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STELLAROrbital computing
STELLAR technology / The physics of orbital data centers

Thermal & Power

Compute in orbit only works when power generation, heat rejection, radiator area, duty cycles, and safe modes are designed as one system.
Waste heat
Primary variable
Duty cycle
Control
Throttle
Safety mode
The physics of orbital data centers/ visual
Spacecraft solar power and thermal radiator panel
Thermal + Power
01 / design principle

The operating principle

STELLAR treats thermal and power limits as first-order product constraints, not afterthoughts. The workload model must obey the spacecraft.

Principle 1

Solar power windows

Payload scheduling follows generation, eclipse behavior, battery state, and mission reserve rules.
Principle 2

Radiator heat rejection

Compute output is translated into heat paths, radiator sizing, and throttle boundaries.
Principle 3

Safe-mode behavior

The system degrades predictably when thermal or power margins narrow.

See how this system advances across missions

STELLAR technology is not presented as a one-off feature list. Every subsystem maps to a mission gate and a harder infrastructure capability.