Is It Really Impossible To Cool A Datacenter In Space?

Scott Manley
Scott ManleyMar 18, 2026

Why It Matters

Effective thermal management makes orbital data centers viable, opening new revenue streams for satellite operators while highlighting the engineering limits of space‑based computing.

Key Takeaways

  • Space cooling relies solely on thermal radiation, not convection.
  • 20 kW of GPU heat needs ~23 m² radiators at 80 °C.
  • Sun and Earth albedo add ~8 kW to thermal load in LEO.
  • Radiator emissivity and orientation critically affect temperature balance.
  • Proper shading and angle control can keep a space data center viable.

Summary

Scott Manley examines whether a data center can be cooled in space using only radiation. He models a Starlink V3 satellite that dissipates roughly 20 kW of GPU power and shows that, under Stefan‑Boltzmann physics, a flat radiator operating at about 80 °C would need roughly 23 m² of surface to reject that heat.

The analysis incorporates emissivity (≈0.8), solar flux (≈1356 W/m²) and Earth albedo/thermal emission (~400 W/m² in low‑Earth orbit). Adding the ~8 kW extra load from Earth radiation raises total dissipation to ~28 kW, still below the ~34 kW radiated at 80 °C, leaving a margin that can be trimmed by lowering radiator temperature or improving shading.

Manley highlights that orientation matters: edge‑on positioning to the Sun and using low‑absorptivity coatings can reduce solar gain, while high‑emissivity surfaces boost radiative loss. He notes that a two‑sided panel at 120 °C would reach equilibrium with solar input, but practical designs must stay below component limits, typically around 65‑80 °C.

The takeaway is that space‑based cooling is not impossible, but it demands precise thermal control, adequate radiator area, and careful attitude management. Successful implementation could enable orbital data‑center services, but engineering margins are tight and any mis‑alignment could quickly overload the thermal budget.

Original Description

Let's actually explain how thermal balance of spacecraft works, and how we'd need to configure a spacecraft to eliminated the heat that's produced by computer equipment crunching numbers in a space data center.
This is all very rough, and I overestimated the size of the starlink V3, but it's still in the ballpark. Real designers of course can't just use 'in the ballpark'.
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