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Trek Aerospace, Inc. · USA

SoloTrek Springtail EFV

Trek Aerospace SoloTrek Springtail EFV

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
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)
160 miles (257 km)
巡航速度
82 mph (132 kph)
最大速度
98 mph (158 kph)
最大起飞重量
834 lb (378 kg)
载荷
未公开/未录入
空重
375 lb (170 kg)
长度
5.31 ft (1.62m)
翼展
未公开/未录入
高度
8.26 ft (2.52m)
动力来源
2-stroke 118 hp Wankel rotary engine. The aircraft can be easily configured with a hybrid-electric power source with a engine for the power and electric motors for the propellers.
电机
未公开/未录入
旋翼/螺旋桨
2 ducted counter-rotating propellers. Each propeller is 42 inches (1,067 mm) wide.
续航时间
2.2 hours
飞行高度
11,400 ft (3,475 m)
安全设计
There are redundancies of critical components in the sub-systems of the aircraft providing safety through redundancy. There is also a whole aircraft emergency ballistic parachute in case of an unexpected inflight emergency. A separate base-jumping parachute is worn by the pilot. The aircraft has two shoulder straps and a waist strap to secure the pilot to the fuselage.

全部原始参数

Specifications:

Aircraft type
One person VTOL backpack helicopter prototype aircraft
Piloting
1 pilot
Cruise speed
82 mph (132 kph)
Maximum speed
98 mph (158 kph)
Range
160 miles (257 km)
Flight time
2.2 hours
Maximum altitude
11,400 ft (3,475 m)
Empty weight
375 lb (170 kg)
Maximum payload weight
175 lb (79 kg)
Normal takeoff weight
622 lb (282 kg)
Maximum takeoff weight
834 lb (378 kg)
Propellers
2 ducted counter-rotating propellers. Each propeller is 42 inches (1,067 mm) wide.
Power source
2-stroke 118 hp Wankel rotary engine. The aircraft can be easily configured with a hybrid-electric power source with a engine for the power and electric motors for the propellers.
Fuselage
Aluminum honeycomb panels with steel tube landing gear legs
Length
5.31 ft (1.62m)
Width
9.71 ft (2.96m)
Height
8.26 ft (2.52m)
Landing gear
Fixed skid landing gear with quadricycle wheels. Two foot rests are located on the aircraft's fixed skid landing gear.
Safety features
There are redundancies of critical components in the sub-systems of the aircraft providing safety through redundancy. There is also a whole aircraft emergency ballistic parachute in case of an unexpected inflight emergency. A separate base-jumping parachute is worn by the pilot. The aircraft has two shoulder straps and a waist strap to secure the pilot to the fuselage.