Rotating Detonation Wave Rocket Engine (RDRE) Model
Underwrite 100kN continuous rotating detonation wave rocket engines (RDRE) replacing traditional deflagration combustion chambers with supersonic shock-wave detonations (delivering a 15% boost in specific impulse and 40% reduction in engine mass for orbital upper stages). Model aerospace propulsion supply contracts ($24M/engine), equipment payback.
1. Capacity & Unit Economics
2. Financial Returns & Yield
15% ISP BOOST PRESSURE-GAIN COMBUSTIONNet Operating Income (NOI)
$0 / yr
Unlevered Cap Rate
0.0%
Gross Revenue
$0 / yr
Total CapEx
$0
Annual OpEx
$0 / yr