Wind-Tunnel Calibration Facilities & Computational Aerospace Partners
Aerodynamic Architecture
Supersonic wave-rider aerodynamics sculpted around moving air
Every contour is an active stealth aerodynamic surface engineered to manipulate shock compression, ingest boundary layers, and eliminate turbulent flow separation.
CFD Aerospace Benchmark Comparison
Hypersonic Flight Regime Hegemony
Direct computational fluid dynamics comparison between Apeiron X-1 Wave-Rider Stealth Interceptor and conventional 5th-Gen combat aircraft.
| Flight Telemetry Metric | Apeiron X-1 (Wave-Rider Stealth) | 5th-Gen Fighter Spec | Advantage / Delta |
|---|---|---|---|
| Max Velocity In Atmosphere | Mach 6.85 (7,240 km/h) | Mach 2.25 (2,410 km/h) | +204% Velocity |
| Supersonic Lift-to-Drag Ratio (L / D) | 4.92 : 1 | 2.40 : 1 | +105% Aero Efficiency |
| Stagnation Thermal Limit (T0) | 2,200 K (Carbon-Carbon C/C) | 850 K (Aluminum-Titanium) | +1,350 K Thermal Window |
| Shock-Induced Wave Lift | 84.2% Compression Capture | 32.0% Parasitic Wave Drag | +52.2% Lift Compression |
| Continuous Scramjet Range | 6,400 km Suborbital | 1,250 km Afterburning | +412% Operational Radius |
Wind-Tunnel Continuous Run Validation
The Apeiron X-1 demonstrated complete boundary layer adhesion at Mach 6.85, exhibiting zero shock stall across a 28-degree pitch sweep in the continuous hypersonic facility.
Dr. Elena Vance, Principal Aerodynamicist, Hypersonic Flight Dynamics
Bespoke Flight Test Commission
Command the future of hypersonic aerospace
A designated flight test batch of 12 suborbital airframes entering wind-tunnel supersonic calibration for 2027 delivery.
Reserve flight test airframe