Constellation Parameters SPACEX 1M
Thermal & Power Subsystems STEFAN-BOLTZMANN
THERMAL DESIGN NOTE: Vacuum cooling is purely radiative ($P = \epsilon \sigma A T^4$). High compute power density requires massive double-sided deployable radiators or elevated coolant loops.
Astrodynamics & Power REAL-TIME TELEMETRY
Orbital Period
95.6 min
7.59 km/s velocity
Eclipse Time
35.8 min
37.4% orbit shadow
Radiator Area / Sat
35.7 m²
700 W/m² rejection
Solar Array Sizing
91.2 m²
39.9 kW gen daylight
Battery Capacity Req.
14.9 kWh
at 80% max DoD
ISL Inter-Sat Latency
4.3 ms
Adjacent node hop @ c
Aggregate Constellation Fleet AI CAPACITY
Constellation ExaFLOPs
1,250.0 EF
FP8 Matrix Tensor Core
Total Fleet Power
25.0 GW
Continuous Orbital Load
• Stefan-Boltzmann: P_rad = ε·σ·A·(T_rad⁴ - T_space⁴)
• Kepler III: T = 2π √(r³ / μ) | μ = 3.986e14 m³/s²
• Laser Mesh: c = 299,792 km/s vacuum optical hop
• Kepler III: T = 2π √(r³ / μ) | μ = 3.986e14 m³/s²
• Laser Mesh: c = 299,792 km/s vacuum optical hop