The civilian version of the autogyro is already certified as an ultralight/experimental aircraft in Europe, the USA, and other countries. The inherent stability of this simple design offers very short take off and landing as well as easy maintenance.

1, 2, 1+2 cabin

We are developing a specific 1+2 airframe for improved mission capacity. It can accommodate 1 pilot and up to 2 passengers/operators. The larger internal volume allows more versatility for mission specific needs.

Pilot only cabin will offer more payload carrying option for light delivery missions.

Crew of 2 options will be offered in side by side and tandem cabin set up to accomodate your mission requirements.

Enclosed cabin autogyro prototype

TOAD Specifications

Crew
1, 2, 1+2
Loiter capability
6 hours+
Payload
700 pounds
Maximum speed
195 km/h
Climb rate
1000 ft/second
Take off distance
50 to 100m
Landing distance
5 m

Specifications and performances subject to change depending on legislation, temperature, barometric pressure and models.

Demonstrator autogyro

The initial demonstration model of the TOAD will feature a 20 Mpixels mapping sensor along with a geotagging and storage interface; completed by a radio and software suite allowing ground operator to review the imagery while the mission is still ongoing.
It will be completed by a 180¡ high resolution pan, tilt and zoom 5 Mpixels camera for surrounding awareness.

Integrated sensors

Our system offers an integrated suite of high resolution sensors, which allow both the people in the air and the people on the ground to track the mission, communicate and transmit images in real-time. Our set of gyro stabilized gimbals includes day and night 5 mega pixels high speed cameras. External mounting points offer the end user the ability to integrate his own specific system if necessary.

C-LVL