One car.Road and sky.

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

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.

The problem

The road stopped being the shortest way.

Traffic, detours and terrain turn forty kilometres in a straight line into a two-hour journey. Aviation solves distance but demands an airfield, a transfer and a timetable. Between the car and the aeroplane there is nothing that covers the route door to door.

In the Kingdom this is felt most sharply: Jeddah to Mecca and Medina during Hajj and Umrah, transfers between industrial clusters, delivery to hard-to-reach locations.

By road2 h 10
Direct air26 min

Illustration of the principle over 80 km. Specific routes are calculated once cruise speed is agreed.

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

Vertically, from existing surfaces — parking lots, rooftops, freight terminals.

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

FLYCAR on a canyon road

01  The form

A car first.

Steering wheel, two pedals, four seats, 100-litre luggage. Carbon-fibre monocoque, 27-inch wheels, adaptive four-wheel-steering suspension. At 6.2 × 2.5 × 1.9 m it parks in a standard space.

Core technology

The wings are already there.

FLYCAR uses a closed-contour double 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 with redundant sensors
FLYCAR from above, showing the ring structure integrated into the rear of the body
Ring structure · technical section to follow

How a flight works

The whole route, without a transfer.

01

Road

Driving to the take-off point on ordinary roads.

02

Pad

Onto an existing surface. No vertiport required.

03

Lift off

Vertical take-off, including in gusts up to 5 m/s.

04

Transition

Tail electric turbines engage above 160 km/h.

05

Cruise

At an altitude of 500 to 4,000 metres.

06

Landing

Vertical landing, then back onto the road.

Safety

A failure must not end the flight.

Active parachute system

Five rocket launchers, rapid ejection and inflation of the rescue canopy, operating at low altitude — down to 100 metres.

Triple redundancy

Key systems are duplicated. Six-phase electric motors with a fault-tolerant architecture. Multiply redundant sensors on the airflow control system.

Automation and wind

Stabilisation, navigation and obstacle avoidance. Active crosswind compensation on take-off and landing.

Specifications

Every figure carries its status.

Confirmed by testing
Engineering calculation
Design target
Air speed
0km/h
Calculation
Road speed
0km/h
Calculation
Flight range
0km
Calculation
Endurance
0h
Calculation
Flight altitude
0.5–4km
Calculation
Seats
0
Calculation
Payload
0kg
Calculation
MTOW
0kg
Calculation
Dimensions
6.2 × 2.5 × 1.9m
Confirmed
Peak power
0kW
Target
Gust tolerance
5m/s
Calculation
Luggage
0l
Calculation

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.

Parameters for which no data yet exists are not published here: cruise speed, landing pad size, noise level, battery capacity.

Competitive position

No one combines it all.

FLYCAREHangXPengAirCar / AskaElectraJoby / ArcherLilium
Road drivingFullNoModularPartialNoNoNo
Vertical take-offYesYesYesPartialNoYesYes
Hybrid powerplantYesNoPartialVariesYesMostly noNo
Payload650 kg220 kgLowLow1360 kgLimitedLimited
Seats4221–4up to 944–6
Endurance4 h20–40 minLimitedLimitedHigh1–1.5 h~1 h
IP control and KSA localisationYesNoNoNoNoNoNo

No existing project combines, in one aircraft, a full road mode, vertical take-off without dedicated infrastructure, payload above 400 kg, a hybrid powerplant that refuels at ordinary filling stations, and dimensions that fit city parking.

Real footage

Filmed, not drawn in a deck.

A vertical film of the build process and photographs from testing will be added as a separate gallery.

What is done

Twelve years before the first render.

2014

Team formed, concept developed, layout and design created.

2020–21

Aerodynamic calculations for the final concept.

2021

Design of units and assemblies.

2021–26

Models at 1:4.6 and 1:3.6. Full-scale assemblies built and tested.

2026

Design of the full-scale flying model.

2027

Flying prototype assembly, Dubai Airshow, patent filing.

Intellectual property: a complete set of design documentation, drawings and schematics of all units, aerodynamic and structural calculations, material specifications, and know-how covering multi-circuit engines, the airflow control system and the rescue system. All documentation is held solely by the project team. 27 patentable solutions, 14 applications in preparation, filing in 2027.

