100 kW milestone
Hit the FCC filing's per-satellite reference: average compute power ≥ 80 kW sustained across eclipses.
- Design power ≥ 100 kW
- Avg delivered power ≥ 80 kW
- Eclipse fraction ≤ 25%
OrbitalForge / missions
Each mission is a set of physics-anchored targets your design has to hit. Completing all targets applies a reward multiplier to your score. Browse by theme — every category maps to a real piece of the multi-planetary roadmap.
Specific power, SBSP precursors, gigawatt pathfinders.
Hit the FCC filing's per-satellite reference: average compute power ≥ 80 kW sustained across eclipses.
Break 280 W/kg specific power (NASA SBSP advanced-array target is 300 W/kg) while delivering real avg power.
Best-in-class avg delivered power in the 500 km sun-sync slot where most Earth-observation constellations live. Reach 70 kW average without leaving the band.
TERAFAB-class building block. Sustain ≥80 kW average delivered power inside the SBSP-friendly 800–1200 km sun-sync band where lighting is most predictable.
High power, high density, in-envelope. Do all three at once.
Master challenge. Specific power at the NASA SBSP target, near-peak average power, altitude inside the main shell. Very few designs satisfy all four at once.
First step toward gigawatt-class space industry. Hold ≥ 200 kW average delivered power per spacecraft with the SBSP-class specific-power target — the configuration TERAFAB-scale operators will want to multiply by thousands.
Push the array close to the SBSP 300 W/kg target while running real compute. The demo case for an SBSP precursor: high specific power and high efficiency in the same bird.
Direct precursor to space-based solar power: meet the NASA SBSP 2024 advanced-array target of 300 W/kg with high cell efficiency, in the canonical SBSP altitude shell.