ORBITALLow-Earth orbit computing

Hardware

An object that powers on
once and never shuts down.

There are no technicians in orbit. Every design decision answers a single question: what happens if this fails and no one can touch it for fourteen years?

Orbital computing node against a black background, with machined cooling fins and a gold thermal blanket.

ORB-N4

Four subsystems.
No critical moving parts.

The aluminum 7075 chassis is machined from a single piece and serves as structure, shielding, and heat sink. The electronics are triplicated with majority voting: a radiation strike that corrupts one core is discarded before it can propagate.

Compute
1.2 PFLOP FP8
Memory
2 TB HBM3e ECC
Storage
96 TB shielded NAND
Peak power
19.2 kW
Dry mass
840 kg
Tolerance
60 krad (Si)
Thermal range
−40 °C to +65 °C
Design life
14 years
Close-up of an orbital node's gold-foil radiator wing in direct sunlight.
Radiator wing · 18-layer MLIThe foil is not decorative: it reflects 96% of incident solar radiation and emits heat from the core into the vacuum.

Thermal control

Cooling without air
or water.

There is no convection in a vacuum. The only way heat can escape is through infrared radiation — which means redesigning the problem from first principles.

01 / Capture

Vapor chambers

Heat from the core travels through phase change to the base of the radiators. No pumps: capillary action sustains the cycle.

18kW transferred
02 / Emission

Deployable radiators

Two 22 m² wings with high-emissivity coatings unfold after separation from the launch vehicle and never move again.

44m² of emitting area
03 / Management

Sun-synchronized workloads

The scheduler knows the ephemerides: heavy workloads run during illuminated phases and migrate to another node before each eclipse.

0jobs lost in 12 months
Two cleanroom-suited engineers beside an orbital computing module in its assembly fixture.

Integration

ISO 5 cleanroom.
Eleven weeks per node.

Each module undergoes thermal-vacuum cycling, random vibration, and pyrotechnic shock before receiving flight clearance. No node leaves the building without surviving a simulated launch.

Thermal vacuum
8 cycles · 96 h
Vibration
14.1 g RMS
Shock
2,000 g · 1 kHz
Acceptance
1,412 points

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