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For aerospace, energy, defense & industrial engineers

Bolted Joint
Margin of Safety
in Minutes.

Fast, reliable margin of safety calculations for bolted joints — generate certification-ready reports in minutes instead of hours.

ECSS
Aerospace-grade
11+
Safety margins
PDF
Report export
BoltCore — M8 8.8 — Assembly analysis
Bolt
DiameterM8
Class8.8
Length40mm
Tightening
MethodTorque wrench
µG / µK0.12
ε±25%
Parts
Steel S355 · 10mm
Steel S355 · 10mm
Tapped w=2
Loads
FA+1200N
T-40/+80°C
BoltCore interface preview: M8 bolted joint assembly diagram with safety margin calculations
① Tightening
Torque
22.4 N·m
Fv min/max
14.2/22.1 kN
MoS tight.
+42%
② In service
Yield rupt.
+138%
Separ.
+17%
Slip
+64%
Stripping
+210%
Joint status: OK
Design: OK
See it in action

From bolt selection to certified report.

Real interface, real calculation, real PDF export — watch a full margin-of-safety verification run in under a minute.

The problem

Still using spreadsheets for bolted joint calculations?

With a spreadsheet, the calculation itself might only take a few minutes — it's writing up the justification report afterward that eats your afternoon.

BoltCore calculates every margin instantly and generates the certification-ready report in the same click — no separate write-up, no formatting.

Spreadsheet + report writing
~45 min
BoltCore — report included
~3 min
−90%
Time saved on reporting

Built by a senior mechanical engineer specializing in bolted joint justification for aerospace and cryogenic structures — the same ECSS-E-ST-32-19C rigor applied here to critical assemblies across aerospace, defense, energy, and industry.

Aurélien Dasquié LinkedIn

Capabilities

Engineering-grade
bolted joint analysis.

Tightening (Von Mises) Bolt rupture (yield) Bolt rupture (ultimate) Separation Sliding Thread stripping Washer bearing (yield) Washer bearing (ultimate) Plate bearing (yield) Plate bearing (ultimate)

Preload & tightening torque

Klein-Kellermann formula with full scatter. MA_min/max with method-specific ε.

Advanced analytical methodology

Full compliance model: δb/δc, loading plane factor Φ, cone model.

Thermal preload variation

CTE-based ΔFv for T_min/T_max conditions with full CTE mismatch analysis.

11 safety margins

Yield & ultimate rupture, separation, sliding, thread stripping, washer & flange bearing.

Dynamic assembly schema

Real-time SVG cross-section with washers, multi-plate stacks, load arrows.

PDF engineering report

Official justification document ready for design review or certification audit.

Pricing

Simple, transparent pricing.

Start for free. Upgrade when your projects demand the full power of BoltCore.

Free
€0 / month

Discover BoltCore. No account required. Ideal for learning the methodology.

Try for Free →
Bolt diameters M6, M8 only
Classes 8.8 / 10.9 only
Tightening torque + preload Fv
Tightening margin (Von Mises)
Assembly schema visualization
Custom friction coefficients
Service safety margins
Thermal analysis
PDF export
Enterprise
Custom

For teams and organisations needing full traceability and collaboration.

Contact us →
Everything in Pro
Multi-user team access
Company bolt & material templates
Branded PDF reports (company logo)
Calculation history & audit trail
API access & integrations
Priority support & training

Full feature comparison

Detailed breakdown of each plan.

Feature Free Pro Enterprise
Bolt Configuration
DiametersM6/M8
Resistance classes8.8/10.9
Stainless A2/A4
Custom bolt geometry
Tightening Parameters
Torque + Fv
Custom µ coefficients
Scatter ε / Mp / FZFixed
Safety Margins
Tightening (Von Mises)
Bolt rupture yield & ult.
Separation / sliding
Thread stripping
Flange & washer bearing
Assembly & Loads
Multi-plate stacks2 plates
Material library
Thermal (CTE mismatch)
FA / FQ external loads
Export & Reporting
Assembly schema (SVG)
PDF engineering report
Branded PDF (logo)
API access
Methodology

Built around critical
engineering standards.

BoltCore implements an advanced analytical methodology rooted in ECSS — the European space standard for bolted joint verification — bringing aerospace-grade rigor to critical assemblies across aerospace, defense, energy, and industry.

Compliance model, thermal analysis, loading plane factor, thread stripping analysis, and bearing margin calculations are all integrated into a unified, traceable workflow designed for critical assemblies — wherever failure is not an option.

Inspired by ECSS Aerospace Defense Oil & Gas Automotive Civil Engineering Energy

Read the full ECSS-E-ST-32-19C methodology guide →

Engineering precision.
Advanced engineering methodology.

Start for free today. No account needed. Upgrade when your projects demand it.