Every unit is the output of an NSGA-II multi-objective optimisation on your exact duty, not an off-the-shelf product. Delivered with a full thermo-hydraulic report.

Patented TRL 5 · 5 prototypes tested Flagship: MST-Q150M50

Modular Shell & Tube Platform

Section-wise parameterisation: (N_t, D_o, P_t, t_w, material) tuned independently per section. Welded partitions eliminate inter-section bypass. Rectangular envelope removes cylindrical dead volume. Result vs TEMA: −50% ΔP, −37% mass, +10 pts effectiveness at iso-duty.

Central hot plenum S0 → symmetric S1–S4 bundles each side
Ultra-thin tubes 0.08–0.15 mm wall · laser-welded or brazed
Inconel/310S hot sections · SS 304/carbon cold sections
Zero shell-side bypass, welded partitions, not baffles
Envelope: 499 × 178 × 689 mm · β ≈ 245 m²/m³
Customisable: per-duty NSGA-II re-run, proposal in 10 working days

85.1%

Effectiveness ε (MST-Q150M50)

157.9 kW

Thermal duty · air-to-air

34.4 mbar

Shell-side ΔP (vs ~55 mbar reference)

NTU 5.71

Balanced counter-flow

Metal SLM/EBM Patented winglet fin Two flagship models

3D-Printed Additive Line

Patented winglet-offset fin architecture, topology-optimised, flow-adaptive, enabled by metal additive manufacturing and impractical to stamp or braze. Printed as a monolithic core in 310S, 309 or Inconel. Demonstrated pressure-drop reductions are reported against the defined reference geometry. Fewer joints reduce potential leak paths.

TITAN-X93

Peak effectiveness

93% · 50 kg · 850 °C · 1000 kg/h · Inconel/310S

AGILE-L85

Mass-optimised

85% · 23 kg · 850 °C · 1000 kg/h · 310S/309

93%

Peak effectiveness (TITAN-X93)

23 kg

Lightest flagship (AGILE-L85)

−40%

Mass vs conventional plate-fin

850 °C

Nominal hot-side inlet

Engineering Services

Thermal design · CFD k-ω SST · thermo-mechanical FEA · NSGA-II optimisation · robotic laser welding · bench testing at 950 °C / 9 bar · full thermo-hydraulic report.

Working days
design proposal

12–16

Weeks to
prototype

→

Calculation software