⚛️ Magneto-Inertial Deep Space Propulsion

Pulsed Fission-Fusion Propulsion Engine Model

Underwrite magnetochemically compressed pulsed fission-fusion nuclear propulsion stages (specific impulse Isp = 5,000s, enabling 45-day Mars transits). Model government & commercial outer-planet payload missions ($150M/mission), and project EBITDA.

1. Capacity & Unit Economics

Annual Deep Space Missions Flown (Missions / Yr)

Deep Space Mission Charter Contract ($M / Mission)

Pellet Fuel & Launch Ops OpEx ($M / Mission)

Magnetic Nozzle & Engine Stage CapEx ($M)

2. Financial Returns & Yield

ISP=5,000s DEEP SPACE

Annual Net EBITDA

$0 / yr

15-Yr Project IRR

0.0%

Gross Revenue

$0 / yr

Total CapEx

Annual OpEx

$0 / yr