Technical Specifications & Parameters
Dynamic Aerodynamic VisualizationPropulsion Engineering Innovations
Engineered for maximum power-to-weight ratio, acoustic stealth, and modular integration with directional vectoring nozzles.
8.5:1 High Thrust-to-Weight Architecture
Lightweight monocoque carbon-fiber shroud and titanium rotor retention ring, delivering an exceptional 8.5:1 static thrust-to-propulsion mass ratio for maximum mission payload capacity.
12-Blade High-Twist Stealth Rotor
Optimized 12-blade high-twist rotor operating at 4000 rpm, eliminating transonic blade-tip shockwaves and ensuring ground noise levels drop below ambient background noise at 50m slant distance.
Modular Directional Jet Vectoring Ring
Supports optional lightweight mechanical exit guide vanes or gimbal vectoring rings, providing ±15° rapid pitch/yaw thrust deflection without requiring external aerodynamic control surfaces.
100V–150V Compact Integrated Controller
Ultra-compact aviation ESC compatible with high-discharge solid-state batteries, fuel-cell stacks, and hybrid range-extender generators with comprehensive over-temperature telemetry.
Target Aircraft Configurations
Proven power allocation models for agile tactical drones, loitering platforms, and compact amphibious support craft.
150–350 kg Tactical VTOL UAV
Quad-rotor or tail-sitter tactical platform offering silent urban launch and agile reconnaissance capabilities with sub-meter precision landing.
High-Speed Loitering Platform & Drone
Enclosed rear pusher configuration capable of sustained 250+ km/h dash speeds while eliminating exposed propeller hazard during transport canister tube launch.
Amphibious All-Terrain Interceptor & USV
Surface-skimming propulsion impervious to riverbed weeds, shallow sandbars, and debris, providing instant static thrust and rapid turn acceleration.
Aerospace Engineering Deliverables
Rapid-integration data package provided for tactical airframe and robotics manufacturers.
Full-Scale Dynamic Thrust Calibration Report
Bench-tested load-cell thrust measurements across throttle steps from 10% to 100% and dynamic forward airspeed conditions up to 40 m/s.
Precision 3D CAD & Mounting Interface
STEP 3D model with exact mounting ring screw dimensions, center of mass position, and mass moments of inertia.
Avionics Communication Protocol (PWM/CAN)
Interface specification supporting standard aviation PWM, DShot, and CAN Aerospace bus communication with internal temperature telemetry.
100-Hour Full-Load Endurance Test Report
Continuous bench trial test data documenting bearing longevity, vibration spectrum peaks, and stator winding temperature stability.
Frequently Asked Questions
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