PBS TJ80-90
The PBS TJ80-90 is a compact jet engine designed for unmanned aerial vehicles or missiles. The engine features a high thrust-to-weight ratio, maintenance-free operation, and an integrated generator with a FADEC control system.
900 N
Thrust
up to
25 hrs
TBO
12.5 kg
Weight
10 000 m
Operating altitude
Technical Parameters
Usage
Applications
Name
Metric units
Imperial units
Thrust
900 N
202-202 lbf
Weight
12,5 kg
27.55 lb
Outer Diameter
235 mm
9.25 in
Length
511 mm
20.12 in
Thrust
Metric units
900 N
Imperial units
202-202 lbf
Weight
Metric units
12,5 kg
Imperial units
27.55 lb
Outer Diameter
Metric units
235 mm
Imperial units
9.25 in
Length
Metric units
511 mm
Imperial units
20.12 in
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