Independent VTOL Configuration Study
VTOL configuration concepts exploring layout tradeoffs, lift strategies, and future CAD / analysis paths, informed by the F-35 lift-fan system and experimental Aurora jet concepts.
Comparative study of VTOL layouts, lift strategies, and subsystem placement before detailed modeling.
- Initial 3D geometry
- Packaging refinement
- First-pass CFD / structural screening
Systems Focus: Compact ducted-lift concept for urban hover and short-range insertion.
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• Compact ducted-lift concept for constrained zones.
• Stability-focused hover layout.
• Candidate for early hover/control analysis.
Systems Focus: Transition-focused layout for cruise-to-hover behavior and low-signature propulsion.
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• Transition-focused thrust-vector concept.
• Useful for mode-change stability studies.
• Strong candidate for first-pass CFD screening.
Systems Focus: Low-signature hover concept for stable close-target deployment.
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• Low-signature hover-oriented layout.
• Supports close-target deployment concepts.
• Good candidate for acoustic/hover comparisons.
Systems Focus: Night-operations concept for sensing and low-visibility navigation.
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• Night-navigation and sensing-oriented concept.
• Useful for compact sensor packaging studies.
• Lower-priority simulation candidate.
Systems Focus: Internal layout study for frame architecture and airflow routing.
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• Internal framing concept for packaging and flow-path reasoning.
• Useful bridge between sketch ideation and future geometry.
• Strong reference layout for later CAD embodiment.
Systems Focus: Vertical-lift concept for constrained launch and thrust-distribution studies.
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• Vertical-boost concept for tight launch zones.
• Useful for thrust distribution and ascent stability comparisons.
• Mid-priority candidate for first-pass hover analysis.
Systems Focus: Stability-augmentation concept for drift correction and disturbance response.
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• Control-oriented concept for drift and turbulence response.
• Useful for mapping control logic against airframe geometry.
• Better framed as a controls study than a lead configuration.
Systems Focus: Thermal mission concept for endurance and environmental survivability.
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• Heat-exposure concept for mission-environment tradeoffs.
• Supports early thinking about high-temperature envelopes.
• Strong fit for the thermal-analysis side of the portfolio.
Systems Focus: Cockpit-display concept for pilot-facing system feedback and interface logic.
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• Interface study for propulsion, energy, and mission-state feedback.
• Useful as a systems-integration layer rather than a pure airframe study.
• Best kept as a supporting systems concept.
Systems Focus: Power-routing concept for subsystem balance, redundancy, and wiring logic.
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• Support study for subsystem distribution and routing priorities.
• Useful for identifying balance and redundancy questions early.
• Better as an architecture support concept than a lead configuration.