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Vapor Chamber Design Tool

iVaporChamber™ Design — Advanced Thermal Solutions

iVaporChamber™ Design

Size and validate a sealed two-phase vapor chamber against the five classical heat-pipe transport limits, the internal thermal network, and pressure-vessel requirements. Enter your heat source and boundary conditions; the engine returns a buildable configuration, flags anything in your request that will not work, and shows exactly what it changed.

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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.
Chamber plus heat sink. Leave at 0 for no limit.
Leave at 0 for no limit.

Heat source

The die, module, or contact footprint that touches the vapor chamber evaporator.
Steady state is sized at 100%.
Peak ÷ steady power.

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.
Internal stack-up
Sets bending span of the flat walls.

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.
Start-up / cold soak.
Vapor temperature ceiling.
Freeze / thaw check.
Use 250 °C if the chamber passes through solder reflow.
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.
Fraction of the opposite face that is actively cooled.
Derates air density.
Liquid cold plate
Convective resistance, K/W per 100 cm² of plate.
Plate-fin heat sink
Forced convection is evaluated with the Teertstra–Yovanovich–Culham composite model for developing flow between parallel plates; natural convection uses Elenbaas channel theory plus radiation.
Bare-chamber convection
0 = still air, natural convection only.
Direct entry
From the condenser face to the coolant or ambient reference temperature.

Design constraints

The engine will not exceed these when it proposes a correction.
Required ratio of the governing transport limit to applied power. ATS default 1.5.
Blocked condenser area reserved for end-of-life NCG.
0 = no limit.

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