⚡ -20% Supersonic Wave Drag via Nanosecond Plasma Jets

Nanosecond DBD Plasma Aerodynamic Actuator Model

Underwrite 100 kHz nanosecond pulsed Dielectric Barrier Discharge (DBD) plasma actuator arrays installed on supersonic aircraft noses (ionizing air to deflect oblique shockwaves and reduce aerodynamic wave drag by 20%). Model avionics retrofit suite sales ($4.8M/aircraft), and 15-yr IRR.

1. Capacity & Unit Economics

Annual Aircraft Plasma Suites Sold (Suites / Yr)

Plasma Drag Reduction System Price ($M / Suite)

Nanosecond High-Voltage Pulser & Dielectric OpEx ($M)

Automated Electrode Fab & Wind Tunnel Test CapEx ($M)

2. Financial Returns & Yield

-20% SUPERSONIC SHOCKWAVE DRAG

Annual Net EBITDA

$0 / yr

15-Yr Project IRR

0.0%

Gross Revenue

$0 / yr

Total CapEx

Annual OpEx

$0 / yr