Cislunar Water Ice Solar Electrolysis LOX/LH2 Tug Model
Underwrite lunar polar water electrolysis plants splitting melted permafrost ice into liquid hydrogen and oxygen propellant to fuel reusable cislunar orbit-to-surface shuttles (displacing $10,000/kg Earth launch propellant costs). Model in-space propellant off-take ($850/kg LOX/LH2), and 20-yr IRR.
1. Capacity & Unit Economics
2. Financial Returns & Yield
$850/KG IN-SPACE PROPELLANTAnnual Net EBITDA
$0 / yr
20-Yr Project IRR
0.0%
Gross Revenue
$0 / yr
Total CapEx
$0
Annual OpEx
$0 / yr