JT-1000N 100kg Thrust Target Drone UAV Turbine Engine (Production & Test 14-21 days)
Technical indexes of engine
1. Overall dimensions of engine
1 Engine model and category JT—800N
2 Rotation direction of engine rotor: clockwise (looking back at engine inlet)
3 Overall dimensions of engine (± 2%)
2. Engine Technical Data
3.(1)Acceleration and deceleration delay of engine
Engine from idle to cart 15s.
Engine from cart to idle 15s.
Curve of thrust variation with altitude and velocity
Engine fuel consumption height (H) - speed (Ma) characteristics
Fuel consumption rate versus flight altitude and speed
JT—1000N The specific engine data shall be subject to the factory data.
When the flight speed and altitude are fixed, the change relationship between thrust and
fuel consumption rate and speed shall be able to provide stable and reliable power for
aircraft flight and meet the flight requirements of aircraft under various design conditions
The engine speed exhaust temperature curve under standard ambient atmospheric pressure as follows:
The speed throttle curve under the standard ambient atmospheric pressure of the engine as follows:
Speed and thrust change curve as folllows:
4.Packing list
5.Engine storage
The engine shall be stored in a dust-free and dry environment and shall not be stored vertically for a long time.