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Shenyang CK-1
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Shenyang CK-1

Shenyang CK-1

Create an aircraft Shenyang CK-1 was initiated by Chinese designers in the spring of 1968 years. The formulation has been almost completely taken the Soviet development of the aircraft under the designation La-17. Despite the fact that this machine was produced in the USSR in 1953 year, China's designers managed to make a lot of innovations in the unmanned vehicle. First of all, it has been significantly redesigned fuselage and fuel system that will allow for better flight performance than the original model.

In the development, it was decided to apply the normal scheme with a wing aerodynamics of rectangular shape. Also for ease of use, horizontal and vertical tail were made equal and could be replaced with each other. As the power plant aircraft used one type of turbojet engine, which is mounted under the body of the machine. Takeoff UAV Shenyang CK-1 was only possible using ground-based launcher and additional propellant boosters, which dispersed the car to a certain speed and altitude, and then run the main engine. The entire flight was controlled from a control point of control placed on the ground, in addition, possible automatic flight by a given program.

Shenyang CK-1.Harakteristiki:



Modification CK-1C
Wingspan, m 7.50
Length m 8.44
Height, m 2.96
Wing area, m2 8.55
Weight, kg  
null 2000
fuel 840
maximum take-off 3340
engine's type 1 TRD WP6
Thrust, kgf X 1 2600
Maximum speed km / h 900
Range, km 600
The flight duration, min 60-70
Practical ceiling, m 18000
Operational ceiling, m 500-5000

 

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