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JT-1350N 135kg Thrust Target Drone UAV Turbine Engine (Production and Test: 14-21 days)
Engine technical specifications
1. Engine appearance parameters
(1)Engine model and category CFP-1300 Turbojet
(2)Engine rotor rotation direction Clockwise rotation (engine intake port looking backwards)
(3)External dimensions of the engine
Engine technical parameters
(1)Engine acceleration and deceleration delay
The engine will idle for 30 seconds until it reaches the crane.
The engine will idle from the crane for 20 seconds.
(2)Speed characteristics
The specific data of the 135KG engine is subject to the factory data.
When the flight speed and altitude are constant, the relationship between thrust and fuel consumption rate with rotational speed should be able to provide stable and reliable power for aircraft flight, meeting the flight requirements of the aircraft in various design states.
Speed and thrust variation curve
Speed and Flow Change Curve
2.Engine usage and maintenance
Engine testing
(1)First time using the engine
Open the transportation box and check the accessory components according to the packing list ; Observe whether there is mechanical damage to the surface of the engine; Manual rotor check for smooth rotation and no noise.
3.Engine packaging diagram
Packing list