M-250 Logistic

Specifications:

Aircraft type

Heavy-lift hybrid-electric VTOL concept design aircraft

Piloting

Autopilot or has remote controlled option

Capacity

Air cargo only

Cruise speed

125-150 km/h (77-92 mph)

Range

320 km (199 m)

Maximum altitude

3,000 m (9,843 ft)

Empty weight

313 kg (690 lb)

Maximum payload weight

250 kg (551 lb)

Maximum takeoff weight

563 kg (1,241 lb)

Propellers

2 propellers

Electric motors

2 electric motors

Power source

Hybrid-electric power source

Fuselage

Carbon fiber composite fuselage

Operating temperature range

-40 C (-40 F) to +50 C (122 F)

Landing gear

Lands on the bottom of the drone's fuselage (there are no landing skids, struts or wheels)

Safety features

Distributed Electric Propulsion (DEP) means having multiple propellers (or electric ducted fans) and multiple electric motors on an aircraft so if one or more propellers (or electric ducted fans) or some electric motors fail, the other working propellers (or electric ducted fans) and electric motors can safely land the aircraft. DEP provides safety through redundancy for its passengers or cargo. There are also redundancies of critical components in the sub-systems of the aircraft providing safety through redundancy for its passengers or cargo. Having multiple redundant systems on any aircraft decreases having any single point of failure.