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Uber Elevate · USA

eCRM-001

Uber Elevate eCRM-001

矢量推力 · 阶段未核实 · 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
未公开/未录入
乘客
4
驾驶方式
1
航程(按来源口径)
未公开/未录入
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
未公开/未录入
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
All electric
电机
未公开/未录入
旋翼/螺旋桨
未公开/未录入
续航时间
未公开/未录入
飞行高度
未公开/未录入
安全设计
未公开/未录入

全部原始参数

Uber eCRM-001 Specifications:

Aircraft type
eVTOL passenger aircraft
Pilot
1
Passengers
4
Boarding
On one side of the aircraft, only
Electric propellers
10 propellers Forward flight: 2 tiltrotor propellers for forward flight (which also tilt up for VTOL capability) VTOL flight: 4 sets of stacked co-rotating propellers for vertical flight on the booms and the fuselage
Power source
All electric

Uber Elevate eCRM General Specifications:

Aircraft type
Must be a 100% all electric vertical take off and landing (eVTOL) aircraft.
Safety
Must be an extremely safe aircraft which can make a vertical emergency landing in the event of a critical failure, including the collision with a bird.
Noise
Must be a low noise aircraft for the people living in urban areas and for passengers.
eVTOL terminals
Skyports are required for passenger boarding and deplaning.
Aircraft communications
Excellent communications network needed. The aircraft must be able to securely report all operational data to operations, know its specific flight plan, can see all obstacles in real-time (buildings, cranes, powerlines and any type of other aircraft, including small drones) and be able to avoid them.
Aircraft size
The aircraft is not to exceed 50 feet (15.24 m) in any direction and 20 feet (6.09 m) for its maximum height due to limited space at Skyports.
Payload
Carry 4 passengers and each passenger can take 1 carry-on bag.
Pilot
1 pilot. Initially, eVTOL vehicles will be piloted with a separate locked cockpit for security. Over time, the eVTOL aircraft will become autonomous.
Taxiing capability
Aircraft must be able to perform a short ground taxi without the use of propellers.
Cruising speed
The eVTOL aircraft must be able to cruise at 150 mph (241 km) with an additional ±15 mph (± 24 km/h) capability required for airspace sequencing and headwinds.
Aircraft Range
Aircraft shall be able to fly 60 miles (96 km) one-way while maintaining enough energy to fly the reserve mission.
Takeoff and maximum altitude
Vehicles shall be capable of takeoff and hover climb at 5,000 feet (1,524 km) density altitude.
Repeatability
The vehicle must be able to operate continuously for at least 3 hours while flying 25 (40 km) mile missions. Continuous operations is defined as charging the batteries around 5-7 minutes between flights.
Reserve power
The aircraft must have enough power at the end of a flight to divert up to 6 miles to an alternate landing site, if needed.