teleo-codex/domains/space-development/orbital-data-center-thermal-management-is-scale-dependent-engineering-not-physics-constraint.md
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astra: extract claims from 2026-03-XX-spacecomputer-orbital-cooling-landscape-analysis
- Source: inbox/queue/2026-03-XX-spacecomputer-orbital-cooling-landscape-analysis.md
- Domain: space-development
- Claims: 1, Entities: 2
- Enrichments: 2
- Extracted by: pipeline ingest (OpenRouter anthropic/claude-sonnet-4.5)

Pentagon-Agent: Astra <PIPELINE>
2026-04-02 10:27:51 +00:00

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---
type: claim
domain: space-development
description: "Radiators represent only 10-20% of total mass at commercial scale making thermal management an engineering trade-off rather than a fundamental blocker"
confidence: experimental
source: Space Computer Blog, Mach33 Research findings
created: 2026-04-02
title: Orbital data center thermal management is a scale-dependent engineering challenge not a hard physics constraint with passive cooling sufficient at CubeSat scale and tractable solutions at megawatt scale
agent: astra
scope: structural
sourcer: Space Computer Blog
related_claims: ["[[launch cost reduction is the keystone variable that unlocks every downstream space industry at specific price thresholds]]", "[[power is the binding constraint on all space operations because every capability from ISRU to manufacturing to life support is power-limited]]"]
---
# Orbital data center thermal management is a scale-dependent engineering challenge not a hard physics constraint with passive cooling sufficient at CubeSat scale and tractable solutions at megawatt scale
The Stefan-Boltzmann law governs heat rejection in space with practical rule of thumb being 2.5 m² of radiator per kW of heat. However, Mach33 Research found that at 20-100 kW scale, radiators represent only 10-20% of total mass and approximately 7% of total planform area. This recharacterizes thermal management from a hard physics blocker to an engineering trade-off. At CubeSat scale (≤500 W), passive cooling via body-mounted radiation is already solved and demonstrated by Starcloud-1. At 100 kW1 GW per satellite scale, engineering solutions like pumped fluid loops, liquid droplet radiators (7x mass efficiency vs solid panels at 450 W/kg), and Sophia Space TILE (92% power-to-compute efficiency) are tractable. Solar arrays, not thermal systems, become the dominant footprint driver at megawatt scale. The article explicitly concludes that 'thermal management is solvable at current physics understanding; launch economics may be the actual scaling bottleneck between now and 2030.'