Scalable microsatellite constellation for clearing near-Earth orbit of space debris.
Cluster launch · Carbon nets · Controlled deorbit.
Megaconstellations are increasing orbital density 10× in five years. A chain of collisions could render entire orbital bands permanently unusable.
30 × 6U CubeSats (12 kg each) on a single Falcon 9 rideshare, operating as a coordinated autonomous swarm at 400–500 km.
30 CubeSats on one dispenser — dramatically lower per-unit cost.
FPGA AI tracks debris via optical camera. NORAD catalog targeting.
Self-tightening graphite composite net. Tensile strength >3 GPa.
3–5 m² aluminized sail. Deorbit in weeks at 400–500 km. Full burnup.
Competitors remove one large object per mission at $50–90M. We target 30 per mission at a fundamentally different cost structure.
Pre-seed projections pending independent validation. Mission targets 400–500 km.
OrbitalNet is at pre-seed stage. If you believe orbital debris is the defining engineering challenge of this decade — let's talk.
CubeSat systems, net deployment, drag sail, onboard AI. Smallsat (6U) experience essential.
Deorbit modeling, target selection, swarm coordination at 400–500 km.
Carbon composite net design, deployment mechanism, hypervelocity testing.
Part-time. Navigate ESA / NASA relationships, grant programs, validate concept.
Pre-seed round + pipeline. Targets: Starlink, OneWeb, Kuiper + space agencies.
Business development, investor relations, regulatory strategy, team assembly.
Co-founder, advisor, investor, or just convinced this problem matters — write to us.
Domain: orbitalnet.co · orbitalnet.ru — registration in progress