Portrait
pending

Founder

Alexander Zdrok

Inventor and Founder, Future Technology Development

The founder’s statement is being agreed.

The story behind FLYCAR, the portrait and an agreed quotation will be added once the materials are confirmed.

Why Saudi Arabia and why now

The entry window is 12–24 months.

90%

Vision 2030 in its final phase

Of 1,290 initiatives, complete or on schedule. 93% of KPIs met. Non-oil GDP is around 55% of real GDP.

Q1 2026

Regulation is being written now

The AAM test site in Riyadh is operating. GACA is signing agreements with Vertical Aerospace, Joby and Archer.

$7.8bn

Expo 2030 Riyadh

1 October 2030 to 31 March 2031. Six million m², more than 40 million visits. Just over four years to opening.

$81bn

Demand confirmed by spend

Tourism 2025: about 123 million visitors. Saudia Group has ordered 50 with an option on 50 more. PIF has approved a strategy centred on aerospace.

Q1 2026

AAM test site, Riyadh

Dec 2025

Archer agreement with GACA

Jul 2026

Vertical Aerospace MoU with GACA

2027

Dubai Airshow — FLYCAR appears

2029

Type certificate

Market and use cases

The market already exists.

$145mKSA AAM market, 2025
$8.97bnForecast by 2031 · CAGR 35.2%
1 000+Potential demand in the Kingdom
$100bnGlobal AAM market by 2035

Logistics

Freight into OXAGON and between industrial clusters.

Tourism and pilgrimage

Hajj and Umrah, the Red Sea, AlUla.

Emergency services

Medical evacuation, search and rescue.

Roadmap

The schedule is anchored to external dates.

Dubai Airshow 2027 and Expo 2030 cannot be moved — the plan is built around them.

Q3 2026 – Q1 2027Team relocation to KSA, company registration, design of the 1:1 and 1:3.6 models, CFD and CAD$1.74m
2027Flying prototype 1:1, static mock-up, Dubai Airshow 2027, dialogue with GACA, patent filing$8.9m
2028Certification prototypes and flight testing, start of factory construction$145m
2029Type certificate for the electric version, factory completion, 10–20 pre-series aircraft$155m
2030Series production, market entry, Expo 2030, start of hydrogen R&D$120m
20311,000 units a year, FAA and EASA validation, hydrogen development$45m
2032Hydrogen version submitted for certification, full-scale hydrogen prototype$25m
Total 2026–2032$500m

Business model

Two to two and a half times cheaper than competitors.

Standard

$600k

Commercial operators, taxi services, emergency services

Unit cost$250k
Margin$350k · 58%
Share of sales80%

Luxury

$1.2–1.5m

Private owners, bespoke finish

Unit cost$300k
Margin$900k–1.2m · 75–80%
Share of sales20%

These are target economics at an output of 1,000 units per year. Unit cost on the first batches is higher.

For comparison: Lilium at $7–9m per aircraft, Joby S4 at roughly $1.2–1.5m, Archer Midnight and Vertical Valo at roughly $1–1.5m. None of them has a wheeled chassis.

Investment offer

The current round is $10.6m.

The full programme to certification and market entry is $500m across 2026–2032.

Industry benchmark: Joby, Archer and Lilium project $1.0–1.5bn to certification; Vertical Aerospace $700m. The FLYCAR programme rests on completed documentation, tested models and localisation with the Kingdom’s support.

$10.6mCurrent stage, 2026–2027
2029Type certificate
2030Market entry at Expo
  • Relocation of the core team to the Kingdom
  • Company registration
  • Assembly of the 1:1 flying prototype
  • Full-scale static mock-up
  • Dubai Airshow 2027 and pre-order collection
  • Patent filing and start of the GACA dialogue

Team and partners

An engineering team, not a list of vacancies.

Founder: Alexander Zdrok, Inventor and Founder, Future Technology Development. The team’s areas of competence:

AerodynamicsComposite materialsHybrid powerplantsMicro-turbinesAvionicsFlight control systemsOnboard software and AIStructural strength and dynamicsSafety and rescue systemsCertificationFlight testingManufacturing and machining

Names, roles and photographs of key team members will be published once confirmed. A partners section will appear only when signed agreements exist.

Contact

Request the deck.

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

Helps us send the right materials.