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Trek Aerospace, Inc. · USA

SoloTrek XFVM

Trek Aerospace SoloTrek XFVM

个人飞行器 · 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
未公开/未录入
乘客
未公开/未录入
驾驶方式
1 pilot
航程(按来源口径)
184 miles (295 km)
巡航速度
113 mph (180 kp/h)
最大速度
未公开/未录入
最大起飞重量
834 lb (378 km)
载荷
358 lb (162 km)
空重
375 lb (170 km)
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
Conventional, all-electric or a hybrid-electric power source
电机
2 electric motors
旋翼/螺旋桨
2 ducted variable-pitch propellers
续航时间
2 hours
飞行高度
未公开/未录入
安全设计
Two shoulder straps and a waist strap to secure the pilot onto the fuselage. Two foot rests are located on the aircraft's fixed strut-type landing gear. An emergency ballistic whole aircraft parachute is fitted at the top of the airframe between the two ducted fans.

全部原始参数

Specifications:

Aircraft type
One person VTOL, eVTOL or hybrid-electric VTOL concept design backpack military helicopter aircraft
Piloting
1 pilot
Cruise speed
113 mph (180 kp/h)
Range
184 miles (295 km)
Flight Time
2 hours
Empty weight
375 lb (170 km)
Maximum payload
358 lb (162 km)
Maximum takeoff weight
834 lb (378 km)
Propellers
2 ducted variable-pitch propellers
Electric Motors
2 electric motors
Power source
Conventional, all-electric or a hybrid-electric power source
Fuselage
Carbon fiber composite
Lights
Is outfitted with 2 spot lights
Landing gear
Fixed tricycle landing gear, a flat landing gear plate is in the front of the aircraft and two rear fixed wheels are the landing gear in the rear of the aircraft. This type of arrangement makes it easy to wheel the aircraft in a hangar, on the tarmac, or in and out of vehicles.
Safety features
Two shoulder straps and a waist strap to secure the pilot onto the fuselage. Two foot rests are located on the aircraft's fixed strut-type landing gear. An emergency ballistic whole aircraft parachute is fitted at the top of the airframe between the two ducted fans.