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SkyDrive Inc. · Japan

SD-05

SkyDrive SD-05

多旋翼 · 概念设计 · 核查 2026-10-01

下列为 VFS 目录披露的参数,包含设计目标及历史版本信息。目录阶段不等于适航或量产状态;不同任务条件的航程与载荷不能直接当作同一条件下的性能。

主要参数

座位/载员
2 passengers and their luggage
乘客
未公开/未录入
驾驶方式
1 pilot
航程(按来源口径)
10 km (6.2 m)
巡航速度
未公开/未录入
最大速度
未公开/未录入
最大起飞重量
1,100 kg (2,425 lb)
载荷
未公开/未录入
空重
未公开/未录入
长度
未公开/未录入
翼展
未公开/未录入
高度
未公开/未录入
动力来源
Battery packs
电机
12 electric motors
旋翼/螺旋桨
12 propellers
续航时间
5-10 minutes
飞行高度
未公开/未录入
安全设计
Distributed Electric Propulsion (DEP), provides safety through redundancy for its passengers and/or cargo. DEP means having multiple propellers (or ducted fans) and motors on the aircraft, so if one or more propellers or motors fail, the other working propellers and motors can safely land the aircraft. There are also redundancies in the sub-systems of the aircraft.

全部原始参数

Specifications:

Aircraft type
Passenger eVTOL aircraft (concept design)
Piloting
1 pilot
Capacity
2 passengers and their luggage
Maximum cruise speed
100 km/h (62 mph)
Maximum range
10 km (6.2 m)
Flight time
5-10 minutes
Maximum takeoff weight
1,100 kg (2,425 lb)
Propellers
12 propellers
Electric motors
12 electric motors
Power source
Battery packs
Fuselage
Carbon fiber composite, aluminum alloy and other materials
Dimensions
13 m x 13 m x 3 m (43 ft x 43 ft x 10 ft) including propellers
Windows
Panoramic wrap around windows allowing forward, left and right visibility for spectacular views with a solid roof above the passenger compartment
Tail
A modified boom mounted tail. The tail extends from the rear of the fuselage with two rear vertical booms that connect to a downward sloping horizontal stabilizer with vertical fins on each end of the horizontal stabilizer.
Landing gear
Fixed skid landing gear, at the rear of each skid is an angled-outward vertical fin
Safety features
Distributed Electric Propulsion (DEP), provides safety through redundancy for its passengers and/or cargo. DEP means having multiple propellers (or ducted fans) and motors on the aircraft, so if one or more propellers or motors fail, the other working propellers and motors can safely land the aircraft. There are also redundancies in the sub-systems of the aircraft.