🛰️ Propellantless LEO Orbit Raising & De-Orbiting

Electrodynamic Tether Propellantless Space Tug Model

Underwrite 10km conductive bare electrodynamic tether (EDT) space tugs utilizing Earth’s magnetic field and ionospheric plasma for zero-fuel orbital inclination changes and satellite orbit raising ($2.2M/transfer). Model commercial fleet EBITDA.

1. Capacity & Unit Economics

Annual Satellite Transfers Completed (Missions / Yr)

Orbital Transfer Contract Fee ($M / Mission)

Ground Telemetry & Flight Dynamics OpEx ($M / Yr)

3-Tug Fleet & Deployable Tether CapEx ($M)

2. Financial Returns & Yield

PROPELLANTLESS LEO TUG

Annual Net EBITDA

$0 / yr

Unlevered Cap Rate

0.0%

Gross Revenue

$0 / yr

Total CapEx

Annual OpEx

$0 / yr