UAV Drone Gasoline Engine The Drone Gasoline Engine is an internal combustion en
Takeoff (S/L; tmb= ts+15℃,Pmm=730 mm Hg) Output shaft power, ehp ...............
Check at every level: from production to testing one-stop service material selec
Turbine Wheels / Shaft & Wheels E&E Turbo can be able to supply an exte
Storage temperature: -40℃~80℃ Working temperature: -20℃~60℃ Temperature range: -
Storage temperature: -30℃~80℃ Operating temperature: -20℃~60℃ Operating voltage:
Excellent thrust-to-weight ratio, low fuel consumption, integrated inspiration,
(S/L static; ISA) Generator terminals power, kW ........ 60 Fuel consumption, kg
TV3-117VMA-SBM1V series 5 Maximum emergency (S/L static; ISA) Power, hp ........
Takeoff(S/L static; ISA) Thrust, kgf................. 3,000...........3,755 Spec
Takeoff(S/L static; ISA) Power, hp ............ 400..........................465
(S/L static; ISA) AI9-3B Aircraft electric system AC power, kVA ........... 16 B
(S/Lstatic; ISA) Aircraft electric system DC power, kW .......... 3 Bleed airflo
(S/L static; ISA) Bleed airflow, kg/s .............................…..…..…......
Specific fuel consumption by 15...20% lower than that of current engines in this
Maximum power rating (S/L static; ISA;=1.0) Thrust, daN ................... ....
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