Aurora Mock-9

Experimental VTOL Testbeds

VTOL concept studies developed from original sketches and inspired by modern lift-fan VTOL principles (e.g., F-35) and Aurora-style experimental aircraft design cues. 3D modeling and CFD analysis in development.

Role: Concept + trade study Planned: CFD (ANSYS) Planned: 3D Models, FEA (LS-DYNA) Focus: VTOL configs
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RAVEN-X VTOL concept—ducted lift, neon contouring
RAVEN-X
Tier 2 CFD: ANSYS (planned) FEA: LS-DYNA (planned)

Systems: Tactical system suite under test conditions.

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Tech Specs for RAVEN-X:
• Quick takeoff/landing in urban zones.
• Dual-duct lift for stability under wind.
• Gyro stabilization for tight navigation.
• Short endurance optimized for recon.
SHADOW VARIANT VTOL concept—variable tilt transition
SHADOW VARIANT
Tier 1 CFD: ANSYS (planned) FEA: LS-DYNA (planned)

Systems: Transition thrust vector systems test.

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Tech Specs for SHADOW VARIANT:
• Silent thrust-vector transition for stealth.
• Low-noise propulsion for hover trials.
• Mid-range capability for covert missions.
• Optimized for tactical insertions.
VEILRUNNER VTOL concept—hoverlock, low-altitude insertion
VEILRUNNER
Tier 1 CFD: ANSYS (planned) FEA: LS-DYNA (planned)

Systems: Silent insertion system.

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Tech Specs for VEILRUNNER:
• Stealth optimized for low altitude ops.
• Hoverlock propulsion minimizes noise.
• Ideal for covert deployment close to target.
NIGHT FLIGHT VTOL concept—IR field navigation
NIGHT FLIGHT
Tier 3 CFD: ANSYS (planned) FEA: LS-DYNA (planned)

Systems: IR field simulation.

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Tech Specs for NIGHT FLIGHT:
• Infrared sensors for night navigation.
• IR beacon tracking for precision flight.
• Built for urban/forest night operations.
• 160 m IR range.
CUTAWAY-9 VTOL concept—structure and airflow reveal
CUTAWAY-9
Tier 1 CFD: ANSYS (planned) FEA: LS-DYNA (planned)

Systems: Airflow and frame analysis.

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Tech Specs for CUTAWAY-9:
• Showcases internal airflow and frame.
• Demonstrates aerodynamic pathways.
• Built for educational/testbed analysis.
MULTIWING ASCENT VTOL concept—confined vertical climb
MULTIWING ASCENT
Tier 2 CFD: ANSYS (planned) FEA: LS-DYNA (planned)

Systems: Confined space vertical ascent.

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Tech Specs for MULTIWING ASCENT:
• High thrust optimized for vertical boost.
• Dual-wing design for stability.
• Handles narrow takeoff zones.
SAGEFRAME VTOL concept—ML stability correction
SAGEFRAME
Tier 2 CFD: ANSYS (planned) FEA: LS-DYNA (planned)

Systems: Machine learning flight correction.

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Tech Specs for SAGEFRAME:
• Machine learning corrects drift/turbulence.
• Improves stability under harsh air.
• Optimized for long-flight reliability.
SCORCH OPS VTOL concept—thermal trial
SCORCH OPS
Tier 2 CFD: ANSYS (planned) FEA: LS-DYNA (planned)

Systems: Thermal resistance optimization.

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Tech Specs for SCORCH OPS:
• Tested under desert high heat.
• Thermal resistance optimized.
• Endurance under extreme climate.
UI-REACTOR HUD concept—cockpit interface mock
UI-REACTOR HUD
Tier 2 CFD: ANSYS (planned) FEA: LS-DYNA (planned)

Systems: Heads-up display & energy/status feedback.

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Tech Specs for UI-REACTOR HUD:
• Heads-up display interface.
• Energy + system status feedback.
• Testbed for cockpit UI concepts.
POWER NODES concept—subsystem power map
POWER NODES
Tier 3 CFD: ANSYS (planned) FEA: LS-DYNA (planned)

Systems: Wiring/balance isolation check.

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Tech Specs for POWER NODES:
• Maps subsystem power distribution.
• Ensures redundancy + balance.
• Critical wiring optimization.
Contact / request details
Additional configurations, analysis outputs, or documentation shared on request.
© Audrey Enriquez. Concepts and documentation are proprietary; please don’t reproduce or repurpose without written permission.