UAV A-2 Tit

UAV A-2 "Tit"

UAV A-2 is a remotely piloted aircraft. The second name – “Tit”. It refers to a miniature aircraft. “Duck” Designed under the scheme. The motor electric with a battery, designed for one hour air flight. UAV A-2 “Tit” is designed in Ukrainian CB “Rise”.

Start unmanned carried out with a specially installed a catapult or a human hand, and planting is done with the help of a parachute. There are several options for operation of the A-2 “Tit”:

  1. Environmental monitoring of the area.
  2. Conducting intelligence activities in the areas of major accidents and disasters.
  3. Inspection of large protected sites.
  4. Reconnaissance protection of the state border.

UAV “Tit” refers to the composition of “SKIF-1” mobile unmanned multipurpose complex.Short name – MMBK “Skif-1.” In addition to this drone, the complex consists of ground equipment, control center and control the flight of the UAV, catapults, the antenna system.

Location, mode and flight direction are displayed on the computer screen ground complex.Also, there is demonstrated the scanned map of the area. The device is perfect for monitoring environmental disasters, because it allows you to calculate exactly the places where the centers of the disaster.

UAV A-2 is equipped with the following equipment:

  1. Developed on the basis of GPS-35 satellite navigation system.
  2. Televizornaya camera or a set of two cameras (Review controlled and the exchange rate).
  3. Digital radio, aircraft control equipment.
  4. Television transmitters with spread spectrum signal.
  5. Control system digital.

Aircraft performance characteristics: takeoff weight – 5 kg; flight distance – 20 km; flight speed – 80 km / h; ceiling – 2 km; the length of the machine – 0.95 m; wingspan – 1.8 m;flight time – 1 hour.

A-2 “Tit” The characteristics:

Modification A-2
Wingspan, m 1.80
Length m  0.95
Height, m
Weight, kg
  null
  maximum take-off 5.0
  payload 1.0
engine’s type  1 ED
power, kWt  1 x 0.4
Cruising speed, km / h  30-80
Practical range, km
Radius of action, km  20
The flight duration, min  60
Practical ceiling, m
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