Twenty-three wireframe and reference assets pulled from PersonFu's engineering coursework, satellite design lifecycle, RF systems study, and presentation slide decks. Each tile crosslinks to a live Sketchfab search so the 3D references stay current.
Real aircraft platforms — AWACS, tankers, and low-observable bombers used in airframe and mission-profile engineering coursework.
Boeing E-3 Sentry airborne early warning platform. Rotodome-mounted AN/APY-2 radar — used in RCS, link-budget, and airspace surveillance coursework.
Boeing KC-135 Stratotanker. Boom refueling system, fuel offload curves, and airspace deconfliction covered in flight-planning study notes.
Northrop Grumman B-2 Spirit. Tailless flying-wing planform — surface continuity and edge alignment study for low-observable geometry.
Northrop Grumman B-21 Raider concept geometry. Faceting, inlet masking, and trailing-edge treatment analyzed for low-observable design methodology.
Lockheed SR-71 Blackbird. Titanium chines, J58 inlet spikes, and skin-temperature profile at Mach 3.2 analyzed for thermal engineering study.
ISS, Apollo, Orion, Sputnik, and launch vehicles from first satellite through Artemis — used in orbital mechanics and CAD lifecycle study.
ISS modular station with photoreal panels and truss segments. Used to stage telemetry overlays and docking approach profiles for symposium demos.
Soviet Sputnik 1 pressure sphere with four whip antennas. First-principles satellite layout: shell topology, antenna geometry, and orbital entry parameters.
Apollo Command and Service Module with solar arrays. Power systems, thermal radiator placement, and S-band antenna boresight study for crewed missions.
Dense mesh of the ISS integrated truss — SOLAR array integration, thermal radiator layout, and mass distribution modeling for station-keeping ops.
Full wireframe topology of the ISS — module joinery, docking nodes, and radiator panel layout review for structural analysis.
NASA Orion MPCV with deployed solar arrays. Payload volume, center-of-gravity analysis, and heat-shield geometry reviewed for Artemis mission architecture.
Orion capsule integrated with ESM — panel break-out, propulsion bay, and avionics annotation pass for Artemis II configuration.
Bottom-view of a reentry capsule heat shield. PICA-X ablative TPS materials and center-of-gravity placement for stable ballistic entry analyzed.
NASA Space Launch System Block 1. Core stage, solid rocket boosters, ICPS upper stage, and Orion fairing — staging sequence and aerodynamic loads reviewed.
Spiral antennas, phased arrays, horn feeds, Helmholtz calibration fixtures, and resonators — crosslinks to HackRF and SDR lab work.
Wideband Archimedean spiral antenna. Circular polarization, phase-center stability, and impedance matching across 1–8 GHz documented for RF coursework.
Toroidal phased-array geometry for omnidirectional beam steering. Pattern coverage, sidelobe suppression, and electronic scanning documented for symposium slides.
Paired Helmholtz coils for uniform-field generation. Used to illustrate IMU magnetometer calibration fixtures — directly applicable to the NASA ASCEND payload.
Pyramidal horn antenna for microwave and millimeter-wave bands. Gain, aperture efficiency, and link-budget walk-through for ground-station receive paths.
Tuned coil resonator at 433 MHz. Impedance matching network visualization — Q-factor, bandwidth, and insertion loss narrative used in RF coursework and HackRF lab notes.
X-15 hypersonics, VTOL experiments, NGAD concepts, recovery systems, and Cold War programs — where engineering fails as hard as it succeeds.
Avro Canada VZ-9 Avrocar — circular VTOL platform. Cold War experimental: Coanda-effect lift, stability failures, and lessons for boundary-layer control research.
Next-generation air dominance concept geometry. Forward-wedge inlet positioning, conformal weapon bay, and reduced-IR-signature planform studied for design methodology.
North American X-15. Mach 6.7 max — skin temperature, RCS thruster authority above 50km, and aerodynamic heating documented for high-speed vehicle design.
Canopy + payload recovery geometry for sounding rocket and balloon payloads. Descent rate, oscillation damping, and GPS ground-track planning for the NASA ASCEND mission.
Hangar assets are open-reference wireframes used in PersonFu's coursework, lecture material, and symposium slide decks. No ITAR / EAR-controlled geometry is published on this site. Where a flight-quality artifact is referenced, it lives behind authenticated tooling — never on this public surface. Sketchfab links resolve to current public search results so 3D references stay live without us pinning expired model UIDs.
Next-gen visualizer: Sketchfab 3D embeds, FAB.com concept vehicles, and curated collections. Cyberpunk, OSINT, and speculative engineering inspiration.
