Engineering Tool

COPV mass & performance calculator.

Estimate cylinder mass and performance for any volume, working pressure, and safety factor. Compare Type IV (Meyer HDRX) against all-metal and Type III aluminium-lined alternatives. See gravimetric efficiency, PV/W performance factor, and burst pressure all in one view.

Volume 3.0 L
0.25 L10 L30 L50 L
Working pressure 350 bar
503005007001000
Safety factor (burst ratio) 3.0×
1.3×2.25×3.0×4.0×

ISO 11119-3 minimum is 2.25×. Aerospace programmes typically use 2.5×–3.5× depending on qualification.

Gas medium (for gravimetric calculation)
Fibre grade

Standard quoteable, ISO-compliant carbon — broad availability, no qualification overhead.

UAV flight-time bonus per kg saved 2 min/kg
05 min10 min
Type IV — Modified PET (Meyer HDRX)
2.0kg
Type III (Al-lined)
3.6kg
Type I (all-metal)
6.7kg
Burst pressure 1050 bar
Gravimetric H₂ % 8.2 %
PV/W performance 36.4 km
Stored gas mass 163 g
Mass saving vs Type III: 1.6 kg (45%)
Mass saving vs all-metal: 4.7 kg (70%)
For a UAV: extra flight time vs Type III ≈ 3.2 min

NoteThese are conservative estimates based on a representative carbon-fibre layup. Real cylinders are often lighter — switching to higher-tensile-strength fibre (T800, T1000, IM-class) typically saves 10–25% on composite mass, and optimised dome geometry can save more. The numbers shown are a sensible baseline, not a ceiling. For a specification-accurate mass — including your fibre choice, dome shape, and qualification target — request a custom quote.

What the numbers mean

Burst pressure

Burst pressure = working pressure × safety factor. ISO 11119-3 sets the minimum burst ratio at 2.25× working for Type IV cylinders. Aerospace and space programmes typically specify higher safety factors — 2.5× to 3.5× — to give qualification headroom. Higher safety factor means more composite, which means more mass.

PV/W performance factor

PV/W is a single number that captures how efficiently a cylinder uses its mass to store pressurised gas. It’s calculated as (burst pressure × volume) / (cylinder mass), expressed in metres of altitude equivalent. For Type IV COPVs, industry-typical values are 25–35 km. Meyer HDRX cylinders run at 35–40 km — among the highest performance factors in production.

Gravimetric efficiency

Gravimetric efficiency = (mass of gas stored at working pressure) / (cylinder mass + gas mass), expressed as a percentage. For hydrogen UAV applications, 7–14% is typical depending on working pressure and cylinder design. The number is dominated by gas density at the working pressure, so it rises sharply with pressure.

How the saving translates

Mass on a moving platform is never just mass. It’s flight time, payload, range, or fuel consumption.

  • Hydrogen UAV (5–25 kg gross): ~2–3 minutes of additional flight time per kg saved on the airframe
  • CubeSat propulsion module: every gram saved on the propellant tank can be re-allocated to payload or fuel
  • Microlauncher upper stage: 1 kg saved on the upper stage ≈ 1 kg additional payload to orbit
  • SCBA / breathing apparatus: wearer fatigue scales with load; even 1–2 kg saved per cylinder makes a daily-use difference

Need a more precise estimate?

This calculator gives directional figures based on typical construction. For a real cylinder mass to a real specification — including your exact volume, pressure, materials, fittings, and qualification target — request a custom quote. Detailed enquiries are routed through our engineering team; turnaround depends on the depth of calculation and modelling required, and we will share an indicative timeline when we acknowledge your request.

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