(S/L static; ISA) AI9-3B Aircraft electric system AC power, kVA ........... 16 B
Takeoff(S/L static; ISA) Thrust, kgf................. 3,000...........3,755 Spec
Check at every level: from production to testing one-stop service material selec
Takeoff (S/L static; ISA) Propeller shaft power, hp..........…........... 400...
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Takeoff (S/L static; ISA), uninstalled Thru. k.............. 7,500...........7,5
Takeoff(S/L static; ISA) Output shaft power, ehp ....................... 2,500 E
Excellent thrust-to-weight ratio, low fuel consumption, integrated inspiration,
Takeoff (S/L; tmb= ts+15℃,Pmm=730 mm Hg) Output shaft power, ehp ...............
Twin cylinder horizontally opposed air-cooled, two-stroke gasoline engine with m
Takeoff (S/L static; ISA), uninstalled Thrust, kgf ................ 23,430 Speci
Cylinder cut-out Test Oil Reset Fuel Trim Reset Elec. Throtle Adaption Sunroof I
Takeoff (S/L static; ISA) Output shaft power, ehp ........ 4,000 ............ 4,
UAV Drone Gasoline Engine The Drone Gasoline Engine is an internal combustion en
Turbine Wheels / Shaft & Wheels E&E Turbo can be able to supply an exte
Model:EEJ-20 Maximum thrust(daN):19 Maximum speed(rpm):120,000 Specific fuel con
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