 |
Power Output...............................................................121 lbs. Thrust
Rpm...............................................................................61,000 rpm
Compressor..................................................................Centrifugal Impeller
Gas Generator Turbine...............................................Axial Flow
Application...................................................................Drones
Overall Dimensions & Weight
Length .........................................................................22.3 in.
Width (Max Diameter) ...............................................10.8 in.
Dry Weight of Engine ...............................................13.6 Kg
