Eight tilting electric rotors; piston-engine generator and battery in a series-hybrid arrangement.
Propulsion Unit Count
8
Redundancy Approach
Flight-test validation pending; no approved single-failure capability established for TD 2.0.
Range / Speed
Manufacturer figures under validation: 200–250 km VFR range, 200 km/h cruise. These are not certified or demonstrated TD 2.0 performance.
Seat Count
Last Updated
October 17, 2026
Technology demonstrator in ground test. Earlier TD 1.0 hover and subscale transition results do not establish TD 2.0 flight.
Ground-test readiness followed by first flight; Q2 2027 is the current company target.
TD 2.0 is Zuri’s uncrewed hybrid-electric technology demonstrator. The current manufacturer page gives a 9.7 m wingspan and 690 kg maximum takeoff weight. Development figures remain under validation.
Eight rotors tilt between intended vertical lift and forward propulsion. A generator and battery feed electric drives. The representative 3D model follows official overhead and structural imagery; exact component placement, blade geometry and aerodynamic surfaces remain approximate.
Zuri reports systems integration and ground testing. The current first-flight target is Q2 2027. Earlier TD 1.0 full-scale hover and subscale transition are separate aircraft records. The full-size display aircraft is non-flying.
TD 2.0 is a proving aircraft rather than an offered passenger product. Zuri’s planned cargo aircraft and longer-term passenger concept have separate specifications and approval pathways.
Loaded hybrid-powertrain tests, cooling, tilt actuation, control integration and envelope expansion precede usable flight performance. No TD 2.0 operating approval or aircraft Type Certificate is established by the reviewed manufacturer evidence.
Current demonstrator configuration; flight/ground record; hybrid architecture; non-flying display aircraft. Image credit: Zuri. Reviewed 17 October 2026. Claims are company-reported.
October 17, 2026
