Orbital Environment
CONFIG-01
Orbital Altitude
550 km
Solar Flux & Albedo
1361 W/m²
Beta Angle (β)
90°
Compute Workload & Power
NVL72-TDP
Radiator Surface Area (Deployable Wings)
145 m²
Optical Inter-Satellite Link (OISL)
800 Gbps
SPACEX STARMIND VACUUM-SEALED CHASSIS
36 Vera Tray Slices · 72 Rubin Die Blocks · NVLink 5 Vacuum Bus · Loop Heat Pipes
Tensor Performance
3,600 PFLOPS
3.60 EFLOPS FP4 Tensor Core
GPU Junction Temp
64.2 °C
Margin: +10.8°C to Throttling
Electrical Bus Draw
102.4 kW
Array Mass: 485 kg (GaAs Multi-Junc)
Constellation Mesh
18.4 ms
Token Sync @ 800 Gbps Laser Link
Stefan-Boltzmann Thermal Equilibrium vs Orbital Arc
Q_in: 112.5 kW · Q_rad: 112.5 kW @ 318 K
Mass & Launch Integration
STARSHIP / F9| Subsystem Element | Qty / Specs | Mass (kg) |
|---|---|---|
| Nvidia Rubin GPUs (BGA modules) | 72 units (Dual-die) | 288 kg |
| Nvidia Vera CPUs & Grace V2 Trays | 36 modular trays | 324 kg |
| SpaceX Carbon-Ti Isogrid Rack | 1.8m × 0.8m × 2.4m | 185 kg |
| Two-Phase Pumped Loop Heat Pipes | Ammonia / Cu-Ni microchannels | 165 kg |
| Deployable Carbon-Composite Radiators | 145 m² Dual Wing | 362 kg |
| UltraFlex Solar Array + GaN Regulators | 128 kW BOL | 512 kg |
| OISL Transceivers (Laser Crosslinks) | 4× Quad-axis Optical heads | 48 kg |
| Total Starmind Orbital Payload Wet Mass | Ready for Integration | 1,884 kg |
Falcon 9 vs Starship Fairing Allocation:
Falcon 9 payload margin: 82.4% available (Single satellite per dedicated launch). Starship payload volume can house up to 24 modular Starmind NVL72 satellites per launch (86.4 EFLOPS orbital cluster).