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Teledrone Ltd. · United Kingdom
Teledrone Mark VII
Teledrone Mk VII
个人飞行器 · 原型机 · 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
- Light weight mannequin
- 乘客
- 未公开／未录入
- 驾驶方式
- Remote radio control, full scale will be flown with 2 joysticks
- 航程（按来源口径）
- 未公开／未录入
- 巡航速度
- No cruise speed as of this time
- 最大速度
- 未公开／未录入
- 最大起飞重量
- 45 kg (99 lb)
- 载荷
- 未公开／未录入
- 空重
- 20 kg (44 lb)
- 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
- 8 battery packs, 6 V each
- 电机
- 8 T-motor U-7 electric motors
- 旋翼／螺旋桨
- 8 propellers, 55.88 cm (22 in)
- 续航时间
- 10 minutes
- 飞行高度
- Low altitude, ~1 meter (3 ft)
- 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 (ducted fans) or motors fail, the other working propellers (or ducted fans) and motors can safely land the aircraft. There are also redundancies of critical components in the sub-systems of the aircraft.
全部原始参数
Specifications:
- Aircraft type
- Sub-scale eVTOL multicopter prototype aircraft
- Piloting
- Remote radio control, full scale will be flown with 2 joysticks
- Capacity
- Light weight mannequin
- Cruise speed
- No cruise speed as of this time
- Flight time
- 10 minutes
- Cruise altitude
- Low altitude, ~1 meter (3 ft)
- Empty weight
- 20 kg (44 lb)
- Maximum payload weight
- 25 kg (55 lb)
- Maximum takeoff weight
- 45 kg (99 lb)
- Propellers
- 8 propellers, 55.88 cm (22 in)
- Electric motors
- 8 T-motor U-7 electric motors
- Power source
- 8 battery packs, 6 V each
- Fuselage
- Aluminum and plastic
- Window
- Open cockpit (the cockpit looks similar to an English telephone booth)
- Landing gear
- Fixed skid landing gear
- 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 (ducted fans) or motors fail, the other working propellers (or ducted fans) and motors can safely land the aircraft. There are also redundancies of critical components in the sub-systems of the aircraft.