AeroTestra ATMK09

Thin Shell Fuselage

AeroTestra uses a proprietary design method similar to modern aircraft, described as a "thin shell" or monocoque structure. It carries both tensile and compression forces within the skin and can be recognized by the absence of a load carrying internal frame. This design allows for a very high strength to weight ratio. This allows for a large, protective internal area for payload capacity.

Primary Vibration Isolation

The largest amount of vibration occurs in the fuselage, at the distal end of the arms where the motors and propellers are located. By isolating the main payload section from the fuselage, we have succeeded at reducing the influence of vibration to imaging payloads substantially.

Autopilot mount

The autopilot mounting position is located centrally in the X and Y axis, and co-planar to the prop discs, coincident to the vehicles center of gravity.
In addition to the vibration isolating design of the super structure from the fuselage of the aircraft, the mounting surface is also isolated from high frequency vibrations not arrested by the primary dampening structure. The result is a virtually noiseless environment for the inertial navigation sensors of the vehicle to operate in.

Battery System

We integrated a battery attachment mechanism that allows for quick exchange and positive locking.
"Smart Battery" technology allows for monitoring vital conditions of battery system including charge state and sell balance with the touch of a button. The advanced battery management system provides additional functionality that will increase the usable life of the battery including:

• Self-balancing function

• Self-discharge function at High Temperature storage

• Over voltage and under voltage alert function

• Over Temperature and low temperature alert function

• Cell abnormal alert function