Aurora Mock-9
Experimental VTOL Testbeds
Concepts developed from original sketches and hybridized lift geometries (Aurora-series cues + F-35B-style VTOL). Models and specs are in active development and will be accompanied by validated CFD (ANSYS) and FEA (LS-DYNA) summaries. AI tools were used for layout/documentation onlyânot for geometry generation or analysis.
Methodology âTier: Tier 2
Systems: Tactical system suite under test conditions.
Tier: Tier 1
Systems: Transition thrust vector systems test.
Tier: Tier 1
Systems: Silent insertion system.
Tier: Tier 3
Systems: IR field simulation.
Tier: Tier 1
Systems: Airflow and frame analysis.
Tier: Tier 2
Systems: Confined space vertical ascent.
Tier: Tier 2
Systems: Machine learning flight correction.
Tier: Tier 2
Systems: Thermal resistance optimization.
Tier: Tier 2
Systems: Heads-up display & energy/status feedback.
Tier: Tier 3
Systems: Wiring/balance isolation check.
Tier: Tier 2
Systems: Tactical system suite under test conditions.
Tier: Tier 1
Systems: Transition thrust vector systems test.
Tier: Tier 1
Systems: Silent insertion system.
Tier: Tier 3
Systems: IR field simulation.
Tier: Tier 1
Systems: Airflow and frame analysis.
Tier: Tier 2
Systems: Confined space vertical ascent.
Tier: Tier 2
Systems: Machine learning flight correction.
Tier: Tier 2
Systems: Thermal resistance optimization.
Tier: Tier 2
Systems: Heads-up display & energy/status feedback.
Tier: Tier 3
Systems: Wiring and balance isolation check.
Aurora Mock-9 Loadout Grid
⢠Quick takeoff/landing in urban zones.
⢠Dual-duct lift for stability under wind.
⢠Gyro stabilization for tight navigation.
⢠Short endurance optimized for recon.
⢠Silent thrust-vector transition for stealth.
⢠Low-noise propulsion for hover trials.
⢠Mid-range capability for covert missions.
⢠Optimized for tactical insertions.
⢠Stealth optimized for low altitude ops.
⢠Hoverlock propulsion minimizes noise.
⢠Ideal for covert deployment close to target.
⢠Infrared sensors for night navigation.
⢠IR beacon tracking for precision flight.
⢠Built for urban/forest night operations.
⢠160 m IR range.
⢠Showcases internal airflow and frame.
⢠Demonstrates aerodynamic pathways.
⢠Built for educational/testbed analysis.
⢠High thrust optimized for vertical boost.
⢠Dual-wing design for stability.
⢠Handles narrow takeoff zones.
⢠Machine learning corrects drift/turbulence.
⢠Improves stability under harsh air.
⢠Optimized for long-flight reliability.
⢠Tested under desert high heat.
⢠Thermal resistance optimized.
⢠Endurance under extreme climate.
⢠Heads-up display interface.
⢠Energy + system status feedback.
⢠Testbed for cockpit UI concepts.
⢠Maps subsystem power distribution.
⢠Ensures redundancy + balance.
⢠Critical wiring optimization.
3D Concept Models & Simulation Data
Immersive 3D models of the VTOL concepts are being finalized for web preview, alongside validated simulation datasets.
The release will include CFD (ANSYS) flow results and FEA (LS-DYNA) structural responses, with concise data specifications and comparison plots.
Status: preparing geometry layers, meshing notes, solver settings, and post-processing pipelines for publication.
Coming soon: interactive 3D preview with data overlays (rotation, section cuts, animation timelines).