Medium Altitude Long Endurance (MALE) Propulsion System Experimental Data

All the data have been taken from 2 types of data acquisition tools. The first is through data acquisition (DAQ), and the second is through the Engine Management Unit. The Thrust data was taken via DAQ-9185. Meanwhile, Ambient Temperature, Ambient Pressure , Throttle Position ,Propeller Rotation, Fuel Pressure , Fuel Flow Rate , Airflow , Manifold Air Pressure , Exhaust Gas Temperature and Cylinder Head Temperature , are taken by EMU. The propeller RPM is calculated from the engine RPM using a reduction gear with a ratio of 2.54.