Turbojet engines
PBS TJ100
Turbojet engine suitable for UAVs, UCAVs, and experimental aircraft. Compact design, low weight, and high reliability; proven in certified aviation applications, including EASA-certified projects.
up to
1,250 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
1,100-1,250 N
247.29 - 281.011 lbf
Weight
17.60 kg
38.80 lb
Outer Diameter
272 mm
10.709 in
Length
636 mm
25.039 in
Thrust
Metric units
1,100-1,250 N
Imperial units
247.29 - 281.011 lbf
Weight
Metric units
17.60 kg
Imperial units
38.80 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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