SpaceX × NVIDIA

Orbital Vera Rubin NVL72 Space Compute Simulator

STABLE
Mission Preset Architecture
Thermal & Power Geometry
1 Rack
148.4 m²
65.0 °C
550 km
150 kWh
100 %
Orbital Vacuum Heat-Dissipation Schematic 1361 W/m² Solar Flux
Orbital Period Position (0 to 95.6 min) 100% Sunlight (No Umbra)
90-Minute Thermal & Battery Telemetry Profile
Thermal Equilibrium & AI Throughput
Net Equilibrium Temp
54.2 °C
Required Radiator Area
148.4 m²
Peak Solar Generation
180.2 kW
Orbital FP8 Compute
288 PFLOPS
Physics & Orbit Telemetry Proof
Stefan-Boltzmann Rejection ($P_{rad}$):125.0 kW
Earth Albedo & IR Influx:14.8 kW
Eclipse Depth Per Orbit:0.0 min
Min Battery Depth-of-Discharge:0.0% (Safe)
Radiator Emissivity ($\epsilon$):0.92 Dual-Sided
Export Trade-Study Spec

    
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