The Flexrotor is a Group 2 small tactical vertical take-off and landing (VTOL) unmanned aircraft system (UAS). It has a maximum take-off weight of 25 kg (55 lbs) and is designed for Intelligence, Surveillance, and Reconnaissance (ISR) missions for more than 12-14 hours in a typical operational configuration. 

It can integrate different types of payloads, including an electro-optical system and advanced sensors to suit customers’ unique mission needs. With the ability to autonomously launch and recover from either land or at sea requiring only a 3.7 by 3.7 m (12 by 12 ft.) area, the Flexrotor is ideal for expeditionary missions requiring minimal footprint. 

Unmanned aerial system (UAS), Flexrotor


Missions

Flexrotor delivers long endurance and high space weight and power (SWaP), enabling the expeditionary UAS to operate a wide array of sensors and capabilities. It can operate from confined land areas and from ships without flight decks, and its expeditionary capability makes it easy to transport and to go from stowed to airborne in less than 14 minutes.

Missions include: 

- ISTAR 
- Maritime warfare (signal Intelligence, electronic warfare, communications relay)
- Search and rescue 
- Parapublic (firefighting, humanitarian missions, border security)
- Civil applications (precision agriculture, geo mapping, wildlife observation & marine science)

Flexrotor launch off of the USS Paul Hamilton


Technical description

Metric

Dimensions

Length2 m
Rotor diameter2.2 m
Maximum launch weight (ISA, SL)25 kg
Wingspan3 m

Performance

Dash speed140 km/h
EnduranceUp to 32 hours
Hover ceiling at max weight with legs closed1300 m
Maximum payload8 kg

Characteristics

PropulsionEngine 28 cc 2 stroke
Imperial

Dimensions

Length7 ft
Rotor diameter7.2 ft
Maximum launch weight (ISA, SL)55 lb
Wingspan9.8 ft

Performance

Dash speed77 kt
EnduranceUp to 32 hours
Hover ceiling at max weight with legs closed4300 ft
Maximum payload18 lb

Characteristics

PropulsionEngine 28 cc 2 stroke

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