MEYER develops custom Type IV composite pressure vessels and HDRX-derived regulators for aerospace, UAV, CubeSat, and bespoke industrial applications. Programme runs from concept review through qualification to production, with a single named engineer-of-record from kick-off to first delivery.

When custom development is the right call

Most cylinder applications fit a stock HDRX product from the 36-cylinder catalog. Custom development is worth the engineering investment when one or more of the following hold:

  • Volume / pressure / mass envelope doesn’t match a stock unit
  • Conformal geometry needed (non-cylindrical, multi-cell, or fitted to airframe cross-section)
  • Programme-specific qualification required (NASA-STD-6016, ECSS-E-ST-32-02C, MIL-STD-810H, customer PPAP)
  • Specific gas service outside the standard catalog (xenon, LH₂-adjacent cryo-cycled, oxygen-cleaned)
  • Co-developed cylinder + regulator for tight integration where catalogue parts compromise mass or volume
  • Production scale outside the catalogue’s stock-supply assumptions (single qualified flight unit; or 100+ identical units to a flight programme)

For everything else, a stock HDRX cylinder is faster, cheaper, and lower-risk. Run the COPV Selector first; if a stock unit fits, that’s the answer.

How a development programme runs

1. Architecture review (1–2 weeks)

Initial conversation captures the system: cylinder volume + working pressure, gas, regulator outlet spec, mass budget, envelope, mission profile, qualification target. Output: a written design brief that captures all constraints together. This step is no-charge under standard NDA and committs you to nothing.

2. Concept design (4–6 weeks)

Notional cylinder geometry, regulator architecture (if applicable), boss design, fibre layup, and qualification scope. Mass and burst-pressure estimates from analytical and FE models. Envelope drawing for your CAD assembly. Indicative cost and lead time. You decide go / no-go at this gate.

3. Detailed design (3–5 months)

Full mechanical design: cylinder mandrel geometry, winding schedule, boss machining, regulator body, integration interfaces. FE analysis with margin-of-safety reports. Materials selection with traceability path. Manufacturing process documentation. Output: design dossier ready for prototype build and notified-body design review.

4. Prototype build & integration test (3–4 months)

First articles produced on the production line. Integration testing in MEYER’s lab — proof, leak, vibration, temperature cycling — before customer delivery. First articles ship for your in-house integration test.

5. Qualification campaign (8–14 months for full aerospace scope)

Full ISO 11119-3 / EN 12245 / EN 17339 / programme-specific qualification: burst, hydrostatic cycling, ambient + extreme temperature cycling, drop, fire, gunfire, permeation, sustained-load. Notified-body design review and certificate issue. Indicative cost and timeline detail here.

6. Production

Stock or programme-specific production lots. Same engineer-of-record who designed the cylinder. Documentation pack ships with each lot.

Typical programme economics

  • Total programme: 12–24 months from spec freeze to production-ready
  • Qualification cost band: €130K–310K for a single design (full ISO 11119-3 path; equivalence-based qualification can reduce to €60–100K if a sister design exists)
  • Tooling investment: €15–40K one-off, amortised across the production run
  • Per-unit cost: dominated by qualification + tooling amortisation at low volumes; marginal cost dominates at 100+ units

For programmes that flex spec to fit a stock cylinder where possible: use the Selector first. The fastest answer is “we have it on the shelf.”

Co-development of cylinder + regulator

For applications where dimensions and mass are critical, MEYER recommends developing the cylinder and the regulator together rather than specifying them independently. Detail: Develop COPV and Regulator Together — When Bespoke Beats Catalogue.

What to bring to the architecture review

  • Required gas mass at working pressure (or working pressure + volume)
  • Maximum cylinder envelope (diameter and length)
  • Mass budget for the cylinder (or system mass budget if integrating cylinder + regulator)
  • Cycle-life requirement
  • Operating temperature range
  • Qualification target (TPED / PED / ISO 11119-3 / programme-specific)
  • Production-volume estimate (1 prototype, 10 flight units, 100+ programme run)
  • Required first-unit date

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