turboprop engine
PBS TP100
Turboprop engine with power output up to 180 kW, suitable for small aircraft and UAVs. Low weight, high‑altitude capability, and fuel efficiency; FADEC automated control.
180 kW
Power
61,6 kg
Weight
up to
9500 m
Operating altitude
Features
Oil Tank
Ensures reliable engine lubrication and stable oil flow under all operating conditions.
Technické parametry
Usage
Applications
Functions
Name
Metric units
Imperial units
Power Supply
28 V DC
28 V DC
Electrical Power Output
720 - 3,700 W
720 - 3,700 W
Specific Fuel Consumption (SFC)
0.548 kg/kW/h
0.901 lb/HP/hr
Length
891 mm
35.08 in
Weight
61.60 kg
135.80 lb
Max. Operating Altitude
9,000 m
29,528 ft
Power Supply
Metric units
28 V DC
Imperial units
28 V DC
Electrical Power Output
Metric units
720 - 3,700 W
Imperial units
720 - 3,700 W
Specific Fuel Consumption (SFC)
Metric units
0.548 kg/kW/h
Imperial units
0.901 lb/HP/hr
Length
Metric units
891 mm
Imperial units
35.08 in
Weight
Metric units
61.60 kg
Imperial units
135.80 lb
Max. Operating Altitude
Metric units
9,000 m
Imperial units
29,528 ft
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