FLYCAR

One car.
Road and sky.

A four-seat vehicle that drives on public roads and takes off vertically.

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The idea

It does not transform.
It simply leaves the ground.

No folding wings. No changing shape. The vehicle drives, lifts off and flies in one unchanged external configuration — because the lifting surfaces are built into the body itself.

FLYCAR on the road
01  On the road

A car first.

Steering wheel, two pedals, four seats. 27-inch wheels, adaptive four-wheel-steering suspension, carbon-fibre monocoque. It parks in a standard space.

The transition

Drive. Lift off. Fly.

One continuous sequence. The silhouette is identical in all three phases.

01 — Road

Drive

Public roads, four-wheel drive, all-electric with onboard generation.

02 — Lift off

Lift off

Vertical take-off from existing surfaces — parking lots, rooftops, freight terminals. No vertiport required.

03 — Flight

Fly

Transition to horizontal flight on the same airframe. Tail turbines engage above 160 km/h.

Nothing opens · Nothing extends · Nothing folds out

Core technology

The wings are already there.

FLYCAR uses a closed-contour ring-wing scheme. The ring is part of the body — a permanent structural element, not a deployable surface. It carries the load in flight and never has to appear or disappear.

  • Higher lift capacity at a small wingspan
  • Stability in strong crosswind — take-off in gusts up to 5 m/s
  • Bicopter distributed powerplant built into the fuselage
  • Rotors enclosed and protected by the structure
  • Active airflow guides for rapid manoeuvring
Ring wing Ring structure · technical section to follow
Specifications

Every figure carries its status.

Confirmed by testing
Engineering calculation
Design target
Sources disagree — to be reconciled
Air speed
280km/h
Calculation
Flight altitude
0.5–4km
Calculation
Endurance
3–4 / 5h
Report vs film
Road speed
150 / 190km/h
Report vs film
Seats
4
Calculation
Payload
650kg
Calculation
MTOW
1790kg
Calculation
Dimensions
6.2 × 2.5 × 1.9m
Both sources agree

Confirmed by testing

Aerodynamic stability and controllability verified on the 1:4.6 model. Wind-tunnel data on thrust-to-weight ratio, vibration and thermal regimes obtained on the 1:3.6 model. Critical full-scale assemblies manufactured and validated in bench and ground testing.

The entry window is 12–24 months.

Regulation in the Kingdom is being written now. Expo 2030 is four years out. We hold the full engineering documentation and the team.

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