Test systems and Instrumentation

Ground Support Equipment

We provide clients with all the necessary equipment to maintain UAS systems as well as logistical material to enhance mobility and tactical operations. Not only do we supply and integrate instrumentation, sensors, and data acquisition systems, but also we offer services regarding mobility, cooling, refueling, storage, power supply, launching and arresting equipment and subsystems, as well as several D-Level, I-Level and O-Level test and calibration systems.

GDT system installed over a single axle all-roads trolley to be coupled to any standard vehicle.

The system includes:

  • Diesel electric generator for power supply to all equipments  (230 VAC)
  • A mast for the UHF antenna of the SDL system
  • Racks bays for communications and electric protections systems
  • Supports for fiber optics cables rolls and for PDL system (Tripod+Plate+Equipment)





 TOTAL mass of GDT

< 3000

 Number of axles


 Draw bar type

  1  Height adjustable
 Draw ball

  1  Civil standard


 Electric generator weight


  Kg  Can be modified
 Time for deployment


  min  Legs and mast extension , power generator start up and initial systems test.


Coolling and Transport cart allowing to carry the UAV over towards the take off runway, with the engine running at the minimum consumption rate and colling down the motor and the electronics bays, using the ambient air which is forced in the UVS systems.

Fast and automatic coupling and decoupling trough special adapters between the system and the air intakes of the UAV, assuring safe operation for personnel even with engine running.

The UAV is driven by the cart to the take of point avoiding damages over the front landing gears. the UAV is automatically loaded up of the cart to avoid damage either on the UAV or  on personnel.

Total Weight  500Kg
Dimensions  1300X900X900mm
Motor  Diesel >10 kW power
Operation time  >3h
Engine air cooling flow rate  ≥ 0.55 Kg/s at 15ºC
Avionics air cooling flow rate  ≥ 0.35 Kg/s at 15ºC


HAS is a simple but efficient arresting system to provide extra braking capacity for an UAV landing over a short length runway.

The system is based in two energy absorption drums, one at each side of the runway, and a flexible cable crossing the track and connected to both drums trough a straps endings.

The energy of braking is dissipated by adjustable and progressive friction loads.

The UAV should be equipped with a compatible hook which connects with the crossing cable for stopping.

The system can be also used for stopping the UAV in case of aborted take off and after non return point in a very short and controllable distance.