A 140 kWe / 140 kWth rack is a heat problem before it's a compute problem. Here's what it takes to remove that heat with a transcritical CO2 loop alone, how far the rack's own waste heat gets you with an ejector chiller, and what happens when you fold in the waste heat from the natural-gas generation that powers the rack in the first place.
AMD's Helios rack-scale platform — the double-wide chassis built around 72 Instinct MI455X accelerators — lands at roughly 140 kW of rack-level power draw. In a liquid-cooled AI rack, essentially all of that electrical input leaves as heat, so the thermal design point is the same number: 140 kWth of waste heat that has to go somewhere. The three questions below walk through three different ways of getting rid of it, using published performance data for each technology class rather than nameplate marketing numbers.
A transcritical CO2 (R744) chiller compresses the refrigerant above its critical point (31.1°C / 73.8 bar) and rejects heat through a gas cooler rather than a condenser. For data center duty with direct-to-chip liquid cooling — where the loop runs warm (typically 25–45°C supply) — CO2 systems perform well because the elevated evaporating temperature favors the cycle. Published COPs for transcritical CO2 data center cooling range from about 3.5 in hot, above-critical ambient conditions up to 5–7+ in favorable climates or with gas-cooler enhancements like adiabatic/evaporative assist.
| Operating condition | Assumed COP | Electrical power required |
|---|---|---|
| Hot ambient, transcritical mode (conservative) | 3.5 | 40.0 kW |
| Design point — moderate climate, warm-water loop | 4.5 | 31.1 kW |
| Favorable ambient, optimized gas cooler | 5.5 | 25.5 kW |
| Best-case, enhanced/subcritical-assisted cycle | 7.2 | 19.4 kW |
~31 kWe at the design point — call it 22% of the rack's own power draw as a mechanical-cooling "tax." That's a reasonable, literature-consistent estimate for a warm-water, direct-to-chip CO2 loop; it gets meaningfully better with a well-designed gas cooler and worse on a hot day with no evaporative assist.
An ejector cooling cycle uses a nozzle and a heat-driven "generator" instead of a mechanical compressor: waste heat boils a working fluid, the resulting high-velocity vapor jet entrains and compresses low-pressure vapor from the evaporator, and cooling is produced without electrical compression work. The tradeoff is a much lower coefficient of performance than a compressor-driven cycle — typically 0.2–0.5 depending on the generator (driving) temperature, condensing conditions, and working fluid. Ejector cycles are known to run effectively off relatively low-grade heat, around 60–80°C, which lines up well with a rack's warm liquid-cooling return.
| Ejector thermal COP | Cooling from 140 kWth waste heat |
|---|---|
| 0.30 (conservative, low-grade source) | 42.0 kW |
| 0.35 (design point) | 49.0 kW |
| 0.40 | 56.0 kW |
| 0.50 (enhanced cycle / better fluid pairing) | 70.0 kW |
~49–56 kW of cooling from the rack's own reject heat at a design-point COP of 0.35–0.4. That's meaningful — on the order of a third to 40% of the 140 kW cooling demand — but on its own, the rack's waste heat isn't hot enough or plentiful enough to fully self-cool. It needs a second heat source. That's where the gas-fired mesh comes in.
At 25 kWe per cell, powering a 140 kWe Helios stack requires 6 cells (140 ÷ 25 = 5.6, rounded up), for 150 kWe of installed capacity — about 7% headroom over the load, which is a sensible margin rather than a redundant spare.
Small natural-gas gensets/microturbines in this size class typically run 25–30% electrical efficiency, with exhaust temperatures in the 500–600°C range and total (electrical + recovered thermal) CHP efficiencies commonly cited at 60–85%. Using a representative 25% electrical efficiency and ~50% recoverable thermal efficiency (consistent with published CHP fact sheets, leaving ~25% as unavoidable stack/radiation loss):
| Per cell | 6-cell mesh | |
|---|---|---|
| Electrical output | 25 kWe | 150 kWe |
| Fuel input (LHV, at 25% elec. eff.) | 100 kW | 600 kW |
| Recoverable waste heat (~50% of fuel) | 50 kWth | 300 kWth |
The gas mesh throws off roughly 300 kWth of recoverable exhaust/jacket heat — more than double the Helios stack's own 140 kWth, and at a notably higher temperature (raw exhaust in the hundreds of °C vs. a ~45–65°C liquid-cooling return), because it's coming straight off high-temperature exhaust rather than a warm chip-cooling loop.
Because the gas-mesh heat is higher grade, it can drive an ejector stage at a better COP (~0.55) than the lower-grade rack waste heat (~0.35). Cascading both streams through a CO2 ejector cooling system:
| Heat source | Available heat | Ejector COP | Cooling produced |
|---|---|---|---|
| AMD Helios stack (liquid-cooling return, ~45–65°C) | 140 kWth | 0.35 | 49.0 kW |
| Gas cluster mesh (recovered exhaust heat) | 300 kWth | 0.55 | 165.0 kW |
| Combined | 440 kWth | — | 214.0 kW |
~214 kW of additional cooling capacity from the combined ejector cascade — a surplus of about 74 kW over the 140 kW the Helios stack actually needs to reject. In practice, that means the two-stream ejector system alone can plausibly cover the entire cooling load thermally, turning the transcritical CO2 compressor loop from the primary cooling system into a trim/backup unit for humidity control and off-design conditions, rather than the ~31 kWe workhorse it would otherwise need to be.