🚀 Mach 10 200 MPa High-Enthalpy Free-Piston Shock Tunnel

Mach 10 Free-Piston Hypersonic Shock Tunnel Model

Underwrite 100-meter long free-piston driven shock expansion tunnels compressing helium gas to 200 MPa (generating true-temperature Mach 10 scramjet inflow and boundary-layer laminar-turbulent transition test conditions for 5 milliseconds). Model aerospace hypersonic flight test charters ($180k/shot), and equipment payback.

1. Capacity & Unit Economics

Hypersonic Shock Tunnels Operated (Facilities)

Annual Hypersonic Test Shots / Tunnel (Shots / Yr)

Hypersonic Test Shot Charter Fee ($k / Shot)

Turnkey 100m Free-Piston Expansion Tube CapEx ($M / Unit)

2. Financial Returns & Yield

MACH 10 200 MPa TRUE-TEMPERATURE FLIGHT SIM

Net Operating Income (NOI)

$0 / yr

Unlevered Cap Rate

0.0%

Gross Revenue

$0 / yr

Total CapEx

Annual OpEx

$0 / yr