ΔL = α × L₀ × ΔT

Thermal expansion calculator for aerospace-grade alloys. In the vacuum, a 0.002-inch misalignment isn't art—it's a breach.

⚙️ Material Selection

23.6

📐 Initial Dimensions

500 mm
+300 K

🎯 Results

Expansion
3.54
mm
Microns
3540
μm
Tolerance Check
PASS
@ ±0.05mm
⚠️ EXPANSION EXCEEDS TOLERANCE BAND
Current: 0μm | Limit: 50μm
✓ Within Spec
Marginal clearance: 0μm
NASA Kennedy Space Center machined component
KSC-98pc620 • Kennedy Space Center • Public Domain
Every micron counts when the atmosphere drops away.
The Equation:
ΔL = α × L₀ × ΔT

Where:
• ΔL = Change in length (mm)
• α = Coefficient of thermal expansion (×10⁻⁶/K)
• L₀ = Initial length (mm)
• ΔT = Temperature difference (K)

Citation: Wikidata Q45760 — coefficient of thermal expansion

🔬 Constants Database

Alloy α (×10⁻⁶/K) Source
Aluminium 6061-T6 23.6 Q447725
Titanium Ti-6Al-4V 8.6 Q3300719
Stainless Steel 316L 16.0 Q447725
Inconel 718 13.0 ASM Handbook Vol 1
Carbon Fiber (0°) -1.5 Hexcel Design Data