Asteroid Electromagnetic Rotary Launcher Model
Underwrite tethered carbon-nanotube centrifugal sling launchers anchored to near-Earth asteroids (flinging refined ore canisters toward lunar orbit at 3 km/s with zero rocket fuel). Model orbital payload delivery tariffs ($850/kg), and 20-yr IRR.
1. Capacity & Unit Economics
2. Financial Returns & Yield
ZERO-FUEL CENTRIFUGAL SLINGAnnual Net EBITDA
$0 / yr
20-Yr Project IRR
0.0%
Gross Revenue
$0 / yr
Total CapEx
$0
Annual OpEx
$0 / yr