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Jetoptera Inc. · USA
J-HS
Jetoptera J-HS
矢量推力 · 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
- 1 passenger
- 乘客
- 未公开／未录入
- 驾驶方式
- 1 pilot, number of passengers unknown
- 航程（按来源口径）
- 400 miles (644 km)
- 巡航速度
- 400 mph (644 km/h)
- 最大速度
- 未公开／未录入
- 最大起飞重量
- 未公开／未录入
- 载荷
- 450-800 lb (204-363 kg)
- 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
- 3 Fluidic Propulsion System (FPS) units (a proprietary and novel Jetoptera propulsion system)
- 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
- If one or more thrusters fail or get clogged, the aircraft can glide to a landing on a runway, road or field. The aircraft has redundant electronics and avionics on board. There are no propellers or rotors on the aircraft (the propulsion system uses oval thrusters expelling compressed air) making the aircraft safe for all people on the ground whether the aircraft parked with its engines off or is ready for takeoff.
全部原始参数
Specifications:
- Aircraft type
- Hybrid-electric VTOL passenger concept design aircraft (future, all electric)
- Piloting
- 1 pilot, number of passengers unknown
- Capacity
- 1 passenger
- Cruise speed
- 400 mph (644 km/h)
- Maximum range
- 400 miles (644 km)
- Maximum payload
- 450-800 lb (204-363 kg)
- Propulsion
- 3 Fluidic Propulsion System (FPS) units (a proprietary and novel Jetoptera propulsion system)
- Power source
- Gas turbine engine (in the future can accept batteries when battery destiny improves)
- Fuselage
- Carbon fiber composite
- Windows
- Canopy over cockpit with gull-wing doors
- Wings
- 1 Front tilt-canard and 1 rear box wing (the box wing is the primary load-carrying structure)
- Landing gear
- Retractable tricycle wheeled landing gear
- Safety features
- If one or more thrusters fail or get clogged, the aircraft can glide to a landing on a runway, road or field. The aircraft has redundant electronics and avionics on board. There are no propellers or rotors on the aircraft (the propulsion system uses oval thrusters expelling compressed air) making the aircraft safe for all people on the ground whether the aircraft parked with its engines off or is ready for takeoff.