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Roxtern Aerospace Private Limited · India
Flying Supercar
Roxtern Aerospace Flying Supercar
升力＋巡航 · 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
- 乘客
- 未公开／未录入
- 驾驶方式
- Unknown
- 航程（按来源口径）
- 500 km (310 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
- 1,450 kg (3,197 lb)
- 载荷
- 未公开／未录入
- 空重
- 1,250 kg (2,756 lb)
- 长度
- 10.5 meters (34 ft, 5-14 in)
- 翼展
- 11 meters (36 ft, 1 in)
- 高度
- 2.3 meters (7 ft, 6 in)
- 动力来源
- Hybrid-electric power source using hydrogen fuel cells
- 电机
- 20 electric motors
- 旋翼／螺旋桨
- 12 electric ducted fans (EDFs) for forward flight, 8 propellers for VTOL flight
- 续航时间
- 1 hour, 40 minutes
- 飞行高度
- 未公开／未录入
- 安全设计
- 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. There is also a whole aircraft emergency ballistic parachute in case of an unexpected inflight emergency. The aircraft will also have airbags inside the cabin.
全部原始参数
Specifications:
- Aircraft type
- Passenger hybrid-electric VTOL concept design aircraft
- Piloting
- Unknown
- Capacity
- 2 passengers
- Maximum cruise speed
- 300 km/h (186 mph)
- Range
- 500 km (310 m)
- Flight time
- 1 hour, 40 minutes
- Empty weight
- 1,250 kg (2,756 lb)
- Maximum payload weight
- 200 kg (441 lb)
- Maximum takeoff weight
- 1,450 kg (3,197 lb)
- Propellers
- 12 electric ducted fans (EDFs) for forward flight, 8 propellers for VTOL flight
- Electric motors
- 20 electric motors
- Power source
- Hybrid-electric power source using hydrogen fuel cells
- Fuselage
- Carbon fiber composite
- Length
- 10.5 meters (34 ft, 5-14 in)
- Height
- 2.3 meters (7 ft, 6 in)
- Wingspan
- 11 meters (36 ft, 1 in)
- Window
- Canopy over cockpit
- Wings
- 1 main high wing with winglets
- Tail
- 1 twin-boom mounted horizontal stabilizer
- Landing gear
- Lands on the bottom of the VTOL propeller housings or has retractable landing gear
- 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. There is also a whole aircraft emergency ballistic parachute in case of an unexpected inflight emergency. The aircraft will also have airbags inside the cabin.