Turbojet engines
PBS TJ100
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.
up to
1250 N
Thrust
up to
300 hrs
TBO
17,6 kg
Weight
10 000 m
Operating altitude
Usage
Applications
Functions
Name
Metric units
Imperial units
Thrust
1100-1250 N
247.29 - 281.011 lbf
Weight
19.70 kg
43.431 lb
Outer Diameter
272 mm
10.709 in
Length
636 mm
25.039 in
Thrust
Metric units
1100-1250 N
Imperial units
247.29 - 281.011 lbf
Weight
Metric units
19.70 kg
Imperial units
43.431 lb
Outer Diameter
Metric units
272 mm
Imperial units
10.709 in
Length
Metric units
636 mm
Imperial units
25.039 in
Features
Salt water Recovery
The engine is adapted for landing in saltwater; suitable for target drones and naval operations.
Oil Tank
Ensures reliable engine lubrication and stable oil flow under all operating conditions.
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