Currently we are conducting an assemly of the first set of D200 engines and drafting the design documentation. We invite aircraft modellers and UAV developers to cooperate. From our side we are happy to provide the installation of the engine to your machine and help with integration into aircraft.
Key parameters of the engine:
- Max. thrust 20 kgf;
- Weight including external components 2.8 kg;
- Fuel consumption 750ml/min;
- Contol on CAN bus;
- Voltage 12 V.
The detailed information of the turbojet engine will be described in User Manual which will be issued in January 2019. For more information please send us an email on email@example.com.