Engineering · Reference
Modulus of elasticity (Young’s modulus).
Stiffness values for the engineering materials we run, in GPa and Msi. Use it for deflection calculations, stiffness-budget analysis, and material substitutions where stiffness is the constraint — not strength. Sorted by modulus, highest to lowest.
| Material | Family | E (GPa) | E (Msi) |
|---|---|---|---|
| Tungsten (W) | Refractory metal | 411 | 59.6 |
| Tool steel A2 | Tool steel | 207 | 30 |
| Tool steel D2 | Tool steel | 207 | 30 |
| Tool steel H13 | Tool steel | 207 | 30 |
| Inconel 625 | Nickel superalloy | 207 | 30 |
| Hastelloy C-276 | Nickel superalloy | 205 | 29.7 |
| Steel 1018 (mild) | Carbon steel | 200 | 29 |
| Steel 4140 | Alloy steel | 200 | 29 |
| Steel 4340 | Alloy steel | 200 | 29 |
| Stainless 17-7PH | PH stainless | 200 | 29 |
| Stainless 410 | Martensitic stainless | 200 | 29 |
| Inconel 718 | Nickel superalloy | 200 | 29 |
| Stainless 17-4PH | PH stainless | 196 | 28.5 |
| Stainless 304 | Austenitic stainless | 193 | 28 |
| Stainless 316L | Austenitic stainless | 193 | 28 |
| Tantalum (Ta) | Refractory metal | 186 | 27 |
| Monel 400 | Nickel alloy | 179 | 26 |
| Beryllium copper C172 | Cu-Be alloy | 131 | 19 |
| Copper C110 (ETP) | Pure copper | 117 | 17 |
| Titanium Ti-6Al-4V | Titanium alloy | 113.8 | 16.5 |
| Niobium (Nb) | Refractory metal | 105 | 15.2 |
| Titanium CP Grade 2 | Pure titanium | 105 | 15.2 |
| Bronze C932 | Bearing bronze | 100 | 14.5 |
| Brass C360 | Free-machining brass | 97 | 14.1 |
| Aluminum 2024-T3 | Aerospace aluminum | 73.1 | 10.6 |
| MIC-6 cast aluminum | Cast aluminum plate | 72 | 10.4 |
| Aluminum 7075-T6 | Aerospace aluminum | 71.7 | 10.4 |
| Aluminum 6061-T6 | Aluminum | 68.9 | 10 |
| Magnesium AZ31 | Magnesium | 45 | 6.5 |
| PEEK | Engineering plastic | 3.6 | 0.52 |
| Ultem (PEI) | Engineering plastic | 3.2 | 0.46 |
| Delrin / POM | Engineering plastic | 3.1 | 0.45 |
How to use this
Stiffness ≠ strength.
- All steels are roughly the same modulus.
4140, 4340, mild steel, stainless, tool steel — all hover around 200 GPa. Heat treatment, alloying, hardness — none of those significantly change Young’s modulus. They change strength and hardness; stiffness stays the same.
- Titanium is half-stiff for half-weight.
Ti-6Al-4V: 114 GPa, 4.43 g/cc. Steel: 200 GPa, 7.85 g/cc. Specific stiffness (E/ρ) is ~25.7 vs ~25.5 — essentially the same. So titanium isn’t stiffer per pound, just lighter for the same stiffness.
- Aluminum is one-third the stiffness of steel.
~69 GPa vs ~200 GPa. For deflection-critical parts (machine bases, optical mounts, structural brackets) you need ~3× the moment of inertia in aluminum to match steel deflection — that’s why aluminum structural sections are dimensionally larger.
- Plastics are 50–60× softer than metal.
PEEK at 3.6 GPa is one of the stiffer engineering plastics; still ~55× softer than steel (and ~19× softer than aluminum). For load-bearing plastic parts, design for plastic stiffness — don’t scale a metal design.
- Beryllium-copper is the stiffness sweet spot in copper alloys.
131 GPa vs 117 GPa for pure copper. BeCu’s combination of conductivity, non-magnetic property, and stiffness makes it valuable for electrical springs and contacts.
- Inconel and steel: same stiffness, different operating temperature.
Inconel 718 = 200 GPa, same as steel. The reason to pay 10× for Inconel is high-temperature creep resistance and corrosion — not stiffness.
Keep exploring
Related tools & references
Companion property reference for the same alloy families.
CTE values to pair with stiffness for thermal-stress analysis.
Estimate strength from hardness alongside modulus.
Full mechanical-property sheets for each material here.
Compare alloys by stiffness, strength, and machinability.
Technically reviewed by the True Precision Machining engineering team · Last reviewed June 2026
Standards referenced: MMPDS (MIL-HDBK-5), ASTM E111
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