Radek Stepan · Czech Republic

Navar Aero

Stepan Navar Aero

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: 1 passenger and luggage (With remote or autonomous piloting, 2 passengers and their luggage)
乘客: 未公开／未录入
驾驶方式: 1 pilot (in the future, remote or autonomous piloting)
航程（按来源口径）: 未公开／未录入
巡航速度: Unknown
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: Hybrid-electric power source (in the future, hydrogen fuel cells, batteries, nuclear or another form of energy)
电机: 4 electric motors
旋翼／螺旋桨: 2 advanced high-performance electric-duct-fan in wing for VTOL flight an precision maneuvering
续航时间: 未公开／未录入
飞行高度: 未公开／未录入
安全设计: There are redundancies of critical components in the sub-systems of the aircraft. The electric motors increase the safety of the aircraft exponentially. In case of a partial or complete power failure, there is a whole aircraft ballistic parachute.

Aircraft type: Long-range high-performance hybrid-electric VTOL passenger concept design aircraft
Piloting: 1 pilot (in the future, remote or autonomous piloting)
Capacity: 1 passenger and luggage (With remote or autonomous piloting, 2 passengers and their luggage)
Cruise speed: Unknown
Propellers: 2 advanced high-performance electric-duct-fan in wing for VTOL flight an precision maneuvering
Forward flight: Turbine jet engine in the rear of the aircraft
Electric motors: 4 electric motors
Power source: Hybrid-electric power source (in the future, hydrogen fuel cells, batteries, nuclear or another form of energy)
Fuselage: Carbon fiber composite
Window: Canopy over cockpit
Wings: 1 main forward swept wing with winglets
Landing gear: Retractable quadricycle strut landing gear.
Safety features: There are redundancies of critical components in the sub-systems of the aircraft. The electric motors increase the safety of the aircraft exponentially. In case of a partial or complete power failure, there is a whole aircraft ballistic parachute.