Atlas

Specifications:

Aircraft type

High performance passenger eVTOL concept design aircraft

Piloting and capacity

1 pilot

Maximum speed (estimated)

102 km/h (63 mph)

Flight time (estimated)

1 hour

Service Ceiling (estimated)

3,000 m (10,000 ft)

Empty weight

130 kg (285 lb)

Maximum payload

90 kg (200 lb)

Maximum takeoff weight

220 kg (485 lb)

Propellers

2 ducted propellers. Proprietary Electric ducted fan units produce up to 350 kgf (760 lbf) of combined thrust.

Electric motors

2 electric brushless direct current motors (BLDC) output up to 150 kW (200 hp) of power

Power source

Battery packs. Wing-integrated 12 kWh lithium ion battery pack ensures up to 1 hour flight time. Full charge in under 2 hours.

Noise output

As quiet as 87 dBA from 15.2 m (50 ft) away

Aircraft certification type

Is legal under Ultralight Part 103 or Certifiable as an experimental aircraft as per the USA's FAA Part 103

Wings

2 canard wings which rotate

Cabin

Unpressurized cabin

Window

Canopy over the cockpit

Aircraft height

2.5 m (8.2 ft)

Aircraft width

1.3 m (4.1 ft)

Wingspan

3.8 m (12.5 ft)

Landing gear

Unknown