Explore the component explanations below the rendering.
1
Coaxial rotor groups
Multiple rotors distribute lift and control.
Illustrated external component · explained below
2
Central cabin
Two-seat passenger capsule.
Illustrated external component · explained below
3
Skid landing gear
Compact vertical-takeoff support.
Internal or non-visible characteristic · explanation only
Engineering profile · verification by field
How to identify this aircraft
Specs checked · Geometry provisional
The following features are supported by the cited manufacturer, regulator, or research authority. Compare them with the educational rendering; mismatches remain open artwork issues.
01 · ROTORSSIXTEEN rotors on EIGHT arms, mounted in pairs along each arm.
02 · AIRFRAMEWingless central two-seat passenger capsule; no conventional cruise wing.
03 · OPERATIONPilotless aircraft designed for autonomous flight with ground oversight.
04 · JURISDICTIONType/production/operator approvals were issued in China; do not imply FAA certification.
Specification conditions: Certification milestones are jurisdiction-specific and do not establish service permissions elsewhere.
Outstanding geometry review: Double-stacked coaxial rotors must be visible as 16; simplified representation needs photo verification.
An alternate-angle CGI visualization of the aircraft. Use the linked sources and specification tables for technical facts; image dimensions and component positions remain illustrative.
Aircraft identity and source controls. The technical figures and configuration facts on this page were checked against the linked primary authorities in October 2026. The aircraft drawing remains an independently generated, illustrative model, NOT validated against OEM geometry; its proportions, angles and component locations must not be used for engineering design.
