 / 130 | 830 / 120 | 4.43 (0.160) | 14 | 114 | 36 HRC | 6.7 | 2 | $$$$ |
| Grade 2 (CP) | 345 / 50 | 276 / 40 | 4.51 (0.163) | 20 | 103 | 170 HB | 16.4 | 3 | $$$$ | |
| Copper / Brass | C360 Brass | 345 / 50 | 125 / 18 | 8.49 (0.307) | 53 | 97 | 65 HB | 115 | 10 | $$ |
| C110 Copper | 220 / 32 | 69 / 10 | 8.92 (0.322) | 45 | 115 | 40 HB | 388 | 5 | $$$ | |
| Nickel / Superalloy | Inconel 718 (aged) | 1240 / 180 | 1035 / 150 | 8.19 (0.296) | 12 | 205 | 36 HRC | 11.4 | 1 | $$$$$ |
| Inconel 625 | 830 / 120 | 415 / 60 | 8.44 (0.305) | 30 | 208 | 220 HB | 9.8 | 1 | $$$$$ |
Engineering Plastics — Mechanical & Thermal Properties
Properties vary with grade, temperature, and moisture content. Max service temperature is for continuous long-term exposure. Water absorption: 24-hour immersion values.
| Material | Trade Name | Tensile (MPa) | Flexural Modulus (GPa) | Density (g/cm³) | Max Service Temp (°C) | Thermal Exp. (10⁻⁶/°C) | Water Absorb (%) | Machinability | Rel. Cost | Key Feature |
|---|---|---|---|---|---|---|---|---|---|---|
| POM / Acetal | Delrin | 65 | 2.8 | 1.41 | 90 | 110 | 0.25 | Excellent | $ | Best machinability, low friction |
| Nylon 6/6 | Zytel | 75 | 2.8 | 1.14 | 120 | 80 | 1.5 | Good | $–$$ | Wear resistance, self-lubricating |
| PEEK | Victrex | 100 | 4.1 | 1.31 | 250 | 47 | 0.10 | Good | $$$ | High-temp metal replacement |
| PEI | Ultem 1000 | 105 | 3.3 | 1.27 | 170 | 56 | 0.25 | Good | $$$ | Flame retardant, electrical insulator |
| Polycarbonate | Lexan | 65 | 2.3 | 1.20 | 120 | 68 | 0.15 | Good | $–$$ | Impact strength, optical clarity |
| PTFE | Teflon | 25 | 0.5 | 2.17 | 260 | 126 | <0.01 | Fair | $$$ | Extreme chemical resistance |
| UHMW-PE | Tivar | 40 | 0.7 | 0.93 | 85 | 198 | <0.01 | Fair | $ | Lowest friction, wear strips |
| Acrylic (PMMA) | Plexiglas | 70 | 3.1 | 1.19 | 65 | 72 | 0.30 | Good | $ | Optical clarity, rigid |
| ABS | Lustran | 42 | 2.1 | 1.05 | 80 | 90 | 0.30 | Good | $ | Impact resistant, economical |
| HDPE | Marlex | 31 | 1.0 | 0.96 | 80 | 120 | <0.01 | Fair | $ | Food-safe, moisture proof |
| PAI | Torlon 4203 | 145 | 4.9 | 1.41 | 260 | 30 | 0.33 | Difficult | $$$$$ | Highest-strength machinable plastic |
| PPS | Ryton | 90 | 3.8 | 1.35 | 220 | 50 | 0.02 | Fair | $$$ | Broad chemical resistance |
ASM Handbook & ASTM References
Data compiled from ASM Handbook Volumes 1 & 2, ASTM material specifications (B209, B211, A240, A276, B265), and manufacturer typical mill cert values.
Material-Specific Properties
Steel, aluminum, and plastic property relationships differ significantly. Converted values are approximate; always verify against material test reports for critical applications.
