Hypersonic Inflatable Aerodynamic Decelerator Model
Underwrite 12-meter deployable inflatable braided silicon-carbide aerodynamic heat shields decelerating 20-tonne payload landers through Mars and Earth upper atmospheres at Mach 25 (enabling high-mass landing with standard rocket fairing constraints). Model planetary cargo landing fees ($28M/flight), and 15-yr IRR.
1. Capacity & Unit Economics
2. Financial Returns & Yield
20-TONNE MACH 25 ATMOSPHERIC BRAKINGAnnual Net EBITDA
$0 / yr
15-Yr Project IRR
0.0%
Gross Revenue
$0 / yr
Total CapEx
$0
Annual OpEx
$0 / yr