Rotating Momentum-Exchange Orbital Sling Catcher Model
Underwrite 100km rotating high-tensile carbon nanotube tethers in LEO catching suborbital rockets and slinging payloads to Geostationary Transfer Orbit (GTO) with zero propellant expenditure. Model satellite injection velocity boost fees ($2.8M/payload), and 20-yr IRR.
1. Capacity & Unit Economics
2. Financial Returns & Yield
PROPELLANT-FREE ORBITAL BOOSTINGNet Operating Income (NOI)
$0 / yr
Unlevered Cap Rate
0.0%
Gross Revenue
$0 / yr
Total CapEx
$0
Annual OpEx
$0 / yr