How to Choose a Material Using This Chart
Follow this five-step framework to narrow your material options systematically, balancing strength, weight, thermal performance, and cost.
Define Requirements
List minimum tensile/yield strength, operating temperature range, exposure to moisture or chemicals, weight budget, and regulatory constraints.
Shortlist by Thresholds
Filter the metals or plastics table to materials that meet all minimum requirements. If nothing qualifies, revisit the requirements — are they based on actual loads or inflated safety margins?
Rank by Machinability
Sort qualifying candidates by machinability rating. A 2/10 material can cost 3–8× more to machine than an 8/10 material. The relative cost column captures this difference.
Compare Total Cost
Raw material cost is only part of the picture. A cheaper material that machines poorly can cost more in total than a more expensive material that cuts fast. Check the cost column, then get an instant quote.
Validate Finishing
Confirm the material accepts the surface finish or coating you need — anodizing works on aluminum but not stainless, passivation enhances stainless corrosion resistance.
Example Workflow: Marine Bracket
You need a corrosion-resistant metal bracket for a saltwater marine application, targeting moderate strength (≥300 MPa yield) and minimum weight. Filter to stainless steel, sort by density. 303 stainless offers 90 ksi tensile and the best machinability of the stainless group (8/10), but lacks the molybdenum that gives 316 its superior pitting resistance. 316 (80 ksi tensile, density 8.00 g/cm³) adds that protection at a modest cost increase. If weight is the overriding factor, titanium Grade 5 halves the density at 4.43 g/cm³, but at 3.5× the machining cost.
Key Property Definitions
Understanding what each column in the chart tells you makes the difference between a well-informed material selection and an expensive mismatch. Here are the properties that matter most for CNC-machined parts.
| Property | What It Measures | Why It Matters for CNC Parts |
|---|---|---|
| Tensile Strength | Maximum stress before fracture (MPa / ksi) | Ultimate failure point. Design around yield strength instead — once a part yields, it’s permanently deformed even if it hasn’t fractured. |
| Yield Strength | Stress at which permanent plastic deformation begins | More important design number. A bracket that bends 0.5 mm under load has failed, regardless of ultimate strength. Design around yield. |
| Density | Mass per unit volume (g/cm³ / lb/in³) | Drives material selection in weight-critical applications. Strength-to-weight ratio = tensile strength ÷ density — Ti-6Al-4V scores 203, 6061 aluminum 115, 304 stainless 65. |
| Thermal Conductivity | Heat flow efficiency (W/m·K) | High conductivity (copper, aluminum) for heat sinks; low conductivity (stainless, plastics) for thermal barriers. Also affects machining — low-conductivity materials concentrate heat at the tool tip. |
| Elastic Modulus | Stiffness — resistance to elastic deformation (GPa) | Steel (205 GPa) is 3× stiffer than aluminum (69 GPa). For stiffness-limited designs, material choice matters more than strength. |
| Elongation | Ductility — % stretch before fracture | High elongation (304 stainless at 40%) gives warning before failure. Low elongation (D2 tool steel at 2%) means brittle failure with no warning. |
| Machinability | Relative ease of machining (1–10 scale) | 10 = easiest (C360 brass), 1 = most difficult (Inconel). A 2/10 material can cost 3–8× more to machine than an 8/10 material. |
Design tip: If your part includes snap-fits, press-fits, or features that must deform elastically during assembly, elongation and elastic modulus together determine whether the design works. A stiff, low-elongation plastic (acrylic) will crack where a more ductile one (nylon, polycarbonate) will flex. For tight-tolerance parts, account for thermal expansion — plastics expand 5–15× more than metals with temperature changes.
Material Properties & CNC Machinability
Material properties directly affect machining strategy, tooling selection, cutting speed, surface finish, and achievable tolerances.
Hardness and strength are the single most important properties for machining strategy. A harder workpiece resists chip formation, cuts slower, wears tools faster, and requires tougher tooling. The machinability rating in the chart (1–10) gives you a practical guide to relative cycle time and tool life.
