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Your design summary is emailed to you and to ATS engineering. Registration is required to access the tool.
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How would you like to use the tool?
Choose the path that matches how much you know about your requirement.
Either path ends with a design summary emailed to you and to ATS engineering at [email protected]. All results are first-order sizing; final performance is confirmed by ATS characterisation.
Quick sizing
Answer these and the engine will figure out the rest.
Heat source
The die, module, or contact footprint that touches the vapor chamber evaporator.
Envelope material
Shell alloy sets conductivity, allowable stress, and — critically — fluid compatibility.
Emissivity used for radiation from exposed faces.
Mixed metals inside a sealed chamber invite galvanic attack.
Chamber geometry & wick
Overall envelope, internal stack-up, and capillary structure.
Working fluid & operating window
Fluid choice is constrained by shell compatibility and by the saturation pressure at both ends of your temperature range.
Charge purity and non-condensable gas control dominate real-world performance; only reagent-grade fluid with a bake-out and evacuation below 10⁻³ mbar should be used.
Copper/water is the reference two-phase pair with >20-year proven life. Practical window 25 to 250 °C; freezes at 0 °C. At 70 °C the saturation pressure is 30.8 kPa and the figure of merit is 3.61×10¹¹ W/m². Required purity: reagent grade, <1 ppm ionic, degassed.
Condenser & heat rejection
Where the vapor gives up its latent heat, and what carries it away.
Bare-chamber convection
Design constraints
The engine will not exceed these when it proposes a correction.
Design result
iVaporChamber™ is a first-order sizing engine intended for concept selection and specification. Predictions assume a properly evacuated, correctly charged, non-condensable-gas-free chamber built to the stated internal geometry. Final performance must be confirmed by ATS thermal characterization. © Advanced Thermal Solutions, Inc. — [email protected] — 1-781-769-2800