0 - 100kN turbojet PBS TJ200

0 - 100kgfor dronesfor UAV

Overview
The PBS TJ200 is a compact turbojet engine delivering 2,280 N of static thrust (rated up to 2,300 N). It is engineered for high-speed UAVs, target drones and defence systems requiring high dynamics, immediate start capability and integration with onboard control and power electronics. The design prioritises compact construction and low weight to simplify airframe integration.

Key metrics

• Thrust: 2,280 N
• TBO (Time Between Overhauls): up to 25 h
• Weight: 28.0 kg
• Operating altitude: 10,000 m

Features

• Pyrotechnic ignition: an electric device with a pyrotechnic element ensuring a reliable and immediate engine start, designed for critical applications.

Technical parameters (table)
Name | Metric units | Imperial units
Thrust | 2,280 N | 512.54 lbf
Weight | 28.0 kg | 61.73 lb
Outer Diameter | 246 mm | 9.68 in
Length | 730 mm | 28.74 in

Technical specifications

• Model: PBS TJ200
• Thrust: 2,280 N (technical table) — also referenced up to 2,300 N
• Weight: 28.0 kg
• Outer diameter: 246 mm
• Length: 730 mm
• TBO: up to 25 h
• Operating altitude: 10,000 m
• Intended usage: Defence
• Applications: high-speed UAVs, target drones, missiles, defence systems
• Functions: pyrotechnic ignition for reliable immediate engine start
• Design: compact construction, low weight, integration of advanced control and power systems