Standard Machining Range
Conventional high-speed steel and standard carbide tooling work well. Covers most machined metals including aluminum, brass, copper, annealed steels, 304/316 stainless, and titanium grades.
Hardened Material Range
Carbide tooling cuts reliably with lower speeds and more careful chip control. Includes hardened 4140/4340, 17-4 PH at H900, and Ti-6Al-4V.
High Hardness Range
Requires carbide or ceramic tooling, reduced cutting speeds, and often grinding or EDM machining for final geometry. Tool steels A2 and D2 fall within this range.
Hardness Effects on Surface Finish and Tolerance
Harder materials can maintain better surface finish because they deflect less under the cutting edge, but they also generate higher cutting forces that can push thin-walled parts out of tolerance. Engineers balance these factors when reviewing CAD files to achieve precision results. For tight-tolerance parts, our precision CNC machining service holds tolerances to ±0.001 inch on metals and engineering plastics alike.
Frequently Asked Questions
6061-T6 aluminum is the default starting point for most CNC-machined parts. It machines quickly (8/10 machinability), resists corrosion, accepts anodizing, and costs less than any other engineering metal. Its 310 MPa tensile and 276 MPa yield strength cover a broad range of applications. For more strength, 7075-T6 aluminum roughly doubles the strength at ~25% higher cost.
It depends. Ti-6Al-4V (900 MPa tensile) is stronger than annealed 304 stainless (515 MPa) and 1018 carbon steel (440 MPa), but weaker than heat-treated 4140 (1,035 MPa) and 17-4 PH (1,310 MPa). However, titanium is 45% lighter than steel, giving it roughly double the strength-to-weight ratio. For weight-critical applications, titanium’s weight advantage justifies its higher machining cost.
6061-T6 offers 310 MPa tensile and 276 MPa yield with excellent corrosion resistance, weldability, and anodizing response — the versatile general-purpose choice. 7075-T6 delivers 572 MPa tensile and 505 MPa yield, nearly double the strength, but sacrifices corrosion resistance, weldability, and about 25% higher cost. Choose 6061 unless you genuinely need the extra strength.
For most indoor and general-purpose applications, 304 provides adequate corrosion resistance at a lower cost. Choose 316 when the part encounters chlorides — saltwater, de-icing salts, swimming pool environments, pharmaceutical processing — as the 2–3% molybdenum content dramatically improves pitting resistance. For better machinability, consider 303 stainless (8/10), but note it is not weldable and has slightly lower corrosion resistance than 304.
Yes, in the right application. Plastics replace metals when the part needs electrical insulation, chemical resistance, low friction, vibration damping, or significant weight reduction, and when loads and temperatures are within the plastic’s capabilities. PEEK replaces stainless steel in some medical and aerospace applications at 20% of the weight, but costs roughly 3× as much to machine as aluminum and cannot match metals’ absolute strength. Plastics creep under sustained load, soften at elevated temperatures, and expand 5–15× more than metals.
Material choice affects cost in three ways: raw material cost, machinability (cycle time and tool wear), and finishing compatibility. A part machined from Delrin might cost 15% less than the same part in 6061 aluminum because Delrin cuts faster with less tool wear. Inconel 718 costs 5–8× more to machine than 6061 aluminum because cutting speeds are roughly one-tenth and tool life is dramatically shorter. The relative cost column in the metals table provides a practical comparison.
Almost never. The strongest material that meets your minimum requirements is rarely the optimal choice because strength almost always trades off against other factors — higher-strength materials typically cost more, machine more slowly, require specialized tooling, and may introduce brittleness. A 17-4 PH stainless part (1,310 MPa) costs roughly 3–4× more to machine than a 304 stainless part (515 MPa) that would carry the same load perfectly well. Match the material to the actual requirements, not to an arbitrary safety margin.
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